发明名称 |
AIRCRAFT WITH A NACELLE-HOUSED MAIN LANDING GEAR |
摘要 |
A main landing gear for aircraft having a fuselage, a wing and a jet engine on opposite sides of the fuselage and housed in a nacelle attached to the wing. The main landing gear includes a landing gear at each side of the wing having wheels coupled to a driving device that moves the wheels between stowed and deployed positions. The engine nacelles each include a well located laterally with respect to the jet engines and configured as a housing space for stowing the wheels of the landing gears. |
申请公布号 |
US2016046365(A1) |
申请公布日期 |
2016.02.18 |
申请号 |
US201514625776 |
申请日期 |
2015.02.19 |
申请人 |
AIRBUS OPERATIONS, S.L. |
发明人 |
González Gonzalbo Alfonso;Díaz Parrila José María |
分类号 |
B64C25/14;B64C3/18;B64C25/34;B64D27/18 |
主分类号 |
B64C25/14 |
代理机构 |
|
代理人 |
|
主权项 |
1. An aircraft comprising:
a fuselage, a wing forming, at least one jet engine on opposite sides of the fuselage and each jet engine is housed in a nacelle attached to the wing, and a main landing gear; wherein the wing comprises a load-bearing structure extending in a span wise direction and the main landing gear comprises at least a landing gear at each side of the wing having one or more wheels coupled to a driving device arranged for moving the landing gear from a stowed position to a deployed position and vice versa, wherein the nacelles include a well located laterally with respect to the jet engines and configured as a housing space of the one or more wheels of a landing gear in its stowed position; said driving device comprises a strut attached by one end to the load-bearing structure of the wing in a rotatory manner and by the other end to the one or more wheels. |
地址 |
Getafe ES |