AU2001277470A1 - Decompression unit for equalizing an explosive air pressure - Google Patents

Decompression unit for equalizing an explosive air pressure

Info

Publication number
AU2001277470A1
AU2001277470A1 AU2001277470A AU7747001A AU2001277470A1 AU 2001277470 A1 AU2001277470 A1 AU 2001277470A1 AU 2001277470 A AU2001277470 A AU 2001277470A AU 7747001 A AU7747001 A AU 7747001A AU 2001277470 A1 AU2001277470 A1 AU 2001277470A1
Authority
AU
Australia
Prior art keywords
air pressure
air
decompression unit
equalizing
chamber
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.)
Abandoned
Application number
AU2001277470A
Inventor
Joachim Barsch
Robert Diehl
Gordon Falk
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.)
Aircabin GmbH
Original Assignee
Aircabin GmbH
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 Aircabin GmbH filed Critical Aircabin GmbH
Publication of AU2001277470A1 publication Critical patent/AU2001277470A1/en
Abandoned legal-status Critical Current

Links

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
    • B64C1/18—Floors
    • 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
    • B64C2001/009—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like comprising decompression panels or valves for pressure equalisation in fuselages or floors
    • 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
    • Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S292/00—Closure fasteners
    • Y10S292/04—Automatic release latches

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Air Bags (AREA)
  • Fluid-Damping Devices (AREA)
  • Nozzles (AREA)
  • Jet Pumps And Other Pumps (AREA)
  • Control Of Fluid Pressure (AREA)

Abstract

The invention relates to a decompression unit for equalizing an explosive air pressure between pressurized areas of an aircraft, which have different air pressure conditions and are separated by a wall structure. An air chamber, whose shape alters by contraction (1), is located inside an exterior zone of the cabin (6) and is subjected to an ambient air pressure (p1), said chamber constituting the decompression unit in concrete terms. The wall of the air chamber (1) is perforated. The air chamber is mounted in the vicinity of the periphery of an air pressure equalization flap (2), which is fixed inside an air equalization cavity (9). Said air chamber is connected to a locking device (4), which likewise fixes the air pressure equalization flap in the air equalization cavity.
AU2001277470A 2000-06-29 2001-06-28 Decompression unit for equalizing an explosive air pressure Abandoned AU2001277470A1 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
DE10031714 2000-06-29
DE10031714A DE10031714C2 (en) 2000-06-29 2000-06-29 Decompression unit for explosive air pressure compensation
PCT/DE2001/002425 WO2002000500A1 (en) 2000-06-29 2001-06-28 Decompression unit for equalizing an explosive air pressure

Publications (1)

Publication Number Publication Date
AU2001277470A1 true AU2001277470A1 (en) 2002-01-08

Family

ID=7647226

Family Applications (1)

Application Number Title Priority Date Filing Date
AU2001277470A Abandoned AU2001277470A1 (en) 2000-06-29 2001-06-28 Decompression unit for equalizing an explosive air pressure

Country Status (7)

Country Link
US (1) US6651932B2 (en)
EP (1) EP1296872B1 (en)
AT (1) ATE280710T1 (en)
AU (1) AU2001277470A1 (en)
CA (1) CA2413349C (en)
DE (2) DE10031714C2 (en)
WO (1) WO2002000500A1 (en)

Families Citing this family (26)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6866226B2 (en) 2001-10-04 2005-03-15 Hartwell Corporation Pressure responsive blowout latch
US7255376B2 (en) * 2001-10-04 2007-08-14 Hartwell Corporation Pressure sensing dead bolt
US20030127563A1 (en) * 2001-10-26 2003-07-10 Laconte Richard J. Differential pressure sensing release system
US7046879B2 (en) * 2002-11-27 2006-05-16 General Electric Company Optical via for three dimensional interconnection
DE102004009017B3 (en) * 2004-02-25 2005-08-04 Aircabin Gmbh Decompression device for two sDEarate regions of aircraft has locking device with release element in control cavity
US7624732B2 (en) * 2005-10-06 2009-12-01 The Boeing Company Method and apparatus for extending flight crew's time of useful consciousness after decompression
DE102007061433B4 (en) * 2007-12-20 2012-10-25 Airbus Operations Gmbh Improved decompression device with adjustable trigger pressure
DE102009006395B4 (en) * 2009-01-28 2014-07-10 Airbus Operations Gmbh Decompression device for an aircraft
DE102009025382B4 (en) * 2009-06-18 2017-01-26 Airbus Operations Gmbh Decompression device for an aircraft
DE102010045197B4 (en) * 2010-09-13 2013-10-24 Airbus Operations Gmbh Decompression device and decompression system
DE102011011976B4 (en) * 2011-02-22 2013-11-14 Airbus Operations Gmbh Decompression assembly for an aircraft
DE102011014674A1 (en) * 2011-03-22 2012-09-27 Global Safety Textiles Gmbh Device for handling objects
DE102011015708B4 (en) * 2011-03-31 2013-12-19 Airbus Operations Gmbh Locking mechanism for use in a decompression assembly
US9440744B2 (en) 2013-10-17 2016-09-13 The Boeing Company Decompression panel assembly and method of equalizing air pressure differential
US9233747B2 (en) 2013-10-25 2016-01-12 The Boeing Company Decompression panel for use in an aircraft assembly
US9566759B2 (en) 2013-10-25 2017-02-14 The Boeing Company Decompression panel for use in an aircraft assembly
US9499251B2 (en) 2013-10-25 2016-11-22 The Boeing Company Decompression panel for use in an aircraft
US10071795B2 (en) 2013-10-25 2018-09-11 The Boeing Company Clamp device for use with a decompression panel in an aircraft assembly
USD817851S1 (en) 2014-03-28 2018-05-15 The Boeing Company Decompression panel
DE102015205939A1 (en) * 2015-04-01 2016-10-06 Lufthansa Technik Ag Device for equalizing a pressure difference for an aircraft
DE102015207599B4 (en) * 2015-04-24 2016-12-01 Lufthansa Technik Ag Device for equalizing a pressure difference for an aircraft
US10220931B2 (en) * 2015-11-09 2019-03-05 The Boeing Company Sidewall panel assembly and return air bridge for use in an aircraft assembly
US9611042B1 (en) 2015-11-19 2017-04-04 International Business Machines Corporation System for securing an aircraft door
US10086947B2 (en) * 2016-04-20 2018-10-02 The Boeing Company System and method of suppressing an unexpected combustion event
DE102017208115A1 (en) * 2017-05-15 2018-11-15 Lufthansa Technik Ag Device for equalizing a pressure difference for an aircraft
JP2022022107A (en) 2020-07-23 2022-02-03 ザ・ボーイング・カンパニー Environment control system for use in aircraft

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3481076A (en) * 1968-03-05 1969-12-02 Norman M Bedard Window operator
FR2306877A1 (en) * 1975-04-11 1976-11-05 Aerospatiale SAFETY DEVICE AGAINST BRUTAL DECOMPRESSION OF AIRCRAFT BEDS
US3938764A (en) 1975-05-19 1976-02-17 Mcdonnell Douglas Corporation Frangible aircraft floor
DE2532350A1 (en) * 1975-07-19 1977-02-03 Ver Flugtechnische Werke DEVICE FOR SECURING DOOR OR FLAP LOCKING IN AIRPLANES
US4049221A (en) 1975-12-24 1977-09-20 Lockheed Aircraft Corporation Relief of inter-compartment differential pressure in aircraft
DE2756726C2 (en) 1977-12-20 1982-04-08 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Device for pressure equalization in an aircraft or spacecraft
US4308695A (en) 1979-09-21 1982-01-05 Eltreva Ag Pressure-relieving facade
DE3011109C2 (en) 1980-03-22 1983-01-05 Vereinigte Flugtechnische Werke Gmbh, 2800 Bremen Safety device for aircraft
FR2630182B1 (en) * 1988-04-18 1990-09-07 Abg Semca VALVE WITH A VALVE AND A VALVE COMPRISING A VALVE AS WELL AS AN AIRCRAFT COMPRISING SUCH A VALVE
DE3922025C1 (en) 1989-07-05 1990-08-09 Messerschmitt-Boelkow-Blohm Gmbh, 8012 Ottobrunn, De
US5118053A (en) * 1989-09-27 1992-06-02 The Boeing Company Pressure equalization systems
DE4002447C1 (en) 1990-01-27 1991-03-14 Deutsche Airbus Gmbh, 2103 Hamburg, De Decompression panel esp. for aircraft - consists of plate which is releasably held in de-compression opening and consists of two inter-strapped plate parts
DE4403896C1 (en) 1994-02-08 1995-09-14 Daimler Benz Aerospace Airbus Holder for decompression panel in wall or floor opening of passenger or freight chamber of aircraft
DE19739161C1 (en) * 1997-09-06 1999-01-07 Draeger Aerospace Gmbh Vent valve for rapid pressure drop in aircraft cabins
DE19910779C2 (en) 1999-03-11 2002-01-24 Airbus Gmbh Hand luggage stowage compartment located in an aircraft cabin

Also Published As

Publication number Publication date
EP1296872A1 (en) 2003-04-02
US20030168553A1 (en) 2003-09-11
US6651932B2 (en) 2003-11-25
CA2413349C (en) 2009-08-11
DE10031714A1 (en) 2002-01-17
CA2413349A1 (en) 2002-01-03
DE50104310D1 (en) 2004-12-02
EP1296872B1 (en) 2004-10-27
ATE280710T1 (en) 2004-11-15
DE10031714C2 (en) 2002-10-10
WO2002000500A1 (en) 2002-01-03

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