WO2003095932A1 - Lightweight gas generator device - Google Patents
Lightweight gas generator device Download PDFInfo
- Publication number
- WO2003095932A1 WO2003095932A1 PCT/ZA2003/000063 ZA0300063W WO03095932A1 WO 2003095932 A1 WO2003095932 A1 WO 2003095932A1 ZA 0300063 W ZA0300063 W ZA 0300063W WO 03095932 A1 WO03095932 A1 WO 03095932A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- gas
- gear
- charge
- safety enhancing
- once
- Prior art date
Links
- 239000007789 gas Substances 0.000 claims abstract description 84
- 238000002485 combustion reaction Methods 0.000 claims abstract description 25
- 239000000567 combustion gas Substances 0.000 claims abstract description 16
- 230000002708 enhancing effect Effects 0.000 claims description 33
- 238000001816 cooling Methods 0.000 claims description 7
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 claims description 6
- CURLTUGMZLYLDI-UHFFFAOYSA-N Carbon dioxide Chemical compound O=C=O CURLTUGMZLYLDI-UHFFFAOYSA-N 0.000 claims description 6
- 239000000203 mixture Substances 0.000 claims description 6
- 230000001681 protective effect Effects 0.000 claims description 6
- 231100000252 nontoxic Toxicity 0.000 claims description 4
- 230000003000 nontoxic effect Effects 0.000 claims description 4
- UGFAIRIUMAVXCW-UHFFFAOYSA-N Carbon monoxide Chemical compound [O+]#[C-] UGFAIRIUMAVXCW-UHFFFAOYSA-N 0.000 claims description 3
- 239000000020 Nitrocellulose Substances 0.000 claims description 3
- SNIOPGDIGTZGOP-UHFFFAOYSA-N Nitroglycerin Chemical compound [O-][N+](=O)OCC(O[N+]([O-])=O)CO[N+]([O-])=O SNIOPGDIGTZGOP-UHFFFAOYSA-N 0.000 claims description 3
- 229910002092 carbon dioxide Inorganic materials 0.000 claims description 3
- 239000001569 carbon dioxide Substances 0.000 claims description 3
- 229910002091 carbon monoxide Inorganic materials 0.000 claims description 3
- 239000002131 composite material Substances 0.000 claims description 3
- 230000000994 depressogenic effect Effects 0.000 claims description 3
- 230000000694 effects Effects 0.000 claims description 3
- 229960003711 glyceryl trinitrate Drugs 0.000 claims description 3
- VUZPPFZMUPKLLV-UHFFFAOYSA-N methane;hydrate Chemical compound C.O VUZPPFZMUPKLLV-UHFFFAOYSA-N 0.000 claims description 3
- 229920001220 nitrocellulos Polymers 0.000 claims description 3
- 229910052757 nitrogen Inorganic materials 0.000 claims description 3
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims description 3
- 229910001868 water Inorganic materials 0.000 claims description 3
- 230000006378 damage Effects 0.000 claims description 2
- 230000015572 biosynthetic process Effects 0.000 claims 2
- 239000000463 material Substances 0.000 claims 2
- 239000000126 substance Substances 0.000 claims 2
- 230000001960 triggered effect Effects 0.000 claims 2
- 230000001737 promoting effect Effects 0.000 claims 1
- 208000027418 Wounds and injury Diseases 0.000 description 2
- 239000003795 chemical substances by application Substances 0.000 description 2
- 208000014674 injury Diseases 0.000 description 2
- 230000001105 regulatory effect Effects 0.000 description 2
- 206010003497 Asphyxia Diseases 0.000 description 1
- 230000003213 activating effect Effects 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 239000004020 conductor Substances 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000000881 depressing effect Effects 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 239000002923 metal particle Substances 0.000 description 1
- 230000035484 reaction time Effects 0.000 description 1
- 238000000926 separation method Methods 0.000 description 1
- 230000001502 supplementing effect Effects 0.000 description 1
- 238000011144 upstream manufacturing Methods 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B3/00—Blasting cartridges, i.e. case and explosive
- F42B3/04—Blasting cartridges, i.e. case and explosive for producing gas under pressure
Definitions
- the invention relates to a lightweight gas generator device utilisable for inflating inflatable equipment dealing with bodily safety amongst other applicable in situations where equipment weight is particularly relevant.
- the invention relates to safety enhancing gear dealing with bodily safety associated with bodily- suspended non-motorised aerial travel, as fitted with the gas generator device.
- the invention finds particular use for serving a safety enhancing function in the field parachuting and paragliding.
- Figure 1 shows a schematic perspective view of a gas generator device in accordance with a first aspect the invention, as fitted to safety enhancing gear, in accordance with a second aspect of the invention
- Figure 2 shows the gas generator device in schematic sectioned side elevation
- Figure 3 shows in schematic side view one embodiment the safety enhancing gear according to the second aspect of the invention, in the form of an airbag layout, in partially deployed state,
- Figure 4 shows a schematic side view of the airbag layout as fully deployed
- Figure 5 shows a schematic frontal view of the airbag layout as deployed according to figure 3
- Figure 6 shows a schematic rear view of the deployed airbag layout
- Figure 7 shows in diagrammatic spread out plan view another embodiment of the safety enhancing gear in the form of a canopy deployment booster used for boosting the deployment or redeployment of the canopy of aerial travel equipment in the form of a parachute, :
- Figure 8 shows in diagrammatic side elevation the booster of figure 7 as operatively filled with combustion gas and fitted to a parachute as deployed during descent,
- Figure 9 shows in detail the central part of the booster as carrying the gas generator
- Figure 10 shows in diagrammatic spread out plan view another embodiment of the canopy deployment booste used for boosting the deployment- or redeployment of the canopy of a paraglider
- Figure 11 shows in diagrammatic side elevation the booster of figure 10 as operatively filled with combustion gas and fitted to a paraglider thus supplementing its lift during flight. (6) DETAILED DESCRIPTION OF THE DRAWINGS
- a gas generator device in accordance with the first aspect of the invention is generally indicated by the reference numeral 10.
- the gas generator device 10 comprises a cartridge generally indicated by reference numeral 12, containing a pyrotechnic charge 14 and igniting means for remotely igniting the pyrotechnic charge.
- the cartridge 12 is in the form of a cylindrical metal tube 16 formed at opposite ends with combustion gas settling chambers 18.
- the chambers 18 are in gas flow communication with an axially formed combustion chamber 20 formed within the charge 14, as annularly lining the casing 22 of the tube 16, via gas outlet nozzles extending along ports 24 divergingly opening up in the chambers 18.
- the inner walls of the chambers 18 are formed by end plates 26 that naturally also close off the combustion chamber 20 and the charge 14 from the settling chambers 18 otherwise that via the nozzles 24, as thus formed through the plates 26.
- the outer walls of the chambers 18 are formed by bulkheads 28 sealably fitting onto the casing 22.
- the charge 14 is blanked off from the casing 22 via an annular protecting shell 30.
- Escaping of gas generated by the combustion reaction for inflating inflatable equipment takes place via a plurality of discharge outlets in the form of circumferentially arranged passages 32 formed through end flanges 34 forming part of the casing 22.
- the flanges 34 are of adequate length in the axial direction of the device 10 to cause the passages 32 to extend capillary fashion.
- the passages 32 are suitably situated relative to one another to limit the possibility of the creation of any resultant thrust on the device 10 once in use by being arranged in pairs thus facing one another alongside the side of the tube 16.
- the pyrotechnic charge 14 is in the form of a nitrocellulose/nitroglycerine mixture or composite based pyrotechnic charge that is relatively non-toxic and cool burning and that produces gases consisting mainly of nitrogen and a mixture of carbon dioxide, carbon monoxide and water.
- the theoretical combustion temperature of the pyrotechnic charge is in the order of 1200K with a conventional burn time of between 1 and 3 seconds.
- the igniting means is conveniently of an electrical type and includes two igniter switches 36 that are connected to an electrical power source such as a battery (not shown) and to the pyrotechnic charge 1 via electrical conductors 38. As a safety precaution both switches 36 must thus be activated simultaneously to ignite the pyrotechnic charge 14.
- the object of the diverging shape of the nozzles extending along the ports 24 is mainly to attain and maintain the correct combustion pressure in the combustion chamber 20. Control of this pressure controls the combustion rate of the pyrotechnic charge and ensures combustion stability.
- Expanded combustion gases thus pass to the settling chambers 18 via the ports 24.
- Thermodynamic expansion along the ports 24 results in a primary cooling of the combustion gases en route to the chambers 18.
- Further convection and conduction cooling of expanded gases takes place in the settling chambers 18 resulting in a substantially cooled product entering the discharge passages 32.
- a final cooling of combustion gases takes place along the passages 32 owing to their relative length that is supplemented by the secondary expansion of the gases on being discharged to the equipment desired to be inflated.
- an annular conventional heat sink such as in the form of sintered metal particles can be located in each of the settling chambers 18 over the divergent nozzles of the ports 24.
- safety enhancing gear comprises an inflatable arrangement in the form of an airbag layout generally indicated by reference numeral 40.
- the layout 40 comprises a plurality of airbag fitted with a gas generator device 10 (of which the exact position is not shown in these drawings) for enabling the rapid inflation of the airbags, that are secured to body suspending non-motorised aerial travel equipment such as a paraglider, via risers lines 41.
- the layout 40 incorporates a harness (not shown) by means of which it is attached to a user's body and for also tying it to the lines of the glider.
- the layout 40 incorporates semi-rigid rear protection means in the form of a semi rigid seat 42 on which the wearer is seatable and to which the harness is secured, a back and side protective airbag 44 that extends around the back and sides of a person wearing the airbag layout 40, a frontal trunk impact protection airbag 46 and head impact protecting airbag 48 as attached to the airbag 46.
- the impact protection airbag 46 is preferably independently inflatable of the back and side protective airbag 44. When inflated it is disposed in front of a wearer's trunk for protection against frontal impact.
- the airbag 48 protects the neck and head region of a wearer once deployed and is operable to deploy in response to partial depressing of the frontal trunk impact protection airbag 46.
- the head impact protection airbag 48 is formed with an opening 50 to permit airflow over a wearer's face thus preventing suffocation once deployed.
- the back and side protective airbag 44 is secured to the wearer's body by means of the harness (not shown).
- the riser lines 41 are also secured to the harness to tie the layout 40 to the paraglider.
- the back and side protective airbag 44 and the frontal trunk impact protection airbag 46 comprise the main airbags while the head impact protection airbag 48 is inflated, in use, with combustion gases from the frontal trunk impact protection airbag 46 when the latter is depressed partially due to impact.
- a pressure-regulating device (not shown) is conveniently provided for regulating the flow of combustion gases from the frontal trunk impact protection airbag 46 to the head impact protection airbag 48.
- the rate of inflation or deflation of the airbags of the layout 40 is conveniently controllable by means of valves (not shown).
- the separate airbags of the layout 40 are attached to each other in a way that resists separation of the airbags from one another upon impact, once in use.
- the airbags of the airbag layout 40 are configured so that their deployment would automatically force the wearer of the layout 40 into an appropriate injury-restricting parachute landing fall (abbreviated as "PLF") position.
- PLF injury-restricting parachute landing fall
- the airbag layout 40 can be either manually or automatically activatable. In the latter case it is in response to a predetermined increased tension being applied to the bridles of the reserve parachute (which is a standard component of paragliders) when its deployment occurs.
- the airbag layout 40 provides effective protection against impact injuries caused by bad landings in paragliding. It also provides a simple, aerodynamic, lightweight non-restrictive fully circumferential impact regulating arrangement, which allows the pilot of a paraglider to maintain maximum control while forcing such person into a PLF position immediately prior to impact.
- the safety enhancing equipment is in the form of a canopy deployment booster generally indicated by reference numeral 60 for boosting the deployment or redeployment of the canopy of aerial travel equipment in the form of a parachute, paraglider or the like once used in conjunction therewith.
- the booster 60 incorporates a flexible non-porous gas distributor 62 that is in gas flow fashion connected to a flexible and inflatable gas tube layout 64 formed with a plurality of gas flow tubes 66 extending in gas flow fashion from the distributor 62.
- the distributor 62 of the booster 60 is fitted with a gas generator device 10 for inflation of the booster 60.
- the booster 60 can either be maintained in inflated form once inflated or can be permitted to slowly deflate. When permitted to deflate it can either be fitted with a manually controllable valve layout (not shown) or it can be allowed to automatically deflate at a rate slower that its charging rate via the device 10 by having the tubes 66 suitably perforated (not shown).
- the distributor 62 when the booster 60 is intended for use with a parachute 68, is centrally situated with the gas flow tubes 66 radiating therefrom.
- the layout 64 also incorporates a circumferentially extending gas tube 70 into which the tubes 66 open up. This arrangement promotes the attainment and maintenance of a uniform pressure throughout the booster 60 once the device 10 is activated. It also ensures that the booster 60 maintains a generally fixed configuration once inflated.
- the dimensions of the booster 60 are naturally selected to cause the gas tube 70 to lie along the brim of a parachute 68, as shown in figure 8, once the booster 60 is inflated.
- the booster 60 can incorporate two booster triggering pull cords of which the one is attached to the centre point of a canopy once the gear is fitted to a parachute and the other to the point at which such parachute is attached to a body being parachuted for activating the device 10.
- the gas tubes 66 of the layout 64 extend finger fashion relative to the distributor 62 while including upstream cross tubes 74 extending laterally from the distributor 62.
- the tubes 74 extend along the leading edge of the paraglider 72 with the other gas tubes 66 extending rearward along the paraglider 72.
Abstract
Description
Claims
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
AU2003230425A AU2003230425A1 (en) | 2002-05-13 | 2003-05-13 | Lightweight gas generator device |
ZA200401171A ZA200401171B (en) | 2003-05-13 | 2004-02-13 | Lightweight gas generating device. |
Applications Claiming Priority (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
ZA200203791 | 2002-05-13 | ||
ZA2002/3791 | 2002-05-13 | ||
ZA200206324 | 2002-08-08 | ||
ZA2002/6324 | 2002-08-08 |
Publications (1)
Publication Number | Publication Date |
---|---|
WO2003095932A1 true WO2003095932A1 (en) | 2003-11-20 |
Family
ID=29423881
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/ZA2003/000063 WO2003095932A1 (en) | 2002-05-13 | 2003-05-13 | Lightweight gas generator device |
Country Status (2)
Country | Link |
---|---|
AU (1) | AU2003230425A1 (en) |
WO (1) | WO2003095932A1 (en) |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3787010A (en) * | 1973-04-06 | 1974-01-22 | Us Army | Inflating apparatus |
US3921944A (en) * | 1972-03-13 | 1975-11-25 | Mcnamara Jr John J | Inflatable safety pack |
US4137847A (en) * | 1977-10-27 | 1979-02-06 | General Motors Corporation | Gas generator |
DE19528864A1 (en) * | 1995-08-05 | 1997-02-06 | Temic Bayern Chem Airbag Gmbh | Gas generator for air bag for protecting motor vehicle occupants - has sprung steel liner inside combustion chamber which holds tablets of propellant charge steady when vehicle is in normal motion |
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 |
-
2003
- 2003-05-13 AU AU2003230425A patent/AU2003230425A1/en not_active Abandoned
- 2003-05-13 WO PCT/ZA2003/000063 patent/WO2003095932A1/en not_active Application Discontinuation
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3921944A (en) * | 1972-03-13 | 1975-11-25 | Mcnamara Jr John J | Inflatable safety pack |
US3787010A (en) * | 1973-04-06 | 1974-01-22 | Us Army | Inflating apparatus |
US4137847A (en) * | 1977-10-27 | 1979-02-06 | General Motors Corporation | Gas generator |
DE19528864A1 (en) * | 1995-08-05 | 1997-02-06 | Temic Bayern Chem Airbag Gmbh | Gas generator for air bag for protecting motor vehicle occupants - has sprung steel liner inside combustion chamber which holds tablets of propellant charge steady when vehicle is in normal motion |
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 |
Also Published As
Publication number | Publication date |
---|---|
AU2003230425A1 (en) | 2003-11-11 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US6607166B1 (en) | Inflatable flying body for the rescue descent of a person | |
US11286051B2 (en) | Aerial vehicle safety apparatus and aerial vehicle | |
US10421552B2 (en) | Apparatus and method for rapid deployment of a parachute | |
US6315245B1 (en) | Ejection seat with blast protection system | |
US7703152B2 (en) | Head and neck restraint system | |
JP2554392B2 (en) | Shock absorber | |
US3921944A (en) | Inflatable safety pack | |
JP4373611B2 (en) | Two stage inflator | |
US6705572B1 (en) | Emergency low altitude parachute wherein canopy is deployed and inflated prior to use | |
US3532358A (en) | Inflatable device | |
CN208021761U (en) | A kind of unmanned plane parachute | |
JP2003528766A (en) | Compact dual nozzle airbag inflator | |
CN110116823B (en) | Recoverable and reusable solid carrier rocket sublevel | |
JPH0885410A (en) | Small-sized inflating device assembly | |
US6422512B1 (en) | Inflatable restraint systems for ejection seats | |
US6857136B1 (en) | Inflatable head and neck support collar | |
US3372893A (en) | Air to ground descent means | |
CN110290983A (en) | Dual air bags system for taking safety measures to biggish occupant's distance | |
US6308917B1 (en) | Ejection seat | |
US3478687A (en) | Very low descent rate,high intensity,illuminating flare | |
KR100751288B1 (en) | Lifesaving parachute for taking refuge with slow descent | |
WO2003095932A1 (en) | Lightweight gas generator device | |
ZA200401171B (en) | Lightweight gas generating device. | |
US6296204B1 (en) | Restraint system for a flight helmet | |
JPH09240595A (en) | Air bag device |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
AK | Designated states |
Kind code of ref document: A1 Designated state(s): AE AG AL AM AT AU AZ BA BB BG BR BY BZ CA CH CN CO CR CU CZ DE DK DM DZ EC EE ES FI GB GD GE GH GM HR HU ID IL IN IS JP KE KG KP KR KZ LC LK LR LS LT LU LV MA MD MG MK MN MW MX MZ NI NO NZ OM PH PL PT RO RU SC SD SE SG SK SL TJ TM TN TR TT TZ UA UG US UZ VC VN YU ZA ZM ZW |
|
AL | Designated countries for regional patents |
Kind code of ref document: A1 Designated state(s): GH GM KE LS MW MZ SD SL SZ TZ UG ZM ZW AM AZ BY KG KZ MD RU TJ TM AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IT LU MC NL PT RO SE SI SK TR BF BJ CF CG CI CM GA GN GQ GW ML MR NE SN TD TG |
|
121 | Ep: the epo has been informed by wipo that ep was designated in this application | ||
WWE | Wipo information: entry into national phase |
Ref document number: 2004/01171 Country of ref document: ZA Ref document number: 200401171 Country of ref document: ZA |
|
122 | Ep: pct application non-entry in european phase | ||
NENP | Non-entry into the national phase |
Ref country code: JP |
|
WWW | Wipo information: withdrawn in national office |
Country of ref document: JP |