Results 31 to 40 of about 106,651 (339)
Effect of Joint Clearance on Landing Gear Retraction Failure
Aerospace, 2021 A simple method of investigating the effect of joint clearances on landing gear retraction failure is presented and applied to the main landing gear with a single sidestay and a hydraulic actuator.
Sungjoon Cho, Hwanjeong Cho, Dooyoul Lee
doaj +1 more source
Analisis Frekuensi Natural Rangka Main Landing Gear Pesawat UAV Menggunakan Ansys Workbench
Jurnal Mesin Nusantara, 2022 The main landing gear is one of the important components in UAV aircraft. This paper aims to analyze the natural frequency of the main landing gear and determine its normal mode shape.
Lasinta Ari Nendra Wibawa
semanticscholar +1 more source
Dynamic Fatigue Tests Of Landing Gears
Fatigue of Aircraft Structures, 2020 Landing gears are one of the main components of an aircraft. The landing gear is used not only during take-off and landing but also, in most cases, during ground manoeuvres.
Skorupka Zbigniew
doaj +1 more source
Influence of Variable Side-Stay Geometry on the Shimmy Dynamics of an Aircraft Dual-Wheel Main Landing Gear [PDF]
, 2013 Commercial aircraft are designed to fly but also need to operate safely and efficiently as vehicles on the ground. During taxiing, take-off, and landing the landing gear must operate reliably over a wide range of forward velocities and vertical loads ...
Howcroft, Chris +3 more
core +2 more sources
DESIGNED AND ANALYSIS OF AN SC-17M MAIN LANDING GEAR LOADING ACTION
FUTA JOURNAL OF ENGINEERING AND ENGINEERING TECHNOLOGY, 2022 The concept of SC-17M aircraft design was initiated to address the shortfalls on the DO-228 and Hawker Beechcraft King Air 350i aircraft. Until recently by using a standard specification, an SC-17M landing gear design has been carried out. Detailed study
Okemini Uguzo Sunny +4 more
semanticscholar +1 more source
Oleo-pneumatic Mixed Shock Absorber Landing Pressure Analysis of Landing Gear
Hangkong gongcheng jinzhan, 2020 The landing gear of an aircraft bears a large impact load during landing, which causes the internal shock absorber to withstand high oil pressure and air pressure, and the buffer performance is greatly influenced.
LOU Rui +3 more
doaj +1 more source
Optimization of a Main Landing Gear Locking Mechanism Using Bifurcation Analysis [PDF]
Journal of Aircraft, 2017 A key part of the main landing gear of a civil aircraft is its locking mechanism that holds the gear in the deployed or downlocked state.
Yin, Yin +4 more
openaire +3 more sources
, 2021 The landing gear is one crucial component in the UAV aircraft structure because it serves as the main supporting component of aircraft load when landing and take-off.
Lasinta Ari Nendra Wibawa
semanticscholar +1 more source
Numerical Continuation Analysis of a Dual-sidestay Main Landing Gear Mechanism [PDF]
AIAA Atmospheric Flight Mechanics Conference, 2012 A model of a three-dimensional dual-sidestay landing gear mechanism is presented and employed in an investigation of the sensitivity of the downlocking mechanism to attachment point deflections. A motivation for this study is the desire to understand the underlying nonlinear behavior, which may prevent a dual-sidestay landing gear from downlocking ...
Knowles, James A C +4 more
openaire +3 more sources
Aerospace, 2023 With the development of next-generation airplanes, the complexity of equipment has increased rapidly, and traditional maintenance solutions have become cost-intensive and time-consuming.
Yuan-Jen Chang +4 more
doaj +1 more source