WO2008135699A3 - 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 Download PDF

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Publication number
WO2008135699A3
WO2008135699A3 PCT/FR2008/050557 FR2008050557W WO2008135699A3 WO 2008135699 A3 WO2008135699 A3 WO 2008135699A3 FR 2008050557 W FR2008050557 W FR 2008050557W WO 2008135699 A3 WO2008135699 A3 WO 2008135699A3
Authority
WO
WIPO (PCT)
Prior art keywords
diverting
retaining
aircraft engine
debris
aircraft
Prior art date
Application number
PCT/FR2008/050557
Other languages
English (en)
Other versions
WO2008135699A2 (fr
Inventor
Gilles Weyland
Bernadette Dulay
David Hardy
Original Assignee
Airbus France
Gilles Weyland
Bernadette Dulay
David Hardy
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 Airbus France, Gilles Weyland, Bernadette Dulay, David Hardy filed Critical Airbus France
Priority to US12/594,055 priority Critical patent/US20100101205A1/en
Priority to BRPI0808617-6A priority patent/BRPI0808617A2/pt
Priority to CN2008800110061A priority patent/CN101652536B/zh
Priority to JP2010500337A priority patent/JP2010523863A/ja
Priority to CA002681365A priority patent/CA2681365A1/fr
Priority to EP08788083A priority patent/EP2129876A2/fr
Publication of WO2008135699A2 publication Critical patent/WO2008135699A2/fr
Publication of WO2008135699A3 publication Critical patent/WO2008135699A3/fr

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)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Sealing Devices (AREA)

Abstract

L'objet de l'invention est un dispositif de protection (40) pour traiter au- moins un débris (54) provenant d'une source (56) d'un aéronef, notamment un étage.de compresseur ou de turbine d'une motorisation d'aéronef, et l'empêcher d'atteindre une cible dudit aéronef, caractérisé en ce qu'il a une géométrie et une position par rapport à la source et à la cible permettant de dévier les débris les plus énergétiques afin de protéger ladite cible disposée dans une zone protégée prédéfinie.
PCT/FR2008/050557 2007-03-30 2008-03-28 Dispositif de deviation et de retention de debris de moteur d'aeronef WO2008135699A2 (fr)

Priority Applications (6)

Application Number Priority Date Filing Date Title
US12/594,055 US20100101205A1 (en) 2007-03-30 2008-03-28 Device for deflection and retention of aircraft engine debris
BRPI0808617-6A BRPI0808617A2 (pt) 2007-03-30 2008-03-28 "dispositivo de proteção"
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
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

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0754160 2007-03-30
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
WO2008135699A2 WO2008135699A2 (fr) 2008-11-13
WO2008135699A3 true WO2008135699A3 (fr) 2009-03-12

Family

ID=38670507

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/FR2008/050557 WO2008135699A2 (fr) 2007-03-30 2008-03-28 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

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3974313A (en) * 1974-08-22 1976-08-10 The Boeing Company Projectile energy absorbing protective barrier
FR2514823A1 (fr) * 1981-10-16 1983-04-22 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
US20020134887A1 (en) * 2001-03-22 2002-09-26 Hersheng Lin Ballistic shield for dual engine single output shaft propulsion system

Family Cites Families (11)

* 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
DE3862989D1 (de) * 1987-04-15 1991-07-04 Mtu Muenchen Gmbh Berstschutzring fuer turbotriebwerksgehaeuse.
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
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

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3974313A (en) * 1974-08-22 1976-08-10 The Boeing Company Projectile energy absorbing protective barrier
FR2514823A1 (fr) * 1981-10-16 1983-04-22 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
US20020134887A1 (en) * 2001-03-22 2002-09-26 Hersheng Lin Ballistic shield for dual engine single output shaft propulsion system

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See also references of EP2129876A2 *

Also Published As

Publication number Publication date
US20100101205A1 (en) 2010-04-29
WO2008135699A2 (fr) 2008-11-13
EP2129876A2 (fr) 2009-12-09
FR2914362B1 (fr) 2012-07-27
CA2681365A1 (fr) 2008-11-13
BRPI0808617A2 (pt) 2014-09-16
CN101652536A (zh) 2010-02-17
RU2009140136A (ru) 2011-05-10
JP2010523863A (ja) 2010-07-15
CN101652536B (zh) 2012-12-26
FR2914362A1 (fr) 2008-10-03

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