ES556054A0 - Mamparo de presion para el fuselaje, que se puede someter a una sobrepresion interior, de un vehiculo aeronautico - Google Patents

Mamparo de presion para el fuselaje, que se puede someter a una sobrepresion interior, de un vehiculo aeronautico

Info

Publication number
ES556054A0
ES556054A0 ES556054A ES556054A ES556054A0 ES 556054 A0 ES556054 A0 ES 556054A0 ES 556054 A ES556054 A ES 556054A ES 556054 A ES556054 A ES 556054A ES 556054 A0 ES556054 A0 ES 556054A0
Authority
ES
Spain
Prior art keywords
fuselage
subject
pressure screen
internal overpressure
wall
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
ES556054A
Other languages
English (en)
Other versions
ES8706545A1 (es
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.)
Airbus Defence and Space GmbH
Original Assignee
Messerschmitt Bolkow Blohm AG
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 Messerschmitt Bolkow Blohm AG filed Critical Messerschmitt Bolkow Blohm AG
Publication of ES556054A0 publication Critical patent/ES556054A0/es
Publication of ES8706545A1 publication Critical patent/ES8706545A1/es
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
    • 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
    • B64C1/10—Bulkheads
ES556054A 1985-09-28 1986-06-13 Mamparo de presion para el fuselaje, que se puede someter a una sobrepresion interior, de un vehiculo aeronautico Expired ES8706545A1 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19853534719 DE3534719A1 (de) 1985-09-28 1985-09-28 Druckwand fuer einen unter inneren ueberdruck setzbaren rumpf eines luftfahrzeuges

Publications (2)

Publication Number Publication Date
ES556054A0 true ES556054A0 (es) 1987-07-01
ES8706545A1 ES8706545A1 (es) 1987-07-01

Family

ID=6282261

Family Applications (1)

Application Number Title Priority Date Filing Date
ES556054A Expired ES8706545A1 (es) 1985-09-28 1986-06-13 Mamparo de presion para el fuselaje, que se puede someter a una sobrepresion interior, de un vehiculo aeronautico

Country Status (8)

Country Link
US (1) US4728059A (es)
EP (1) EP0217117B1 (es)
JP (1) JPS6274796A (es)
AT (1) ATE34958T1 (es)
BR (1) BR8604674A (es)
CA (1) CA1324598C (es)
DE (1) DE3534719A1 (es)
ES (1) ES8706545A1 (es)

Families Citing this family (31)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0357599Y2 (es) * 1986-08-07 1991-12-27
DE3844080C2 (de) * 1988-12-28 1993-12-23 Deutsche Aerospace Airbus Druckwand für einen Flugzeugrumpf
DE3923871A1 (de) * 1989-02-28 1991-01-31 Dornier Luftfahrt Druckspant
DE3906170A1 (de) * 1989-02-28 1990-08-30 Dornier Luftfahrt Druckspant
US5031862A (en) * 1990-01-26 1991-07-16 Rhodes James R Aircraft with passenger safety net
US5058830A (en) * 1990-02-08 1991-10-22 Rockwell International Corporation Escape mechanism for crew of aircraft
US5071091A (en) * 1991-02-22 1991-12-10 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Load limiting energy absorbing lightweight debris catcher
US5482230A (en) * 1993-06-25 1996-01-09 B E Aerospace, Inc. Vehicle bulkhead safety system
DE19503939C1 (de) * 1995-02-07 1996-06-05 Daimler Benz Aerospace Airbus Verfahren und Vorrichtung zum Herstellen eines Druckspants
US5893534A (en) * 1995-12-22 1999-04-13 The Boeing Company Structural apparatus and design to prevent oil can movement of webs in aircraft pressure bulkheads
US6510961B1 (en) 1999-04-14 2003-01-28 A&P Technology Integrally-reinforced braided tubular structure and method of producing the same
US6213426B1 (en) 1999-07-09 2001-04-10 The Boeing Company Monolithic structure with redundant load paths
FR2864020B1 (fr) * 2003-12-19 2006-02-10 Airbus France Nez d'avion avec bouclier
US7104306B2 (en) 2004-06-14 2006-09-12 The Boeing Company Cast unitized primary truss structure and method
FR2901240B1 (fr) * 2006-05-17 2009-01-09 Airbus France Sas Poutre interne composite pour renforcer la structure d'un aeronef
FR2901536B1 (fr) * 2006-05-23 2009-01-30 Airbus France Sas Poutre pour plancher pressurise d'aeronef
DE102006029231B4 (de) * 2006-06-26 2013-09-26 Airbus Operations Gmbh Druckschott für einen Rumpf für die Luft- und Raumfahrt
DE102007044388B4 (de) * 2007-09-18 2012-08-02 Airbus Operations Gmbh Druckschott und Verfahren zum Unterteilen eines Luft- oder Raumfahrzeugs
DE102007052140B4 (de) * 2007-10-31 2012-10-25 Airbus Operations Gmbh Struktur, insbesondere Rumpfstruktur eines Luft- oder Raumfahrzeugs
DE102008040213B4 (de) * 2008-07-07 2011-08-25 Airbus Operations GmbH, 21129 Verfahren zur Montage eines kalottenförmigen Druckschotts in einer Hecksektion eines Flugzeugs sowie Vorrichtung zur Durchführung des Verfahrens
ES2347122B1 (es) * 2009-03-31 2011-08-11 Airbus Operations, S.L. Estructura de ensamblaje del mamparo de presion de una aeronave.
DE102012005451A1 (de) 2012-03-20 2013-09-26 Airbus Operations Gmbh Druckrumpf eines Luftfahrzeuges, mit einer Rumpfschale und einem hierin angeordneten Druckschott
DE102012011027A1 (de) 2012-06-05 2013-12-05 Airbus Operations Gmbh Druckrumpf eines Luftfahrzeugs, mit einer Rumpfstruktur und einem hierin speziell befestigten Druckschott
CN103112581B (zh) * 2012-12-21 2016-02-24 中国飞行试验研究院 基于y8货运飞机的气密套舱
US10189578B2 (en) * 2013-06-12 2019-01-29 The Boeing Company Self-balancing pressure bulkhead
US9187168B2 (en) * 2013-07-30 2015-11-17 The Boeing Company Natural-path tearstraps and stiffeners for spherical composite pressure bulkheads
DE102013114391A1 (de) * 2013-12-18 2015-06-18 Airbus Operations Gmbh Druckrumpf eines Flugzeuges, umfassend ein bewegbar relativ zur Rumpfstruktur befestigtes Druckschott
ES2902069T3 (es) * 2014-10-16 2022-03-24 Airbus Operations Gmbh Deflector para aeronave y método asociado
US10926857B2 (en) * 2016-06-17 2021-02-23 The Boeing Company Pressurized bulkhead
US10933967B2 (en) 2017-12-15 2021-03-02 Airbus Americas, Inc. Partition wall in cabin of aircraft supporting monuments
ES2909500T3 (es) * 2019-07-30 2022-05-06 Airbus Sas Mamparo de presión

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1219125A (en) * 1916-06-22 1917-03-13 Thomas R Macmechen Airship.
US2109529A (en) * 1936-12-21 1938-03-01 Robert H Goddard Reenforced construction for light hollow members
US2669402A (en) * 1951-08-11 1954-02-16 Douglas Aircraft Co Inc High strength cable network for impact bulkheads
US2982501A (en) * 1955-09-08 1961-05-02 Rolls Royce Aircraft
US3910447A (en) * 1974-03-01 1975-10-07 Combustion Eng Vessel restraint device
DE2536231C3 (de) * 1975-08-14 1980-01-17 Messerschmitt-Boelkow-Blohm Gmbh, 8000 Muenchen Einrichtung zum Verzögern des Druckabfalls in Flugzeugen bei Notfällen
US4055317A (en) * 1976-06-30 1977-10-25 The Boeing Company Aft main deck split level galley
DE2913050A1 (de) * 1979-03-31 1980-10-02 Brueggemann & Brand Kg Zwischen frachtraum und cockpit eines flugzeugs anzuordnende einrichtung zum abfangen von lasten

Also Published As

Publication number Publication date
DE3534719A1 (de) 1987-04-02
US4728059A (en) 1988-03-01
EP0217117A1 (de) 1987-04-08
ATE34958T1 (de) 1988-06-15
DE3534719C2 (es) 1992-07-02
EP0217117B1 (de) 1988-06-08
BR8604674A (pt) 1987-06-16
JPS6274796A (ja) 1987-04-06
JPH0466759B2 (es) 1992-10-26
CA1324598C (en) 1993-11-23
ES8706545A1 (es) 1987-07-01

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Legal Events

Date Code Title Description
FD1A Patent lapsed

Effective date: 19980202