EP2340201A4 - Pyrotechnic egress system - Google Patents

Pyrotechnic egress system

Info

Publication number
EP2340201A4
EP2340201A4 EP08877199.3A EP08877199A EP2340201A4 EP 2340201 A4 EP2340201 A4 EP 2340201A4 EP 08877199 A EP08877199 A EP 08877199A EP 2340201 A4 EP2340201 A4 EP 2340201A4
Authority
EP
European Patent Office
Prior art keywords
pyrotechnic
egress system
egress
pyrotechnic egress
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.)
Withdrawn
Application number
EP08877199.3A
Other languages
German (de)
French (fr)
Other versions
EP2340201A1 (en
Inventor
Honmartin K Au-Yeung
David J Goldschmidt
Anthony Z Stobiecki
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.)
Sikorsky Aircraft Corp
Original Assignee
Sikorsky Aircraft Corp
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 Sikorsky Aircraft Corp filed Critical Sikorsky Aircraft Corp
Publication of EP2340201A1 publication Critical patent/EP2340201A1/en
Publication of EP2340201A4 publication Critical patent/EP2340201A4/en
Withdrawn legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C1/00Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/14Windows; Doors; Hatch covers or access panels; Surrounding frame structures; Canopies; Windscreens accessories therefor, e.g. pressure sensors, water deflectors, hinges, seals, handles, latches, windscreen wipers
    • B64C1/1476Canopies; Windscreens or similar transparent elements
    • B64C1/1492Structure and mounting of the transparent elements in the window or windscreen
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C1/00Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/32Severable or jettisonable parts of fuselage facilitating emergency escape
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B1/00Explosive charges characterised by form or shape but not dependent on shape of container
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42DBLASTING
    • F42D3/00Particular applications of blasting techniques
EP08877199.3A 2008-09-30 2008-09-30 Pyrotechnic egress system Withdrawn EP2340201A4 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/US2008/078241 WO2010039119A1 (en) 2008-09-30 2008-09-30 Pyrotechnic egress system

Publications (2)

Publication Number Publication Date
EP2340201A1 EP2340201A1 (en) 2011-07-06
EP2340201A4 true EP2340201A4 (en) 2013-05-29

Family

ID=42073734

Family Applications (1)

Application Number Title Priority Date Filing Date
EP08877199.3A Withdrawn EP2340201A4 (en) 2008-09-30 2008-09-30 Pyrotechnic egress system

Country Status (3)

Country Link
US (1) US20110167994A1 (en)
EP (1) EP2340201A4 (en)
WO (1) WO2010039119A1 (en)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10739112B1 (en) * 2013-08-15 2020-08-11 The United States Of America As Represented By The Secretary Of The Navy Impulse dampening system for emergency egress
US20180003468A1 (en) * 2015-01-29 2018-01-04 Sikorsky Aircraft Corporation Vehicle hatch system, an aircraft employing same and method of armoring a hatch of a vehicle
US10837747B2 (en) * 2018-02-15 2020-11-17 Goodrich Corporation High explosive firing mechanism
US10711515B2 (en) * 2018-06-07 2020-07-14 Goodrich Corporation Cockpit canopy cutting gas generator
US11319260B2 (en) * 2019-11-05 2022-05-03 Goodrich Corporation Detonating cord stress concentrators

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4090447A (en) * 1975-02-26 1978-05-23 Johnsen Oscar A Directional blasting tubes and method of use
US4301707A (en) * 1979-10-29 1981-11-24 Mcdonnell Douglas Corporation Embedded explosive severance of non-metallic materials
US4407468A (en) * 1981-04-30 1983-10-04 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Explosively activated egress area
US4512538A (en) * 1982-03-04 1985-04-23 Societe Nationale Industrielle Et Aerospatiale Device for maintaining a detonating cord against a transparent aircraft canopy member
EP0142717A1 (en) * 1983-11-17 1985-05-29 Manfred Meul Blasting device for precision blasting
WO1999042362A1 (en) * 1998-02-18 1999-08-26 Teledyne Industries, Inc. Aircraft canopy fracture system
US6286430B1 (en) * 1998-06-02 2001-09-11 AEROSPATIALE SOCIéTé NATIONALE INDUSTRIELLE Device for the pyrotechnic cutting of non-metallic parts
US7086629B2 (en) * 1999-12-22 2006-08-08 Mccormick Selph, Inc. Severance of polycarbonates and polycarbonate laminates with linear shaped charge

Family Cites Families (42)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2255725A (en) * 1940-07-11 1941-09-09 Continental Rubber Works Knock-out window setting for busses and the like
US2412787A (en) * 1943-05-22 1946-12-17 Adlake Co Jettisoning means for the escape panels of aircraft
US2554442A (en) * 1945-03-30 1951-05-22 Adlake Co Latching device for knockout windows
US2572124A (en) * 1946-06-14 1951-10-23 Gen Motors Corp Window construction
US2549110A (en) * 1949-05-31 1951-04-17 Northrop Aircraft Inc Panel hinge
US2830843A (en) * 1953-12-21 1958-04-15 O M Edwards Company Escape sash release mechanism for vehicles
US3374737A (en) * 1967-02-15 1968-03-26 Earl A. Pike Detonating tape
US3658006A (en) * 1969-02-05 1972-04-25 Explosive Tech Explosively actuated egress and ingress device and method
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
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
US4395001A (en) * 1978-03-27 1983-07-26 The United States Of America As Represented By The Secretary Of The Navy Attitude selective aircrew escape control
US4437628A (en) * 1979-06-29 1984-03-20 The United States Of America As Represented By The Secretary Of The Navy Position and restraint system for aircrewman
US4279405A (en) * 1979-11-26 1981-07-21 Buryakov Valery M Device for making emergency exits in a crushed transport means
US4375281A (en) * 1981-03-30 1983-03-01 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Aircraft canopy lock
SE443963B (en) * 1981-10-22 1986-03-17 Bofors Ab SET AND DEVICE TO QUICKLY CLOSE LIMITS AND SURFACES OF LIMITED SIZE
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
US4580746A (en) * 1983-05-31 1986-04-08 Stencel Aero Engineering Corporation Capsule and rocket extraction system
US4649795A (en) * 1984-05-16 1987-03-17 Hi-Shear Corporation Structural shroud system incorporating a pyrotechnic
US4673147A (en) * 1985-02-21 1987-06-16 Rockwell International Corporation Programmable ejection seat system
FR2634171B1 (en) * 1988-07-13 1990-09-28 Aerospatiale PYROTECHNIC SYSTEM FOR PROVIDING A EMERGENCY EXIT IN A WALL OF AN AIRCRAFT AND AIRCRAFT EQUIPPED WITH SAID SYSTEM
US4911382A (en) * 1989-01-17 1990-03-27 Grumman Aerospace Corporation Safe electro ballistic escape sequencing system
GB9112928D0 (en) * 1991-06-15 1991-08-14 British Aerospace Venting a space to relieve pressure generated by an explosion
US5297761A (en) * 1992-06-15 1994-03-29 Kendall Jr Robert T Multi-axis g-compensating escape cockpit capsule
EP0590688B1 (en) * 1992-10-02 1996-07-24 Grumman Aerospace Corporation Power source for an electroballistic sequencing system
US5301904A (en) * 1993-03-17 1994-04-12 The United States Of America As Represented By The Secretary Of The Navy Canopy breaking device
US5826824A (en) * 1996-11-08 1998-10-27 Sikorsky Aircraft Corporation Emergency egress system for aircraft
FR2766156B1 (en) * 1997-07-18 1999-10-01 Eurocopter France WINDOW FRAME ALLOWING THE RELEASE OF A HELICOPTER DOOR
AU8620298A (en) * 1997-08-05 1999-03-01 Her Majesty The Queen as represented by The Minister of Nati onal Defence of Her Majesty's Canadian G Emergency exit system
GB9906987D0 (en) * 1999-03-25 1999-05-19 Baker Martin Aircraft Co An ejection seat
EP1048562A3 (en) * 1999-04-29 2002-02-06 Her Majesty The Queen In Right Of Canada As Represented By The Minister Of National Defence Emergency exit system
US6315245B1 (en) * 2000-03-14 2001-11-13 Martin-Baker Aircraft Company, Limited Ejection seat with blast protection system
GR1003755B (en) * 2000-03-31 2002-01-15 Aircraft with detachable cabin equipped with shock-absorbing parachutes-airbags-seats and conventional aircraft equipped with said safety systems
US6786453B2 (en) * 2001-10-25 2004-09-07 The Boeing Company Snap-in window assembly and method
US7070153B1 (en) * 2002-01-02 2006-07-04 John Kevin Stenard Shock-limiting interface, compact (SLIC)
DE10204544B4 (en) * 2002-02-05 2004-04-01 Airbus Deutschland Gmbh Access device to the driver's cab of a means of transport, in particular to the cockpit of a commercial aircraft
US6752355B1 (en) * 2003-02-13 2004-06-22 The Boeing Company Method and system for emergency escape from an aircraft
US6776373B1 (en) * 2003-02-19 2004-08-17 Robert N. Talmage, Jr. Aircraft escape cabin
US7300693B2 (en) * 2003-09-04 2007-11-27 The Boeing Company Resin infused transparent skin panel and method of making same
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
US7195198B2 (en) * 2005-08-25 2007-03-27 William Spencer Boice Helicopter blade emergency detachment system
US8006621B1 (en) * 2008-02-07 2011-08-30 Cherry Christopher R Linear explosive breaching apparatus and method

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4090447A (en) * 1975-02-26 1978-05-23 Johnsen Oscar A Directional blasting tubes and method of use
US4301707A (en) * 1979-10-29 1981-11-24 Mcdonnell Douglas Corporation Embedded explosive severance of non-metallic materials
US4407468A (en) * 1981-04-30 1983-10-04 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Explosively activated egress area
US4512538A (en) * 1982-03-04 1985-04-23 Societe Nationale Industrielle Et Aerospatiale Device for maintaining a detonating cord against a transparent aircraft canopy member
EP0142717A1 (en) * 1983-11-17 1985-05-29 Manfred Meul Blasting device for precision blasting
WO1999042362A1 (en) * 1998-02-18 1999-08-26 Teledyne Industries, Inc. Aircraft canopy fracture system
US6286430B1 (en) * 1998-06-02 2001-09-11 AEROSPATIALE SOCIéTé NATIONALE INDUSTRIELLE Device for the pyrotechnic cutting of non-metallic parts
US7086629B2 (en) * 1999-12-22 2006-08-08 Mccormick Selph, Inc. Severance of polycarbonates and polycarbonate laminates with linear shaped charge

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See also references of WO2010039119A1 *

Also Published As

Publication number Publication date
US20110167994A1 (en) 2011-07-14
WO2010039119A1 (en) 2010-04-08
EP2340201A1 (en) 2011-07-06

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RIN1 Information on inventor provided before grant (corrected)

Inventor name: STOBIECKI, ANTHONY, Z.

Inventor name: GOLDSCHMIDT, DAVID, J.

Inventor name: AU-YEUNG, HONMARTIN, K.

DAX Request for extension of the european patent (deleted)
A4 Supplementary search report drawn up and despatched

Effective date: 20130425

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Ipc: B64C 1/14 20060101AFI20130419BHEP

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