COMPACT SHOCK ABSORBER FOR AIRCRAFT AIRCRAFT AND LANDSCAPER COMPRISING SUCH SHOCK ABSORBER

摘要

The absorber has a rod (2) mounted on a main cylinder (1), and pneumatic chambers (12, 22) filled with gas. Laminating units (14, 24) are arranged such that the gas is compressed and hydraulic fluid is laminated when the absorber is pushed. The chambers are contained in auxiliary cylinders (10, 20). Pistons (11, 21) separate the pneumatic chambers from fluid chambers (13, 23) that are in fluid communication with the main cylinder. The units are integrated to the main cylinder and are placed at an inlet of fluidic connection e.g. rigid tube, between the main and auxiliary cylinders.