Vibration Qualification Campaign on Main Landing Gear System for High-Speed Compound Helicopter
AerospaceVibrations in helicopters have strong implications for their performance and safety, leading to the increased fatigue of components and reduced operational efficiency.
Antonio Chiariello +6 more
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Design challenge of a new monolithic concept for the main landing gear bay of a large passenger aircraft [PDF]
MATEC Web of Conferences, 2018 In this paper, ITEMB team in the contest of the Clean Sky 2 framework, with the scope of a new architecture for the Main Landing Gear of a single isle aircraft type, presents its development in designing the two major item of the Main Landing Gear Bay ...
Cerreta Pietro +3 more
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A case study to estimate costs using Neural Networks and regression based models [PDF]
Decision Science Letters, 2012 Bombardier Aerospace’s high performance aircrafts and services set the utmost standard for the Aerospace industry. A case study in collaboration with Bombardier Aerospace is conducted in order to estimate the target cost of a landing gear. More precisely,
Nadia Bhuiyan +2 more
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Vibration Response Aspects of a Main Landing Gear Composite Door Designed for High-Speed Rotorcraft
Aerospace, 2021 One of the crucial issues affecting the structural safety of propeller vehicles is the propeller tonal excitation and related vibrations. Propeller rotation during flight generates vibrating sources depending upon its rotational angular velocity, number ...
Maurizio Arena +3 more
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Manufacturing and Validation of a Novel Composite Component for Aircraft Main Landing Gear Bay [PDF]
Journal of materials engineering and performance (Print), 2019 Composite materials may reduce the final weight of the aircraft structural components, in addition to improve fatigue performance and corrosion resistance.
M. Viscardi +4 more
semanticscholar +3 more sources
Simulasi umur fatik rangka main landing gear menggunakan metode elemen hingga
, 2020 The landing gear is one crucial component in an Unmanned Aerial Vehicle (UAV) aircraft construction. Landing gear serves as the main supporting component of aircraft load when landing and take off. This research aims to investigate the fatigue design life of the main landing gear on the UAV aircraft.
Lasinta Ari Nendra Wibawa
semanticscholar +3 more sources
Preliminary calculation of the landing gear of a military training aircraft [PDF]
INCAS Bulletin, 2020 The paper presents a preliminary calculation method, which is easy to apply for pre-dimensioning the landing gear. Preliminary calculation of the landing gear includes estimating the loads on landing and determining the position of the nose landing gear ...
Ilie NICOLIN, Bogdan Adrian NICOLIN
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Research on the nose landing gear of a military training aircraft [PDF]
INCAS Bulletin, 2020 This paper presents the analysis of the landing gear configurations and the proposal of a solution for a military training aircraft. The paper presents both landing gears: nose and main because they are inextricably linked.
Ilie NICOLIN, Bogdan Adrian NICOLIN
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Design and Research on Landing Gear Overall Parameters of Pusher Propeller Reconnaissance/Strike UAV
Hangkong gongcheng jinzhan, 2022 The existing specifications and requirements for the overall layout parameter design of aircraft landing gear are mainly applicable to traditional fighters.If the landing gear of pusher propeller reconnaissance/strike unmanned aerial vehicle(UAV)is ...
ZHENG Yongfeng, SHEN Junyan
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Preliminary Estimation Methods for the Definition of the Landing Gear [PDF]
INCAS Bulletin, 2018 The landing gear of an aircraft is an important part of the aircraft structure. The landing and the taking off are most critical parts of a flight mission.
Daniela BARAN +2 more
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