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FR2951436B1 - Mat d'accrochage de turbomoteur d'aeronef a canalisations d'air chaud concentriques - Google Patents

Mat d'accrochage de turbomoteur d'aeronef a canalisations d'air chaud concentriques

Info

Publication number
FR2951436B1
FR2951436B1 FR0957239A FR0957239A FR2951436B1 FR 2951436 B1 FR2951436 B1 FR 2951436B1 FR 0957239 A FR0957239 A FR 0957239A FR 0957239 A FR0957239 A FR 0957239A FR 2951436 B1 FR2951436 B1 FR 2951436B1
Authority
FR
France
Prior art keywords
turbohomoter
aircraft
hot air
handling machine
air piping
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.)
Active
Application number
FR0957239A
Other languages
English (en)
Other versions
FR2951436A1 (fr
Inventor
Lionel Diochon
Yann Murer
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
Application filed by Airbus Operations SAS filed Critical Airbus Operations SAS
Priority to FR0957239A priority Critical patent/FR2951436B1/fr
Priority to US12/892,374 priority patent/US8459588B2/en
Publication of FR2951436A1 publication Critical patent/FR2951436A1/fr
Application granted granted Critical
Publication of FR2951436B1 publication Critical patent/FR2951436B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • B64D15/00—De-icing or preventing icing on exterior surfaces of aircraft
    • B64D15/02—De-icing or preventing icing on exterior surfaces of aircraft by ducted hot gas or liquid
    • B64D15/04—Hot gas application
    • 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
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02—Aircraft characterised by the type or position of power plants
    • B64D27/10—Aircraft characterised by the type or position of power plants of gas-turbine type 
    • B64D27/14—Aircraft characterised by the type or position of power plants of gas-turbine type  within, or attached to, fuselages
    • 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
    • B64D29/04—Power-plant nacelles, fairings or cowlings associated with fuselages
    • 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
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D2027/005—Aircraft with an unducted turbofan comprising contra-rotating rotors, e.g. contra-rotating open rotors [CROR]
    • 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
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02—Aircraft characterised by the type or position of power plants
    • B64D27/026—Aircraft characterised by the type or position of power plants comprising different types of power plants, e.g. combination of a piston engine and a gas-turbine
    • 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
    • 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
    • Y10T137/8593—Systems
    • Y10T137/85938—Non-valved flow dividers

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR0957239A 2009-10-15 2009-10-15 Mat d'accrochage de turbomoteur d'aeronef a canalisations d'air chaud concentriques Active FR2951436B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR0957239A FR2951436B1 (fr) 2009-10-15 2009-10-15 Mat d'accrochage de turbomoteur d'aeronef a canalisations d'air chaud concentriques
US12/892,374 US8459588B2 (en) 2009-10-15 2010-09-28 Attachment pylon for an aircraft turbo-shaft engine with concentric hot air channels

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0957239A FR2951436B1 (fr) 2009-10-15 2009-10-15 Mat d'accrochage de turbomoteur d'aeronef a canalisations d'air chaud concentriques

Publications (2)

Publication Number Publication Date
FR2951436A1 FR2951436A1 (fr) 2011-04-22
FR2951436B1 true FR2951436B1 (fr) 2011-12-09

Family

ID=42144935

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0957239A Active FR2951436B1 (fr) 2009-10-15 2009-10-15 Mat d'accrochage de turbomoteur d'aeronef a canalisations d'air chaud concentriques

Country Status (2)

Country Link
US (1) US8459588B2 (fr)
FR (1) FR2951436B1 (fr)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2959209B1 (fr) * 2010-04-27 2013-03-29 Airbus Operations Sas Mat de support de turbomachine pour aeronef
EP2785590B1 (fr) * 2011-11-29 2016-06-08 Short Brothers Plc Système et procédé de refroidissement d'un aile d'aéronef
WO2015010315A1 (fr) 2013-07-26 2015-01-29 Mra Systems, Inc. Mât d'accrochage de moteur pour aéronef
US10393020B2 (en) * 2015-08-26 2019-08-27 Rohr, Inc. Injector nozzle configuration for swirl anti-icing system
JP2017136893A (ja) * 2016-02-01 2017-08-10 三菱航空機株式会社 防氷装置、及び、航空機
US11203437B2 (en) 2016-06-30 2021-12-21 Bombardier Inc. Assembly and method for conditioning engine-heated air onboard an aircraft

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB485395A (en) * 1936-12-03 1938-05-19 John Carr Brookfield Means for preventing the formation of ice on the wings and/or fuselage of aircraft
US2393792A (en) * 1942-08-28 1946-01-29 Mccollum Thelma Heating apparatus
IL78786A0 (en) * 1985-06-03 1986-08-31 Short Brothers Plc Duct for hot air
US4783026A (en) * 1987-05-22 1988-11-08 Avco Corporation Anti-icing management system
US4976396A (en) * 1987-11-13 1990-12-11 The Boeing Company Aircraft configuration with aft mounted engines
US5011098A (en) * 1988-12-30 1991-04-30 The Boeing Company Thermal anti-icing system for aircraft
US5841079A (en) * 1997-11-03 1998-11-24 Northrop Grumman Corporation Combined acoustic and anti-ice engine inlet liner
FR2820716B1 (fr) * 2001-02-15 2003-05-30 Eads Airbus Sa Procede de degivrage par circulation forcee d'un fluide, d'un capot d'entree d'air de moteur a reaction et dispositif pour sa mise en oeuvre
FR2820715B1 (fr) * 2001-02-15 2003-05-30 Eads Airbus Sa Procede de degivrage d'un capot d'entree d'air de moteur a reaction et dispositif pour sa mise en oeuvre
US6698687B2 (en) * 2002-02-13 2004-03-02 The Boeing Company Aircraft wing heat exchanger apparatus and method
US7975966B2 (en) * 2008-02-04 2011-07-12 Embraer - Empresa Brasileira De Aeronautica S.A. Icing protection for aircraft air inlet scoops

Also Published As

Publication number Publication date
US8459588B2 (en) 2013-06-11
US20110108662A1 (en) 2011-05-12
FR2951436A1 (fr) 2011-04-22

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