GB1383513A

GB1383513A – Aircrew escape systems
– Google Patents

GB1383513A – Aircrew escape systems
– Google Patents
Aircrew escape systems

Info

Publication number
GB1383513A

GB1383513A
GB1998471A
GB1998471A
GB1383513A
GB 1383513 A
GB1383513 A
GB 1383513A
GB 1998471 A
GB1998471 A
GB 1998471A
GB 1998471 A
GB1998471 A
GB 1998471A
GB 1383513 A
GB1383513 A
GB 1383513A
Authority
GB
United Kingdom
Prior art keywords
canopy
cord
june
transparency
aircraft cockpit
Prior art date
1971-06-10
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
GB1998471A
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.)

Hawker Siddeley Aviation Ltd

Original Assignee
Hawker Siddeley Aviation Ltd
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.)
1971-06-10
Filing date
1971-06-10
Publication date
1974-02-12

1971-06-10
Application filed by Hawker Siddeley Aviation Ltd
filed
Critical
Hawker Siddeley Aviation Ltd

1971-06-10
Priority to GB1998471A
priority
Critical
patent/GB1383513A/en

1972-06-08
Priority to DE2228481A
priority
patent/DE2228481C3/en

1972-06-09
Priority to FR7220779A
priority
patent/FR2140605B1/fr

1972-06-12
Priority to US00262034A
priority
patent/US3806069A/en

1973-11-08
Priority to US413827A
priority
patent/US3902945A/en

1974-02-12
Publication of GB1383513A
publication
Critical
patent/GB1383513A/en

Status
Expired
legal-status
Critical
Current

Links

Espacenet

Global Dossier

Discuss

Classifications

B—PERFORMING OPERATIONS; TRANSPORTING

B64—AIRCRAFT; AVIATION; COSMONAUTICS

B64C—AEROPLANES; HELICOPTERS

B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like

B64C1/32—Severable or jettisonable parts of fuselage facilitating emergency escape

Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS

Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC

Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION

Y10T156/00—Adhesive bonding and miscellaneous chemical manufacture

Y10T156/10—Methods of surface bonding and/or assembly therefor

Y10T156/1002—Methods of surface bonding and/or assembly therefor with permanent bending or reshaping or surface deformation of self sustaining lamina

Abstract

1383513 Aircraft cockpit canopy HAWKER SIDDELEY AVIATION Ltd 8 June 1972 [10 June 1971] 19984/71 Heading B7G An aircraft cockpit transparency is provided with detonating cords to shatter it prior to an aircrew ejection, there being one cord (not shown) around the the periphery of the canopy and another 12 on the top of the canopy in the area through which the crew member has to pass when ejected. The cord 12 is symmetrically disposed about the canopy centre line 7a and is formed with a plurality of sharp loops 18 which serve, when the cord is detonated to inititate cracks in selected areas of the canopy. The cord is secured to the canopy transparency by adhesive, the canopy being abraded over the profile of the cord to ensure a good bond. Apparatus and a method of use are described for preforming the detonating cord and applying it to the canopy in its correct position prior to bonding.

GB1998471A
1971-06-10
1971-06-10
Aircrew escape systems

Expired

GB1383513A
(en)

Priority Applications (5)

Application Number
Priority Date
Filing Date
Title

GB1998471A

GB1383513A
(en)

1971-06-10
1971-06-10
Aircrew escape systems

DE2228481A

DE2228481C3
(en)

1971-06-10
1972-06-08

Canopy for the cockpit of aircraft

FR7220779A

FR2140605B1
(en)

1971-06-10
1972-06-09

US00262034A

US3806069A
(en)

1971-06-10
1972-06-12
Aircrew escape systems

US413827A

US3902945A
(en)

1971-06-10
1973-11-08
Method of making an aircrew escape systems

Applications Claiming Priority (1)

Application Number
Priority Date
Filing Date
Title

GB1998471A

GB1383513A
(en)

1971-06-10
1971-06-10
Aircrew escape systems

Publications (1)

Publication Number
Publication Date

GB1383513A
true

GB1383513A
(en)

1974-02-12

Family
ID=10138401
Family Applications (1)

Application Number
Title
Priority Date
Filing Date

GB1998471A
Expired

GB1383513A
(en)

1971-06-10
1971-06-10
Aircrew escape systems

Country Status (4)

Country
Link

US
(2)

US3806069A
(en)

DE
(1)

DE2228481C3
(en)

FR
(1)

FR2140605B1
(en)

GB
(1)

GB1383513A
(en)

Cited By (1)

* Cited by examiner, † Cited by third party

Publication number
Priority date
Publication date
Assignee
Title

EP0312385A2
(en)

*

1987-10-14
1989-04-19
British Aerospace Public Limited Company
Corona discharge surface treatment, and aircraft cockpit canopies so treated

Families Citing this family (16)

* Cited by examiner, † Cited by third party

Publication number
Priority date
Publication date
Assignee
Title

GB1550352A
(en)

*

1975-03-26
1979-08-15
Secr Defence
Cockpit canopy shattering apparatus

US4275858A
(en)

*

1976-03-25
1981-06-30
The Secretary Of State For Defence In Her Britannic Majesty’s Government Of The United Kingdom Of Great Britain And Northern Ireland
Panel breaking systems

CA1102295A
(en)

*

1977-12-14
1981-06-02
Henry W. Turner
Panel breaking apparatus

US4405104A
(en)

*

1977-12-14
1983-09-20
The Secretary Of State For Defence In Her Britannic Majesty’s Government Of The United Kingdom Of Great Britain And Northern Ireland
Panel breaking apparatus

FR2445799A1
(en)

*

1979-01-04
1980-08-01
Aerospatiale

ICE PROVIDED WITH A PYROTECHNIC CUTTING DEVICE

US4301707A
(en)

*

1979-10-29
1981-11-24
Mcdonnell Douglas Corporation
Embedded explosive severance of non-metallic materials

US4279405A
(en)

*

1979-11-26
1981-07-21
Buryakov Valery M
Device for making emergency exits in a crushed transport means

DE2949778C2
(en)

*

1979-12-11
1984-11-08
Gosudarstvennyj naučno-issledovatel’skij institut graždanskoj aviacii, Moskva

Device for rapid and simultaneous severing of the wall of a means of transport, in particular the fuselage wall of an aircraft

DE3213380A1
(en)

*

1982-04-10
1983-10-20
Dornier Gmbh, 7990 Friedrichshafen

ARRANGEMENT OF DEVICES FOR SEPARATING AND REMOVING WALL PARTS OF THE CANOPY OF PILOT CANNERS

FR2542697B1
(en)

*

1983-03-14
1986-03-21
Dassault Avions

METHOD AND PYROTECHNIC DEVICE FOR EJECTION OUTSIDE AN AIRPLANE

DE8914921U1
(en)

*

1989-12-19
1991-04-18
Dynatech Otto Sebald Gmbh, 8000 Muenchen, De

EP0950576B1
(en)

1998-04-09
2003-03-12
Certime Amsterdam B.V.
Collapsible panel and method for controlled collapsing thereof

US6609464B1
(en)

*

1999-12-22
2003-08-26
Mccormick Selph, Inc.
Severance of polycarbonates and polycarbonate laminates with linear shaped charge

US20020166924A1
(en)

*

2001-05-08
2002-11-14
Wm. David Fahey
Methods and apparatus for canopy fragilization

US6845947B1
(en)

*

2003-10-09
2005-01-25
The United States Of America As Represented By The Secretary Of The Navy
Aircraft canopy jettison apparatus with airbag

US11174001B2
(en)

*

2020-03-03
2021-11-16
The Boeing Company
Fracturing system for a canopy of an aircraft

Family Cites Families (12)

* Cited by examiner, † Cited by third party

Publication number
Priority date
Publication date
Assignee
Title

US2629423A
(en)

*

1949-08-02
1953-02-24
Sorg Paper Company
Machine for fabricating laminated signatures provided with sheet metal inserts

US2626338A
(en)

*

1952-05-08
1953-01-20
Trans Sonics Inc
Measuring device

US3135163A
(en)

*

1962-05-08
1964-06-02
Jr George F Mechlin
Self-rupturing diaphragm assembly

US3172330A
(en)

*

1962-07-06
1965-03-09
Svenska Aeroplan Ab
Jettisonable end cone for aircraft rocket missile pods

DE1254998B
(en)

*

1964-04-20
1967-11-23
Dornier System Gmbh

Altitude research rocket

CH411628A
(en)

*

1964-05-08
1966-04-15
Contraves Ag

Transport container for small rockets

US3323544A
(en)

*

1965-03-24
1967-06-06
Francis Gus
Method and apparatus for draining liquid from containers

US3465482A
(en)

*

1967-12-26
1969-09-09
Nasa
Spacecraft radiator cover

US3561703A
(en)

*

1969-07-07
1971-02-09
Stencel Aero Eng Corp
Canopy breaking by shaped charge

FR2077846A1
(en)

*

1970-02-18
1971-11-05
Dassault Aeronautique

US3674227A
(en)

*

1970-03-23
1972-07-04
Hughes Aircraft Co
Fragmenting cover

US3670998A
(en)

*

1970-07-10
1972-06-20
Us Air Force
Severance of polycarbonate material canopy transparency

1971

1971-06-10
GB
GB1998471A
patent/GB1383513A/en
not_active
Expired

1972

1972-06-08
DE
DE2228481A
patent/DE2228481C3/en
not_active
Expired

1972-06-09
FR
FR7220779A
patent/FR2140605B1/fr
not_active
Expired

1972-06-12
US
US00262034A
patent/US3806069A/en
not_active
Expired – Lifetime

1973

1973-11-08
US
US413827A
patent/US3902945A/en
not_active
Expired – Lifetime

Cited By (3)

* Cited by examiner, † Cited by third party

Publication number
Priority date
Publication date
Assignee
Title

EP0312385A2
(en)

*

1987-10-14
1989-04-19
British Aerospace Public Limited Company
Corona discharge surface treatment, and aircraft cockpit canopies so treated

US4892271A
(en)

*

1987-10-14
1990-01-09
British Aerospace Plc
Corona discharge surface treatment and aircraft cockpit canopies so treated

EP0312385A3
(en)

*

1987-10-14
1990-03-14
British Aerospace Public Limited Company
Corona discharge surface treatment, and aircraft cockpit canopies so treated

Also Published As

Publication number
Publication date

US3806069A
(en)

1974-04-23

DE2228481C3
(en)

1978-09-21

FR2140605B1
(en)

1977-12-23

US3902945A
(en)

1975-09-02

DE2228481B2
(en)

1978-01-26

DE2228481A1
(en)

1972-12-28

FR2140605A1
(en)

1973-01-19

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Preliminary airworthiness evaluation EH-1 H helicopter quick fix, phase 1 A[Final Report]

Maureau

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UMANSKIY

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G-suits, pressure suits and protective helmets. Accelerations during parachute jumps(Protective gear and devices for pilot safety during acceleration of flight, parachute jumps, and ejection)

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(en)

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SAFETY AND PARACHUTE OPENING MECHANISM FOR FLIGHT AVIATION PUMPS.

Legal Events

Date
Code
Title
Description

1975-06-25
PS
Patent sealed [section 19, patents act 1949]

1980-03-05
732
Registration of transactions, instruments or events in the register (sect. 32/1977)

1981-05-28
732
Registration of transactions, instruments or events in the register (sect. 32/1977)

1992-07-08
PE20
Patent expired after termination of 20 years

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