Crane brings industry-leading aircraft electronic and hydraulic subsystems for landing gear together in solutions that add value and offer superior performance you can count on. We deliver custom-engineered brake control systems, reliable hydraulic compo
The present invention relates to a system for driving the landing gear of an aircraft. An aircraft having wheel driving means associated with at least one of the wheels of the landing gear is described. Preferably, the nose gear is driven, having two wheels (11), both wheels being drivable...
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280 Valor aircraft. Based on the agreement, Safran Landing Systems will develop and manufacture a fully integrated Landing Gear System consisting of the Main Landing Gear, Tail Landing Gear, Wheels and Brakes, Extension/Retraction System, Steering System, Brake Control System, and Indication sensors....
the aircraft landing gear system mathematical model is built including tire model,ole-pneumatic shock strut model,landing gear walking model and main wheel brake device model.Considering ABS(anti-skid brake system) control and nose wheel manipulation,the landing gear system model is applied to ...
In this chapter, first, basic information about the landing gear (definition, purpose, and duties, etc.) is given. Examples of different aircraft are given throughout the chapter. Systems in large aircraft such as extend-retract mechanisms are explained on Boeing 737 aircraft. As mentioned in ...
Tricycle-type landing gear is arguably the most common type of aircraft landing gear system and has been in use for the past several decades. This landing gear type is actually the combination of two separate landing gears – the main landing gear, which is located under the fuselage, and th...
Most aircraft today have three landing gear.许多现代飞机使用三点式起落架。Two main landing gear struts located near the middle of the aircraft usually support about 90% of the plane’s weight while a smaller nose strut supports the rest.重心附近的两个大的主轮，承担约 90% 的重量，小轮子承担...
The invention relates generally to an aircraft landing gear steering system 110, (210, 310 see figs 2 and 3) comprising a turning member 118, (218, 318 see figs 2 and 3) that is operably coupled to a landing gear leg 116, (216, 316 see figs 2 and 3) through a harmonic drive mec...
However, in terms of a thicker EMAS, the whole wheel of the puddle-jumper may sink into the foam material completely, leading to the break off of the landing gear; while for a thinner EMAS, the arrestor system can't provide enough resistance to arrest an overrunning airplane. In order to...