Emergency low altitude parachute wherein canopy is deployed...

Aeronautics and astronautics – Safety lowering devices – Parachutes

Reexamination Certificate

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Details

C244S147000, C244S148000, C244S15100A

Reexamination Certificate

active

06705572

ABSTRACT:

BACKGROUND OF THE INVENTION
1. Field of the Invention
The present invention relates generally to parachutes and, more specifically, to emergency low altitude parachutes consisting of a parachute canopy that inflates by the introduction of compressed gas. A compressed gas canister is located within the housing of the inflatable portion of the device and is activated by an activation ring. The device is a self-contained device that is deployed manually by pulling an activation ring which activates a compressed gas canister, inflating the canopy pontoons and expanding the canopy of the parachute. The device is stored within a carrying case prior to use.
When the low altitude emergency parachute is removed from its storage case, the user attaches the shoulder, crotch and waist harness to their body. A helmet with breathing apparatus is supplied. Once the user is harnessed in, the device is held in the front of the body and is ready for deployment. An activation ring is provided as means of activating the compressed gas canister, located within the housing of the parachute. Once activated the parachute pontoons fill with the gas rapidly, expanding them and unfolding the parachute canopy. The device is then released through the threshold of the escape route. When the parachute has fully deployed, the parachute has sufficient surface air that a user may propel themselves from a low altitude without requiring a substantial distance before the canopy is able to support the user's weight. The device is designed for users not familiar with parachute use and avoids the potential of entanglement of the user in the chute cord, which may occur as a body in free-fall rolls uncontrollably.
2. Description of the Prior Art
There are other parachute devices designed for emergency use. Typical of these is U.S. Pat. No. 1,854,996 issued to Palagonia on Apr. 19, 1932.
Another patent was issued to Hovland on Oct. 27, 1953 as U.S. Pat. No. 2,656,996. Yet another U.S. Pat. No. 2,924,409 was issued to Burke Jr. on Feb. 9, 1960 and still yet another was issued on Jan. 10, 1961 to Magnuson as U.S. Pat. No. 2,967,685.
Another patent was issued to Stencel on May 19, 1964 as U.S. Pat. No. 3,133,718. Yet another U.S. Pat. No. 3,193,223 was issued to Davis on Jul. 6, 1965. Another was issued to Chappell on May 17, 1966 as U.S. Pat. No. 3,251,566 and still yet another was issued on Jun. 3, 1969 to Stencel et al. as U.S. Pat. No. 3,447,769.
Another patent was issued to Nimylowycz on Sep. 18, 1973 as U.S. Pat. No. 3,759,469. Yet another U.S. Pat. No. 4,257,568 was issued to Bücker on Mar. 24, 1981 and still yet another was issued on Oct. 26, 1982 to Koenig as U.S. Pat. No. 4,355,774. And another was issued on Dec. 8, 1992 to Schoffl as U.S. Pat. No. 5,169,093.
The invention has for an object the provision of a compressed air parachute characterized by a parachute sail having a transverse plate across its top portion to divide off a small chamber which is connected to a flexible air tube extending along the axis of the parachute sail to the bottom for connection with a supply of air which is capable of straightening out the tube and inflating the small compartment and thus insuring the opening of the parachute.
The present invention relates to parachutes and especially to arrangements and means adapted to provoke and accelerate the opening of a parachutist as he jumps.
The present invention provides a unique parachute construction and assembly which an be effectively and safely utilized at extremely low altitudes which will function effectively to permit safe descent of personnel and equipment from points of fall originating below 300 feet.
This invention relates generally to pilot chute ejection devices and more particularly to ejection devices employing ballistic and mechanical means for launching a pilot chute a sufficient distance from the aircraft to insure its operation.
A deployable parachute, comprising a collapsed parachute canopy; a plurality of suspension lines attached to the periphery of said canopy, and adapted to be attached to a load; a first explosive means independent of the launching source having a first and second member, said first member attached to said canopy and second member attached to said load.
The present invention relates to a parachute release control which may be held in the hand during sky diving prior to releasing the parachute from the pack.
The invention is a bail-out device comprising a collapsed balloon, a canister means at least partly inside the balloon having an opening therein, said opening having edges, lower fastening means on said canister.
A compact gun device for spreading the canopy of a parachute, including a main or central body means and a plurality of telescoping drive assemblies disposed radially about the body means.
A parachute arrangement having a hydraulic parachute spreader positioned internally of the canopy skirt and connected at one end by a lanyard to a load when deployed, such that upon operation of the drogue chute the initiator will ignite a propellant charge in the spreader to eject liquid coolant through peripherally spaced lateral orifices in the spreader sidewall against the skirt to facilitate a quick opening thereof.
The improvement refers to an inflatable device for quick expansion of parachutes for low altitude jumping, comprising elements of bags firmly connected to the canopy and sheathed into by tubes of the expansion structure, as well as lines tied between those bags and tubes, the object of the improvement being to permit a reduction of the dimensions of the expansion structure and to increase its expansion speed.
This is an improvement in circular canopies of the flat, conical, or hemispherical type, some of which have extended skirts with the canopies being of gore construction. External additional gores of porous material cover selected canopy gores and are arranged to insure circular balance of the canopy. Each external gore covering is mounted on radial seams of the canopy gore which it covers beginning at a point above the canopy skirt and extending along the radial seams and across the apex hem to define a compartment for accepting external air flow turbulence existing on the elongated canopy prior to normal inflation. The external gore is closed at the top thereof and incorporates an anti-oscillation vent with the lower end thereof being open and terminating at an elevation of approximately 4 to 14 inches above and in spaced relation to the skirt of the canopy.
A parachute associated with an object unfolds faster in an airstream if the object is first accelerated in the direction of descent. This principle can be applied advantageously to a mine system combating military targets from the air because the time between starting from an ambush position in the terrain to the onset of searching movements in the air can be shortened.
While these parachutes may be suitable for the purposes for which they were designed, they would not be as suitable for the purposes of the present invention, as hereinafter described.
SUMMARY OF THE PRESENT INVENTION
The present invention discloses an emergency low altitude parachute having a parachute canopy that inflates by the introduction of compressed gas. A compressed gas canister is located within the housing of the inflatable portion of the device and is activated by an activation ring . The device is stored within a carrying case prior to use. When the low altitude emergency parachute is removed from its storage case, the user attaches the attachment harness to their body. A helmet with breathing apparatus is supplied. Once the user is harnessed in, the device is held in the front of the body and an activation ring is provided as means of activating the compressed gas canister. Once activated the parachute pontoons fill with the gas rapidly, expanding them and unfolding the parachute canopy. The device is then released through the threshold of the escape route. When the parachute has fully deployed, the parachute has sufficient surface air that a user may propel themselves from a low alti

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