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Littérature scientifique sur le sujet « Aerospace alloy »

Auteur : Grafiati

Publié le 4 juin 2021

Mis à jour le 4 février 2022

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Articles de revues sur le sujet "Aerospace alloy"

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Warner, Timothy. "Recently-Developed Aluminium Solutions for Aerospace Applications." Materials Science Forum 519-521 (July 2006): 1271–78. http://dx.doi.org/10.4028/www.scientific.net/msf.519-521.1271.

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Two principal approaches are available to materials’ engineers to improve the overall cost-weight balance of metallic airframe structures: improving alloy performance and optimising materials’ utilisation. Although both approaches have been successful in the past, they are most effective when applied concomitantly. The Aluminium industry has a long record of improving aerospace alloys’ performance. Nevertheless, even in apparently well-explored alloy systems such as the 7xxx family, products with improved damage tolerance-strength balances have recently been developed, thanks to an improved un

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Barnes, Anthony J., Hari Raman, Andrew Lowerson, and David Edwards. "Recent Application of Superformed 5083 Aluminum Alloy in the Aerospace Industry." Materials Science Forum 735 (December 2012): 361–71. http://dx.doi.org/10.4028/www.scientific.net/msf.735.361.

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Traditionally the Aerospace Industry has, most often, selected heat treatable aluminum alloys for its sheet metal fairings, panels and skins. With the introduction of superplastic forming (SPF) in the late 70’s and early 80’s the initial applications of SPF aluminum utilized the heat treatable superplastic alloys that were available then (ie. 2004 and 7475). When superplastic 5083 alloy sheet became commercially available in the late 1980’s applications were focused on the ‘high end’ automobile and the European rail markets. More recently, the qualification of SP5083 to aerospace standards, co

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MATSUO, Mamoru. "Application of aluminum alloy superplasticity in aerospace." Journal of Japan Institute of Light Metals 36, no. 1 (1986): 43–50. http://dx.doi.org/10.2464/jilm.36.43.

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Vrabeľ, Marek, and Martin Eckstein. "Hole Making of Inconel 718 Aerospace Alloy." Acta Mechanica Slovaca 20, no. 1 (2016): 10–13. http://dx.doi.org/10.21496/ams.2016.002.

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Woodfield, Andrew, and Gérard Lemaitre. "Aerospace Titanium Alloy Melt Process Quality Improvements." MATEC Web of Conferences 321 (2020): 04008. http://dx.doi.org/10.1051/matecconf/202032104008.

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This Jet Engine Titanium Quality Committee (JETQC) paper describes industry quality improvements since 1990. Quality refers to freedom from melt-related hard-alpha and high-density inclusions (HDI). JETQC, formed under the auspices of the U.S. Federal Aviation Administration (FAA) following the Sioux City aircraft accident in 1989, is comprised of U.S., E.U. and Japanese aircraft engine manufacturers to address the quality of premium / rotor quality titanium alloy production. Titanium suppliers provide melt-related inclusion data. JETQC focuses on hard-alpha and HDI inclusion rates in premium

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Ramesh Narayanan, P., Satyam Suwas, K. Sreekumar, Parameshwar Prasad Sinha, and Srinivasa Ranganathan. "Evolution of Crystallographic Texture in Cold Rolled Al-Zn-Mg Alloys Used in Space Applications." Materials Science Forum 702-703 (December 2011): 315–19. http://dx.doi.org/10.4028/www.scientific.net/msf.702-703.315.

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The aerospace industry uses a variety of materials in different forms like sheets, forgings, extruded rods, welded components and machined components for launch vehicle and satellite applications. As lighter and stronger materials are the aims of the aerospace industry, aluminium alloys are the most widely used materials in the in the aircraft and aerospace industries. These aluminum alloys used in the aerospace industry are subjected to a variety of processing operations, either in the sheet form after rolling, forging, heat treatment and machining conditions, to realize the final product imp

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Kemp, R. M. J., R. N. Wilson, and P. J. Gregson. "A Comparison of the Corrosion Fatigue Properties of Plate Aluminium Alloys for Aerospace Applications." Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 207, no. 2 (1993): 97–104. http://dx.doi.org/10.1243/pime_proc_1993_207_253_02.

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A corrosive environment such as salt water can severely degrade the fatigue properties of aluminium alloys used in aerospace applications. The corrosion fatigue crack growth rate properties of two conventional alloys, that is Al-Zn-Mg-Cu-Zr alloy (7010-T7651) and Al-Cu-Mg alloy (2024–T351) have been compared with the more recently developed Al-Li-Cu-Mg alloy (8090-T8771). Increased growth rates were observed in salt water compared to air for 7010 and 8090 but not for 2024. Comparing the three alloys, the 8090 alloy corrosion fatigue rates were similar to those of 2024 which were considerably l

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Batool, Syeda Ammara, Akhlaq Ahmad, Abdul Wadood, Abdul Mateen, and Syed Wilayat Hussain. "Development of Lightweight Aluminum-Titanium Alloys for Aerospace Applications." Key Engineering Materials 778 (September 2018): 22–27. http://dx.doi.org/10.4028/www.scientific.net/kem.778.22.

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Aluminum (Al) and Titanium (Ti) based lightweight alloys have been a topic of discussion and research for a few decades now. Resulting alloys with hard intermetallic phases in Al-Ti binary system have good microstructural and mechanical properties including low densities, high specific strength, better resistance against oxidation and corrosion which are highly desirable in aerospace industry. Such an alloy system was studied in our research. Powder metallurgy (PM) was used as processing route because of its economical and easy operation. Samples were prepared using metallic powders of Aluminu

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Vijayakumar, T., T. Senthilvelan, and R. Venkatakrishnan. "Wear Behaviour of Polyurethane Coated Aerospace Aluminium Alloy (7075)." Applied Mechanics and Materials 813-814 (November 2015): 252–56. http://dx.doi.org/10.4028/www.scientific.net/amm.813-814.252.

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This paper envisages to predict the life of an aircraft coating using high strength precipitation hardening 7000 series aluminum alloys, such as 7075 which is used extensively in aerospace industry. Aerospace aluminum alloy 7075 has been researched upon especially for aircraft materials. The intention of protective coating is to save the aerospace aluminium alloy 7075 metal surface from weatherability and, at the same time, to obtain the required degree of cosmetic finish for the object. One was epoxy polyamide as primer layer and other was the polyurethane as top-coat layer of coating through

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Krämer, A., Dieter Lung, and Fritz Klocke. "High Performance Cutting of Aerospace Materials." Advanced Materials Research 498 (April 2012): 127–32. http://dx.doi.org/10.4028/www.scientific.net/amr.498.127.

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Titanium and nickel-based alloys belong to the group of difficult-to-cut materials. The machining of these high-temperature alloys is characterized by low productivity and low process stability as a result of their physical and mechanical properties. Major problems during the machining of these materials are low applicable cutting speeds due to excessive tool wear, long machining times, and thus high manufacturing costs, as well as the formation of ribbon and snarled chips. Under these conditions automation of the production process is limited. This paper deals with strategies to improve machi

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Thèses sur le sujet "Aerospace alloy"

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YANG, LIN. "CORROSION INHIBITOR SYSTEM FOR SUPERPRIMER COATINGS ON AEROSPACE ALLOY." University of Cincinnati / OhioLINK, 2005. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1135970650.

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Mojarad, Farimani Saeed. "Experimental process development and aerospace alloy formability studies for hydroforming." Mémoire, École de technologie supérieure, 2013. http://espace.etsmtl.ca/1261/1/MOJARAD_FARIMANI_Saeed.pdf.

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Dans le procédé d’hydroformage, la pression d’un fluide est utilisée pour déformer plastiquement un tube paroi mince à l’intérieur d’une matrice fermée afin de remplir la cavité de la matrice. L’hydroformage des tubes possède de nombreux avantages qui rendent ce procédé très intéressant pour plusieurs industries telles que l’automobile et l’aérospatiale. Mais, à cause de différents facteurs tels que la formabilité des matériaux, l’ordre et les séquences du chargement (force de compression axiale et pression interne pendant le procédé), la géométrie de l’outil et la friction, c’est un procédé d

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Baxter, Gavin James. "Fatigue damage accumulation in titanium alloy IMI 834." Thesis, University of Sheffield, 1994. http://etheses.whiterose.ac.uk/14764/.

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As current aerospace materials are subjected in service to increasingly onerous conditions of stress and temperature, the hazard of fatigue failure becomes more acute. Engineers utilise the methodology of fracture mechanics to estimate fatigue crack growth rates but fatigue crack initiation, which involves the interplay of many microprocesses, is only investigated empirically. The aim of this study was to investigate the fatigue damage accumulation mechanisms in the titanium alloy IMI 834 in order to develop a fundamental understanding of the controlling physical processes and the micromechani

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Henry, Dilys M. "The nature and effects of hydrogen in weldalite aerospace alloy and other commercial aluminium-lithium alloys." Thesis, Brunel University, 1995. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.340935.

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Roets, Philip J. "Development of a hybrid light alloy - carbon fibre aerospace structural panel." Thesis, Stellenbosch : University of Stellenbosch, 2010. http://hdl.handle.net/10019.1/4151.

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Thesis (MScEng (Mechanical and Mechatronic Engineering))--University of Stellenbosch, 2010.<br>ENGLISH ABSTRACT: The development of light and sti aerospace structural panels is very important in the aerospace industry, e.g. a lighter satellite requires less fuel to launch it into space which in turn saves money for the owner of the satellite. This thesis describes the design, optimisation, manufacturing and testing of a ribbed light alloy core - carbon bre face sheets, sandwich-type, satellite panel operating at launch loading conditions (115 m/s2 accelerations and requiring a minimum s

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Whittaker, Jarrod Talbott. "Ductility and Use of Titanium Alloy and Stainless Steel Aerospace Fasteners." Scholar Commons, 2015. http://scholarcommons.usf.edu/etd/5796.

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The main purpose of this thesis is to investigate the ductility and application of titanium alloys, like titanium 6Al-4V, when used in aerospace fasteners compared to more conventional stainless steel aerospace fasteners such as A286. There have been concerns raised about the safe usability of titanium 6-4 in the aerospace industry due to its lack of strain hardening. However, there is a lack of data pertaining to this concern of safe usage which this thesis aims to address. Tensile tests were conducted to find the ductility indexes of these fasteners which quantify the amount of plastic to el

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Derry, Christopher Graham. "Characterisation and modelling of toughness in aerospace aluminium alloy friction stir welds." Thesis, University of Manchester, 2008. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.494597.

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The effect of friction stir welding (FSW) on the toughness properties of two aerospace aluminium alloys has been investigated. Two typical aerospace alloys, high strength AA7449 and medium strength AA6013 have been studied in detail. The mechanical properties have been characterised via hardness testing, toughness testing and tensile testing incorporating strain analysis via digital image correlation. A notched 5ar test has been used to produce a profile of toughness across each of the welds and, in AA7449, through the depth of the welded plate. Each fracture surface was examined via FEGSEM to

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Nabhani, Farhad. "The performance of ultra-hard cutting tool materials in maching aerospace alloy TA48." Thesis, University of Hull, 1991. http://hydra.hull.ac.uk/resources/hull:4627.

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A study has been made of the respective performance of cubic boron nitride (CBN) and polycrystalline diamond (PCD) cutting tool materials and compared to various coated and uncoated tungsten carbide grades when cutting titanium alloy workpieces. Two important experimental techniques were employed during the course of this work, firstly a quasi-static contact method was employed to establish the workpiece/tool interfacial temperature above which strongly adherent layers may be formed. This technique revealed that the critical temperatures which marked adhesion and welding, were 740, 820 and 800

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Boag, Adam Paull, and adam boag@gmail com. "The Relationship Between Microstructure and Stable Pitting Initiation in Aerospace Aluminium Alloy 2024-T3." RMIT University. Applied Science, 2009. http://adt.lib.rmit.edu.au/adt/public/adt-VIT20091028.114831.

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Aluminium alloys are essential to a variety of industry sectors, particularly transport, where they are used in the production of cars and aeroplanes. However, aluminium alloys are susceptible to degradation through corrosion which can compromise the integrity of components manufactured from this material. Therefore research into the means by which these alloys degrade is important. This thesis aims to understand how one of the more potentially damaging types of corrosion, known as pitting corrosion, occurs in the important aluminium alloy 2024-T3 (AA2024-T3). In order to study this pheno

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Jerrard, Peter George Eveleigh. "Selective laser melting of advanced metal alloys for aerospace applications." Thesis, University of Exeter, 2011. http://hdl.handle.net/10036/3576.

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Research focused on the selective laser melting (SLM) of stainless steels and aluminium alloys. For steels, the possibility of creating a magnetically graded material was demonstrated as well as the ability to improve consolidation with austenitic and martensitic stainless steel powder mixtures. Stainless Steel/CoCr hybrid samples were also manufactured and tested to investigate the advantages of functionally graded materials (FGMs). Al alloy research began with examining the requirements for successful Al alloy consolidation in SLM and through experimentation it was found that Al alloys with

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Livres sur le sujet "Aerospace alloy"

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Gangloff, R. P. NASA-UVa light aerospace alloy and structures technology program (LA²ST). National Aeronautics and Space Administration, 1996.

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Gangloff, R. P. NASA-UVa light aerospace alloy and structures technology program (LA²ST). National Aeronautics and Space Administration, 1996.

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Gangloff, R. P. NASA-UVa light aerospace alloy and structures technology program (LA²ST). National Aeronautics and Space Administration, 1996.

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Xian jin hang kong lü he jin cai liao yu ying yong: Advanced areanautical aluminum alloy materials technology and application. Guo fang gong ye chu ban she, 2012.

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Starke, E. A. NASA-UVa Light Aerospace Alloy and Structure Technology Program supplement: aluminum-based materials for high speed aircraft. Langley Research Center, 1993.

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Gangloff, R. P. NASA-UVa Light Aerospace Alloy and Structures Technology Program (LA2ST): A progress report, January 1, 1991 to June 30, 1991. School of Engineering & Applied Science, University of Virginia, 1991.

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Gangloff, R. P. NASA-UVa Light Aerospace Alloy and Structures Technology Program (LA2ST): A progress report, January 1, 1991 to June 30, 1991. School of Engineering & Applied Science, University of Virginia, 1991.

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Tack, Andrew J. The effect of microstructure and loading variables on fatigue crack propagation in three aerospace bearing steels anda low alloy steel. University of Birmingham, 1989.

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Gialanella, Stefano, and Alessio Malandruccolo. Aerospace Alloys. Springer International Publishing, 2020. http://dx.doi.org/10.1007/978-3-030-24440-8.

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Starke, E. A. NASA-UVa light aerospace alloy and structures technology program supplement: aluminum-based materials for high speed aircraft: semi-annual report, July 1, 1992-December 31, 1992. Langley Research Center, 1995.

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Chapitres de livres sur le sujet "Aerospace alloy"

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Bhattacharjee, A., B. Saha, and J. C. Williams. "Titanium Alloys: Part 2—Alloy Development, Properties and Applications." In Aerospace Materials and Material Technologies. Springer Singapore, 2016. http://dx.doi.org/10.1007/978-981-10-2134-3_6.

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Balan, K. P., and A. Venugopal Reddy. "Aero Steels: Part 1—Low Alloy Steels." In Aerospace Materials and Material Technologies. Springer Singapore, 2016. http://dx.doi.org/10.1007/978-981-10-2134-3_7.

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Srinivas, M., and A. Venugopal Reddy. "Aero Steels: Part 2—High Alloy Steels." In Aerospace Materials and Material Technologies. Springer Singapore, 2016. http://dx.doi.org/10.1007/978-981-10-2134-3_8.

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Wanhill, R. J. H. "Structural Alloy Testing: Part 1—Ambient Temperature Properties." In Aerospace Materials and Material Technologies. Springer Singapore, 2016. http://dx.doi.org/10.1007/978-981-10-2143-5_9.

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Schick, Justin R., Darren J. Hartl, and Dimitris C. Lagoudas. "Incorporation of Shape Memory Alloy Actuators into Morphing Aerostructures." In Morphing Aerospace Vehicles and Structures. John Wiley & Sons, Ltd, 2012. http://dx.doi.org/10.1002/9781119964032.ch10.

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Zheng, Qingjun, Banqiu Wu, and Ramana G. Reddy. "In-SituFormation of AIN Reinforced Al Alloy Composites Using Ammonia." In Lightweight Alloys for Aerospace Application. John Wiley & Sons, Inc., 2013. http://dx.doi.org/10.1002/9781118787922.ch27.

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Reynolds, Anthony P., Bob Wheeler, and Kumar V. Jata. "Deformation, Fracture and Fatigue in a Dispersion Strengthened Aluminum Alloy." In Lightweight Alloys for Aerospace Application. John Wiley & Sons, Inc., 2013. http://dx.doi.org/10.1002/9781118787922.ch8.

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Fleck, P., K. Koziar, G. Davila, et al. "The Effect of Retrogression and Reaging on 7249 Aluminum Alloy." In Lightweight Alloys for Aerospace Application. John Wiley & Sons, Inc., 2013. http://dx.doi.org/10.1002/9781118787922.ch9.

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Sinha, V., M. J. Mills, and J. C. Williams. "Dwell-Fatigue Behavior of Ti-6Al-2Sn-4Zr-2Mo-0.1Si Alloy." In Lightweight Alloys for Aerospace Application. John Wiley & Sons, Inc., 2013. http://dx.doi.org/10.1002/9781118787922.ch18.

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Verhaeghe, Geert, and Paul Hilton. "Laser Welding of Low-Porosity Aerospace Aluminum Alloy." In Proceedings of the 34th International MATADOR Conference. Springer London, 2004. http://dx.doi.org/10.1007/978-1-4471-0647-0_36.

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Actes de conférences sur le sujet "Aerospace alloy"

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Shrimpton, G. R. D., and H. C. Angus. "Aluminum-Lithium Alloy Forgings for Aerospace." In Aerospace Technology Conference and Exposition. SAE International, 1988. http://dx.doi.org/10.4271/881404.

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Henriques, Vinicius Andr\ae Rodrigues, Jos\ae Luis de Oliveira, Edevaldo Faria Diniz, and Ana Carolina Silva Machado Dutra. "Gamma Ti-Al Alloy Production for Aerospace Applications." In SAE Brasil 2011 Congress and Exhibit. SAE International, 2011. http://dx.doi.org/10.4271/2011-36-0042.

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Naydenkin, E. V., I. P. Mishin, I. V. Ratochka, and V. A. Vinokurov. "High-strength nanostructured titanium alloy for aerospace industry." In ADVANCED MATERIALS WITH HIERARCHICAL STRUCTURE FOR NEW TECHNOLOGIES AND RELIABLE STRUCTURES. AIP Publishing LLC, 2015. http://dx.doi.org/10.1063/1.4932850.

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Novotny, Paul M., and Thomas J. McCaffrey. "An Advanced Alloy for Landing Gear and Aircraft Structural Applications - Aerometr® 100 Alloy." In Aerospace Technology Conference and Exposition. SAE International, 1992. http://dx.doi.org/10.4271/922040.

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Verhaeghe, G., P. Hilton, and S. Barnes. "Achieving Low-Porosity Laser Welds in Aerospace Aluminium Alloy." In Aerospace Manufacturing Technology Conference & Exposition. SAE International, 2003. http://dx.doi.org/10.4271/2003-01-2895.

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Yoshinouchi, T., H. Yoshizawa, N. Tsuno, and S. Ikeda. "Metal Injection Molding of Alloy 718 for Aerospace Applications." In Superalloys. John Wiley & Sons, Inc., 2014. http://dx.doi.org/10.7449/2014/superalloys_2014_437_446.

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Roach, T. A. "Alloy 718 Fasteners: Versatility and Reliability for Aerospace Design." In Superalloys. TMS, 1989. http://dx.doi.org/10.7449/1989/superalloys_1989_381_389.

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Keener, Steven G. "Advanced Low-cost Titanium-alloy Materials for Aerospace Fastener Applications." In Aerospace Technology Conference and Exposition. SAE International, 2007. http://dx.doi.org/10.4271/2007-01-3839.

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Yan, Jingxuan, Xierong Hu, Jiaxiong Fang, and Guosen Xu. "Study of the recombination mechanisms and carrier lifetimes in Hg0.8Cd0.2Te alloy." In Aerospace Sensing, edited by Eustace L. Dereniak and Robert E. Sampson. SPIE, 1992. http://dx.doi.org/10.1117/12.137806.

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Haag, Chris, Monish Tandale, and John Valasek. "Characterization of Shape Memory Alloy Behavior and Position Control Using Reinforcement Learning." In Infotech@Aerospace. American Institute of Aeronautics and Astronautics, 2005. http://dx.doi.org/10.2514/6.2005-7160.

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Rapports d'organisations sur le sujet "Aerospace alloy"

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Rodriguez, Salvador, Andrew Kustas, and Graham Monroe. Metal Alloy and RHEA Additive Manufacturing for Nuclear Energy and Aerospace Applications. Office of Scientific and Technical Information (OSTI), 2020. http://dx.doi.org/10.2172/1644167.

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Dawson, Paul, Matthew Miller, Kevin McNelis, Amanda Oczkowski, Jun-Sang Park, and James Williams. A New Multiscale Methodology for Evaluating Distributions of Residual Stress in Processed Aerospace Alloys. Defense Technical Information Center, 2013. http://dx.doi.org/10.21236/ada582421.

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