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Статті в журналах з теми "Cargo cabin"

Автор: Grafiati

Опубліковано: 30 травня 2022

Оновлено: 31 липня 2025

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1

Shen, Yang. "An Anti-Collision Method of Slip Barrel for Automatic Ship Loading in Bulk Terminal." Polish Maritime Research 23, s1 (2016): 144–51. http://dx.doi.org/10.1515/pomr-2016-0059.

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Анотація:

Abstract During the loading operation of a ship loader in bulk terminal, in order to bring bulk cargo, such as coal and ore, precisely into every corner of the cabin and not to raise dust at the same time, the slip barrel mechanism usually is placed fully inside the ship cabin near the cargo as close as possible. However, if too close, it will increase the risk of collision between slip barrel and cargo, which poses a security risk to loading operation. This article proposes an anti-collision method for slip barrel in the process of automatic ship loading in bulk terminal. This method can accu

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2

Çiçek, Oktay, and A. Cihat Baytaş. "Local thermal non-equilibrium conjugate forced convection and entropy generation in an aircraft cabin with air channel partially filled porous insulation." Aircraft Engineering and Aerospace Technology 94, no. 2 (2021): 210–25. http://dx.doi.org/10.1108/aeat-02-2021-0039.

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Анотація:

Purpose The purpose of this study is to numerically investigate heat transfer and entropy generation between airframe and cabin-cargo departments in an aircraft. The conjugate forced convection and entropy generation in a cylindrical cavity within air channel partly filled with porous insulation material as simplified geometry for airframe and cabin-cargo departments are considered under local thermal non-equilibrium condition. Design/methodology/approach The non-dimensional governing equations for fluid and porous media discretized by finite volume method are solved using the SIMPLE algorithm

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3

Liu, Mingtao, Youshuang Jin, and Gang Chen. "Kinetic Characteristics Analysis of Hydraulic Boom of In-Cabin Palletizer Considering Working Condition Parameters." Journal of Research in Science and Engineering 7, no. 4 (2025): 38–43. https://doi.org/10.53469/jrse.2025.07(4).8.

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To address collision risks and spatial limitations of hydraulic booms in in-cabin palletizers operating within confined cargo holds, this study proposes a safety framework integrating kinematic analysis and collision detection. The method constructs a kinematic model mapping hydraulic cylinder displacements to boom rotation angles, incorporating geometric constraints from cylinder parameters and boom cross-sectional dimensions. Forward/inverse kinematic solutions generate motion trajectories compliant with workspace boundaries. Obstacle geometric models embedded in the kinematic framework enab

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4

Cui, Hongwei, Chenran Ruan, Shengdong Wang, Song Lu, Heping Zhang, and Minqiang Wang. "Study on Response Time Hysteresis Model of Smoke Detectors in Aircraft Cargo Compartment." Fire 7, no. 9 (2024): 317. http://dx.doi.org/10.3390/fire7090317.

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Анотація:

A fire in the cargo compartment has a major impact on civil aviation flight safety, and according to the airworthiness clause of the CCAR-25, the detector must sound an alarm within 1 min of a fire in the cargo compartment. As for the cargo compartment of large transport aircrafts, the internal space is high and open, and the smoke movement speed becomes slower with significant cooling in the process of diffusion. Hysteresis can occur in smoke detectors because of their internal labyrinth structure, which causes the detector’s internal and external response signals to be out of sync. This rese

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5

Schomaker, Ralf, Björn Knickrehm, and Jürgen Langediers. "Safety Release Fasteners Enable New Cabin/Cargo Decompression Concept." SAE International Journal of Aerospace 9, no. 1 (2016): 177–80. http://dx.doi.org/10.4271/2016-01-2082.

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6

Gao, Tianhe, Ziyu Xu, Zengcong Li, Pei Liu, and Kuo Tian. "Two-Stage Intelligent Layout Design of Curved Cabin Door." Aerospace 10, no. 1 (2023): 89. http://dx.doi.org/10.3390/aerospace10010089.

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As one of the most complex and critical components of spacecraft, the structural design of the curved cabin door faces two challenges. On the one hand, it is difficult to obtain innovative configurations for the cabin door in the preliminary design stage. On the other hand, the traditional optimization design algorithm is inefficient in the detailed design stage. In this paper, a two-stage intelligent method for the layout design of the curved cabin door is proposed. In the first stage, the innovative stiffener layout of the cabin door is obtained based on the topology optimization method. The

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7

Huang, Weixing, Tonghui Yang, and Zhengye Lv. "Analysis of fire test methods and airworthiness requirements for materials in the cabin of civil aircraft." Journal of Physics: Conference Series 2961, no. 1 (2025): 012011. https://doi.org/10.1088/1742-6596/2961/1/012011.

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Abstract The safety of aircraft cabin materials is related to the safety of passengers and aircraft. With the development of science and technology, the types of materials are becoming more and more abundant, with frequent applications in the aircraft cabin, cargo compartment, and other locations. A large number of these materials improve the economic comfort of the aircraft. When a fire occurs, the performance of the materials involved can significantly influence the fire’s progression, which in turn affects the safety of passengers and the aircraft. Additionally, it can impact emergency evac

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8

Raul, Payri, Martí-Aldaraví Pedro, Carvallo César, and Gimeno Jaime. "Parametrical study of the dispersion of an alternative fire suppression agent through a real-size extinguisher system nozzle under realistic aircraft cargo cabin conditions." Process Safety and Environmental Protection 141 (September 1, 2020): 110–22. https://doi.org/10.5281/zenodo.3906068.

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Nearly all active fire extinguishing systems consist of injecting an agent into the space set on fire. For aircraft cargo cabins, the agent widely used up to date is Halon 1301. The FAA provides a level of safety for this fire suppression agent that needs to be used in a volumetric concentration of 6% and needs to be acting for a duration of 0.5 s. On the other hand, Halon 1301 is known to contribute to the retrenchment of Earth's atmospheric ozone layer, therefore it is going to be prohibited in the incoming years. The FAA has defined an equivalent level of safety in terms of the per

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9

Tuncel, Ozan, Polat Sendur, Murat Ozkan, and Ahmet Guney. "Technical note: Ride comfort optimisation of Ford cargo truck cabin." International Journal of Vehicle Design 52, no. 1/2/3/4 (2010): 222. http://dx.doi.org/10.1504/ijvd.2010.029645.

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10

Guo, Liang, Li Duan, Xuemei Zou, et al. "Development and Experimental Study of Supercritical Flow Payload for Extravehicular Mounting on TZ-6." Entropy 26, no. 10 (2024): 847. http://dx.doi.org/10.3390/e26100847.

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This paper provides a detailed description of the development and experimental results of the supercritical flow experiment payload carried on the TZ-6 cargo spacecraft, as well as a systematic verification of the out-of-cabin deployment experiment. The technical and engineering indicators of the payload deployment experiment are analyzed, and the functional modules of the payload are shown. The paper provides a detailed description of the design, installation location, size, weight, temperature, illumination, pressure, radiation, control, command reception, telemetry data, downlink data, and

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11

Zhu, Shuhua, Kai Liu, Xulong Xi, et al. "Influence of Cargo Luggage on the Vertical Drop Crashworthiness of Aircraft Mid-Fuselage Section." Applied Sciences 13, no. 23 (2023): 12921. http://dx.doi.org/10.3390/app132312921.

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The evaluation of structural crashworthiness is important for the development of civil aircraft. In this study, cargo luggage was considered in the vertical drop simulation of an aircraft mid-fuselage section. First, quasi-static compression tests on three types of luggage made of different materials were conducted. Then, a finite element model (FEM) of the cargo luggage was developed with a crushable foam material in LS-PrePost4.5 software. The finite element analysis results of the luggage made of different materials were consistent with the corresponding compression experiments. Secondly, t

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12

Xu, Haijun, Yuanhang Hou, Haonan Li, Meng Bao, and Haishang Liu. "Random/Cognitive Hybrid Uncertainty Analysis of Ship Multitasking Cabin Layout." Journal of Marine Science and Engineering 12, no. 1 (2024): 120. http://dx.doi.org/10.3390/jmse12010120.

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Identifying the optimal cabin layout is an important way to improve the efficiency of ship systems and ensure the efficient circulation of personnel and materials. The ship task state refers to the state maintained by the joint actions of ship machinery and equipment, cargo, and personnel when facing different jobs and tasks during operation. A cabin layout that facilitates multitasking states can improve the efficiency of collaboration between systems and ensure the operation of the ship. The demand for human flow and logistics is different in multitasking states. To express the demand in mat

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13

Sun, Zhongmiao, and Baoli Shi. "Dynamic Emission Reduction Strategy for Shipping Company Considering Shipper's Cancellation of Cabin Space." Studies in Social Science Research 5, no. 3 (2024): p221. http://dx.doi.org/10.22158/sssr.v5n3p221.

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As a major carbon emitting industry, the shipping industry urgently needs to actively reduce emissions. This article introduces parameters such as the shipper's low-carbon preference coefficient, cabin cancellation rate, and compensation rate, considering the shipper's low-carbon preference and cabin cancellation behavior. Based on the state changes of shipping emission reduction, an optimal control method is used to construct a dynamic decision-making model for shipping companies to reduce emissions. The optimal emission reduction effort of shipping companies is solved to clarify the optimal

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14

Jiang, Xuan. "Experimental Study on Rapid Pressure Relief in the Cargo Compartment of Civil Aircraft." Advances in Engineering Technology Research 1, no. 2 (2022): 286. http://dx.doi.org/10.56028/aetr.1.2.286.

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The rapid pressure relief device in the cargo compartment of civil aircraft can avoid the structural damage of aircraft caused by sudden pressure relief in a pressurized compartment. Based on a typical rapid pressure relief device in the cargo hold of civil aircraft, a test bench was built to carry out experimental research on the pressure magnitude and pressure relief process of the device. To simulate the real pressure relief situation of the aircraft pressurized cabin, two experimental studies of forwarding pressure and reverse pressure were carried out, and the pressure relief process of t

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15

Jiang, Xuan. "Experimental Study on Rapid Pressure Relief in the Cargo Compartment of Civil Aircraft." Advances in Engineering Technology Research 2, no. 1 (2022): 286. http://dx.doi.org/10.56028/aetr.2.1.286.

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Анотація:

The rapid pressure relief device in the cargo compartment of civil aircraft can avoid the structural damage of aircraft caused by sudden pressure relief in a pressurized compartment. Based on a typical rapid pressure relief device in the cargo hold of civil aircraft, a test bench was built to carry out experimental research on the pressure magnitude and pressure relief process of the device. To simulate the real pressure relief situation of the aircraft pressurized cabin, two experimental studies of forwarding pressure and reverse pressure were carried out, and the pressure relief process of t

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16

Ba, Zhongfeng, Zhijie Zhang, and Yonggang Zong. "Design and research on intelligent ventilation system of ship cargo hold." Journal of Physics: Conference Series 2131, no. 3 (2021): 032120. http://dx.doi.org/10.1088/1742-6596/2131/3/032120.

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Abstract Ventilation in the cargo hold of ships, which can adjust the temperature and humidity in the cargo hold, is a necessary measure to ensure the safety of maritime cargo. Traditional ship cargo hold ventilation includes natural ventilation and mechanical ventilation. Its ventilation effect is limited, which often leads to cargo damage accidents such as mildew of the cargo in the cabin. Based on the research of intelligent cargo hold ventilation technology, this paper proposes a design scheme of ship cargo hold ventilation system. The ventilation system includes a system platform and elec

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17

Hemme, Dan. "Quantification of the noise control benefit realized by installing an aerodynamic fairing to a passenger vehicle." INTER-NOISE and NOISE-CON Congress and Conference Proceedings 264, no. 1 (2022): 188–97. http://dx.doi.org/10.3397/nc-2022-713.

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The purpose of this study is to quantify the reduction of cabin noise inside a vehicle due the installation of an aerodynamic fairing to the cargo rack to the roof of the vehicle. Sound level measurements were taken inside the vehicle with and without the fairing installed, and with and without the sunroof open, over a variety of vehicle speeds. The measurement results are compared on a one-third-octave-band basis, in terms of A-weighted decibels, and in terms of Speech Intelligibility Index ratings.

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18

Cho, S. H., C. Bil, and R. Adams. "Design and optimisation of the external load bearing carry through structure of a columned multi bubble fuselage." Aeronautical Journal 117, no. 1187 (2013): 97–108. http://dx.doi.org/10.1017/s0001924000007879.

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Abstract The blended wing-body configuration holds a major structural design challenge at the centre-body where the structure must support both wing bending loads and internal cabin pressure. A membrane approach is proposed which decouples the loads to allow their resistance by two independent structures: an inner membrane for cabin pressure and an outer structure to resist wing loads. A columned multi-bubble fuselage is proposed for the inner membrane structure, which are multispherical configuration to efficiently withstand the pressure loads. Considering this configuration, the carry-throug

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19

Han, Yanhua. "Modeling and control for ultra-low altitude cargo airdrop." Aircraft Engineering and Aerospace Technology 90, no. 1 (2018): 219–28. http://dx.doi.org/10.1108/aeat-09-2015-0209.

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Purpose The purpose of this paper is to model the aircraft-cargo’s coupling dynamics during ultra-low altitude heavy cargo airdrop and to design the aircraft’s robust flight control law counteracting its aerodynamic coefficients perturbation induced by ground effect and the disturbance from the sliding cargo inside. Design/methodology/approach Aircraft-cargo system coupling dynamics model in vertical plane is derived using the Kane method. Trimmed point is calculated when the cargo fixed in the cabin and then the approximate linearized motion equation of the aircraft upon it is derived. The ro

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20

Zhao, Yuechao, Zeya Miao, Yuan Gao, Qifei Wang, Dihao Ai, and Yubo Li. "Research on the Propagation Law of Explosion Shock Waves in Ship Engine Rooms Based on OpenFOAM." Fire 8, no. 3 (2025): 115. https://doi.org/10.3390/fire8030115.

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To investigate the propagation of explosion shock waves within a ship’s engine room, a two-story engine room of a cargo ship was selected as the research object. The BlastFOAM solver in OpenFOAM-9 software was utilized to conduct numerical simulations of the explosion dynamics in the engine room. The results demonstrate that the explosion impact force escalates with the quantity of explosives. Following a liquefied natural gas (LNG) explosion, the shock waves exerted on the ventilation duct and control room are significantly stronger in terms of maximum pressure and intensity compared with tho

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21

Wu, Wenfeng, Jiakuo Zhang, Jinshu Lu, et al. "Temperature field distribution analysis for cargo oil on microwave heating process." Thermal Science 24, no. 5 Part B (2020): 3413–21. http://dx.doi.org/10.2298/tsci191226133w.

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This paper uses microwave technology to study the heating process of cargo oil in tanker side cabin under the static environment. The research is aimed to improve the heat transfer efficiency of cargo oil and solve the problems of uneven temperature distribution and energy consumption during the heating process of traditional crude-oil in oil tank. Based on the theory of microwave heating and heat transfer, the finite element simulation software is used to couple the microwave and temperature field during the cargo oil is heated to simulate the changing characteristics of the temperature field

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22

Dergachev, A. N., and M. V. Klychnikova. "Geometric constraints system formation for helicopter construction." E3S Web of Conferences 458 (2023): 03028. http://dx.doi.org/10.1051/e3sconf/202345803028.

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The paper presents a methodology of forming a system of geometric constraints in helicopter design. The methodology is based on the synthesis of the requirements in terms of ensuring operation on marine vessels, transportability, and capacity of the cargo (transport) cabin of the helicopter. The universality of this approach allows to adapt the formed system of geometrical constraints to helicopters of different purposes, both to newly developed and modernised helicopters. This methodology allows to define general geometrical characteristics of the helicopter, nomenclature of units requiring s

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23

Bardaro, Danilo, Alessandro Bozzolo, and Donato Zangani. "Advanced Technologies for Bombproof Cargo Containers and Blast Containment Units for the Retrofitting of Passenger Airplanes." International Journal of Aviation Systems, Operations and Training 2, no. 1 (2015): 33–47. http://dx.doi.org/10.4018/ijasot.2015010103.

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Commercial aviation can be protected from the threat of explosives in two ways, either by preventing explosives from reaching the aircraft or by mitigating the effects of an explosive by protecting the aircraft from an onboard explosion. The containment units under study aim at acting as complementary and passive security measures for passengers and cabin crew. The proposed concept is a container where an internal high strength layer made of ballistic textiles is used to stop blast fragments, coupled with an external layer deforming in a controlled way during the explosion, designed to fully c

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24

Wang, Xiao Wei, Hai Bing Hu, Jun Qin, and Yong Ming Zhang. "A New Method to Detect Fire and Alarm in Confined Space Based on Electronic Nose." Applied Mechanics and Materials 390 (August 2013): 383–87. http://dx.doi.org/10.4028/www.scientific.net/amm.390.383.

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This paper presents a new method to detect fire and alarm in confined space based on electronic nose. Common confined space includes some distribution cabinet, machine room, warehouse, air cargo compartment and spacecraft cabin, etc. Combined with the characteristics of the confined space, a fire detection and alarm system is schematically designed. This system is based on electronic nose and is an aspirated configuration. With this system, this method adopts PNN as the recognition algorithm, and introduces steady status and warning time to the monitoring host. The CO, O2, CO2and temperature a

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25

Zhu, Yulong, Changzheng Li, Shupei Tang, et al. "Deep-Learning-Driven Technique for Accurate Location of Fire Source in Aircraft Cargo Compartment." Fire 8, no. 8 (2025): 287. https://doi.org/10.3390/fire8080287.

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Accurate fire source location in an aircraft cargo compartment cannot be determined by common design practices. This study proposes an advanced fire location inversion framework based on a Convolutional Long-Short-Term Memory (ConvLSTM) network. A self-designed interpolation preprocessing module is introduced to realize the integration of spatial and temporal sensor data. The model was trained and validated using a comprehensive database generated from large-scale fire dynamics simulations. Hyperparameter optimization, including a learning rate of 0.001 and a 5 × 5 convolution kernel size, can

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26

Raju, A. V. K., Ranjan Sarkar, Vijay V. Joshi, and N. K. Tripathy. "Retro-fitment of an oxygen system in a transport aircraft of Indian Air Force: Decompression chamber trials to assess system functionality." Indian Journal of Aerospace Medicine 66 (October 21, 2022): 43–47. http://dx.doi.org/10.25259/ijasm_28_2021.

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The aeromedical concerns of sudden onset hypoxia and rapid decompression are an omnipresent threat to flight safety when flying over 10,000 ft. The concept of Time of Useful Consciousness (TUC) provides the aircrew a window to correct his predicament. The issues of hypoxia are mitigated in transport aircraft with cabin pressurization. However, the requirement of an oxygen system in these aircraft is considered essential in an emergency in case of cabin failure of cabin pressurization or rapid decompression, despite adequate TUC, as it provides immediate succor from anxiety, and subtle performa

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27

Gräschke, Lucia. "Flying cats and dogs: Relationality, empathy and care in the transportation of animals by air." TRACE ∴ Journal for Human-Animal Studies 10 (April 15, 2024): 86–104. http://dx.doi.org/10.23984/fjhas.124730.

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The carrying of companion animals by air has grown into an international business involving approved vets, pet travel agencies, airlines, and animal terminals. This study investigates how the experience of transportation is shaped and draws theoretically on an approach of more-than-human mobility. In detail, I approach mobility through relationality, empathy, and caring practices by considering air transportation as an anthropocentric means of animal movement. Movement, including the specific conditions used to carry companion animals, influences the experience of mobility, triggering multispe

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28

Leon Muñoz, C., D. Kohlgrüber, and B. Langrand. "Analysis of the application of fuselage skin reinforcements with beam element representations in flexible full aircraft models for ditching simulations." IOP Conference Series: Materials Science and Engineering 1226, no. 1 (2022): 012057. http://dx.doi.org/10.1088/1757-899x/1226/1/012057.

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Abstract The aim of this paper is the application of beam element representations for structural skin reinforcements in flexible full aircraft FE models used in ditching simulations. To verify this approach, it was initially analyzed on flexible reinforced bottom-aircraft panels under guided ditching conditions, considering also structural mesh size variations and partly corresponding fluid mesh densities. For this analysis two different numerical methods were used for comparisons, the coupled Finite Element-Smoothed Particle Hydrodynamics and the Arbitrary Lagrangian Eulerian methods. For the

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29

Ivanov, Nikolay, Evgueni Smirnov, Chang H. Son, and Denis Telnov. "CFD Evaluation of Directional Variation Effects of the Air Supply Diffuser for the International Space Station Cabin Atmosphere." E3S Web of Conferences 111 (2019): 01034. http://dx.doi.org/10.1051/e3sconf/201911101034.

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The International Space Station (ISS) crew health and safety depend on ventilation system performance. The ISS ventilation system comprises of numerous air supply diffusers. For each ISS module design of the ventilation system and, in particular, supply diffuser distribution and configuration, is based on the assumption that the cabin aisle way is clear of any objects. However, on-orbit operations could lead to short- or long-term blockage of the area near the air supply diffuser due to some items or stowed bags necessary for the station operation. Partial blockage of the diffuser could disrup

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30

Popov, M., and A. Negodin. "Failures of safety services in case of emergency fall of cargo-passenger elevator’s cabin exploited in industrial and civil premises." IOP Conference Series: Materials Science and Engineering 1118, no. 1 (2021): 012028. http://dx.doi.org/10.1088/1757-899x/1118/1/012028.

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31

Łusiak, Tomasz, Radosław Witczak, and Arkadiusz Małek. "Analysis of the performance of a new type of rotorcraft." AUTOBUSY – Technika, Eksploatacja, Systemy Transportowe 24, no. 6 (2019): 206–11. http://dx.doi.org/10.24136/atest.2019.152.

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The article analyses the performance of the newly designed rotorcraft. A new concept for the equipment and use of rotorcraft for transport purposes was also presented. The work focuses on the use of gyroplanes for these purposes as a special type of rotorcraft with specific properties. The initial aircraft design developed and described includes structural assumptions, technological solutions, cabin / cargo ergonomics, economy and operational safety. Particular attention has been paid to rotorcraft equipment depending on which version it is to be configured to. The work also includes the desig

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32

Bulat, P. V., S. Yu Dudnikov, N. V. Prodan, and P. S. Chernyshov. "History of propulsive aerodynamic surface research." Aerospace Engineering and Technology 3, no. 1 (2025): 13–47. https://doi.org/10.52467/2949-401x-2025-3-1-13-47.

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Анотація:

Studies conducted between 2018 and 2021 as part of the Aeronet roadmap under the National Technology Initiative revealed a demand for a transport aircraft capable of operating on confined sites without prior preparation, featuring short or vertical take-off and landing (VTOL), and performing horizontal flight in the manner of a conventional airplane. A promising concept involves the use of a load-bearing fuselage composed of specialized propulsive (thrust-generating) airfoils, which–due to their geometry–feature considerable structural depth. This allows for convenient internal placement of ca

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33

Kapp, E. Andrew, David S. Wroth, and J. Thomas Chapin. "Analysis of Thermal Runaway Incidents Involving Lithium Batteries in U.S. Commercial Aviation." Transportation Research Record: Journal of the Transportation Research Board 2674, no. 11 (2020): 584–92. http://dx.doi.org/10.1177/0361198120947711.

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Thermal runaway incidents involving lithium batteries as cargo, in luggage, or as personal property in the cabin have been associated with fatalities, the destruction of cargo, and even the loss of entire aircraft. This research represents the first examination of the incidence of lithium battery thermal runaway incidents involving a variety of rechargeable lithium-ion and lithium metal batteries on commercial flights in the U.S.A. The objective is to examine the occurrence of these thermal runaway incidents and the circumstances surrounding them from the best available data source, the Pipeli

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34

Ottogalli, Kiara, Daniel Rosquete, Javier Rojo, Aiert Amundarain, José María Rodríguez, and Diego Borro. "Framework for the Simulation of an Aircraft Final Assembly Line." MATEC Web of Conferences 233 (2018): 00010. http://dx.doi.org/10.1051/matecconf/201823300010.

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The EU ACCLAIM project as part of the European Clean Sky 2 activities is oriented to improve the aircraft assembly process. The SIMFAL H2020 Clean Sky 2 project is part of the ACCLAIM project, whose objective is to analyse, plan and optimize automated assembly tasks of cabin and cargo interior parts, with a coexistence between human workforce and machines (lightweight robots and AGVs). SIMFAL framework integrates VR and AR systems to help the user to work in limited spaces, collaborating with automation systems. The VR system aids the user to visualize different assembly processes in an immers

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Pourasad, Yaghoub, Amirhossein Ghanati, and Mehrdad Khosravi. "Optimal design of aerodynamic force supplementary devices for the improvement of fuel consumption and emissions." Energy & Environment 28, no. 3 (2016): 263–82. http://dx.doi.org/10.1177/0958305x16681686.

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One of the primary concerns in the automotive industry is energy saving, protecting the global environment and fuel consumption reduction. The main purpose of this study is to develop optimal supplementary parts for reduction of aerodynamic force of highway tractor and trailer combinations to reduce aerodynamic drag, without negatively affecting the usefulness or profitability of the vehicles. In this article, the possibility to improve the aerodynamic performance for boosting fuel economy of trucks is studied by optimal designing of supplementary devices. That will be carried out by using int

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Gilligan, J. E., P. Goon, G. Maughan, W. Griggs, R. Haslam, and A. Scholten. "An Airborne Intensive Care Facility (Fixed Wing)." Anaesthesia and Intensive Care 24, no. 2 (1996): 245–53. http://dx.doi.org/10.1177/0310057x9602400218.

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A fixed-wing aircraft (Beechcraft KingAir B200 C) fitted as an airborne intensive care facility is described. It completed 2000 missions from 1987–1992, for distances up to 1300 km. Features include: 1. Space for carriage of two stretchers, medical cabin crew of up to five persons and equipment and two-pilot operation if necessary. A third stretcher may be carried in emergencies. 2. Two CARDIOCAP™ fixed monitors for ECG, invasive and noninvasive pressures, pulse oximetry and end-tidal CO2 plus SIEMENS 630™/PROPAQ™ compact monitors for the ground transport phase of missions, or the total durati

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Wang, Shanran, Xiaodong Cao, Dan Miao, Liping Pang, and Jiayu Li. "A Review of In-Flight Thermal Comfort and Air Quality Status in Civil Aircraft Cabin Environments." Buildings 14, no. 7 (2024): 2001. http://dx.doi.org/10.3390/buildings14072001.

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The civil aircraft cabin is enclosed and highly occupied, making it susceptible to a decline in indoor environmental quality. The environmental quality of civil aircraft cabins not only depends on objective factors such as temperature, relative humidity, and the presence of air pollutants such as carbon dioxide (CO2), carbon monoxide (CO), ozone (O3), particle matter (PM), and volatile organic compounds (VOCs) but also the subjective factors pertaining to the perceptions and health symptoms of passengers and crew. However, few studies have thoroughly examined the air quality and thermal comfor

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Payri, Raul, Jaime Gimeno, Pedro Martí-Aldaraví, and César Carvallo. "Parametrical study of the dispersion of an alternative fire suppression agent through a real-size extinguisher system nozzle under realistic aircraft cargo cabin conditions." Process Safety and Environmental Protection 141 (September 2020): 110–22. http://dx.doi.org/10.1016/j.psep.2020.04.022.

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Sipahutar, Anjani. "Pertanggungjawaban Pidana Terhadap Pencurian Barang Penumpang Pesawat Studi Dibandara Udara Kualanamu Internasional Airport." Jurnal Hukum Kaidah: Media Komunikasi dan Informasi Hukum dan Masyarakat 20, no. 1 (2021): 118–26. http://dx.doi.org/10.30743/jhk.v20i1.3469.

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This study aims to determine that there are still many events that are still require the liability from the commercial air transportation company, both from the carrier company and those who are related to the carrier, such as flight delays (flight delay) either caused by weather factors or internal factors from the carrier company, the occurrence of negligence from the transport officer which causes the loss of goods owned by passengers, or because of there is an event for which the reason is unknown so that the aircraft experiences interference during the flight, from the results of this res

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Sausan, Misk Sausan Ghina, Mufti Arifin, and Ade Julizar. "Analysis Of Maximum Range And Operational Cost Of Airbus A320-200 And Boeing 737-800 Aircraft From Dhoho Kediri Airport For Domestic Flights." Jurnal Teknologi Kedirgantaraan 10, no. 1 (2025): 39–47. https://doi.org/10.35894/jtk.v10i1.239.

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Domestic flights are a type of flight carried out within a country, without crossing international borders. Airbus A320-200 and Boeing 737-800 aircraft are aircraft that are often used in Indonesia for domestic flights. To determine the maximum range and runway capacity for both aircraft, it is necessary to consider the technical specifications of both aircraft, such as the weight of the aircraft for takeoff, and the strength of the runway. Based on the results of the calculation of the maximum distance obtained with the same capacity for both aircraft, 180 passengers and 20 kg cargo weight an

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Лопухов, А. А., Ю. Н. Осипов, Е. В. Павлов, and В. И. Ершов. "Mathematical modeling of loading of heavy-class robotic complexes on a tracked chassis into transport aircraft of EMERCOM of Russia." Pozharnaia bezopasnost`, no. 3(104) (October 5, 2021): 80–85. http://dx.doi.org/10.37657/vniipo.pb.2021.56.30.009.

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Рассмотрен один из возможных подходов к математическому моделированию загрузки робототехнического комплекса (РТК) тяжелого класса на гусеничном шасси с независимой торсионной подвеской в транспортный самолет. Данный подход представляет собой часть обоснованной оценки авиатранспортабельности специальных РТК. Он базируется на построении и решении системы линейных уравнений, в результате чего определяются параметры, по которым оценивается факт «вписывания» конструкции образца РТК в размеры грузовой кабины самолета. Актуальность статьи обусловливается, во-первых, потребностью в создании специальны

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Yovchenko, Alla. "Development and Modeling of a Device to Improve Safety Control of Freight Transport With Trailers." Central Ukrainian Scientific Bulletin. Technical Sciences 1, no. 11(42) (2025): 230–35. https://doi.org/10.32515/2664-262x.2025.11(42).1.230-235.

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Ensuring vehicle safety is a major issue for the Ukrainian transport industry, the level of which is influenced by numerous factors, including: road network congestion; road network expansion; road quality and markings; increasing vehicle fleet and population growth; low discipline and culture of road users; insufficient driver qualifications; technical condition of vehicles and their improper operation, etc. Of particular concern are frequent and serious accidents involving large-sized freight transport. Active safety systems reduce the risk of dangerous situations on the road and contribute

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Johari, Mohd Hafiz, Khairil Anwar Abu Kassim, Yahaya Ahmad, Najihah Wahi, Nor Kamaliana Khamis, and Mohd Radzi Abu Mansor. "Safety Levels and Occupant Injury Risk for Light Commercial Vehicles in the ASEAN Region: Results of Crashworthiness Data." Jurnal Kejuruteraan 33, no. 4 (2021): 955–67. http://dx.doi.org/10.17576/jkukm-2021-33(4)-18.

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The logistics industry in Malaysia has greatly evolved in recent years. With regard to the freight industry, business operations depend on transportation service using commercial vehicles to deliver products in a timely manner. Technically categorised as N1 vehicle, the Light Commercial Vehicle (LCV) or light duty truck is designed to carry goods with maximum load not exceeding 3.5 tons. To maximize cargo size, the occupant cabin space has been pushed forward, hence, becoming a ‘flat head type’ vehicle. Nevertheless, the flat head vehicle fared poorly in terms of its crashworthiness performanc

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Güler, Zeynep, and Garip Genç. "Design and analysis of composite hydraulic cylinders developed for aerospace applications." International Journal of New Findings in Engineering, Science and Technology 3, no. 1 (2025): 25–31. https://doi.org/10.61150/ijonfest.2025030103.

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Nowadays, aviation and space applications are technologies that are becoming increasingly important. It is essential that these technologies are highly energy efficient and can be applied effectively. The central systems of an aircraft can be listed as navigation and communication, power control systems, flight control systems, and collision avoidance systems. Hydraulic energy is required for the flight control systems, one of the central systems of the aircraft. In an aircraft, hydraulic systems can generally be used in flight control (such as ailerons, horizontal elevators, high-lift gear),

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Chaturvedula, Sowgandhi, Anjana Thattil, Stuti Mishra, and N. K. Tripathy. "Coping styles and subjective well-being of indian civil aircrew in the context of COVID-19." Indian Journal of Aerospace Medicine 66 (October 21, 2022): 32–38. http://dx.doi.org/10.25259/ijasm_13_2022.

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Objectives: The novel coronavirus (COVID-19) infection has emerged into a widespread pandemic that stalled the world. Humanitarian missions like Vande Bharat during the first wave of COVID-19 and passenger as well as cargo services during its second wave were carried out extensively by civil aircrew. Operating under such challenging circumstances is likely to affect the well-being and psychological health of the aircrew. Exploring different coping strategies adopted by civil aircrew and assessment of their subjective well-being while operating during the pandemic was the desired objective of t

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Agarwal, Shivani, Rekha Mewarfarosh, and Vijender Kumar Solanki. "The role of various forms of subjective well being with quality of work life in the aviation industry." Journal of Economics and Management 46 (2024): 353–86. http://dx.doi.org/10.22367/jem.2024.46.14.

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Aim/purpose – This study explores the crucial link between the quality of work life (QWL) and subjective well-being (SWB) among aviation industry employees. By delv- ing into the current state of QWL and its relationship with key aspects of SWB, such as life satisfaction, positive affect, and negative affect, this research aims to offer valuable insights that can help employee well-being and job satisfaction in the aviation industry. Design/methodology/approach – A sample of 350 employees, including front-line execu- tives such as cabin crew, airport staff, cargo handlers, and administrative p

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Begerskyi, Dmytro B., Ivan V. Vityk, Andriy O. Koval, and Serhii V. Tsymbal. "Influence of the geometric parameters of the vehicle on its aerodynamic characteristics." Journal of Mechanical Engineering and Transport 18, no. 2 (2024): 10–15. http://dx.doi.org/10.31649/2413-4503-2023-18-2-10-15.

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In the article, the authors analyzed the relevance of the research topic, defined the goal, task, subject and object of the research. They also provided an analysis of well-known studies related to the study of the peculiarities of the formation of air resistance during the movement of motor vehicles. On the basis of the analysis of known studies on the factors affecting the geometric parameters of road trains on aerodynamic resistance, the relevance of the studies is substantiated, and their purpose and tasks are formulated.The purpose of the article is to determine the influence of geometric

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Muratori, Luca, Lorenzo Peretto, Beatrice Pulvirenti, Raffaella Di Sante, Giovanni Bottiglieri, and Federico Coiro. "Optimal Control of Air Conditioning Systems by Means of CO2 Sensors in Electric Vehicles." Sensors 22, no. 3 (2022): 1190. http://dx.doi.org/10.3390/s22031190.

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Considering the consistent reduction in battery range due to the operation of the Heating Ventilation and Air Conditioning (HVAC) system, this study deals with the CO2 measurement inside the cabin of an electric crane and aims to reduce the energy consumption through the control of the air recirculation. A control strategy was defined and tested through an experimental set-up where the presence of a driver was simulated as a source of CO2. The cabin was placed inside a climatic wind tunnel and the benefits of this control strategy on the HVAC system energy consumption were assessed, both in th

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Pankova, Vera B., Mikhail F. Vilk, Evgeny V. Zibarev, and Irina N. Fedina. "On the issue of taking into account new factors in the pathogenesis of occupational hearing loss (on the example of transport workers)." Russian Journal of Occupational Health and Industrial Ecology 62, no. 8 (2022): 488–500. http://dx.doi.org/10.31089/1026-9428-2022-62-8-488-500.

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Introduction. In the period from 2013 to 2021, industrial enterprises saw a reduction in jobs that did not meet sanitary and hygienic requirements for the level of exposure to noise, vibration, illumination, microclimate parameters and electromagnetic fields on the workers' bodies. However, the proportion of unfavorable workplaces that do not meet the standards for noise levels remains the largest, which determines the peculiarities of the structure of the occupational pathology of workers in the Russian Federation: professional pathology of the hearing organ - professional sensorineural heari

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Cho, Gyu Seong. "Requirements for the Insurer to be liable for Compensation in the First Party Injury Insurance: Focusing on Supreme Court Decision 2022Da26652 Decided February 2, 2023." Korean Insurance Law Association 18, no. 1 (2024): 119–62. http://dx.doi.org/10.36248/kdps.2024.18.1.119.

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In order for an insurer to be liable for compensation in the first party injury insurance case, the accident must have occurred “while the insured was in possession, use, or control of the insured automobile, and (1) was caused by the operation of the insured automobile, or (2) was caused by the operation of the insured automobile if the insured was a passenger in the insured automobile.” The case concerned the recognition of the insurer's liability for compensation for bodily injury in an accident in which the driver of a small truck slipped and fell while climbing on the roof of the dr

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