Energy recovery apparatus and method
First Claim
1. An energy recovery apparatus for recovering energy from a flight control element, and assisting in moving said flight control element through the use of the recovered energy, comprising:
- a single-acting, ram-like system having a piston operably associated with the flight control element and movable in response to movement of said flight control element;
a compressible medium in communication with the ram-like system, the compressible medium able to store energy acting on the piston when the flight control element is moved in a first direction, thus causing the piston to be moved in said first direction, said stored energy being usable by the ram-like system to assist in moving the flight control element in a second direction, wherein the flight control element is extended aft in a longitudinal direction; and
wherein said piston is moved in said first direction into a retracted position solely by a force exerted by said flight control element as said flight control element moves in said first direction.
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Accused Products
Abstract
An energy recovery and storage apparatus especially well adapted for use with flight control surfaces on airborne mobile platforms, such as aircraft. In one form the apparatus includes a ram-like element coupled to a portion of a flight control surface. An accumulator holds a flexible container having a compressible medium contained within the flexible container. The accumulator is in fluid communication with a housing of the ram-like element. When the flight control surface is moved from a deployed to a retracted position, the energy acting on the surface is recovered and stored in the compressible medium as the ram-like element forces fluid from its housing into the accumulator. When the flight control surface is to be deployed again in a subsequent cycle, the stored energy in the compressible medium is used to urge the ram-like element into an extended position, thus assisting in deploying the flight control surface. The various preferred embodiments all enable lower power, smaller and less expensive actuators to be used to control a flight control surface.
39 Citations
6 Claims
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1. An energy recovery apparatus for recovering energy from a flight control element, and assisting in moving said flight control element through the use of the recovered energy, comprising:
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a single-acting, ram-like system having a piston operably associated with the flight control element and movable in response to movement of said flight control element; a compressible medium in communication with the ram-like system, the compressible medium able to store energy acting on the piston when the flight control element is moved in a first direction, thus causing the piston to be moved in said first direction, said stored energy being usable by the ram-like system to assist in moving the flight control element in a second direction, wherein the flight control element is extended aft in a longitudinal direction; and wherein said piston is moved in said first direction into a retracted position solely by a force exerted by said flight control element as said flight control element moves in said first direction. - View Dependent Claims (2, 3, 4, 5)
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6. An energy recovery apparatus for recovering energy from a flight control element located in a flight surface of an airborne mobile platform, and assisting in moving said flight control element through the use of the recovered energy, comprising:
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a single-acting ram-like system having a piston operably associated with the flight control element and movable in response to movement of said flight control element; a compressible medium used in the ram-like system, the compressible medium able to store energy acting on the piston via the flight control element when the flight control element is moved in a first direction, said stored energy being usable by the ram-like system to assist in moving the flight control element in a second direction, wherein the flight control element is extended aft in a longitudinal direction; and wherein said piston is moved in said first direction into a retracted position by a force exerted by said flight control element as said working element moves in said first direction.
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Specification