US3602463A - Fail-safe raft system - Google Patents
Fail-safe raft system Download PDFInfo
- Publication number
- US3602463A US3602463A US811070A US3602463DA US3602463A US 3602463 A US3602463 A US 3602463A US 811070 A US811070 A US 811070A US 3602463D A US3602463D A US 3602463DA US 3602463 A US3602463 A US 3602463A
- Authority
- US
- United States
- Prior art keywords
- raft
- cover member
- rolled
- boot members
- boot
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
- 230000004083 survival effect Effects 0.000 claims abstract description 11
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims abstract description 11
- 230000002093 peripheral effect Effects 0.000 claims abstract description 9
- KAATUXNTWXVJKI-UHFFFAOYSA-N cypermethrin Chemical compound CC1(C)C(C=C(Cl)Cl)C1C(=O)OC(C#N)C1=CC=CC(OC=2C=CC=CC=2)=C1 KAATUXNTWXVJKI-UHFFFAOYSA-N 0.000 claims description 10
- IWEDIXLBFLAXBO-UHFFFAOYSA-N dicamba Chemical compound COC1=C(Cl)C=CC(Cl)=C1C(O)=O IWEDIXLBFLAXBO-UHFFFAOYSA-N 0.000 claims description 6
- 238000004806 packaging method and process Methods 0.000 abstract description 7
- 230000002028 premature Effects 0.000 abstract description 4
- 239000004677 Nylon Substances 0.000 description 5
- 229920001778 nylon Polymers 0.000 description 5
- 238000005188 flotation Methods 0.000 description 2
- 238000013459 approach Methods 0.000 description 1
- 230000000712 assembly Effects 0.000 description 1
- 238000000429 assembly Methods 0.000 description 1
- 210000001217 buttock Anatomy 0.000 description 1
- 239000004744 fabric Substances 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 229920002635 polyurethane Polymers 0.000 description 1
- 239000004814 polyurethane Substances 0.000 description 1
- 238000000926 separation method Methods 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63C—LAUNCHING, HAULING-OUT, OR DRY-DOCKING OF VESSELS; LIFE-SAVING IN WATER; EQUIPMENT FOR DWELLING OR WORKING UNDER WATER; MEANS FOR SALVAGING OR SEARCHING FOR UNDERWATER OBJECTS
- B63C9/00—Life-saving in water
- B63C9/22—Devices for holding or launching life-buoys, inflatable life-rafts, or other floatable life-saving equipment
- B63C9/23—Containers for inflatable life-saving equipment
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D25/00—Emergency apparatus or devices, not otherwise provided for
Definitions
- the present invention relates to a novel and improved packaging system for an inflatable raft in survival apparatus used by a pilot after an ejection from his aircraft over water.
- the improved packaging system involves use of a pair of cup-shaped boot members that fit over opposite ends of the compactly rolled raft and a cover member that overlies the rolled raft and boot members. Studs on the outer peripheral surface of one flap of the cover member engage grommets in the ends of tabs attached to the boot members as well as grommets on the other flap of the cover member and prevent premature inflation of the raft until the cover member and boot members are removed.
- FIG. 1 is a diagrammatic side view of a pilot wearing the improved water survival apparatus of the invention
- FIG. 2 is a diagrammatic perspective view of the pilot's seat cushion, his parachute pack and the improved inflatable raft package of the invention
- FIG. 3 is a perspective view of the improved raft package of the invention with its cover member in its opened condition;
- FIG. 4 is a perspective view of the improved raft package of the invention with its cover member in its closed condition.
- the parachute pack 3 and the seat cushion 5 are positioned behind the buttocks area of the pilot 7 by the various conventional strap and harness assemblies.
- the improved inflatable raft assembly 9 of the invention is secured to the bottom edge of the seat cushion 5 by the heavy duty zipper mechanism 11 and to the parachute pack 3 by straps 13 and suitable interconnecting lift-a-dot fastening devices associated therewith.
- the strap-buckle interconnection 12 also preferably connects the raft assembly 5 with the parachute pack 3.
- the raft assembly 9 includes an inflatable raft 15, a pair of cup-shaped boot members 17 which fit over opposite ends of the raft when it is rolled into a compact cylindrical configuration, and a cover member 19 which encloses the raft and the boot members when the assembly is in its normal packed condition.
- the inflatable raft 15 is preferably constructed of a polyurethane coated nylon fabric material which has been found to be highly durable, light in weight and readily rolled into a small compact package.
- the pressurized CO, gas cartridge 21 permits automatic inflation of the raft when the cover member 19 and the boot members 17 are removed and the herringbone nylon tape or line 23, which is secured to a control valve of the cartridge 21 as well as to one boot member 17, is operated.
- the boot member 17 are preferably connected to one another by the nylon tape or the like 18 that extends therebetween.
- Each of the boot members 17 also has an integral tab 25 that extends inwardly toward the center of the rolled raft 15 when the boot members 17 are positioned over its opposite ends.
- a pair of studs 27 are secured to the outer peripheral surface of the cover member 19 adjacent one of its side edges and extend outwardly therefrom.
- Conventional ripcord pins 33 which are connected to one end of the control cable 35, extend through apertures in the ends of studs 27 and secure the grommets 29 and 31 in position over studs 27 when the raft is rolled in its normal packaged condition.
- the endof the flap 19a of cover member 19 is folded back over the studs and pins and secured in that position by snap fasteners so as to enclose the ripcord pin interconnection with the studs.
- the cable 35 passes through a flexible housing that is preferably attached to the top of the parachute pack 3 as at 37.
- the other end of cable 35 is connected to the D-ring 41 which is normally positioned in the D-ring retainer pocket 43 also attached to the top of the parachute pack 3.
- the cable 35 is preferably severable as at 45 by a suitable male-female interconnection or the like so as to facilitate separation of the raft package from the seat cushion 5 and the parachute pack 3'when it is desirable to do so.
- the bowed spring metallic strap 47 is sewed into a pocket between the grommets 31 on the flap 19a of cover member 19 as shown in FIG. 3 of the drawing.
- the raft 15 is first rolled into a suitable compact cylindrical configuration.
- the boot members 17 are then slipped over opposite ends of the rolled raft 15.
- the flap of the cover member 19 to which the studs 27 are secured is then wrapped about the rolled raft 15.
- the grommets 29 in the ends of the tabs 25 on boot members 17 are then positioned on their respective studs 27.
- the other flap of cover member 19 is then wrapped about the rolled raft 15 and grommets 31 herein are positioned on studs 27.
- Ripcord pins 33 are then inserted into the apertures adjacent the ends of studs 27 to maintain the cover member 19 and boot members 17 in their normal packaging position about the raft 15.
- flap 19a is then folded back over ripcord pins 33 and cable 35 and secured by the snap fasteners.
- the packaged raft assembly is then secured to the front edge of the seat cushion 5 by the zipper mechanism 11 and to the parachute pack 3 by the snap fasteners and by the strap-buckle connection 12.
- D-ring 41 When the pilot approaches his parachute landing in the water after ejection from his aircraft, he reaches behind him and pulls D-ring 41. Actuation of D-ring 41 withdraws ripcord pins 33 from studs 27 and the bowed spring strap member 47 automatically opens cover member 19. Actuation of the nylon tape 23 then opens the control valve of the CO cartridge 21 and the raft l5 quickly inflates. Tape 23 is preferably connected to the pilot in some suitable manner so that the pilot and the raft cannot be separated during the landing operation.
- Water survival apparatus for use with an aviators parachute pack, said apparatus comprising:
- a cover member that overlies the outer peripheral surface of the rolled raft and the boot members on the opposite ends thereof;
- Water survival apparatus for use with an aviators parachute pack, said apparatus comprising:
- a cover member that overlies the outer peripheral surface of the rolled raft and the boot members on. the opposite ends thereof;
- each boot member having a grommet through which the adjacent stud on the cover member also passes;
- a ripcord pin which passes through an aperture adjacent the outer end of each stud and normally maintains the grommets in the cover and boot members fixed on the studs;
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Ocean & Marine Engineering (AREA)
- Business, Economics & Management (AREA)
- Emergency Management (AREA)
- Aviation & Aerospace Engineering (AREA)
- Buffer Packaging (AREA)
Abstract
The present invention relates to a novel and improved packaging system for an inflatable raft in survival apparatus used by a pilot after an ejection from his aircraft over water. The improved packaging system involves use of a pair of cup-shaped boot members that fit over opposite ends of the compactly rolled raft and a cover member that overlies the rolled raft and boot members. Studs on the outer peripheral surface of one flap of the cover member engage grommets in the ends of tabs attached to the boot members as well as grommets on the other flap of the cover member and prevent premature inflation of the raft until the cover member and boot members are removed.
Description
Chris T. Koochembere [72] Inventor Glendora, NJ. [21] AppL No. 811,070 [22] Filed Mar. 27, 1969 [45] Patented Aug. 31, 1971 [73] Assignee The United States of America as represented by the Secretary of the Navy [54] FAIL-SAFE RAFT SYSTEM 3 Claims, 4 Drawing Figs.
[52] US. Cl 244/148 [5!] int. Cl 864d 17/40 [50] Field of Search 244/148, 147, l, 142; 9/2; 206/65 [56] References Cited UNITED STATES PATENTS 2,114,301 4/1938 Harrigan 244/148 2,366,455 1/1945 Patten 244/147 2,444,859 7/1948 Sturtevant 9/2 2,467,038 4/1949 Kajdan 244/148 3,057,472 9/1962 Douty 206/65 Primary Examiner-Milton Buchler Assistant ExaminerCarl A. Rutledge Attorneys-E. J. Brower and A. W, Collins ABSTRACT: The present invention relates to a novel and improved packaging system for an inflatable raft in survival apparatus used by a pilot after an ejection from his aircraft over water. The improved packaging system involves use of a pair of cup-shaped boot members that fit over opposite ends of the compactly rolled raft and a cover member that overlies the rolled raft and boot members. Studs on the outer peripheral surface of one flap of the cover member engage grommets in the ends of tabs attached to the boot members as well as grommets on the other flap of the cover member and prevent premature inflation of the raft until the cover member and boot members are removed.
PATENIEU AUB31 I91! 3. 602 ,463
sum 1 [IF 2 INVENTOR.
CHRIS T. KOOCHEMBERE mum Arron/vs) FAIL-SAFE RAFT SYSTEM Survival equipment to be effective when a pilot must make an emergency exit from his aircraft over water must meet certain essential requirements. The equipment must not only eject the pilot safely from his aircraft and effect his safe descent to the water. It must also provide an effective flotation means for the pilot for prolonged periods of time on the water. Although various types of satisfactory flotation devices have been devised in the past, considerable difficulty has been experienced heretofore in packaging such devices in a compact suitable manner for satisfactory disposition in the confined cockpit area of the aircraft.
It is therefore a principal object of the present invention to provide a novel and improved packaging technique for the inflatable survival or other flotation device in survival equipment used by a pilot in an ejection from his aircraft over water.
It is a further object of the invention to provide a novel and improved inflatable raft package for aircraft water survival equipment which includes a fail-safe feature that prevents inadvertent premature inflation of the raft.
It is a further object of the invention to provide a novel and improved inflatable raft package for aircraft water survival equipment which includes a package opening feature that permits rapid unrestricted inflation of the raft when its CO inflation cartridge is actuated.
Other objects and many of the attendant advantages of this invention will be readily appreciated as the same becomes better understood by reference to the following detailed description when considered in connection with the accompanying drawing wherein:
FIG. 1 is a diagrammatic side view of a pilot wearing the improved water survival apparatus of the invention;
FIG. 2 is a diagrammatic perspective view of the pilot's seat cushion, his parachute pack and the improved inflatable raft package of the invention;
FIG. 3 is a perspective view of the improved raft package of the invention with its cover member in its opened condition; and
FIG. 4 is a perspective view of the improved raft package of the invention with its cover member in its closed condition.
Referring now to the various FIGS. of the drawing, it will be noted that the parachute pack 3 and the seat cushion 5 are positioned behind the buttocks area of the pilot 7 by the various conventional strap and harness assemblies. The improved inflatable raft assembly 9 of the invention is secured to the bottom edge of the seat cushion 5 by the heavy duty zipper mechanism 11 and to the parachute pack 3 by straps 13 and suitable interconnecting lift-a-dot fastening devices associated therewith. The strap-buckle interconnection 12 also preferably connects the raft assembly 5 with the parachute pack 3.
The raft assembly 9 includes an inflatable raft 15, a pair of cup-shaped boot members 17 which fit over opposite ends of the raft when it is rolled into a compact cylindrical configuration, and a cover member 19 which encloses the raft and the boot members when the assembly is in its normal packed condition. The inflatable raft 15 is preferably constructed of a polyurethane coated nylon fabric material which has been found to be highly durable, light in weight and readily rolled into a small compact package. As will be more apparent hereinafter, the pressurized CO, gas cartridge 21 permits automatic inflation of the raft when the cover member 19 and the boot members 17 are removed and the herringbone nylon tape or line 23, which is secured to a control valve of the cartridge 21 as well as to one boot member 17, is operated.
The boot member 17 are preferably connected to one another by the nylon tape or the like 18 that extends therebetween. Each of the boot members 17 also has an integral tab 25 that extends inwardly toward the center of the rolled raft 15 when the boot members 17 are positioned over its opposite ends. A pair of studs 27 are secured to the outer peripheral surface of the cover member 19 adjacent one of its side edges and extend outwardly therefrom. When the boot members 17 are positioned over the ends of the rolled raft 15 and the cover member 19 is wrapped about the raft 15, the studs 27 pass through the grommets 29 adjacent the end of each respective tab 25 and through similarly spaced grommets 31 in the other flap of the cover member 19. Conventional ripcord pins 33, which are connected to one end of the control cable 35, extend through apertures in the ends of studs 27 and secure the grommets 29 and 31 in position over studs 27 when the raft is rolled in its normal packaged condition. When the ripcord pins 33 are positioned in studs 27, the endof the flap 19a of cover member 19 is folded back over the studs and pins and secured in that position by snap fasteners so as to enclose the ripcord pin interconnection with the studs. The cable 35 passes through a flexible housing that is preferably attached to the top of the parachute pack 3 as at 37. The other end of cable 35 is connected to the D-ring 41 which is normally positioned in the D-ring retainer pocket 43 also attached to the top of the parachute pack 3. The cable 35 is preferably severable as at 45 by a suitable male-female interconnection or the like so as to facilitate separation of the raft package from the seat cushion 5 and the parachute pack 3'when it is desirable to do so. The bowed spring metallic strap 47 is sewed into a pocket between the grommets 31 on the flap 19a of cover member 19 as shown in FIG. 3 of the drawing.
In operation, the raft 15 is first rolled into a suitable compact cylindrical configuration. The boot members 17 are then slipped over opposite ends of the rolled raft 15. The flap of the cover member 19 to which the studs 27 are secured is then wrapped about the rolled raft 15. The grommets 29 in the ends of the tabs 25 on boot members 17 are then positioned on their respective studs 27. The other flap of cover member 19 is then wrapped about the rolled raft 15 and grommets 31 herein are positioned on studs 27. Ripcord pins 33 are then inserted into the apertures adjacent the ends of studs 27 to maintain the cover member 19 and boot members 17 in their normal packaging position about the raft 15. The end of flap 19a is then folded back over ripcord pins 33 and cable 35 and secured by the snap fasteners. The packaged raft assembly is then secured to the front edge of the seat cushion 5 by the zipper mechanism 11 and to the parachute pack 3 by the snap fasteners and by the strap-buckle connection 12.
When the pilot approaches his parachute landing in the water after ejection from his aircraft, he reaches behind him and pulls D-ring 41. Actuation of D-ring 41 withdraws ripcord pins 33 from studs 27 and the bowed spring strap member 47 automatically opens cover member 19. Actuation of the nylon tape 23 then opens the control valve of the CO cartridge 21 and the raft l5 quickly inflates. Tape 23 is preferably connected to the pilot in some suitable manner so that the pilot and the raft cannot be separated during the landing operation.
It will be noted that until the D-ring 41 is operated for the removal of cover member 19 and boot members 17, tension on the nylon tape 23 cannot actuate the control valve of the CO cartridge 21. This fail-safe feature of the invention prevents inadvertent premature inflation of the raft 15.
Obviously, many modifications and variations of the present invention are possible in the light of the above teachings. It is therefore to be understood that within the scope of the appended claims, the invention may be practiced otherwise than as specifically described.
What is claimed is:
1. Water survival apparatus for use with an aviators parachute pack, said apparatus comprising:
a. a lightweight inflatable raft rolled into a compact cylindrical configuration;
b. a pair of cup-shaped boot members that fit over opposite ends of the rolled raft;
c. a cover member that overlies the outer peripheral surface of the rolled raft and the boot members on the opposite ends thereof;
d. means for manually controlling removal of the cover member and the boot members from the rolled raft when the raft is to be inflated;
e. and a line which is connected at one end to the control valve of a raft-inflating gas cartridge and at its other end to the aviator, said line being secured to and passing through one of said boot members.
2. Water survival apparatus for use with an aviators parachute pack, said apparatus comprising:
a. a lightweight inflatable raft rolled into a compact cylindrical configuration;
b. a pair of cup-shaped boot members that fit over opposite ends of the rolled raft;
c. a cover member that overlies the outer peripheral surface of the rolled raft and the boot members on. the opposite ends thereof;
d. a pair of studs which are secured to the outer peripheral surface of the cover member adjacent one side edge thereof;
e. a pair of grommets adjacent the other side edge of the cover member through which the studs pass when the cover member is wrapped about the rolled raft;
f. a tab connected to each boot member having a grommet through which the adjacent stud on the cover member also passes;
g. a ripcord pin which passes through an aperture adjacent the outer end of each stud and normally maintains the grommets in the cover and boot members fixed on the studs;
h. and a D-ring which is centrally positioned between the aviator's seat cushion and his parachute pack and which is connected to each of the ripcord pins.
3. The apparatus substantially as described in claim 2 wherein a bowed spring strap is secured to one side edge of the cover member.
Claims (3)
1. Water survival apparatus for use with an aviator''s parachute pack, said apparatus comprising: a. a lightweight inflatable raft rolled into a compact cylindrical configuration; b. a pair of cup-shaped boot members that fit over opposite ends of the rolled raft; c. a cover member that overlies the outer peripheral surface of the rolled raft and the boot members on the opposite ends thereof; d. means for manually controlling removal of the cover member and the boot members from the rolled raft when the raft is to be inflated; e. and a line which is connected at one end to the control valve of a raft-inflating gas cartridge and at its other end to the aviator, said line being secured to and passing through one of said boot members.
2. Water survival apparatus for use with an aviator''s parachute pack, said apparatus comprising: a. a lightweight inflatable raft rolled into a compact cylindrical configuration; b. a pair of cup-shaped boot members that fit over opposite ends of the rolled raft; c. a cover member that overlies the outer peripheral surface of the rolled raft and the boot members on the opposite ends thereof; d. a pair of studs which are secured to the outer peripheral surface of the cover member adjacent one side edge thereof; e. a pair of grommets adjacent the other side edge of the cover member through which the studs pass when the cover member is wrapped about the rolled raft; f. a tab connected to each boot member having a grommet through which the adjacent stud on the cover member also passes; g. a ripcord pin which passes through an aperture adjacent the outer end of each stud and normally maintains the grommets in the cover and boot members fixed on the studs; h. and a D-ring which is centrally positioned between the aviator''s seat cushion and his parachute pack and which is connected to each of the ripcord pins.
3. The apparatus substantially as described in claim 2 wherein a bowed spring strap is secured to one side edge of the cover member.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US81107069A | 1969-03-27 | 1969-03-27 |
Publications (1)
Publication Number | Publication Date |
---|---|
US3602463A true US3602463A (en) | 1971-08-31 |
Family
ID=25205467
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US811070A Expired - Lifetime US3602463A (en) | 1969-03-27 | 1969-03-27 | Fail-safe raft system |
Country Status (1)
Country | Link |
---|---|
US (1) | US3602463A (en) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4775119A (en) * | 1987-03-30 | 1988-10-04 | Grumman Aerospace Corporation | Aircraft crew multipurpose, unitary backpack for bailout and survival |
US4793575A (en) * | 1987-05-01 | 1988-12-27 | Butler Manley C | Emergency parachute pack |
US5072727A (en) * | 1988-06-06 | 1991-12-17 | Grumman Aerospace Corporation | Multi-purpose jerkin |
FR3072547A1 (en) * | 2017-10-25 | 2019-04-26 | Asap France Sarl | CONTAINER HARNESS BAG FOR THE PACKAGING, TRANSPORT AND USE OF INFLATABLE RAFT AERONAUTICAL PLATFORM |
US11014641B1 (en) | 2019-11-11 | 2021-05-25 | Aerial Machine & Tool Corporation | Wearable flotation device |
-
1969
- 1969-03-27 US US811070A patent/US3602463A/en not_active Expired - Lifetime
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4775119A (en) * | 1987-03-30 | 1988-10-04 | Grumman Aerospace Corporation | Aircraft crew multipurpose, unitary backpack for bailout and survival |
US4793575A (en) * | 1987-05-01 | 1988-12-27 | Butler Manley C | Emergency parachute pack |
US5072727A (en) * | 1988-06-06 | 1991-12-17 | Grumman Aerospace Corporation | Multi-purpose jerkin |
FR3072547A1 (en) * | 2017-10-25 | 2019-04-26 | Asap France Sarl | CONTAINER HARNESS BAG FOR THE PACKAGING, TRANSPORT AND USE OF INFLATABLE RAFT AERONAUTICAL PLATFORM |
US11014641B1 (en) | 2019-11-11 | 2021-05-25 | Aerial Machine & Tool Corporation | Wearable flotation device |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US4508294A (en) | Air bag restraint system | |
US3768761A (en) | Inflatable life raft | |
US4488691A (en) | Torso restraint system | |
US3508727A (en) | Apparatus for saving of the passengers of a crash landing,ditching or diving and in danger to be diving,respectively,airplane | |
US4187570A (en) | Ship escape and survival system | |
US3973645A (en) | Inflatable evacuation slide | |
US4793575A (en) | Emergency parachute pack | |
CN107344624B (en) | System and method for retaining removable panels when deploying an evacuation system | |
US3179360A (en) | Inflatable personnel restraint system for advanced flight vehicles | |
US4667902A (en) | Passive arm retention curtain | |
US5253826A (en) | Lightweight sealed parachute and harness assembly | |
US3083938A (en) | Ejection seat and personnel separation device | |
US3602463A (en) | Fail-safe raft system | |
US5072727A (en) | Multi-purpose jerkin | |
US2836382A (en) | Leg restraining means for ejection seats for aircraft | |
US2605065A (en) | Net-suit, or combined g-suit, parachute, safety and crash harness | |
EP1575829B1 (en) | Skyhook reserve parachute deployment system | |
US3908937A (en) | Parachute pack | |
US3258230A (en) | High speed delivery container | |
US5979829A (en) | In-flight evacuation system | |
US3672609A (en) | Inflatable body-attachments for marine life-saving | |
US6296204B1 (en) | Restraint system for a flight helmet | |
US3248746A (en) | Life jacket, especially for flying personnel | |
US6629671B1 (en) | Airline seat parachute | |
US3188027A (en) | Parachute deployment bag |