Hydraulic distributor for airplane landing gear

Aeronautics and astronautics – Landing gear – Wheel

Reexamination Certificate

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C244S1020SS

Reexamination Certificate

active

07810755

ABSTRACT:
A hydraulic distributor10assembles in a single body an assembly of hydraulic components that assure the supply of actuators for controlling the movements of the moving elements of an airplane landing gear, for which the movements of the landing-gear legs and of the trap-doors are assured by hydraulic actuators. The airplane includes two or more landing-gear systems, each including a distributor10with a single body. The body of each single-body distributor is advantageously created by removing unused parts from a body that can satisfy the needs of all of the landing-gear systems of an airplane, or by addition of extensions onto a minimal body that can satisfy the needs common to all of the landing-gear systems of the airplane.

REFERENCES:
patent: 2701695 (1955-02-01), Irwin
patent: 3107886 (1963-10-01), Bossler, Jr.
patent: 3669387 (1972-06-01), Lucien
patent: 4573649 (1986-03-01), Yourkowski et al.
patent: 7093795 (2006-08-01), Lindahl et al.
patent: 1 495 961 (2005-01-01), None
patent: 2 529 859 (1984-01-01), None
patent: 2 875 475 (2006-03-01), None
patent: 04000502 (2003-12-01), None

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