BRPI0922872A2 - escotilha de sobrepressão destinada a ser montada sobre uma parede de uma nacela de motor turbojato e nacela - Google Patents

escotilha de sobrepressão destinada a ser montada sobre uma parede de uma nacela de motor turbojato e nacela

Info

Publication number
BRPI0922872A2
BRPI0922872A2 BRPI0922872A BRPI0922872A BRPI0922872A2 BR PI0922872 A2 BRPI0922872 A2 BR PI0922872A2 BR PI0922872 A BRPI0922872 A BR PI0922872A BR PI0922872 A BRPI0922872 A BR PI0922872A BR PI0922872 A2 BRPI0922872 A2 BR PI0922872A2
Authority
BR
Brazil
Prior art keywords
nacelle
wall
turbojet engine
overpressure
hatch intended
Prior art date
Application number
BRPI0922872A
Other languages
English (en)
Inventor
Guy Bernanrd Vauchel
Original Assignee
Aircelle Sa
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 Aircelle Sa filed Critical Aircelle Sa
Publication of BRPI0922872A2 publication Critical patent/BRPI0922872A2/pt

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D29/00—Power-plant nacelles, fairings or cowlings
    • 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
    • Y10T137/00—Fluid handling
    • Y10T137/0536—Highspeed fluid intake means [e.g., jet engine intake]
    • Y10T137/0645—With condition responsive control means

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Pressure Vessels And Lids Thereof (AREA)
  • Wind Motors (AREA)
BRPI0922872A 2008-12-12 2009-11-18 escotilha de sobrepressão destinada a ser montada sobre uma parede de uma nacela de motor turbojato e nacela BRPI0922872A2 (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0806991A FR2939768B1 (fr) 2008-12-12 2008-12-12 Trappe de surpression destinee a etre montee sur une paroi d'une nacelle de turboreacteur
PCT/FR2009/001324 WO2010066958A1 (fr) 2008-12-12 2009-11-18 Trappe de surpression destinée à être montée sur une paroi d'une nacelle pour turboréacteur

Publications (1)

Publication Number Publication Date
BRPI0922872A2 true BRPI0922872A2 (pt) 2016-01-12

Family

ID=40873456

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0922872A BRPI0922872A2 (pt) 2008-12-12 2009-11-18 escotilha de sobrepressão destinada a ser montada sobre uma parede de uma nacela de motor turbojato e nacela

Country Status (9)

Country Link
US (1) US20110240137A1 (pt)
EP (1) EP2356028B1 (pt)
CN (1) CN102245473B (pt)
BR (1) BRPI0922872A2 (pt)
CA (1) CA2742748A1 (pt)
ES (1) ES2416979T3 (pt)
FR (1) FR2939768B1 (pt)
RU (1) RU2509687C2 (pt)
WO (1) WO2010066958A1 (pt)

Families Citing this family (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2966435B1 (fr) * 2010-10-25 2013-04-26 Aircelle Sa Nacelle de turboreacteur a section de sortie de ventilation adaptable
US9108736B2 (en) 2012-06-05 2015-08-18 United Technologies Corporation Nacelle inner flow structure leading edge latching system
US9239030B2 (en) * 2012-09-19 2016-01-19 United Technologies Corporation Nacelle electrical locking system for leading edge of openable panel
US9988940B2 (en) 2013-03-14 2018-06-05 United Technologies Corporation Latching actuation mechanism for nacelle mounted latching system
US10060287B2 (en) * 2015-07-09 2018-08-28 Rohr, Inc Pressure relief door assembly
DE102016215036A1 (de) * 2016-08-11 2018-02-15 Rolls-Royce Deutschland Ltd & Co Kg Turbofan-Triebwerk mit Überdruckklappe an einer im Sekundärstromkanal liegenden Verkleidung
US10634060B2 (en) 2016-11-20 2020-04-28 Mra Systems, Llc Engine door with burst seal
GB201704841D0 (en) * 2017-03-27 2017-05-10 Rolls Royce Plc Gas Turbine Engine
GB201704888D0 (en) * 2017-03-28 2017-05-10 Rolls Royce Plc Gas turbine engine
GB201720831D0 (en) 2017-10-12 2018-01-31 Rolls-Royce Ltd A pressure relief arrangement for a gas turbine engine
US10589869B2 (en) * 2018-07-25 2020-03-17 General Electric Company Nacelle inlet lip fuse structure
US11008089B2 (en) 2018-10-24 2021-05-18 Gulfstream Aerospace Corporation Fireproof pressure relief assembly
US11077956B2 (en) 2018-11-07 2021-08-03 Rohr, Inc Pressure relief assembly
DE102019110693A1 (de) * 2019-04-25 2020-10-29 Rolls-Royce Deutschland Ltd & Co Kg Druckentlastungsvorrichtung mit einer Druckentlastungsklappe
US11702994B2 (en) * 2019-05-06 2023-07-18 Rohr, Inc. Pressure relief latch
FR3098253B1 (fr) * 2019-07-02 2021-09-17 Safran Aircraft Engines Turbomachine à double flux comprenant une tuyère compacte
FR3109142B1 (fr) * 2020-04-10 2022-03-04 Safran Nacelles Organe d’obturation amovible pour une partie femelle logée dans une ouverture extérieure d’une nacelle d’aéronef
FR3136447A1 (fr) * 2022-06-09 2023-12-15 Airbus Operations (S.A.S.) Dispositif de surpression et aéronef équipé d’au moins un tel dispositif
FR3136746A1 (fr) * 2022-06-16 2023-12-22 Airbus Operations (S.A.S.) Dispositif de surpression comprenant une paroi mobile maintenue en position fermée tant que sa déformation ne dépasse pas un état déformé donné et aéronef équipé d’au moins un tel dispositif
EP4420985B1 (fr) * 2023-02-22 2025-04-16 Airbus Operations (S.A.S.) Ensemble de propulsion d aéronef comprenant au moins un dispositif de surpression et aéronef comportant au moins un tel ensemble de propulsion
FR3152497B3 (fr) 2023-08-28 2025-11-21 Daher Aerospace Porte de surpression pour un capotage d’extrémité arrière d’un mât support de moteur d’un aéronef

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CA459251A (en) * 1949-08-30 Beatty Bros. Safety device for pressure vessels
US4232513A (en) * 1977-10-19 1980-11-11 Rolls-Royce Limited Pressure relief panel for aircraft powerplant
US4825644A (en) * 1987-11-12 1989-05-02 United Technologies Corporation Ventilation system for a nacelle
RU1766020C (ru) * 1989-12-20 1994-08-15 Авиационный комплекс им.С.В.Ильюшина Створка гондолы двигателя летательного аппарата
US5765883A (en) * 1995-07-14 1998-06-16 Hartwell Corporation Adjustable pressure relief latch
GR1003755B (el) * 2000-03-31 2002-01-15 Αεροσκαφος με αποχωριζομενη καμπινα διαφυγης επιβατων εξοπλισμενη με αλεξιπτωτα-αεροσακκους-καθισματα απορροφησης κρουσεως και συμβατικο αεροσκαφος εξοπλισμενο με τα συστηματα αυτα ασφαλειας
FR2920134B1 (fr) * 2007-08-20 2010-02-26 Aircelle Sa Nacelle equipee d'au moins une trappe de surpression
FR2920135B1 (fr) * 2008-07-21 2009-11-20 Aircelle Sa Nacelle equipee d'au moins une trappe de surpression

Also Published As

Publication number Publication date
FR2939768B1 (fr) 2011-09-09
RU2011128147A (ru) 2013-01-20
EP2356028A1 (fr) 2011-08-17
RU2509687C2 (ru) 2014-03-20
EP2356028B1 (fr) 2013-03-27
ES2416979T3 (es) 2013-08-05
WO2010066958A1 (fr) 2010-06-17
FR2939768A1 (fr) 2010-06-18
CN102245473A (zh) 2011-11-16
US20110240137A1 (en) 2011-10-06
CN102245473B (zh) 2013-10-02
CA2742748A1 (fr) 2010-06-17

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Legal Events

Date Code Title Description
B08F Application dismissed because of non-payment of annual fees [chapter 8.6 patent gazette]

Free format text: REFERENTE A 6A ANUIDADE.

B08K Patent lapsed as no evidence of payment of the annual fee has been furnished to inpi [chapter 8.11 patent gazette]

Free format text: EM VIRTUDE DO ARQUIVAMENTO PUBLICADO NA RPI 2383 DE 06-09-2016 E CONSIDERANDO AUSENCIA DE MANIFESTACAO DENTRO DOS PRAZOS LEGAIS, INFORMO QUE CABE SER MANTIDO O ARQUIVAMENTO DO PEDIDO DE PATENTE, CONFORME O DISPOSTO NO ARTIGO 12, DA RESOLUCAO 113/2013.