FR2914362B1 - Dispositif de deviation et de retention de debris de moteur d'aeronef. - Google Patents

Dispositif de deviation et de retention de debris de moteur d'aeronef.

Info

Publication number
FR2914362B1
FR2914362B1 FR0754160A FR0754160A FR2914362B1 FR 2914362 B1 FR2914362 B1 FR 2914362B1 FR 0754160 A FR0754160 A FR 0754160A FR 0754160 A FR0754160 A FR 0754160A FR 2914362 B1 FR2914362 B1 FR 2914362B1
Authority
FR
France
Prior art keywords
aircraft engine
debris
detecting
retaining debris
retaining
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.)
Expired - Fee Related
Application number
FR0754160A
Other languages
English (en)
Other versions
FR2914362A1 (fr
Inventor
Gilles Weyland
Bernadette Dulay
David Hardy
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 Operations SAS
Original Assignee
Airbus Operations SAS
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 to FR0754160A priority Critical patent/FR2914362B1/fr
Application filed by Airbus Operations SAS filed Critical Airbus Operations SAS
Priority to BRPI0808617-6A priority patent/BRPI0808617A2/pt
Priority to CA002681365A priority patent/CA2681365A1/fr
Priority to EP08788083A priority patent/EP2129876A2/fr
Priority to PCT/FR2008/050557 priority patent/WO2008135699A2/fr
Priority to US12/594,055 priority patent/US20100101205A1/en
Priority to RU2009140136/06A priority patent/RU2009140136A/ru
Priority to CN2008800110061A priority patent/CN101652536B/zh
Priority to JP2010500337A priority patent/JP2010523863A/ja
Publication of FR2914362A1 publication Critical patent/FR2914362A1/fr
Application granted granted Critical
Publication of FR2914362B1 publication Critical patent/FR2914362B1/fr
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D21/00—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for
    • F01D21/04—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for responsive to undesired position of rotor relative to stator or to breaking-off of a part of the rotor, e.g. indicating such position
    • F01D21/045—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for responsive to undesired position of rotor relative to stator or to breaking-off of a part of the rotor, e.g. indicating such position special arrangements in stators or in rotors dealing with breaking-off of part of rotor
    • 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
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Sealing Devices (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

L'objet de l'invention est un dispositif de protection pour traiter au moins un débris provenant d'un étage de compresseur ou de turbine d'une motorisation d'aéronef, caractérisé en ce qu'il est de type ponctuel et disposé de manière à être sécant avec la trajectoire privilégiée dudit débris et a une géométrie permettant au moins de dévier les débris les plus énergétiques.
FR0754160A 2007-03-30 2007-03-30 Dispositif de deviation et de retention de debris de moteur d'aeronef. Expired - Fee Related FR2914362B1 (fr)

Priority Applications (9)

Application Number Priority Date Filing Date Title
FR0754160A FR2914362B1 (fr) 2007-03-30 2007-03-30 Dispositif de deviation et de retention de debris de moteur d'aeronef.
CA002681365A CA2681365A1 (fr) 2007-03-30 2008-03-28 Dispositif de deviation et de retention de debris de moteur d'aeronef
EP08788083A EP2129876A2 (fr) 2007-03-30 2008-03-28 Dispositif de deviation et de retention de debris de moteur d'aeronef
PCT/FR2008/050557 WO2008135699A2 (fr) 2007-03-30 2008-03-28 Dispositif de deviation et de retention de debris de moteur d'aeronef
BRPI0808617-6A BRPI0808617A2 (pt) 2007-03-30 2008-03-28 "dispositivo de proteção"
US12/594,055 US20100101205A1 (en) 2007-03-30 2008-03-28 Device for deflection and retention of aircraft engine debris
RU2009140136/06A RU2009140136A (ru) 2007-03-30 2008-03-28 Устройство для отклонения и задержания обломков двигателя летательного аппарата
CN2008800110061A CN101652536B (zh) 2007-03-30 2008-03-28 一种阻止和偏移飞行器发动机碎片的装置
JP2010500337A JP2010523863A (ja) 2007-03-30 2008-03-28 航空機のエンジンからの離脱破片の飛翔偏向兼保持用装置

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0754160A FR2914362B1 (fr) 2007-03-30 2007-03-30 Dispositif de deviation et de retention de debris de moteur d'aeronef.

Publications (2)

Publication Number Publication Date
FR2914362A1 FR2914362A1 (fr) 2008-10-03
FR2914362B1 true FR2914362B1 (fr) 2012-07-27

Family

ID=38670507

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0754160A Expired - Fee Related FR2914362B1 (fr) 2007-03-30 2007-03-30 Dispositif de deviation et de retention de debris de moteur d'aeronef.

Country Status (9)

Country Link
US (1) US20100101205A1 (fr)
EP (1) EP2129876A2 (fr)
JP (1) JP2010523863A (fr)
CN (1) CN101652536B (fr)
BR (1) BRPI0808617A2 (fr)
CA (1) CA2681365A1 (fr)
FR (1) FR2914362B1 (fr)
RU (1) RU2009140136A (fr)
WO (1) WO2008135699A2 (fr)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2467155B (en) * 2009-01-26 2011-10-12 Rolls Royce Plc A fan assembly
GB201417415D0 (en) 2014-10-02 2014-11-19 Rolls Royce Plc Fan track liner assembly
FR3139119A1 (fr) * 2022-08-30 2024-03-01 Airbus Operations Ensemble propulsif pour aéronef

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2216174B1 (fr) * 1973-02-02 1978-09-29 Norton Co
US3974313A (en) * 1974-08-22 1976-08-10 The Boeing Company Projectile energy absorbing protective barrier
FR2514823B1 (fr) * 1981-10-16 1986-06-27 Poudres & Explosifs Ste Nale Dispositif de protection contre l'eclatement d'elements rotatifs d'une machine tournante
DE3712829A1 (de) * 1987-04-15 1988-11-03 Mtu Muenchen Gmbh Berstschutzring fuer turbotriebwerksgehaeuse
EP0286815B1 (fr) * 1987-04-15 1991-05-29 Mtu Motoren- Und Turbinen-Union MàœNchen Gmbh Anneaux de rétention pour carter de turbomachine
CA2042198A1 (fr) * 1990-06-18 1991-12-19 Stephen C. Mitchell Ecran protecteur contre les projectiles
US5431532A (en) * 1994-05-20 1995-07-11 General Electric Company Blade containment system
US5725181A (en) * 1996-05-01 1998-03-10 The Boeing Company Aircraft engine thrust mount
US6059524A (en) * 1998-04-20 2000-05-09 United Technologies Corporation Penetration resistant fan casing for a turbine engine
GB0116988D0 (en) * 2000-08-11 2001-09-05 Rolls Royce Plc A gas turbine engine blade containment assembly
US6484970B2 (en) * 2001-03-22 2002-11-26 Honeywell International, Inc. Ballistic shield for dual engine single output shaft propulsion system
DE10259943A1 (de) * 2002-12-20 2004-07-01 Rolls-Royce Deutschland Ltd & Co Kg Schutzring für das Fan-Schutzgehäuse eines Gasturbinentriebswerks
GB2416192B (en) * 2004-07-14 2006-09-27 Rolls Royce Plc Ducted fan with containment structure
EP1719879B1 (fr) * 2005-05-03 2008-01-30 ABB Turbo Systems AG Dispositif de protection en cas d'éclatement pour compresseur radial
ITMI20062408A1 (it) * 2006-12-14 2008-06-15 Alenia Aermacchi Spa Pannello di protezione per veicoli

Also Published As

Publication number Publication date
RU2009140136A (ru) 2011-05-10
CA2681365A1 (fr) 2008-11-13
EP2129876A2 (fr) 2009-12-09
WO2008135699A3 (fr) 2009-03-12
JP2010523863A (ja) 2010-07-15
BRPI0808617A2 (pt) 2014-09-16
FR2914362A1 (fr) 2008-10-03
CN101652536A (zh) 2010-02-17
US20100101205A1 (en) 2010-04-29
WO2008135699A2 (fr) 2008-11-13
CN101652536B (zh) 2012-12-26

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Legal Events

Date Code Title Description
CA Change of address

Effective date: 20110916

CD Change of name or company name

Owner name: AIRBUS HOLDING, FR

Effective date: 20110916

CJ Change in legal form

Effective date: 20110916

TP Transmission of property

Owner name: AIRBUS HOLDING, FR

Effective date: 20110913

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ST Notification of lapse

Effective date: 20211105