EP0085686A4 - Fourniture de provisions par un ralentisseur. - Google Patents
Fourniture de provisions par un ralentisseur.Info
- Publication number
- EP0085686A4 EP0085686A4 EP19820902341 EP82902341A EP0085686A4 EP 0085686 A4 EP0085686 A4 EP 0085686A4 EP 19820902341 EP19820902341 EP 19820902341 EP 82902341 A EP82902341 A EP 82902341A EP 0085686 A4 EP0085686 A4 EP 0085686A4
- Authority
- EP
- European Patent Office
- Prior art keywords
- store
- container
- retarder
- mouth
- canopy
- 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.)
- Ceased
Links
- 238000000034 method Methods 0.000 claims abstract description 6
- 238000012856 packing Methods 0.000 claims description 2
- 230000000717 retained effect Effects 0.000 claims 1
- 239000000463 material Substances 0.000 description 3
- 238000010276 construction Methods 0.000 description 2
- 210000000245 forearm Anatomy 0.000 description 2
- 230000003068 static effect Effects 0.000 description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 2
- 230000000694 effects Effects 0.000 description 1
- 230000000977 initiatory effect Effects 0.000 description 1
- 238000004806 packaging method and process Methods 0.000 description 1
- 210000000707 wrist Anatomy 0.000 description 1
Classifications
-
- 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
- B64D17/00—Parachutes
- B64D17/40—Packs
-
- 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
- B64D1/00—Dropping, ejecting, releasing, or receiving articles, liquids, or the like, in flight
- B64D1/02—Dropping, ejecting, or releasing articles
- B64D1/08—Dropping, ejecting, or releasing articles the articles being load-carrying devices
-
- 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
- B64D17/00—Parachutes
- B64D17/40—Packs
- B64D17/52—Opening, e.g. manual
Definitions
- This invention relates to store delivery by retarder and in particular it relates to a store of the type which is launched from a height to the ground by means of a parachute which is deployed as the store is launched, the store being of the type which can best be hand launched such as a water container or other relatively fragile member.
- the invention can be used wherever there is a need to drop a store from an aircraft or helicopter or other airborne unit with the provision of a retarder to ensure that the landing velocity of the store is within proper limits.
- the present invention has as its object the provision of a system which can be readily launched and this is achieved by using a parachute,- preferably of a cruciform shape, which is packed into a container, which container can be formed of flexible material of tubular form closed at one end and having at the closed end a loop which can engage around the arm of a person launching the device or fixed to a suitable adjacent point, the retarder being packed inside of the container with the apex tied to the closed end of the container by means of a fracturable member.
- a loop on the shroud lines, which are also packed within the container, is tied to the mouth of the container by a mouth tie cord so arranged that normally the cord holds the container closed to retain its content, and to hold it to the store, but when the store is to be launched, the person launching it places the loop around his forearm or attaches it to a suitable reaction point and grips, not the container, but the store, such as a water bottle, and simply throws the store in the required direction, this having the effect of firstly breaking the cord tie allowing the shroud lines to be pulled out of the container until the parachute or retarder is itself pulled out of the container, and when fully extended the tie at the closed end of the container fractures and the store and retarder are launched, leaving the container attached to the thrower so that the maximum load can be carried by the retarder, and the store and parachute are clear of extraneous matter.
- An advantage of the device, the subject of this invention is effective packaging of the retarder in the container which results, and the novel method of launching it by attaching the container to the forearm of the person effecting the launching or other reaction support and simply throwing the store, this initiating the opening of the container and the release of the retarder and store in a correct sequence without any subsequent involvement with the container.
- the cruciform parachute which it is preferred to use consists of a cruciform piece of material to which the shroud lines are sewn in two directions across the cruciform shape to form the retarder, the shroud lines being looped at the end, the shroud lines thus being continuous across, and extending from, the parachute to the loop on the store to provide an effective construction.
- the method consists in packing a retarder com ⁇ prising a canopy and shroud lines into a container having at one end an external attachment member to be engaged on the thrower and an internal tie member and having at its other end an openable mouth, attaching the centre of the said canopy to the said internal tie member, joining the said shroud lines to the store with the store positioned outside of the said container, closing the said mouth of the said container over the said shroud lines by tie means also connected to the said store, and delivering the said store by attaching the said external attachment member of the said container to the thrower and grasping in the hand of the thrower the said store and throwing it in the direction of the required launch, whereby the said tie means at the mouth of the said container are severed by store inertia and the said shroud lines and canopy are sequentially drawn out of the container and the canopy pull severs the said internal tie means whereby to launch the said store and retarder but retain the said container on the said thrower.
- FIGS. 1, 2 and 3 show somewhat diagrammatically a launching action, showing the container in section
- FIG. 4 is an enlarged fragmentary view of the junction of the retarder and store and the mouth of the container
- FIG. 5 is a plan view of the preferred form of retarder.
- the container 1 which is of a suitable pliable material is of cylindrical shape with the one end 2 closed but open at the other end 3, which end forms the mouth 4 of the container 1.
- a tie member 5 which is attached both to the container and to the centre of the canopy 6 of the parachute, and the canopy 6 is packed into the container 1 with the shroud lines 7 towards the mouth 4 of the container 1, the shroud lines 7 being attached to a loop 8 on the store 9 itself.
- the store 9 is held to the container 1 by mouth tie means 10 extending from the mouth 4 of the container 1 to the store 9 to hold the store 9 to the container 1 with the store 9 projecting from the end of the container 1, that is the mouth end.
- the closed end 2 of the container 1 has an external attachment member in the form of a hand loop .11 project- ing from the container 1.
- the loop 11 can simply be put around the wrist of the person launching the store, and the store is then grasped in the hand of the launcher with the container 1 positioned between the end of the store 9 and the hand loop 11.
- the first action is for the mouth tie means 10 which can be simple tie cords, to break allowing the mouth 4 of the container 1 to open, continued movement of the store 9 then pulling the parachute out of the container progressively as the shroud lines 7 are pulled out of the container by the store 9, and when the canopy 6 has been pulled outwardly to its full extent the tie member 5 between the centre of the canopy 6 and the container 1 breaks to allow the parachute to be pulled fully out of the container whereupon it deploys and the store is safely carried by means of the parachute retarder.
- the mouth tie means 10 which can be simple tie cords
- the above method allows a neat and effective retarder 6-7 to be formed with a container 1 simply projecting from the end of the store 9 in a position where the hand can readily be placed through the hand loop which forms the external attachment member 11 of the container 1 and the store 9 grasped to throw the store, this action separating the store 9 and retarder 6-7 from the container 1 which remains connected to the arm of the thrower by the hand loop.
- the external attachment member 11 can be other than a loop, such as tie cords which can be engaged on the arm or other convenient part of the thrower.
- the retarder comprises the canopy 6 and the shroud lines 7 as shown particularly in FIG. 6.
- the shroud lines 7 are continuous and are sewn to the edges of the canopy and are looped at the ends 12 to pass around the loop 8 on the store 9, the loop 8 itself being a tie, or the ends 12 of the shrouds can be clipped or otherwise attached to the loop 8.
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Packaging Of Annular Or Rod-Shaped Articles, Wearing Apparel, Cassettes, Or The Like (AREA)
- Toys (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
AUPF031081 | 1981-08-18 | ||
AU310/81 | 1981-08-18 |
Publications (2)
Publication Number | Publication Date |
---|---|
EP0085686A1 EP0085686A1 (fr) | 1983-08-17 |
EP0085686A4 true EP0085686A4 (fr) | 1984-04-04 |
Family
ID=3769171
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP19820902341 Ceased EP0085686A4 (fr) | 1981-08-18 | 1982-08-05 | Fourniture de provisions par un ralentisseur. |
Country Status (2)
Country | Link |
---|---|
EP (1) | EP0085686A4 (fr) |
WO (1) | WO1983000671A1 (fr) |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2532482A (en) * | 2014-11-20 | 2016-05-25 | Michael Cook George | Packaging for a parachute |
JP6629791B2 (ja) * | 2017-05-26 | 2020-01-15 | ソフトバンク株式会社 | パラシュート装置及び飛行体 |
Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2315436A1 (fr) * | 1975-06-23 | 1977-01-21 | Aerazur Constr Aeronaut | Dispositif d'ouverture automatique de parachute |
FR2340244A1 (fr) * | 1976-02-09 | 1977-09-02 | Fabrications Aeronautique Et | Parachute perfectionne |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1369395A (en) * | 1919-09-08 | 1921-02-22 | E R Calthrop S Aerial Patents | Parachute |
US2508754A (en) * | 1945-08-17 | 1950-05-23 | Frieder | Parachute container of folded paper |
FR1183999A (fr) * | 1957-10-07 | 1959-07-16 | Aerazur Constr Aeronaut | Empaquetage de parachute |
US3001746A (en) * | 1958-07-15 | 1961-09-26 | Herschel D King | Triple purpose parachute vehicle |
-
1982
- 1982-08-05 WO PCT/AU1982/000124 patent/WO1983000671A1/fr not_active Application Discontinuation
- 1982-08-05 EP EP19820902341 patent/EP0085686A4/fr not_active Ceased
Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2315436A1 (fr) * | 1975-06-23 | 1977-01-21 | Aerazur Constr Aeronaut | Dispositif d'ouverture automatique de parachute |
FR2340244A1 (fr) * | 1976-02-09 | 1977-09-02 | Fabrications Aeronautique Et | Parachute perfectionne |
Non-Patent Citations (1)
Title |
---|
See also references of WO8300671A1 * |
Also Published As
Publication number | Publication date |
---|---|
WO1983000671A1 (fr) | 1983-03-03 |
EP0085686A1 (fr) | 1983-08-17 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US4337913A (en) | Means for releasably attaching strands | |
US4004764A (en) | Drogue chute extraction | |
US2702679A (en) | Means for the deployment of parachutes at high speeds | |
US3690604A (en) | Parachute stowage and deployment | |
US5388786A (en) | Escape apparatus | |
US3724817A (en) | Long line loiter technique | |
US10518888B2 (en) | Cinched parachute | |
EP0085686A4 (fr) | Fourniture de provisions par un ralentisseur. | |
US2505954A (en) | Pilot parachute | |
US2906125A (en) | Sampling device | |
US3064568A (en) | Stabilized line dispensing device | |
US5054398A (en) | Process and apparatus for dispersing submunition bodies | |
US2967677A (en) | Apparatus for launching balloons | |
US4970937A (en) | Anti-ice protection for projectiles | |
US2998950A (en) | Integrated parachute deployment pack | |
US1894954A (en) | Aerial flare | |
US2326813A (en) | Multiple launching of parachute borne equipment containers from aircraft | |
US2439318A (en) | Parachute pack | |
US2979294A (en) | Parachute combination and ejection device | |
US3351010A (en) | Air-dropped segmental line explosive charge | |
US3497168A (en) | Apparatus for coupling and decoupling a load | |
US2481507A (en) | Parachute target | |
US2957664A (en) | Fast-acting parachutes | |
US6651934B2 (en) | Rescue system for rescuing persons by air | |
US3018074A (en) | Parachute pack |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PUAI | Public reference made under article 153(3) epc to a published international application that has entered the european phase |
Free format text: ORIGINAL CODE: 0009012 |
|
17P | Request for examination filed |
Effective date: 19830420 |
|
AK | Designated contracting states |
Designated state(s): BE CH DE FR GB LI SE |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: THE APPLICATION HAS BEEN REFUSED |
|
18R | Application refused |
Effective date: 19861123 |
|
RIN1 | Information on inventor provided before grant (corrected) |
Inventor name: BAILEY, EDWIN HAROLD |