Flexible bellows actuation system
AssigneeMcDonnell Douglas Helicopter Company
InventorsJeffrey M. Hein, Richard Piechowicz
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AssigneeMcDonnell Douglas Helicopter Company
InventorsJeffrey M. Hein, Richard Piechowicz
Estimating the term…
A closed loop fully self-contained actuation system for converting a mechanical input motion into a mechanical output motion, which actuates a device such as a flight control surface on an aircraft, comprises an input actuator including a first fluid pressurizing means responsive to the mechanical input motion, and an output actuator including a second fluid pressurizing means, as well as a flexible fluid line extending between the first and second fluid pressurizing means to provide fluid communication therebetween. The second fluid pressurizing means is responsive to fluid flow through the fluid line, thereby initialing the output motion. The system is advantageous because it requires no hydraulic pumps, no accumulators, no reservoirs, and no dynamic seals or mechanical joints, permitting great reliability. The actuation system may be easily folded in conjunction with the apparatus on which it is employed, for compact storage.
An actuation system for converting a mechanical input motion into a mechanical output motion wherein said mechanical output motion actuates a device, said actuation system comprising:
An actuation system for converting a linear mechanical input motion into a rotary mechanical output motion wherein said mechanical output motion actuates a device, said actuation system comprising:
Dependencies are inferred from the claim text.