Oleopneumatic suspension with variable throttle orifices, especially for aircraft landing gear
AssigneeMessier-Hispano-Bugatti
InventorsJean Masclet, Andre Turiot
Life of this patent
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AssigneeMessier-Hispano-Bugatti
InventorsJean Masclet, Andre Turiot
Estimating the term…
An oleopneumatic suspension with variable throttle orifices, particularly for aircraft landing gear comprising a rod (1) enclosing a pneumatic spring (2) and being fixed with respect to a piston (4) sliding in a cylinder (3), two valves (6) and (7) with permanent throttle orifices, the valve (6), which is of greater cross-section, throttling in the compression phase and the valve (7), which is of lesser cross-section, throttling in the extension phase, the suspension comprising in addition a throttle device, the section of whose orifice varies in dependence on the position and the direction of displacement of the piston (4) in the cylinder (3) so that over a given distance around a predetermined equilibrium position the orifices ensuring throttling in the compression and extension phases are of cross-sections respectively greater than the corresponding orifices over the remainder of the distance covered by the piston (4) in the cylinder (3). While primarily for use in connection with landing gear or support bogies of aircraft, the suspension is also suitable for land vehicles or for testing.
An oleopneumatic suspension, comprising:
An oleopneumatic suspension for use in an aircraft landing gear, comprising:
Dependencies are inferred from the claim text.