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Main Landing Gear Conceptual Design and Analysis for M.A.L.E U.C.A.V
2021 Seventh International Conference on Aerospace Science and Engineering (ICASE), 2021Among the major components for any Unmanned Combat Aerial Vehicle (UCAV) landing gear is of significant importance, as it performs the function of supporting weight, shock-absorbing structure, taxiing, and providing stable ground support during the ...
Asim Mehmood +3 more
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Prediction of fatigue life of a main landing gear
AIP Conference Proceedings, 2023Utkarsh Verma +2 more
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Structural Testing of Sandwich Composite Main Landing Gear Door
AIAA SCITECH 2024 ForumMary Dimitroff +3 more
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Generative design of main landing gear for a remote-controlled aircraft
Materials Today: Proceedings, 2023Aditya Gupta +3 more
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Approach to Designing a Construction of Typical Main Landing Gear Brackets of an Aircraft
2023 16th International Conference Management of large-scale system development (MLSD), 2023The design of the main landing gears meets the requirements of the Federal aviation regulations. One of the requirements is to prevent the transfer of dangerous loads during emergency landing.
Egor Titov, S. Serebryansky
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Main Landing Gear Operation powered by Multifunctional High-Lift PCUs
2021For conventional aircraft, the high-lift and main landing gear systems are hydraulic/electric consumers with high power demands. The paper shows how the supply systems of these can be combined to save system weight and cost for future more electric aircraft.
Nordmann, Lennard, Thielecke, Frank
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A steerable landing gear for vehicles with main gear skids
Journal of Spacecraft and Rockets, 1969Steerable landing gear system consisting of freely castoring corotating wheel nose gear, tiltable axle and main gear skids for lifting body ...
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Multi-Fault Analysis of Aircraft Main Landing Gear Retraction Hydraulic System
SAE technical paper seriesAiming at the common health performance influencing factors of the aircraft’s main landing gear retracting hydraulic system, based on its hydraulic structure, the landing gear retracting control AMESim hydraulic system model is established to carry out ...
Yahui Yu, Wenhao Cui
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C-5A Main Landing Gear Bogie Pitching Control
Journal of Aircraft, 1970The C-5A six-wheel main landing gear bogie, as the result of a high flotation requirement, poses a problem for designing a wheel braking torque compensating mechanism which stabilizes bogie pitching during braking. For ground operation, the bogie is also required to pitch ±12° with respect to the shock strut. During retraction of the main gear, however,
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Strength analysis of main landing gear stiffness test support clamp for wide-body aircraft
Journal of Physics: Conference SeriesDuring civil aircraft operations, the landing gear sustains both static and dynamic loads generated during ground impact, effectively absorbing and dissipating energy produced by landing and ground manoeuvres[1].
Chuanqi Xu, Lei Li, Lijian Zou
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