GB1316815A - - Google Patents

Info

Publication number
GB1316815A
GB1316815A GB1316815DA GB1316815A GB 1316815 A GB1316815 A GB 1316815A GB 1316815D A GB1316815D A GB 1316815DA GB 1316815 A GB1316815 A GB 1316815A
Authority
GB
United Kingdom
Prior art keywords
inflatable
walkway
wing
aircraft
separate
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
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 filed Critical
Publication of GB1316815A publication Critical patent/GB1316815A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D25/00—Emergency apparatus or devices, not otherwise provided for
    • B64D25/08—Ejecting or escaping means
    • B64D25/14—Inflatable escape chutes

Abstract

1316815 Inflatable emergency escape shoot GARRETT CORP 26 May 1970 25204/70 Heading B7J An inflatable escape shoot, suitable for use with aircraft, comprises an inflatable mattress like structure 10 having a substantially horizontal walkway portion 22 supportable at 12 on the wing of an aircraft, and an integral slide portion 24 extending downwardly to ground level. The portions 22 and 24 which are constructed of air impervious fabric each have strips of fabric within them tying the top wall of the section to the bottom wall, thus preventing "ballooning" when in use. Inflatable handrails 46, 50, 56, 58, 60 and 62 are provided which are erected on inflation of the structure 10. A separate, similarly constructed portion 34 is provided on the wing 14. In an alternative embodiment Fig. 5, the walkway and slide sections are separate, and the walkway section is provided with a support 108.
GB1316815D 1970-05-26 1970-05-26 Expired GB1316815A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2520470 1970-05-26

Publications (1)

Publication Number Publication Date
GB1316815A true GB1316815A (en) 1973-05-16

Family

ID=10223925

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1316815D Expired GB1316815A (en) 1970-05-26 1970-05-26

Country Status (1)

Country Link
GB (1) GB1316815A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4846422A (en) * 1984-05-14 1989-07-11 The Bfgoodrich Company Single piece evacuation system for aircraft or the like
EP3118118A1 (en) * 2015-07-17 2017-01-18 Goodrich Corporation Off wing evacuation system control strap

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4846422A (en) * 1984-05-14 1989-07-11 The Bfgoodrich Company Single piece evacuation system for aircraft or the like
EP3118118A1 (en) * 2015-07-17 2017-01-18 Goodrich Corporation Off wing evacuation system control strap
CN106347678A (en) * 2015-07-17 2017-01-25 古德里奇公司 Off wing evacuation system control strap
US9725181B2 (en) 2015-07-17 2017-08-08 Goodrich Corporation Off wing evacuation system control strap
CN106347678B (en) * 2015-07-17 2020-10-30 古德里奇公司 Control belt of off-wing evacuation system

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Legal Events

Date Code Title Description
414F Notice of opposition given (sect. 14/1949)
414E Application relinquished (sect. 14/1949)
CSNS Application of which complete specification have been accepted and published, but patent is not sealed