CA2964252A1 - Assemblage de panneau de decompression et methodes d'assemblage associees - Google Patents

Assemblage de panneau de decompression et methodes d'assemblage associees Download PDF

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Publication number
CA2964252A1
CA2964252A1 CA2964252A CA2964252A CA2964252A1 CA 2964252 A1 CA2964252 A1 CA 2964252A1 CA 2964252 A CA2964252 A CA 2964252A CA 2964252 A CA2964252 A CA 2964252A CA 2964252 A1 CA2964252 A1 CA 2964252A1
Authority
CA
Canada
Prior art keywords
panel
frame
face
decompression
accordance
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.)
Granted
Application number
CA2964252A
Other languages
English (en)
Other versions
CA2964252C (fr
Inventor
Douglas Alan Brown
Adam Robert Weston
Brian Tatsuo Imada
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.)
Boeing Co
Original Assignee
Boeing Co
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
Priority claimed from US15/174,154 external-priority patent/US10279887B2/en
Priority claimed from US15/174,064 external-priority patent/US10399660B2/en
Application filed by Boeing Co filed Critical Boeing Co
Publication of CA2964252A1 publication Critical patent/CA2964252A1/fr
Application granted granted Critical
Publication of CA2964252C publication Critical patent/CA2964252C/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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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
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/066—Interior liners
    • 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
    • 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
    • B64C1/14—Windows; 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
    • 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/40—Weight reduction

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Air-Flow Control Members (AREA)
  • Specific Sealing Or Ventilating Devices For Doors And Windows (AREA)

Abstract

Un assemblage de panneau de décompression destiné à être utilisé dans un aéronef comprend un cadre comprenant une première surface et une seconde surface opposée, où le cadre définit une ouverture de grille et définit au moins partiellement une ouverture de trajet découlement qui sont chacune définies entre les première et seconde surfaces. Lassemblage panneau de décompression comprend également un premier panneau de face et un second panneau de face couplés de manière pivotante ensemble au niveau dune charnière centrale. Une plaque de retenue est couplée de manière amovible aux premier et second panneaux et est configurée pour se déplacer entre une position fermée et une position ouverte. Les premier et second panneaux de face recouvrent au moins partiellement louverture de grille dans une position plane lorsque la plaque de retenue est dans la position fermée, et les premier et second panneaux de face séloignent de louverture de grille vers une position pliée lorsque la plaque de retenue est dans la position ouverte.
CA2964252A 2016-06-06 2017-04-12 Assemblage de panneau de decompression et methodes d'assemblage associees Active CA2964252C (fr)

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
US15/174,154 US10279887B2 (en) 2016-06-06 2016-06-06 Decompression panel assembly and methods of assembling the same
US15/147064 2016-06-06
US15/174,064 US10399660B2 (en) 2016-06-06 2016-06-06 Decompression panel assembly and methods of assembling the same
US15/174154 2016-06-06

Publications (2)

Publication Number Publication Date
CA2964252A1 true CA2964252A1 (fr) 2017-12-06
CA2964252C CA2964252C (fr) 2021-04-27

Family

ID=59220613

Family Applications (1)

Application Number Title Priority Date Filing Date
CA2964252A Active CA2964252C (fr) 2016-06-06 2017-04-12 Assemblage de panneau de decompression et methodes d'assemblage associees

Country Status (3)

Country Link
CN (1) CN107458573B (fr)
CA (1) CA2964252C (fr)
GB (1) GB2552877B (fr)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114348234B (zh) * 2022-02-25 2024-04-12 中国商用飞机有限责任公司 货网组件及飞机货舱

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102005063076A1 (de) * 2005-12-29 2007-07-12 Airbus Deutschland Gmbh Erweiterte Dekompressionsklappenanordnung
US20100032031A1 (en) * 2008-08-11 2010-02-11 Halliburton Energy Services, Inc. Fluid supply system
DE102009012015A1 (de) * 2009-03-06 2010-09-09 Airbus Deutschland Gmbh Dekompressionsanordnung für ein Luftfahrzeug
DE102009025382B4 (de) * 2009-06-18 2017-01-26 Airbus Operations Gmbh Dekompressionseinrichtung für ein Luftfahrzeug
US9796245B2 (en) * 2013-09-24 2017-10-24 The Boeing Company Grille for vehicle wall opening
US9611028B2 (en) * 2014-01-17 2017-04-04 William J. Boyer Pressure relief panel guard
EP3170739B1 (fr) * 2015-11-20 2019-02-27 Airbus Operations GmbH Ensemble de décompression avec deux ouvertures de décompression
EP3170738B1 (fr) * 2015-11-20 2020-04-08 Airbus Operations GmbH Ensemble de décompression avec un canal d'air

Also Published As

Publication number Publication date
BR102017008228A2 (pt) 2017-12-19
GB2552877B (en) 2019-03-13
CA2964252C (fr) 2021-04-27
GB2552877A (en) 2018-02-14
GB201708161D0 (en) 2017-07-05
CN107458573B (zh) 2022-02-25
CN107458573A (zh) 2017-12-12

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