Journal articles: 'Aircraft Industries'

1

Gershon, B., I. Arbel, S. Hevlin, Y. Milo, and D. Saltoun. "Industrial Superplastic Forming Research and Application for Commercial Aircraft Components at Israel Aircraft Industries." Materials Science Forum 357-359 (January 2001): 527–32. http://dx.doi.org/10.4028/www.scientific.net/msf.357-359.527.

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Yamafuji, Kazuo. "Factory Tour to ShinMaywa Industries, Ltd." International Journal of Automation Technology 3, no. 5 (September 5, 2009): 620–22. http://dx.doi.org/10.20965/ijat.2009.p0620.

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The ShinMaywa Industries, Ltd., predecessor, Kawanishi Aircraft Ltd., was famed for its high-performance World War II planes, including the Type II Flying Boat, codenamed “Emily” by the Allied Forces, and the Interceptor Siden-Kai, codenamed “George.” Following defeat, Kawanishi Aircraft Ltd. was renamed ShinMaywa Industries, Ltd., founded officially in 1949. The new company, which started out producing dump trucks, but resumed aircraft manufacture in 1960. ShinMaywa now holds a high market share among Special Purpose Trucks such as dump trucks and in aircraft business exemplified by the STOL (Short Take Off Landing) Amphibian. It also manufactures Automatic Wire Terminating Machines, Thin Film Coating System, Aircraft Passenger Boarding Bridges, Car Parking System, and Water Treatment Equipment. In fiscal 2008 business, industrial machinery accounted for 37%, special purpose truck 35%, aircraft 19%, and others 9% in the company’s ¥127.7 billion sales (US$1.277 billion). Current employees based on consolidated accounts number 3,883. The enterprise philosophy is “contributing to society through outstanding technology and service.” Concretely, harmonization with society should be achieved in daily activities of an enterprise, and enterprise value should be raised by management taking stake holders into account.

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Moreno-Andrade, Iván, Gloria Moreno, Gopalakrishnan Kumar, and Germán Buitrón. "Biohydrogen production from industrial wastewaters." Water Science and Technology 71, no. 1 (November 22, 2014): 105–10. http://dx.doi.org/10.2166/wst.2014.471.

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The feasibility of producing hydrogen from various industrial wastes, such as vinasses (sugar and tequila industries), and raw and physicochemical-treated wastewater from the plastic industry and toilet aircraft wastewater, was evaluated. The results showed that the tequila vinasses presented the maximum hydrogen generation potential, followed by the raw plastic industry wastewater, aircraft wastewater, and physicochemical-treated wastewater from the plastic industry and sugar vinasses, respectively. The hydrogen production from the aircraft wastewater was increased by the adaptation of the microorganisms in the anaerobic sequencing batch reactor.

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Karthigeyan, P., M. Senthil Raja, R. Hariharan, R. Karthikeyan, and S. Prakash. "Performance evaluation of composite material for aircraft industries." Materials Today: Proceedings 4, no. 2 (2017): 3263–69. http://dx.doi.org/10.1016/j.matpr.2017.02.212.

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YAMANAKA, Takeshi. "Movement of Quality Assurance Systems in Aircraft Industries." Journal of the Society of Mechanical Engineers 102, no. 972 (1999): 677–79. http://dx.doi.org/10.1299/jsmemag.102.972_677.

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Ismail Muzakir, Muhammad Athar. "Government- Pulled Triple Helix for Supporting National Aircraft Industry in the Global Value Chain with Tipology Hierarchy." Perspektif : Jurnal Ilmu Administrasi 1, no. 1 (May 2, 2019): 63–83. http://dx.doi.org/10.33592/perspektif.v1i1.78.

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This study reconstructs the government- pulled triple helix for supporting national aircraft industry in the Global Value Chain (gvc) with tipology hierarchy. By employing Soft Systems Methodology (SSM), this research revealed that Triple Helix Model for development aircraft industry directed to design Macro Policy, revitalize test laboratories, strengthen aircraft financing policy, building supporting Industries and empower aerospace human resources. The government-pulled triple helix model has overlapping the role played by Academia (A), Busines (B), and Government (G) in the development of the aircraft industry. In fact, according to Etkowitz, H. (2008) that overlapping of role only occurs in university pushed triple helix model. In addition, the configuration of actor G in the triple helix needed for development national aircraft industry is not generic but based on specific context. In aircraft development, especially for strengthening the aerospace industry cluster, the role of association is also important. In the GVC of Aircraft Industry with typology of hierarchy, PT DI is required to be able to build networks with industry partners, domestic and foreign research institutions and aircraft component industry associations. The Government will obtain lesson learnt on how the strategy for supporting the national aircrafts development such as program of N 219, N 245 or R 80 which developed at present.

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Li, Guang Jun, Sheng Yuan, and Xu Dong Xu. "The Development and Application of Object-Oriented Finite Element Analysis System for Sheet Metal Forming." Advanced Materials Research 756-759 (September 2013): 33–36. http://dx.doi.org/10.4028/www.scientific.net/amr.756-759.33.

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Recently, the finite element (FE) numerical simulation technology has become an effective approach to solve problems in precise manufacturing of sheet metal parts in aircraft industries. Based on FE analysis software Pam-Stamp, Chengdu Aircraft Industrial Company developed a FE system for analysis of typical sheet metal forming. This system has been successfully applied in the development of new products, which shortens the preparation cycle of process and enhances the capability for rapidly researching and developing.

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Ramdani, Danny. "Formulasi Strategi Pengembangan SDM Perawatan Pesawat Terbang." Organum: Jurnal Saintifik Manajemen dan Akuntansi 2, no. 1 (June 30, 2019): 46–61. http://dx.doi.org/10.35138/organum.v2i1.56.

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The lack of level human resources capabilities in narrow-body aircraft maintenance (Airbus & Boeing), which implies the achievement of all operator's maintenance revenue in Indonesia. The research focused on the business unit of Aircraft Services of Indonesian-aircraft Industries. The purpose of this study was to analysis and make a formulation strategy development of aircraft maintenance knowledge workers at the business unit of Aircraft Services of Indonesian-aircraft Industries. The research used a case study with a qualitative method and SWOT analysis used as a tool in the implementation process. The datas collect conducted through some literature, documents, and in-depth interviews. The subjects were managers, senior engineers, instructors, inspectors, technicians, and mechanics seniors, which focused on the development of knowledge workers (direct workers). The result of SWOT Analysis showed that unit business Aircraft Services should make an arranging program development for aircraft maintenance knowledge workers, namely: a training program for acquiring an Aircraft Maintenance Engineer License (AMEL), human resources procure system, career path, reward & compensation, and performance system. The finding was the lack of unit business Aircraft Services within preparing a business development plan program for aircraft maintenance wide-body because of corporate's response in supporting aircraft maintenance and technician/mechanics education center facilities were very slow. The conclusion was that unit business Aircraft Services, will have a competitive advantage for Aircraft maintenance narrow-body (Airbus & Boeing) if the result of strategy formulation has thoughtfully been implemented.

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Guadagno, Liberata, Fabiana Foglia, Roberto Pantani, Maria Dolores Romero-Sanchez, Blanca Calderón, and Luigi Vertuccio. "Low-Voltage Icing Protection Film for Automotive and Aeronautical Industries." Nanomaterials 10, no. 7 (July 9, 2020): 1343. http://dx.doi.org/10.3390/nano10071343.

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High-performance heater films are here proposed. They manifest great applicative potentiality in the de-icing technology of aircraft and motor vehicles. The films are suitable to be integrated into composite structures for the de/anti-icing function, which can be activated if the need arises. The heating is based on the joule effect of the current flowing through the electrically conductive films. Voltage and current parameters have been set based on the generators’ capacities on-board an aircraft and a car, as well as on the energy consumption during the operating conditions and the autonomy in the time. Green processes have been employed through all preparative steps of the films, which are composed of expanded graphite (60% wt/wt) and polyvinyl alcohol (PVA) (40% wt/wt). The results reveal a very significant influence of the aspect ratio of the filler on the heating and de-icing performance and suggest how to enhance the de-icing efficiency saving energy and adapting the current on-board aircraft/car generators for de-icing operations.

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Rawahi, Said Hamed Al, Zaharuzaman Bin Jamaluddin, and Abul Bashar Bhuiyan. "THE CONCEPTUAL FRAMEWORK FOR THE RESOURCES MANAGEMENT ATTRIBUTES AND AIRCRAFT MAINTENANCE EFFICIENCY IN THE AVIATION INDUSTRIES IN OMAN." International Journal of Accounting & Finance Review 5, no. 3 (October 14, 2020): 31–40. http://dx.doi.org/10.46281/ijafr.v5i3.808.

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The main purpose of the study is to investigate existing available literature for determining of relevant factors that have cause and effects on the ensuring of aircraft maintenance efficiency in the aviation industry in Oman. Therefore, the study uses available sources of existing literature based on the four main keywords ‘aircraft maintenance efficiency’, ‘aircraft maintenance and resource management attributes ‘or ‘effective planning and aircraft maintenance, and ‘internal control and aircraft maintenance, etc., and explored to covers from Google Scholar, ProQuest, and Scopus, and other online resources. The study also justified of above summary literature gap by the most relevant theories such as stakeholder, agency, and resource-based theories accordingly. Based on this extensive review, the study developed a conceptual framework, where effective planning and internal control have moderating role on the relationship between the resource management attributes and aircraft maintenance efficiency in the aviation industry in the sultanate of Oman. The summary review findings of the study will fill the gap in the existing body knowledge especially prime factors affecting the attainment of aircraft maintenance efficiency, resource management attributes, effective planning and ‘internal control and aircraft maintenance in the aviation industry in the sultanate of Oman. The study recommends to justify this conceptual framework by empirical data from the in the aviation industry in the sultanate of Oman and draw a policy guideline for ensuring of determining of relevant factors that have cause and effects on the ensuring of aircraft maintenance efficiency in the aviation industry in Oman.

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Wang, Zheng-Xin. "A GM(1,N)-based economic cybernetics model for the high-tech industries in China." Kybernetes 43, no. 5 (April 29, 2014): 672–85. http://dx.doi.org/10.1108/k-10-2013-0227.

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Purpose – The purpose of this paper is to propose an economic cybernetics model based on the grey differential equation GM(1,N) for China's high-tech industries and provide the necessary support to assist high-tech industries management departments with their policy making. Design/methodology/approach – Based on the principle of grey differential equation GM(1,N), the grey differential equations of five high-tech industries in China are established using the net fixed assets, labor quantity and patent application quantity as cybernetics variables. After the discretization and first-order subtraction reduction to the simultaneous equation of the five grey models, a linear cybernetics model is resulted in. The structure parameters in the cybernetics system show explicit economic significance and can be identified through least square principle. At last, the actual data in 2004-2010 are introduced to empirically analyze the high-tech industrial system in China. Findings – The cybernetics system for China's high-tech industries are stable, observable, and controllable. On the whole, China's high-tech industries show higher output coefficients of the patent application quantity than those of net fixed assets and labor quantity. This suggests that China's industry development mainly depends on technological innovation rather than capital or labor inputs. It is expected that the total output value of China's high-tech industries will grow at an average annual rate of 15 percent in 2011-2015, with contributions of pharmaceuticals, aircraft and spacecraft, electronic and telecommunication equipments, computers and office equipments, medical equipments and meters by 21, 16, 13, 10, and 28 percent, respectively. In addition, pharmaceuticals, as well as medical equipments and meters, present upward proportions in the gross of Chinese high-tech industries significantly. Electronic and telecommunication equipments, plus computers and office equipments exhibit an obvious decreasing proportion. The proportion of the output value of aircraft and spacecraft is basically stable. Practical implications – Empirical analysis results are helpful for related management departments to formulate reasonable industrial policies to keep the sustained and stable development of the high-tech industries in China. Originality/value – Based on the grey differential equation GM(1,N), this research puts forward an economic cybernetics model for the high-tech industries in China. This model is applicable to the economic system with small sample data set.

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Ivanov, Dmitry Urevich, G. Grishanov, and V. Zaskanov. "Development Prospects of Production of Composite Materials in Russian Federation." Key Engineering Materials 746 (July 2017): 305–10. http://dx.doi.org/10.4028/www.scientific.net/kem.746.305.

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The paper analyzes the current state of production of composite materials in the Russian Federation. It is conceded the use of composites in aircraft design of various aircraft manufacturers. Concluded the feasibility of using composite materials in various industries. Peculiarities and prospects of prepreg application in the production of various parts are revealed.

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13

Asmatulu, Eylem, Michael Overcash, and Janet Twomey. "Recycling of Aircraft: State of the Art in 2011." Journal of Industrial Engineering 2013 (January 2, 2013): 1–8. http://dx.doi.org/10.1155/2013/960581.

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Recently, the end-of-service life for aging aircraft and related parts has become a key subject in recycling industries worldwide. Over the next 20 years, approximately 12,000 aircraft currently utilized for different purposes will be at the end of service. Thus, reclaiming retired aircraft by environmentally responsible methods while retaining some of the value becomes a significant need. Recycling aircraft components and using these in different applications will reduce the consumption of natural resources as well as landfill allocations. Compared to the production of virgin materials, recycling aircraft will also reduce air, water, and soil contaminations, as well as energy demand. In the present study, we have investigated the environmental benefits of recycling and reusing aircraft components in the same or similar applications as low-energy input materials. During the aircraft recycling, most of the aircraft components can be recycled and reused after reasonable modifications and investments.

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14

Rawahi, Said Hamed Al, Zaharuzaman Bin Jamaluddin, and Abul Bashar Bhuiyan. "THE REVIEW ON THE EFFECT OF THE RESOURCES MANAGEMENT ATTRIBUTES AND AIRCRAFT MAINTENANCE EFFICIENCY OF THE AVIATION INDUSTRIES IN OMAN." Indian Journal of Finance and Banking 4, no. 3 (October 14, 2020): 53–62. http://dx.doi.org/10.46281/ijfb.v4i3.813.

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As the aircraft maintenance is one of the very essential resources to enhance the aircraft productivities those facilities such as spears, human, and financial add to that the organizational factors in which will help to make the maintenance more efficient and safe because the safety is the priority part in maintenance in which the organization should take in consideration. The main purpose of the study is to investigate existing available literature for determining of relevant factors that have cause and effects on the ensuring of aircraft maintenance efficiency in the aviation industry in Oman. Therefore, the study uses available sources of existing literature explored to covers from Google Scholar, ProQuest, and Scopus, and other online resources. Based on this extensive review, the study determined the resource management attributes and aircraft maintenance efficiency and have moderating role effective planning and internal control in the aviation industry in the sultanate of Oman. The summary review findings of the study will fill the gap in the existing body knowledge especially prime factors affecting the attainment of aircraft maintenance efficiency, resource management attributes, effective planning and ‘internal control and aircraft maintenance in the aviation industry in the sultanate of Oman. The study recommends for policy guideline for ensuring of determining of relevant factors that have cause and effects on the ensuring of aircraft maintenance efficiency in the aviation industry in Oman.

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15

Gershon, B., and I. Eldror. "Research and Application of Superplastic Forming Titanium Alloys for Commercial Aircraft Parts." Materials Science Forum 475-479 (January 2005): 3047–50. http://dx.doi.org/10.4028/www.scientific.net/msf.475-479.3047.

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Titanium alloys sheets have many attractions for the aerospace industry owing to their high strength, low density, heat resistance and other useful properties. Many of the sheet metal structures in airframes have complex shapes and compound curvatures with intricate details. Superplastic forming (SPF), a most recent advancement in titanium sheet forming technology, exploits the excellent characteristic of >1000% elongation potential for the fabrication of complex configurations not achievable by conventional methods. SPF technology can also reduce manufacturing cost by shortening the preparation time, eliminating the need for extensive welding or other joining methods and by reducing the number of manufacturing steps. Consequently, high profit margins may be achieved in serial aircraft production. This paper outlines the research at Israel Aircraft Industries (IAI) of SPF technology and its application in producing complex-shape Ti sheet parts for the new IAI commercial aircrafts, models “G-150” and “G-200”. Examples of both actual and experimental parts are given, together with details of the manufacturing parameters employed. An economical analysis is also included.

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Bockmair, Georg. "Non-Chromate Surface Protection for Aircraft Maintenance." Advanced Materials Research 38 (March 2008): 7–13. http://dx.doi.org/10.4028/www.scientific.net/amr.38.7.

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While chromates as anti-corrosion pigments in primers and wash primers have disappeared in most industries, there are still quite a lot of chromated paints used in the aircraft industry. Intensive efforts to develop alternative pre-treatments to chromate conversion coatings and to chromic acid anodization have begun. The intention of this report is to give an overview of the state-of-the-art techniques about such pre-treatment/coating systems of aluminium for aircraft maintenance, which are in accordance with the latest environmental policies. The objective is to evaluate the combination of surface pre-treatment and paint as a whole.

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Uzgur, Sinem Cevik, Yagiz Uzunonat, S. Fehmi Diltemiz, Melih Cemal Kushan, and Rabia Gunay. "State-of-Art Technology ALLVAC 718 Plus Superalloy for Gas Turbine Engine Parts." Advanced Materials Research 213 (February 2011): 131–35. http://dx.doi.org/10.4028/www.scientific.net/amr.213.131.

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Innovations on the aerospace and aircraft industry have been throwing light upon building to future’s engineering architecture at the today’s globalization world where technology is the indispensable part of life. On the basis of aviation sector, the improvements of materials used in aircraft gas turbine engines which constitute 50 % of total aircraft weight must protect its actuality continuously. Utilization of super alloys in aerospace and defense industries can not be ignored because of excellent corrosion and oxidation resistance, high strength and long creep life at elevated temperatures. The newly innovated ALLVAC 718 Plus superalloy which is the last version of Inconel 718 has been proceeding in the way to become a material that aerospace and defense industries never replace of any other material with combining its good mechanical properties, easy machinability and low cost. However because it is a newly developed superalloy, in present paper its properties including chemistry, microstructure, strengthening mechanisms, weldability and cost will be discussed and the superiority of the ALLVAC 718 plus will be addressed.

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Wang, Yan Shan, Mei Ju Zhang, and De Feng Liu. "On-Line Oil Monitoring Sensors Fusion for Aircraft Health Management." Applied Mechanics and Materials 128-129 (October 2011): 652–56. http://dx.doi.org/10.4028/www.scientific.net/amm.128-129.652.

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Monitoring oil quality on-line has become an important issue in today’s military, transportation and manufacturing industries. Although laboratory analysis procedures are comprehensive and detailed, they do not provide the timely information about oil for the aircraft health management. Condition monitoring is a preventive maintenance tool which has been used for over 50 years. In this paper we discuss several aircraft oil analysis methods and instruments or sensors. A new methodology of the aircraft oil health management is presented. It can assist realizing autonomous maintenance and dramatically reduce maintenance costs through the data integration from individual oil monitoring sensors. It offers a more comprehensive figure of the whole situation and a more accurate evaluation of the system condition. Therefore the aircraft safety will be greatly improved.

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Lebedev, Konstantin, and Alina Marchuk. "Socio-Cultural Background of Technological Development of Russia and Choice of Its Priorities." Vestnik Volgogradskogo gosudarstvennogo universiteta. Ekonomika, no. 3 (December 2019): 5–14. http://dx.doi.org/10.15688/ek.jvolsu.2019.3.1.

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The purpose of this article is to further confirm the author’s concept of supporting industries from the socio-cultural characteristics of the country on the facts of the history of the Russian national economy and its use for the formation of proposals for the choice of technological priorities of Russia. X–Y-theory of S.G. Kirdina explains the formation of sectoral priorities under the influence of socio-cultural characteristics of the country by the preference of forms of production organization used in industries – collective and monopoly ones in societies of “Eastern” (X) type, which include Russia, private and competitive ones in societies of “Western” (Y) type. However, this mechanism does not explain many phenomena of industry dynamics in Russia. At the same time, socio-cultural features of the country are not taken into account when forming the priorities of its technological development. The article provides an additional confirmation of the author’s concept of supporting industries from the socio-cultural characteristics of the country, based on the preference by X-societies of industries producing products of collective use or destination, and by Y-societies – of industries producing products of individual use or destination. The paper shows that, based on the proposed concept of industry preferences, industries traditionally considered as unpromising for successful development in Russia (road and passenger aircrafts construction) in fact correspond to the industry socio-cultural preferences of the Russian people. The author proposes to include aircraft construction, shipbuilding, construction and education, mainly producing products for collective use and purpose, in the Russia’s priorities of technological development.

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Park, Hyun Bum, Chang Duk Kong, and Kyung Sun Lee. "Investigation on Damage Tolerance of Carbon/Epoxy Laminate for Aircraft Structural Design." Key Engineering Materials 488-489 (September 2011): 460–63. http://dx.doi.org/10.4028/www.scientific.net/kem.488-489.460.

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In Korea, the KC-100, which is a small scale piston propeller general aviation aircraft, has been developed to establish a domestic certificate infrastructure and system through the BASA(Bilateral Aviation Safety Agreement) program by KAI(Korea Aerospace Industries, Ltd.). This aircraft adopted the whole composite structure concept for an environmental friendly aircraft through low fuel consumption due to structure weight reduction. However the carbon/epoxy composite structure, which is mainly used for this aircraft, is very weak against foreign object damage. Therefore the purpose of the damage tolerance design philosophy is to ensure that the aircraft can operate safely for a period of time with damage present within the airframe. This study is to investigate the residual compressive strength of the carbon/epoxy UD and fabric laminate due to impact damages. Through investigation on compressive strength, design allowable of carbon/epoxy laminate is determined by the experiment to address design criteria of the composite structure.

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Bouissiere, Francois, Claude Cuiller, Pierre-Eric Dereux, Corentin Malchair, Claudio Favi, and Giovanni Formentini. "Conceptual Design for Assembly in Aerospace Industry: A Method to Assess Manufacturing and Assembly Aspects of Product Architectures." Proceedings of the Design Society: International Conference on Engineering Design 1, no. 1 (July 2019): 2961–70. http://dx.doi.org/10.1017/dsi.2019.303.

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AbstractIn recent years, the air transport market has quickly grown, creating new civil aircrafts demand, challenging the actual production rate of aerospace industries. The bottleneck of the current civil aircrafts production rate lies in the capability of the manufacturing and assembly facilities in relation to the aircrafts architecture design.The aim of this work is to develop a methodology and a related mathematical model that can be used at the conceptual design phase for the assessment of criticalities related to the product assemblability. The methodology allows to recognize modules and/or interfaces which are mostly affecting the assembly time providing a design tool for the comparison and evaluation of product architecture alternatives.A preliminary application has been done on the nose-fuselage of a civil aircraft for passenger transport. The test case provides interesting outcome in the identification of modules and module interfaces which are strongly affecting the assembly phase and required a re-arrangement (new architecture design) for the process improvement.

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Heinrich, Thomas B. "Jack of All Trades: Cramp Shipbuilding, Mixed Production, and the Limits of Flexible Specialization in American Warship Construction, 1940–1945." Enterprise & Society 11, no. 2 (June 2010): 275–315. http://dx.doi.org/10.1017/s146722270000906x.

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Naval shipbuilding was one of the most ambitious industrial undertakings of World War II. A marginal business, in 1939 employing only twelve shipyards, it expanded over the course of the war into a massive network of shipbuilding firms, engineering works, steel mills, and specialty producers that built the world's largest fleet. At its peak in 1944, warship building employed one million shipyard workers, a million others in collateral industries, and consumed one-fifth of the nation's steel output in the construction of aircraft carriers, battleships, cruisers, destroyers, and thousands of smaller combatants.

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Zhang, Y., K. Cao, and W. Dong. "Research on improvement and optimisation of modelling method of China’s civil aircraft market demand forecast model." Aeronautical Journal 125, no. 1289 (April 14, 2021): 1157–91. http://dx.doi.org/10.1017/aer.2021.16.

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ABSTRACTWith the development of China’s economy, China’s aviation market has expanded, and related industries have also developed rapidly. For the long-term development of the industry, many countries and enterprises began to make demand forecasts with different levels for the product market. The same is true for China’s civil aircraft-related industries. There are a variety of predictive models, but not all of them are appropriate for the prediction of civil aircraft market demand. This paper introduces a variety of modelling methods for forecasting models, including time series forecasting models and causal analysis forecasting models. The contribution of our work is the adoption of a new coefficient determination method to establish a variable-weight combination forecasting model, which greatly improves the forecasting accuracy. In addition, we also propose a new and more stable prediction model, the chain prediction model. Simulation prediction is carried out for each model in this work. Through the analysis and comparison of the prediction results, we conclude that the prediction effects of the variable weight combination prediction model and the chain prediction model are superior to those of other single prediction models. The chain prediction model in particular has better performance in medium- and long-term prediction, compared with the other prediction models. Finally, the model is applied to predict the demand of Chinese civil aircraft in the next 20 years, which confirms that the Chinese civil aircraft market will expand in the future.

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Xie, Xue Dong, Xin Kuan Liu, and Jun Ting Cheng. "Measurement Technique Based on the Three-Dimensional White-Light Scanner." Applied Mechanics and Materials 397-400 (September 2013): 993–96. http://dx.doi.org/10.4028/www.scientific.net/amm.397-400.993.

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White light scanner plays a vital role in reverse engineering. It has penetrated into all industries. It includes cars, grinding, aircraft, and mobile phone industry and so on. The paper introduces the basic principle of white light scanner and the measurement techniques.

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Chen, Wen Liang, Yue Yang, Hong Yu Wei, Hong Yu Jiang, Zhi Xiang Huang, Yu Bo Wang, and Lu Yu. "Analysis on Fatigue for Aircraft Riveting Thin-Walled Components." Applied Mechanics and Materials 246-247 (December 2012): 122–26. http://dx.doi.org/10.4028/www.scientific.net/amm.246-247.122.

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Fatigue damage of airframe often caused by riveting defects, which resulting in failure of aircraft structure in service. Based on the theory of classical fatigue fracture, the effects of Interference-fit gap on capabilities of safe service are examined and a new method of measuring the dimension of Interference-fit gap under the different conditions is introduced by cutting test and fatigue test of typical aluminum alloy 2024-T3 in aero industries. And the admissible value of Interference-fit gap for riveting is given, which offered the technological basis to achieve long fatigue of the aircraft.

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Engel, Avner, Michael Winokur, Drora Goshen, and Izhak Geva. "7.5.4 Improving the Systems Engineering Process At Israel Aircraft Industries - A Case Study." INCOSE International Symposium 11, no. 1 (July 2001): 824–29. http://dx.doi.org/10.1002/j.2334-5837.2001.tb02377.x.

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Eisenhut, Dominik, Nicolas Moebs, Evert Windels, Dominique Bergmann, Ingmar Geiß, Ricardo Reis, and Andreas Strohmayer. "Aircraft Requirements for Sustainable Regional Aviation." Aerospace 8, no. 3 (February 26, 2021): 61. http://dx.doi.org/10.3390/aerospace8030061.

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Recently, the new Green Deal policy initiative was presented by the European Union. The EU aims to achieve a sustainable future and be the first climate-neutral continent by 2050. It targets all of the continent’s industries, meaning aviation must contribute to these changes as well. By employing a systems engineering approach, this high-level task can be split into different levels to get from the vision to the relevant system or product itself. Part of this iterative process involves the aircraft requirements, which make the goals more achievable on the system level and allow validation of whether the designed systems fulfill these requirements. Within this work, the top-level aircraft requirements (TLARs) for a hybrid-electric regional aircraft for up to 50 passengers are presented. Apart from performance requirements, other requirements, like environmental ones, are also included. To check whether these requirements are fulfilled, different reference missions were defined which challenge various extremes within the requirements. Furthermore, figures of merit are established, providing a way of validating and comparing different aircraft designs. The modular structure of these aircraft designs ensures the possibility of evaluating different architectures and adapting these figures if necessary. Moreover, different criteria can be accounted for, or their calculation methods or weighting can be changed.

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Şöhret, Yasin. "Defining the Ecological Coefficient of Performance for an Aircraft Propulsion System." International Journal of Turbo & Jet-Engines 35, no. 2 (May 25, 2018): 171–80. http://dx.doi.org/10.1515/tjj-2017-0042.

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Abstract The aircraft industry, along with other industries, is considered responsible these days regarding environmental issues. Therefore, the performance evaluation of aircraft propulsion systems should be conducted with respect to environmental and ecological considerations. The current paper aims to present the ecological coefficient of performance calculation methodology for aircraft propulsion systems. The ecological coefficient performance is a widely-preferred performance indicator of numerous energy conversion systems. On the basis of thermodynamic laws, the methodology used to determine the ecological coefficient of performance for an aircraft propulsion system is parametrically explained and illustrated in this paper for the first time. For a better understanding, to begin with, the exergy analysis of a turbojet engine is described in detail. Following this, the outputs of the analysis are employed to define the ecological coefficient of performance for a turbojet engine. At the end of the study, the ecological coefficient of performance is evaluated parametrically and discussed depending on selected engine design parameters and performance measures. The author asserts the ecological coefficient of performance to be a beneficial indicator for researchers interested in aircraft propulsion system design and related topics.

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Faltsman, V. "Russia’s Economy Diversification." Voprosy Ekonomiki, no. 5 (May 20, 2015): 48–62. http://dx.doi.org/10.32609/0042-8736-2015-5-48-62.

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The article studies import substitution potential in a new geopolitical situation for the four most “import-intensive” industries that are characterized with the highest volume of import and negative foreign trade balance: agri-food sector, mechanical engineering, chemicals, transportation services and traveling. Prospects, preconditions and threats for import substitution of certain foodstuffs, tractors, rail cars, trucks, passenger cars, civil aircraft, plastics, tires, transportation services and traveling are analyzed. The import substitution process will be accompanied by diversification of industrial production. Potential reducing of the burden on primary exports due to contraction of imports in certain market niches and filling them with domestic manufacturing goods is assessed.

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Johnston, David W. "Unoccupied Aircraft Systems in Marine Science and Conservation." Annual Review of Marine Science 11, no. 1 (January 3, 2019): 439–63. http://dx.doi.org/10.1146/annurev-marine-010318-095323.

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The use of unoccupied aircraft systems (UASs, also known as drones) in science is growing rapidly. Recent advances in microelectronics and battery technology have resulted in the rapid development of low-cost UASs that are transforming many industries. Drones are poised to revolutionize marine science and conservation, as they provide essentially on-demand remote sensing capabilities at low cost and with reduced human risk. A variety of multirotor, fixed-wing, and transitional UAS platforms are capable of carrying various optical and physical sampling payloads and are being employed in almost every subdiscipline of marine science and conservation. This article provides an overview of the UAS platforms and sensors used in marine science and conservation missions along with example physical, biological, and natural resource management applications and typical analytical workflows. It concludes with details on potential effects of UASs on marine wildlife and a look to the future of UASs in marine science and conservation.

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Marai, Murhaf, Li Hui Lang, Shao Hua Wang, Li Jin Lin, Chun Lei Yang, and Xuan Luo. "Investigation on the Effect of Liquid Hammer Geometry to the Pressure Distribution of Innovative Hybrid Impact Hydroforming." Advanced Materials Research 941-944 (June 2014): 1843–49. http://dx.doi.org/10.4028/www.scientific.net/amr.941-944.1843.

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The innovative hybrid impact hydroforming (IHF) technology is a kind of high energy forming technique which can be used for forming complex parts with small features, such as convex tables, bars etc. which are widely employed in automotive and aircraft industries. The impact hydroforming technology means the most features are formed by hydroforming and the small features are rapidly reshaped by high intensity impact energy in a very short time after the traditional hydroforming. The impact pressure rises to the peak in 10ms which belongs to dynamic loading. The present work investigates IHF using a numerical /experimental approach. Finite element simulations using MSC.Patran were carried out changing the geometrical shape of liquid hammer.. Using this shock wave loading condition we did forming experiments. During forming process, stress distribution in the blank is comparatively better as compared with traditional methods so possibility of fracture is reduced. Inertia is also an important factor which affects control quality. Therefore, the research is very useful for improving forming quality of complicated products. It will be widely applied in automotive and aircraft industries.

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Varshavskii, A. E., and M. G. Dubinina. "Synergy of the military and civilian production: A case study of the aircraft industries." Национальные интересы: приоритеты и безопасность 13, no. 1 (January 27, 2017): 20–33. http://dx.doi.org/10.24891/ni.13.1.20.

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Kahrizi, Mohammad. "Cross Shaped Hydroforming Process Comparing of Finite Element Methodand Practical Works." Advanced Materials Research 705 (June 2013): 41–45. http://dx.doi.org/10.4028/www.scientific.net/amr.705.41.

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Recently, production of complex parts in car and aircraft industries, gas, water and hydraulic systems by hydroforming process has widely been used. Resistance of these parts, strain and displacement are factors whosedetermination isimportant. Strain and displacement are factors which determine the strength of the part. In this research,we will compare distance between latticed results obtained from theoretical method and practical works.

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Thian, Chow Vi. "CIVIL AND MILITARY AIRWORTHINESS CHALLENGES IN ASIA." Aviation 19, no. 2 (June 24, 2015): 78–82. http://dx.doi.org/10.3846/16487788.2015.1057993.

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Aviation is one of the most regulated industries in the world. The massive expansion and growth of aviation in the South-East Asia region has brought up many challenges in ensuring airworthiness of aircraft, both in the civil and military aviation domain. These challenges not only affect the safe operations of aircraft but also result in various issues in the areas of cost, infrastructure, human capital and resources. From the point of view of civil aviation, local authorities in the region have taken several initiatives to tackle these challenges, based on the foundations laid out by the International Civil Aviation Organization (ICAO). When it comes to military aviation, agencies, such as the Directorate General Technical Airworthiness (DGTA) of Malaysia, have initiated the regulation of the compliance of military aircraft operations. There has also been an increased focus on awareness of the importance of airworthiness and safety as well as the development of a risk-based approach which is both proactive and cost-efficient.

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Suchkov, A. N., V. T. Fedotov, O. N. Sevryukov, В. A. Kalin, A. A. Ivannikov, I. V. Fedotov, P. V. Morokhov, and A. E. Grigoryev. "Brazing of Metals, Alloys and Ceramics Using Rapidly Quenched Ribbon-Type Filler Metal STEMET." Advances in Science and Technology 88 (October 2014): 156–61. http://dx.doi.org/10.4028/www.scientific.net/ast.88.156.

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The work shows the main results on the development at NRNU MEPhI of rapidly quenched amorphous and nanocrystalline ribbon-type and powder brazing filler metals based on Al, Cu, Ni, Ti and Zr and their application for brazing of a wide range of materials in nuclear, thermonuclear, aerospace, automotive, aircraft and other industries: from steels, alloys and refractory metals to various ceramics without metallization of their surfaces.

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Podashev, Dmitriy, and Yuriy Dimov. "Processing of the edges of the parts on the robot complex." MATEC Web of Conferences 298 (2019): 00029. http://dx.doi.org/10.1051/matecconf/201929800029.

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In some fields of industry (especially in aircraft- and helicopter buildings) high requirements are made to the quality of the processed parts surfaces on the final operations. At the same time many operations (surface conditioning, edge cutting, radiussing etc) are done manually with expenditure of sufficient manpower. That’s why problem of mechanization and automatizaton of such final operations for these industries is very acute.

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Afyan, Aram I. "THE ROLE OF THE STATE IN FORMING THE COMPETITIVE ADVANTAGES OF THE RUSSIAN AIRCRAFT PRODUCTS ON THE WORLD MARKET." Scientific Review. Series 1. Economics and Law, no. 4 (2020): 69–77. http://dx.doi.org/10.26653/2076-4650-2020-4-06.

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The aviation industry for Russia is traditionally one of the important backbone elements of the national economy due to its belonging to knowledge-intensive and high-tech industries, the possibility of embedding in international technical and technological cooperation and cooperation, as well as its impact on innovative development and sustainability of economic growth. Despite the stagnation in the post-Soviet decade and the resulting trend towards lagging behind the leading aircraft-building countries, the development of the industry has always been of strategic importance for Russia, primarily in terms of ensuring the country's transport security. To implement integration tasks in such a huge country, a developed system of air transportation, including a national park of civil aircraft, needs to function.

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Mall, Yogesh Kumar, Md Sajid, Ramineni Jitendra Sai, Rambarki Deepak, and Guravtar Singh Mann. "Study of Additive Manufacturing for the Aircraft Industry." International Journal of Engineering and Advanced Technology 10, no. 2 (December 30, 2020): 181–87. http://dx.doi.org/10.35940/ijeat.b2051.1210220.

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This is a review paper on 3D printing, its significance, and future scope in the aircraft industry.In this article, additive manufacturing is compared with traditional manufacturing in the context of the aircraft industry that gives more accurate knowledge about how additive manufacturing is more effective in terms of cost-cutting, waste prevention, customization, and large-scale production. We will go into the need for 3D printing technology, how it has taken in step over other manufacturing process and are being used for a host of different applications. The paper gives sufficient information about various types of material used in additive manufacturing with the applications, examples, requirements, and process moreover some overview of limitations as well. How Rapid tooling is used with a different process to reduce time and get more productive and efficient parts for the aircraft industries. The use of 3D printing technology in the aircraft industry plays a major role and gained immense applications. It has greatly affected the production line due to its flexibility and ease of production. It is capable of producing intricate parts, a more resilient and lightweight structure that achievesa weight reduction of 40-60%, subsequently result in a leaner cost structure, material saving, and lower fuel consumption.The last section deals with the future scope of additive manufacturing in the aircraft industry with various parameters design aircraft wings, complex design parts, additive manufacturing in space. More companies and the aerospace industry continue to see the value of 3D printing and begin developing on-site 3D printing operations and investing in the technology.

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Das, Raj, and Rhys Jones. "Residual Strength Optimisation of a Vent Hole in an Aircraft Component Using a Heuristic Method." Advanced Materials Research 275 (July 2011): 105–8. http://dx.doi.org/10.4028/www.scientific.net/amr.275.105.

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The paper presents application of damage tolerance optimisation principles to the design of industrial components. It is illustrated via design optimisation of a Fuel Flow Vent Hole (FFVH) located in the Wing Pivot Fitting (WPF) of an F-111 aircraft. The aim is to determine the shape of the cutout that will maximise its residual strength under the operating loading conditions. Damage tolerance shape optimisation is performed using a heuristic optimisation method known as the ‘Biological algorithm’. The maximum stress intensity factor (SIF) for all of the cracks around the boundary of the optimal cutout is found to be significantly lower compared to that of the initial shape. This shows that an improved residual (fracture) strength is achieved for the optimal designs. The variability in SIF around the cutout boundary is reduced, thereby making the shape more evenly fracture critical. The shapes of the residual strength optimal vent holes are found to depend on the initial crack sizes. It is also shown that a damage tolerance optimisation additionally produces a lighter WPF component design, which is highly desirable for aerospace industries.

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SIADKOWSKA, Ksenia, and Zbigniew CZYŻ. "Selecting a material for an aircraft diesel engine block." Combustion Engines 178, no. 3 (July 1, 2019): 4–8. http://dx.doi.org/10.19206/ce-2019-301.

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Selecting appropriate materials is presently a complex task as material databases cover tens of thousands of different types of mate-rials. Product designing proceeds in numerous stages and in most of them there are open questions with not only one correct solution but better and worse ones. This paper overviews the Diesel engine body construction materials mentioned in the literature and discusses a certain practical method to select materials for a cylinder head and a Diesel engine block as a prototype. The engine body, depending on its purpose, is most frequently iron or aluminum. If it is important to optimize parts to achieve low weight, aluminum alloys are usual-ly applied, especially in the automotive and aviation industries. In the latter case, weight is even more important so new types of magne-sium alloys which are even lighter than aluminum ones are developed and used. However, magnesium alloys are, for example, more flammable and not enough strong so, for safety reasons, this type of material is not used solely in engine bodies.

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Frigant, Vincent, and Damien Talbot. "Technological Determinism and Modularity: Lessons from a Comparison between Aircraft and Auto Industries in Europe." Industry & Innovation 12, no. 3 (September 2005): 337–55. http://dx.doi.org/10.1080/13662710500195934.

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Vahdati, N. "A Detailed Mechanical Model of a Double Pumper Fluid Mount." Journal of Vibration and Acoustics 120, no. 2 (April 1, 1998): 361–70. http://dx.doi.org/10.1115/1.2893839.

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Conventional passive elastomenc mounts have been used as noise and vibration isolators in the automotive and aircraft industries for many years. For even better noise and vibration isolation, passive fluid mounts have been replacing elastomeric mounts in both the automotive and aerospace industries during the past few years. With more increase in the popularity of fluid mounts, it is important to characterize the dynamics of the fluid mounts more accurately. Many papers have been published on the modeling of these devices, but mostly on single pumper fluid mounts. In this paper, we focus on double pumper fluid mounts. The intent of this paper is to develop a very detailed model of a double pumper fluid mount including all dampings.

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Shanmugasundaram, Sureshkumar Manickam, Lakshmanan Damodhiran, and Makesh Kumar Rajendran. "Delamination Analysis Using Digital Image Processing for Developing a Prediction Model for Drilling on GFRP Composite Laminates." Applied Mechanics and Materials 446-447 (November 2013): 403–7. http://dx.doi.org/10.4028/www.scientific.net/amm.446-447.403.

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The growing demand for light weight materials for the application in the aircraft industries, aerospace industries, marine, sports and recreation industries has attracted the usage of fiber reinforced materials especially GFRP composites. Usage of these kind of materials are exponentially increasing because of its specific engineering characteristics like high strength to weight ratio. Drilling of these materials has been always a challenge because of its heterogeneous nature. Better hole quality is required for these materials for the assembly into components. In this work delamination analysis was attempted using digital image processing, experiments are carried out for 27 holes using full factorial design and it was observed that scanned images obtained using a flat bed scanner (HP, 1300 DPI) used for digital image processing, gives better visualization for delamination. The feed rate is the most influencing parameter out of the three process input parameters considered.

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Yang, Xiao, and Bo Jiang. "Multi-Objective Fleet Assignment Problem Based on Self-Adaptive Genetic Algorithm." Advanced Materials Research 694-697 (May 2013): 2895–900. http://dx.doi.org/10.4028/www.scientific.net/amr.694-697.2895.

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Since the beginning of the twenty-first century, energy conservation has become the theme of the development of the world. China government set the emissions-reduction targets in various industries on the 12th Five-Year Plan. And the airlines were committed to reduce their carbon emissions. From an operational perspective, the airline model assignment problem is a key factor of the total carbon emissions on the entire route network. But the traditional aircraft assignment models approach did not account for this purpose to reduce carbon emissions. By constructing the multi-objective optimization models consider carbon emissions assignment model using a genetic algorithm, numerical example shows that the model is able to meet all aspects demand which include meeting route network capacity demand, minimizing operating costs and reducing total aircraft fleet carbon emissions.

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Featherston, C. A., Mark J. Eaton, S. L. Evans, Karen M. Holford, Rhys Pullin, and Matthew Cole. "Development of a Methodology to Assess Mechanical Impulse Effects Resulting from Lightning Attachment to Lightweight Aircraft Structures." Applied Mechanics and Materials 24-25 (June 2010): 129–34. http://dx.doi.org/10.4028/www.scientific.net/amm.24-25.129.

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The effect of lightning attachment to structures and vehicles is a cause of major concern to a number of different industries, in particular the aerospace industry, where the consequences of such an event can be catastrophic. In 1963, a Boeing 707 was brought down in Maryland killing 81 people on board, triggering the improvement of lightning protection standards. However, commercial jets are still struck on average once every 10,000 hours of flight time and between 1963 and 1989 forty lightning related accidents were recorded within the U.S.A alone. The rapid increase in the use of composite materials in aircraft design and the consequent increase in complexity when determining the effects of a lightning strike, has led to new challenges in aircraft protection and the requirement for improved understanding and standardisation.

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Ng, Yang Siong Robson, and Hamad Rashid. "Enhancing human performance reliability in aircraft pushback operations." International Journal of Quality & Reliability Management 36, no. 4 (April 1, 2019): 485–509. http://dx.doi.org/10.1108/ijqrm-01-2018-0008.

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Purpose The purpose of this paper is to investigate the aircraft pushback operations to predict and manage human errors, particularly those associated with the complex team work of carrying out the pushback operation. This should improve air ramp operations reliability. Design/methodology/approach The study applied the human reliability assessment “Systematic Human Error Reduction and Prediction Approach” that involved a total of 60 semi-structured interviews with practicing experts. Past ramp accident reports were also reviewed to provide more in-depth insights to the problem. Findings Some of the key performance reliability-degrading errors identified relate to some frequent critical technical inabilities within the team of headset operator and tug driver, as well as the vulnerable intra-team communications. Several best practices were similarly identified. Practical implications Based on its findings, this study proposes a new technological concept that can help enhancing safety of aircraft pushback operations. This should enhance reliability of aircraft ground handling and improve aircraft availability. It also provided a generic methodological approach to improve safety-critical operations within high-risk industries. Social implications This study responses to the increasing trend in ramp accidents worldwide. Originality/value The research conducted to date in this area is still quite limited compared to that of flight and aircraft maintenance safety. The relevant existing studies focus more on ramp safety holistically, and do not go into the details of how safety and reliability of a ramp operation can be improved. The current paper aims at filling this gap.

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Varyukhina, E. V., and V. V. Klochkov. "Modelling of the Impact of National Standardization on Duopolistic Competition in the Civil Aircraft Market." Zhurnal Economicheskoj Teorii 17, no. 4 (2020): 859–73. http://dx.doi.org/10.31063/2073-6517/2020.17-4.10.

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The purpose of this study is to analyze standards as one of the main tools of protectionism in global markets of industrial goods. We use standards for modeling of market competition and adapt this approach for civil aviation markets. The role of local noise standards in civil aircraft markets is discussed. Imposition of more stringent aviation noise standards is modelled in the form of a two-person non-zero-sum game. Players are aircraft corporations that conduct research and development to reduce noise and lobby for stricter regulations in their controlled markets. The model can be used to predict that tighter aviation noise standards will be imposed and to justify the strategy of Russian aviation industry and science. The proposed approach can be adapted for other industries with strict regulations (in terms of safety, ecology). Such estimation allows us to assess whether it is in the country’s interests to participate in the standards race or not. It is shown that the equilibrium degree of standards tightening is higher if the players’ market shares are close to equal or individual players have advantages in the cost of production and/or product improvement is highly likely due to the company’s R&D progress.

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Полупан, А. С. "ДОСЛІДЖЕННЯ ПИТАННЯ ВПРОВАДЖЕННЯ АДИТИВ-НИХ ТЕХНОЛОГІЙ В АВІАБУДІВНУ ГАЛУЗЬ." Open Information and Computer Integrated Technologies, no. 88 (November 6, 2020): 112–22. http://dx.doi.org/10.32620/oikit.2020.88.09.

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The article deals the issues of improving the quality, reducing time, cost of manufacturing domestic aircraft and reducing their weight by modernizing technological processes taking into account a wide range of functionalities for the use of additive technologies for the production of structural elements of aircraft from titanium alloys. The article provides is determined that titanium and its alloys, due to their unique chemical and mechanical characteristics, continue to be relevant and in demand metal used in the construction of modern aircraft. But traditional methods of manufacturing parts made of titanium are high cost and do not allow the use of this metal in large quantities. The solution proposed to this problem is the use of additive manufacturing technologies for the manufacture of aircraft structural elements from titanium. Data are given about of the use of titanium alloys in the aerospace, automotive, biomedical and chemical industries due to the excellent combination of strength, low density, as well as very high corrosion resistance and fatigue strength are given. The efficiency of using titanium alloys for the manufacture of structural elements of aircraft in terms of reducing the total weight of the aircraft and high reliability of the structure as a whole. The article provides descriptive information about additive technologies in mechanical engineering. The review of works of foreign scientists concerning research of differences in mechanical characteristics, microstructure and macrostructure of samples made by means of additive technologies is resulted, their advantages and lacks are noted. The list of advantages of additive technologies in mechanical engineering which cause economic efficiency from their use is resulted. Attention is drawn to the most common methods of additive production: substrate synthesis (PBF), direct energy and material supply (DED). It is given the tasks of research are defined and the decision of optimization of technology of manufacturing of elements of a design of aircraft. Research will further improve the technology of aircraft production.

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Zębala, Wojciech, and Andrzej Matras. "Aspects of Fibre Composite Machining." Technological Engineering 9, no. 2 (December 1, 2012): 18–20. http://dx.doi.org/10.2478/teen-2012-0005.

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Abstract Paper presents some aspects of fibre composite milling. Composites are particularly applied in the sectors such as aircraft, aerospace and automotive industries for they are light and relatively easy can be forming in the desired shapes. The purpose of research was optimization of free form milling considering the machined surface quality (mainly roughness). After proper cutting parameters selection (feed and cutting speed) the example parts with free form surface were machined.

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Ahrens, Ralf. "The importance of being European: Airbus and West German industrial policy from the 1960s to the 1980s." Journal of Modern European History 18, no. 1 (December 20, 2019): 63–78. http://dx.doi.org/10.1177/1611894419894475.

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Focusing on the time span from the 1960s to the late 1980s, that is, on the period during which Airbus established itself as a serious competitor on the world market, this article analyses the German aircraft industry’s interests, its representation within the transnational Airbus project, and the relevance of what might be called ‘Europeanness’. Occasionally also touching upon the situation in its partner countries, the central question is whether the respective political strategies of collaboration in the German aircraft industry were motivated by self-serving national interests or broader European ones. The article is divided into three sections. It begins by scrutinizing the motivations of German politics in the establishment and promotion of the Airbus project. Second, it deals with the representation of national interests in the allocation of production shares and the organization of cooperation, and, finally, with the European aspects of the massive subsidization of national manufacturers. It comes to the conclusion that the German case in particular illustrates that European collaboration in the aircraft sector was appreciated as an instrument to facilitate the survival of national industries pursuing their own business interests. The establishment of Airbus was supported as a European project to ensure the survival of the German aircraft industry and sometimes even as an instrument of business concentration. Nevertheless, notions about European integration or Franco-German friendship certainly increased the willingness to spend a lot of money on the Airbus project as the flagship of entanglement and interconnectedness in a ‘future industry’.

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Journal articles on the topic 'Aircraft Industries'

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