US1861784A - Parachute opener - Google Patents

Parachute opener Download PDF

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Publication number
US1861784A
US1861784A US485668A US48566830A US1861784A US 1861784 A US1861784 A US 1861784A US 485668 A US485668 A US 485668A US 48566830 A US48566830 A US 48566830A US 1861784 A US1861784 A US 1861784A
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Prior art keywords
valve
pack
gas
parachute
tank
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Expired - Lifetime
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US485668A
Inventor
Thomas B Brown
Marion L Stansell
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Individual
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Individual
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Priority to US485668A priority Critical patent/US1861784A/en
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D17/00Parachutes
    • B64D17/62Deployment
    • B64D17/72Deployment by explosive or inflatable means

Definitions

  • This invention relates to new and useful improvements in parachute openers.
  • Figure 1- is a perspective view of an openparachute, showing how our opener is embodied therein as well as how the gas tank is attached to a pack strapped to the back of the user.
  • Figure 2 is a perspective view of a portion of the canopy, showing how a branch of the flexible expanding tube is secured to it.
  • Figure 3 is aperspective view of the discharge end of the gas tank, showing the valve opening means.
  • Fi ure 4 is a longitudinal sectional view takent rough the release valve.
  • Figure 5 is av perspective view of the pack containing the parachute and our opening means.
  • the numeral 1 designates a conventional parachute sustainin sheet or canopy from which sustaining cor s 2 run to a ring 3. To the latter are attached the connected ends of straps 4 whose lower ends are secured to a harness 5 that is worn by the user.
  • the numeral 6 designates a conventional pack secured to the harness 5. Mounted within this pack is a small tank 7 filled with helium or other .tubularextension 11. for a suitable gas for assisting in the openingof the canopy. l i
  • a plug valve 9 constructed as'follows. Referring to Figure 4, this valve come 55 prises a cylindrical member having a central bore communicating at its rear end with.
  • the plug 12 will be snapped forward by the spring 13 until it hits a cap 16 screwed on the front end of the valve body.
  • the valve plug 12 will permit gas under pressure to flow fromthe tank? into the tubular extension 11' to which one end of a flexible tube 17 is connected.
  • the tube 17 projectsupwardly under the canopy 1 where it is secured to an annular flexible tube 18 which is stitched or otherwise secured to the under surface of said canopy near its fluted marginal edge. (See Figures 1 and 2.) r
  • a flexible compartment 19 Secured under the middle top part of the canopy l is a flexible compartment 19 which is in communication with the annular gas tube 18 through radial flexible tubes 20 that are also attached to the under surface of the canopy.
  • this tubular network When this tubular network is and denly filled with gas, it will bulge out the canopy to assist in forcing it from the pack 6 and opening it to its maximum limits within a short period of time.
  • This gas which the upper compartment 19 receives will make I it sufiiciently buoyant to materially assist in carrying the parachute user slowly to the ground.
  • valve on the tank will be operated at the same time to permit gas to rush into the tubular network within the canopy to force it'out of the pack, open it up and hold it open for a slow and safe descent.

Description

June 7, 1932.
T. B BROWN ET AL PARAdHUTE OPENER Filed Oct. 1. 1930 mnz f Y 9 7X; ATTORNEY Patented June 7, 1932 UNITED STATES PATENT omen,
moms a. :saown AND mlnron n s'ransnrln, or narrow. 1110 rnnaonurn orphan Application filed October 1, 1930; Serial No. 485,668.
This invention relates to new and useful improvements in parachute openers.
It is the principal object of our invention to provide means whereby helium or other gas under pressure may be employed to quick- 1y force a parachute from a pack, then to assist in speedily opening it out and thereafter contributing to its buoyancy.
Our invention contemplates the attachment gas will assist in carrying the user safely to the ground. Other important and incidental objects 7 will be brought out in the following specification and particularly set forth in the subjoined claims.
In the accom anying drawing illustrating our invention, Figure 1-is a perspective view of an openparachute, showing how our opener is embodied therein as well as how the gas tank is attached to a pack strapped to the back of the user. Figure 2 is a perspective view of a portion of the canopy, showing how a branch of the flexible expanding tube is secured to it. Figure 3 is aperspective view of the discharge end of the gas tank, showing the valve opening means. Fi ure 4 is a longitudinal sectional view takent rough the release valve. And Figure 5 is av perspective view of the pack containing the parachute and our opening means.
Referring to the accompanying drawing for a detailed description of our invention,
the numeral 1 designates a conventional parachute sustainin sheet or canopy from which sustaining cor s 2 run to a ring 3. To the latter are attached the connected ends of straps 4 whose lower ends are secured to a harness 5 that is worn by the user.
,Referring to Figures 1 and 5, the numeral 6 designates a conventional pack secured to the harness 5. Mounted within this pack is a small tank 7 filled with helium or other .tubularextension 11. for a suitable gas for assisting in the openingof the canopy. l i
Screwed into a tapped hole in one end 8 of the tank 7 is a plug valve 9 constructed as'follows. Referring to Figure 4, this valve come 55 prises a cylindrical member having a central bore communicating at its rear end with. a
.counterhore 10. Projecting from the middle partof the body of the valve 9 is an inclined purpose herein- 00 after to be described. Longitudinally movable within the bore of the valve 9 is a-cylindrical plug 12 between which and the shoulder at the rear end of the valvebody is a helical spring 13. The'latter is adapted to move the plug 12 forward toclear the bore 14 in the projection 11 when said plug is not restrained from such movement by a-wire 15 that projects through two holes in the valve body. When released by. pulling the wire 15 through these holes,
the plug 12 will be snapped forward by the spring 13 until it hits a cap 16 screwed on the front end of the valve body. In this 130- V sition the valve plug 12 will permit gas under pressure to flow fromthe tank? into the tubular extension 11' to which one end of a flexible tube 17 is connected. The tube 17 projectsupwardly under the canopy 1 where it is secured to an annular flexible tube 18 which is stitched or otherwise secured to the under surface of said canopy near its fluted marginal edge. (See Figures 1 and 2.) r
Secured under the middle top part of the canopy l is a flexible compartment 19 which is in communication with the annular gas tube 18 through radial flexible tubes 20 that are also attached to the under surface of the canopy. When this tubular network is and denly filled with gas, it will bulge out the canopy to assist in forcing it from the pack 6 and opening it to its maximum limits within a short period of time. This gas which the upper compartment 19 receives will make I it sufiiciently buoyant to materially assist in carrying the parachute user slowly to the ground.
For the purpose of releasing gas from the tank 7 at the same time the rip cord 21 of the m0 pack 6 is pulled, we attach the wire 15 to the inner end of the cord.
Therefore, when the pack is opened bythe rip cord, the valve on the tank will be operated at the same time to permit gas to rush into the tubular network within the canopy to force it'out of the pack, open it up and hold it open for a slow and safe descent.
Having described our invention, we claim:
1. The combination with a parachute, of flexible tubing secured to the canopy thereof, a gas tank carried by said parachute in communication with said flexible tubing, a valve for admitting gas to the latter from the tank, a slidable closure member in said valve, 8. spring for moving said closure member to a position to permit the flow of gas from the tank to the tubing, a pack for containing said parachute and tank, a rip cord for opening said pack, and a Wire for holding said valve closure member. in 'a closed position against the tension of said spring, said wire being secured to the rip cord and adapted to be drawn by it from the valve to release the latter when the rip cord is pulled to open the pack.
2. The combination with a parachute, of a flexible receptacle secured to the *canopy thereof, a gas tank carried by said parachute in communication with said flexible receptacle, a valve for admitting gas to the latter from the tank, a closure member in said valve, a pack for containing said parachute and tank, a rip cord for opening said pack, and means for holdin said valve closure member in a closed position, said means being secured to the rip cord and adapted to be drawn b it to open the valve when the rip cord is pul ed to 0 en the pack.
In testimony w ereof we havev hereunto this 29th day of September,
set our hands 1930.
THOMAS B.'BROWN.- 4
MARION L.
US485668A 1930-10-01 1930-10-01 Parachute opener Expired - Lifetime US1861784A (en)

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US485668A US1861784A (en) 1930-10-01 1930-10-01 Parachute opener

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Cited By (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2656996A (en) * 1950-03-15 1953-10-27 Hovland Abraham Nilsen Parachute having an inflatable opening means
US2778599A (en) * 1953-01-16 1957-01-22 Jr Herman J Paul Parachute inflating means
US2847174A (en) * 1956-10-23 1958-08-12 Sribny Bohdan Releasable airplane chair with parachute
US2974912A (en) * 1958-09-26 1961-03-14 Goodyear Tire & Rubber Shock absorber
US2992793A (en) * 1956-02-17 1961-07-18 Devantier Karl Edmund Aircraft provided with a device for hurling a location signal emitter in cases of accidents
US3165763A (en) * 1963-01-15 1965-01-19 Koch & Sons Inc H Safety locking device for the inflating means in aerial survival kits
US3384328A (en) * 1966-04-15 1968-05-21 G F Schjeldahl Co Self-expanding rib
US5028018A (en) * 1986-04-07 1991-07-02 Burghardt Krebber Device for accelerating the opening and/or extension of aviation devices, such as canopy parachutes, square or sliding parachutes, gliders (hang-gliders) and others
US5058831A (en) * 1989-05-19 1991-10-22 Shigeki Takahashi Emergency escape unit
EP1101697A2 (en) * 1999-11-15 2001-05-23 Roger Gorlero Wearable safety system for persons, with air brake unfolding itself automatically in case of danger
EP1101698A1 (en) * 1999-11-15 2001-05-23 Roger Gorlero Wearable safety system for persons with air brake deploying itself automatically in case of danger
WO2003033072A2 (en) * 2001-10-12 2003-04-24 Kurt Koch Rescue and survival case
WO2003033078A1 (en) * 2001-10-12 2003-04-24 Kurt Koch Parachute (survival air guard)
WO2005012086A2 (en) * 2003-08-05 2005-02-10 Aip Evacuation Systems Ltd. Rescue parachute device
US9889941B1 (en) * 2017-02-03 2018-02-13 Indemnis, Inc. Inflatable deployment apparatus for descent-restraint system for aerial vehicles
US11286051B2 (en) * 2017-08-24 2022-03-29 Nippon Kayaku Kabushiki Kaisha Aerial vehicle safety apparatus and aerial vehicle
US11332253B2 (en) 2014-08-14 2022-05-17 The Government Of The United States Of America, As Represented By The Secretary Of The Navy High-altitude payload retrieval (HAPR) apparatus and methods of use
US11530046B2 (en) 2017-08-24 2022-12-20 Nippon Kayaku Kabushiki Kaisha Aerial vehicle safety apparatus and aerial vehicle

Cited By (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2656996A (en) * 1950-03-15 1953-10-27 Hovland Abraham Nilsen Parachute having an inflatable opening means
US2778599A (en) * 1953-01-16 1957-01-22 Jr Herman J Paul Parachute inflating means
US2992793A (en) * 1956-02-17 1961-07-18 Devantier Karl Edmund Aircraft provided with a device for hurling a location signal emitter in cases of accidents
US2847174A (en) * 1956-10-23 1958-08-12 Sribny Bohdan Releasable airplane chair with parachute
US2974912A (en) * 1958-09-26 1961-03-14 Goodyear Tire & Rubber Shock absorber
US3165763A (en) * 1963-01-15 1965-01-19 Koch & Sons Inc H Safety locking device for the inflating means in aerial survival kits
US3384328A (en) * 1966-04-15 1968-05-21 G F Schjeldahl Co Self-expanding rib
US5028018A (en) * 1986-04-07 1991-07-02 Burghardt Krebber Device for accelerating the opening and/or extension of aviation devices, such as canopy parachutes, square or sliding parachutes, gliders (hang-gliders) and others
US5058831A (en) * 1989-05-19 1991-10-22 Shigeki Takahashi Emergency escape unit
EP1101698A1 (en) * 1999-11-15 2001-05-23 Roger Gorlero Wearable safety system for persons with air brake deploying itself automatically in case of danger
EP1101697A2 (en) * 1999-11-15 2001-05-23 Roger Gorlero Wearable safety system for persons, with air brake unfolding itself automatically in case of danger
EP1101697A3 (en) * 1999-11-15 2001-08-08 Roger Gorlero Wearable safety system for persons, with air brake unfolding itself automatically in case of danger
WO2003033072A2 (en) * 2001-10-12 2003-04-24 Kurt Koch Rescue and survival case
WO2003033078A1 (en) * 2001-10-12 2003-04-24 Kurt Koch Parachute (survival air guard)
WO2003033072A3 (en) * 2001-10-12 2003-12-11 Kurt Koch Rescue and survival case
US20050087653A1 (en) * 2001-10-12 2005-04-28 Kurt Koch Parachute (survival air guard)
WO2005012086A2 (en) * 2003-08-05 2005-02-10 Aip Evacuation Systems Ltd. Rescue parachute device
WO2005012086A3 (en) * 2003-08-05 2005-07-07 Aip Evacuation Systems Ltd Rescue parachute device
US11332253B2 (en) 2014-08-14 2022-05-17 The Government Of The United States Of America, As Represented By The Secretary Of The Navy High-altitude payload retrieval (HAPR) apparatus and methods of use
US9889941B1 (en) * 2017-02-03 2018-02-13 Indemnis, Inc. Inflatable deployment apparatus for descent-restraint system for aerial vehicles
US11286051B2 (en) * 2017-08-24 2022-03-29 Nippon Kayaku Kabushiki Kaisha Aerial vehicle safety apparatus and aerial vehicle
US11530046B2 (en) 2017-08-24 2022-12-20 Nippon Kayaku Kabushiki Kaisha Aerial vehicle safety apparatus and aerial vehicle

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