Aircraft landing gear of the rocker-arm and deformable-parallelogram type
View Patent ↗The invention relates to an aircraft landing gear of deformable-parallelogram type, including: a leg including a casing ( 1 ) having a lower end on which a rocker arm ( 3 ) carrying at least one wheel is hinged by means of a pivot ( 2 ), a shock absorber ( 5 ) being connected between the rocker arm and the casing; two panels ( 10, 11 ) each hinged on the one hand on the structure of the aircraft and on the other hand on the leg, about parallel axes; According to the invention, one of the panels ( 11 ) is hinged on the leg while being connected to the casing by a pin on one end of the pivot ( 2 ) of the rocker arm.
1. An aircraft landing gear of deformable-parallelogram type, comprising:
a leg, including a casing ( 1 ), having a lower end on which a rocker arm ( 3 ) carrying at least one wheel is hinged by means of a pivot ( 2 ), a shock absorber ( 5 ) being connected between the rocker arm and the casing;
two panels ( 10 , 11 ), each hinged at a first portion on a structure of the aircraft and at a second portion on the leg, about parallel axes;
wherein one of the panels ( 11 ) is hinged on the leg whilst being connected to the casing by a pin on one end of the pivot ( 2 ) of the rocker arm.
2. The aircraft landing gear as claimed in claim 1 , including a bracing member that is connected to the two panels.
3. The aircraft landing gear as claimed in claim 1 , including a maneuvering member ( 6 ) that is connected to the two panels.