FR3009339B1 - Turbomachine comprenant un dispositif de refroidissement du pylone - Google Patents

Turbomachine comprenant un dispositif de refroidissement du pylone Download PDF

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Publication number
FR3009339B1
FR3009339B1 FR1357534A FR1357534A FR3009339B1 FR 3009339 B1 FR3009339 B1 FR 3009339B1 FR 1357534 A FR1357534 A FR 1357534A FR 1357534 A FR1357534 A FR 1357534A FR 3009339 B1 FR3009339 B1 FR 3009339B1
Authority
FR
France
Prior art keywords
pylon
turbomachine
cooling device
cooling
pylon cooling
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
FR1357534A
Other languages
English (en)
Other versions
FR3009339A1 (fr
Inventor
Matthieu LEYKO
Jean BERTUCCHI
Julien Szydlowski
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.)
Safran Aircraft Engines SAS
Original Assignee
Safran Aircraft Engines SAS
SNECMA 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 Safran Aircraft Engines SAS, SNECMA SAS filed Critical Safran Aircraft Engines SAS
Priority to FR1357534A priority Critical patent/FR3009339B1/fr
Priority to US14/446,552 priority patent/US9540109B2/en
Publication of FR3009339A1 publication Critical patent/FR3009339A1/fr
Application granted granted Critical
Publication of FR3009339B1 publication Critical patent/FR3009339B1/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
    • B64D13/00—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft
    • B64D13/006—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft the air being used to cool structural parts of the aircraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C7/00—Structures or fairings not otherwise provided for
    • B64C7/02—Nacelles
    • 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 
    • B64D27/12—Aircraft characterised by the type or position of power plants of gas-turbine type  within, or attached to, wings
    • 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
    • B64D27/40—Arrangements for mounting power plants in aircraft
    • 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
    • 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
    • B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/04—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of exhaust outlets or jet pipes
    • 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
    • B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/08—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of power plant cooling systems
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/20—Mounting or supporting of plant; Accommodating heat expansion or creep
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/78—Other construction of jet pipes
    • F02K1/82—Jet pipe walls, e.g. liners
    • F02K1/822—Heat insulating structures or liners, cooling arrangements, e.g. post combustion liners; Infrared radiation suppressors
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00—Function
    • F05D2260/20—Heat transfer, e.g. cooling
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00—Function
    • F05D2260/20—Heat transfer, e.g. cooling
    • F05D2260/231—Preventing heat transfer
    • 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)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Health & Medical Sciences (AREA)
  • General Health & Medical Sciences (AREA)
  • Pulmonology (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR1357534A 2013-07-30 2013-07-30 Turbomachine comprenant un dispositif de refroidissement du pylone Active FR3009339B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR1357534A FR3009339B1 (fr) 2013-07-30 2013-07-30 Turbomachine comprenant un dispositif de refroidissement du pylone
US14/446,552 US9540109B2 (en) 2013-07-30 2014-07-30 Turbomachine comprising a device for the cooling of a pylon

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1357534 2013-07-30
FR1357534A FR3009339B1 (fr) 2013-07-30 2013-07-30 Turbomachine comprenant un dispositif de refroidissement du pylone

Publications (2)

Publication Number Publication Date
FR3009339A1 FR3009339A1 (fr) 2015-02-06
FR3009339B1 true FR3009339B1 (fr) 2018-01-26

Family

ID=49326704

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1357534A Active FR3009339B1 (fr) 2013-07-30 2013-07-30 Turbomachine comprenant un dispositif de refroidissement du pylone

Country Status (2)

Country Link
US (1) US9540109B2 (fr)
FR (1) FR3009339B1 (fr)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3009339B1 (fr) * 2013-07-30 2018-01-26 Safran Aircraft Engines Turbomachine comprenant un dispositif de refroidissement du pylone
FR3045012B1 (fr) * 2015-12-11 2017-12-08 Airbus Operations Sas Mat d'accrochage d'une turbomachine muni d'un element de protection thermique
CA3028989A1 (fr) * 2016-06-30 2018-01-04 Bombardier Inc. Ensemble et procede de conditionnement d'air chauffe par moteur a bord d'un aeronef
US20180100468A1 (en) * 2016-10-07 2018-04-12 Rolls-Royce North American Technologies Inc. System and method for reduction of turbine exhaust gas impingement on adjacent aircraft structure
FR3101670B1 (fr) * 2019-10-08 2021-10-08 Safran Aircraft Engines Injecteur pour une turbine haute pression
CN117823281B (zh) * 2024-03-06 2024-06-04 中国空气动力研究与发展中心空天技术研究所 一种品字形排列的多通道宽速域可调进气道

Family Cites Families (26)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4712750A (en) * 1986-05-02 1987-12-15 The Boeing Company Temperature control device for jet engine nacelle associated structure
US4825648A (en) * 1987-03-02 1989-05-02 General Electric Company Turbofan engine having a split cowl
US5156353A (en) * 1987-04-13 1992-10-20 General Electric Company Aircraft pylon
US5012639A (en) * 1989-01-23 1991-05-07 United Technologies Corporation Buffer region for the nacelle of a gas turbine engine
US5887822A (en) * 1997-03-28 1999-03-30 The Boeing Company Segmented engine flow control device
US6554224B2 (en) * 2001-08-31 2003-04-29 The Boeing Company Out-of-plane thrust reverser sleeve lock
FR2920195B1 (fr) * 2007-08-23 2009-11-20 Snecma Turbomachine a double flux a reduction de bruit de jet
FR2930235B1 (fr) * 2008-04-21 2011-09-30 Airbus France Mat de suspension pour turbomoteur.
FR2931133B1 (fr) * 2008-05-14 2010-06-18 Airbus France Mat d'accrochage de moteur comprenant des moyens de fixation des longerons et des panneaux agences en dehors de l'espace interieur de caisson
FR2953490B1 (fr) * 2009-12-07 2012-02-24 Aircelle Sa Ensemble arriere de nacelle pour turboreacteur
US8869507B2 (en) * 2010-01-13 2014-10-28 United Technologies Corporation Translatable cascade thrust reverser
FR2956855B1 (fr) * 2010-02-26 2012-07-27 Snecma Dispositif de reduction du bruit de paroi sur les pylones des turboreacteurs
GB201011056D0 (en) * 2010-07-01 2010-08-18 Rolls Royce Plc Pylon for attaching a gas turbine engine
US9022311B2 (en) * 2010-08-20 2015-05-05 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Active aircraft pylon noise control system
FR2967398B1 (fr) * 2010-11-16 2012-11-02 Aircelle Sa Structure de renforcement d'une nacelle de turboreacteur
FR2973443B1 (fr) * 2011-03-30 2016-07-22 Snecma Capot primaire poreux pour turboreacteur
FR2977567B1 (fr) * 2011-07-07 2014-12-26 Airbus Operations Sas Procede de refroidissement d'un plancher de protection thermique d'un carenage aerodynamique arriere d'un mat d'accrochage d'un ensemble propulsif d'aeronef
FR2979613B1 (fr) * 2011-09-01 2014-06-13 Snecma Ensemble forme par un turbomoteur et son systeme d'attache a une structure d'aeronef
FR2980173B1 (fr) * 2011-09-16 2013-10-25 Aircelle Sa Ensemble arriere de nacelle pour turboreacteur
FR2983172B1 (fr) * 2011-11-25 2014-05-16 Airbus Operations Sas Carenage arriere pour mat d'accrochage d'un moteur
CA2854050C (fr) * 2011-11-29 2018-09-04 Short Brothers Plc Systeme et procede de refroidissement d'une aile d'avion
US9303590B2 (en) * 2012-05-22 2016-04-05 Spirit Aerosystems, Inc. Variable area fan nozzle actuation system
EP2938845A4 (fr) * 2012-12-29 2016-01-13 United Technologies Corp Architecture de carter de sortie de turbine
WO2014105781A1 (fr) * 2012-12-29 2014-07-03 United Technologies Corporation Trous de refroidissement de montant de châssis
FR3009339B1 (fr) * 2013-07-30 2018-01-26 Safran Aircraft Engines Turbomachine comprenant un dispositif de refroidissement du pylone
FR3020798B1 (fr) * 2014-05-09 2017-12-22 Airbus Operations Sas Ensemble propulsif pour aeronef comprenant un conduit formant barriere thermique integre au caisson de la structure rigide du mat d'accrochage

Also Published As

Publication number Publication date
US9540109B2 (en) 2017-01-10
FR3009339A1 (fr) 2015-02-06
US20150284098A1 (en) 2015-10-08

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