GB1376144A - Parachutes - Google Patents

Parachutes

Info

Publication number
GB1376144A
GB1376144A GB5442471A GB5442471A GB1376144A GB 1376144 A GB1376144 A GB 1376144A GB 5442471 A GB5442471 A GB 5442471A GB 5442471 A GB5442471 A GB 5442471A GB 1376144 A GB1376144 A GB 1376144A
Authority
GB
United Kingdom
Prior art keywords
socket
spring
plate
parachute
collar
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
Application number
GB5442471A
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Safran Aerosystems SAS
Original Assignee
Aerazur Constructions Aeronautiques SA
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Aerazur Constructions Aeronautiques SA filed Critical Aerazur Constructions Aeronautiques SA
Publication of GB1376144A publication Critical patent/GB1376144A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D17/00Parachutes
    • B64D17/40Packs
    • B64D17/52Opening, e.g. manual

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Tents Or Canopies (AREA)
  • Toys (AREA)

Abstract

1376144 Extractor device for parachute AERAZUR CONSTRUCTIONS AERONAUTIQUES 23 Nov 1971 [23 Nov 1970] 54424/71 Heading B7G [Also in Divisions E2 and F2] An extractor device for a parachute comprises a base-plate B carrying a central collar 7 and a first socket 1 carrying an annular plate C, the plates B and C being connected by a flexible tubular sheath 9 enclosing a compression spring 8 deployed between the plates, and a second socket 3 engaging in the first socket and retained therein by a member 5 and enclosing a compression spring 4. The spring 4 is stiffer than the spring 8 so that if support plate 6 carried by the second socket 3 is depressed the spring 8 is compressed first until the first socket 1 enters the collar 7; further depression causes the spring 4 to be compressed and the second socket to be pressed into the first socket, bevelled edge 17 forcing locking balls 2 carried by the first socket into an annular groove 10 in the collar 7. The plate 6 is then held down by clamps on the parachute pack. When they are released spring 4 urges the second socket 3 out of socket 1, releasing the locking balls 2 and allowing spring 8 to move the plate C, thus deploying an extractor parachute canopy V disposed thereon.
GB5442471A 1970-11-23 1971-11-23 Parachutes Expired GB1376144A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR7041978A FR2115017B1 (en) 1970-11-23 1970-11-23

Publications (1)

Publication Number Publication Date
GB1376144A true GB1376144A (en) 1974-12-04

Family

ID=9064554

Family Applications (1)

Application Number Title Priority Date Filing Date
GB5442471A Expired GB1376144A (en) 1970-11-23 1971-11-23 Parachutes

Country Status (3)

Country Link
DE (1) DE2157643C2 (en)
FR (1) FR2115017B1 (en)
GB (1) GB1376144A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN115384781A (en) * 2022-06-20 2022-11-25 中国空气动力研究与发展中心空天技术研究所 Reverse tail rotation device of aircraft and aircraft

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105480421A (en) * 2015-12-16 2016-04-13 湖北青铜汇航空科技有限公司 Sewing method for drogue parachute opening spring

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE661220C (en) * 1938-06-14 Fallschirmfabrikation Kohnke & Spring frame for the auxiliary parachute
GB735499A (en) * 1953-03-19 1955-08-24 Pioneer Parachute Co Pilot parachute
US2967685A (en) * 1957-12-19 1961-01-10 Gen Dynamics Corp Pilot chute ejection device

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN115384781A (en) * 2022-06-20 2022-11-25 中国空气动力研究与发展中心空天技术研究所 Reverse tail rotation device of aircraft and aircraft
CN115384781B (en) * 2022-06-20 2024-04-16 中国空气动力研究与发展中心空天技术研究所 Anti-tail-spin device of aircraft and aircraft

Also Published As

Publication number Publication date
DE2157643C2 (en) 1983-07-14
FR2115017A1 (en) 1972-07-07
DE2157643A1 (en) 1972-06-29
FR2115017B1 (en) 1973-12-07

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Legal Events

Date Code Title Description
PS Patent sealed
PE20 Patent expired after termination of 20 years