Parachute reefing device
AssigneeIrvin Great Britain Limited
InventorChristopher John Winchurch
Life of this patent
Estimating the term…
Abstract
A parachute having a reefing device for securing together normally spaced parts of the canopy to provide a canopy that is reduced in size by the substantial elimination of a reefed section thereof as an effective drag area, and including a release device for releasing the reefed section of the canopy after initial parachute development to thereby permit the reefed section to inflate in full deployment of the canopy. The parachute may be conventional; a single skin gliding parachute having one or more wing sections wholly or in part reefed; or a multicellular double-skin ram-air inflated gliding parachute with some of the central cells reefed.
Claims15
A gliding parachute including a canopy having first and second stable stages of development and comprising a pair of wing sections having a keel line separating the same, said keel line extending from the leading edge of said canopy to the trailing edge of said canopy, reefing mean for releasably securing together normally spaced apart sections of each said wing sections to each side of the central portion thereof to provide a reefed section for each said wing sections, each said reefed section comprising a central portion of each said wing sections reefed by said reefing means from at least substantially the leading edge to at least substantially the trailing edge of said canopy, each reefed section of said canopy being substantially operably eliminated by said reefing means as a drag area of said parachute in the first of said stable stages of development of said canopy, and release means operable independently of the forces of inflation of said canopy for releasing said reefing means to allow each said reefed section to inflate as an operable drag area of said parachute in full deployment of said canopy as the second of said stable stages of development thereof.
A gliding parachute including a canopy comprising a plurality of sections and having first and second stable stages of development, said canopy being in an aerodynamically balanced configuration in each of said stages of development thereof, reefing means extending along and at least adjacent opposite side edges of at least a section of said canopy for releasably securing opposed side edges thereof together and said section of said canopy having the same comprises a reefed section of said canopy, said reefing means being substantially interengagable with and along the length of said opposed siide edges of said reefed section, said reefed section of said canopy being substantially operably eliminated by said reefing means as a drag area of said parachute in the first of said stable stages of development of said canopy, and release means operable independently of the forces of inflation of said canopy for releasing said reefing means to allow said reefed section to inflate as an operable drag area of said parachute in full deployment of said canopy as the second of said stable stages of development thereof.
A parachute having a plurality of gores extending radially from a central region thereof and including smoothly releasable reefing means for securing together normally spaced parts of the canopy thereof as a reefed section in a first stable stage of canopy development wherein the canopy thereof is reduced in size by the elimination of said reefed section thereof intermediate said parts as an effective drag area of said parachute, said reefed section comprising at least one of said gores, and release means operable independently of the forces of inflation of said canopy for releasing said reefing means after said first stable stage of canopy development to allow said reefed section thereof to smoothly inflate and providing a second stable stage of canopy development wherein the canopy is fully developed.
A parachute having a canopy including a plurality of elongate sections and smoothly releasable reefing means for securing together normally spaced parts of at least an elongate section of each canopy thereof as a reefed section in a first stable stage of canopy development wherein the canopy thereof is reduced in size by the elimination of said reefed section thereof intermediate said parts as an effective drag area of said parachute, said reefing means and said reefed section provided thereby extending longitudinally along substantially the entire length of said at least an elongate section of said canopy, and release means operable independently of the forces of inflation of said canopy for releasing said reefing means after said first stable stage of canopy development to allow said reefed section thereof to smoothly inflate and providing a second stable stage of canopy development wherein the canopy is fully developed.
A gliding parachute including a canopy comprising a plurality of elongate sections and having first and second stable stages of development, said canopy being in an aerodynamically balanced configuration in each of said stages of development thereof, reefing means for releasably securing together at least a pair of normally spaced apart elongate sections of said canopy to each side of at least an elongate section of said canopy, said at least an elongate section of said canopy intermediate said secured together at least a pair of normally spaced apart elongate sections of said canopy comprising a reefed section of said canopy and being substantially operably eliminated by said reefing means as a drag area of said parachute in the first of said stable stages of development of said canopy, said reefing means and said reefed section provided thereby extending longitudinally along substantially the entire length of said at least an elongate section of said canopy, and release means operable independently of the forces of inflation of said canopy for releasing said reefing means to allow said reefed section to inflate as an operable drag area of said parachute in full deployment of said canopy as the second of said stable stages of development thereof.
Dependencies are inferred from the claim text.