FR2959209B1 - Mat de support de turbomachine pour aeronef - Google Patents

Mat de support de turbomachine pour aeronef

Info

Publication number
FR2959209B1
FR2959209B1 FR1053200A FR1053200A FR2959209B1 FR 2959209 B1 FR2959209 B1 FR 2959209B1 FR 1053200 A FR1053200 A FR 1053200A FR 1053200 A FR1053200 A FR 1053200A FR 2959209 B1 FR2959209 B1 FR 2959209B1
Authority
FR
France
Prior art keywords
aircraft
support mat
turbomachine support
turbomachine
mat
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
FR1053200A
Other languages
English (en)
Other versions
FR2959209A1 (fr
Inventor
Christelle Rinjonneau
Pierre Guillaume
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 FR1053200A priority Critical patent/FR2959209B1/fr
Priority to US13/094,363 priority patent/US8714477B2/en
Publication of FR2959209A1 publication Critical patent/FR2959209A1/fr
Application granted granted Critical
Publication of FR2959209B1 publication Critical patent/FR2959209B1/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
    • 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
    • B64D33/10—Radiator arrangement
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28—HEAT EXCHANGE IN GENERAL
    • F28D—HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
    • F28D21/00—Heat-exchange apparatus not covered by any of the groups F28D1/00 - F28D20/00
    • F28D2021/0019—Other heat exchangers for particular applications; Heat exchange systems not otherwise provided for
    • F28D2021/0021—Other heat exchangers for particular applications; Heat exchange systems not otherwise provided for for aircrafts or cosmonautics

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR1053200A 2010-04-27 2010-04-27 Mat de support de turbomachine pour aeronef Active FR2959209B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR1053200A FR2959209B1 (fr) 2010-04-27 2010-04-27 Mat de support de turbomachine pour aeronef
US13/094,363 US8714477B2 (en) 2010-04-27 2011-04-26 Turbomachine support pylon for aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1053200A FR2959209B1 (fr) 2010-04-27 2010-04-27 Mat de support de turbomachine pour aeronef

Publications (2)

Publication Number Publication Date
FR2959209A1 FR2959209A1 (fr) 2011-10-28
FR2959209B1 true FR2959209B1 (fr) 2013-03-29

Family

ID=43410727

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1053200A Active FR2959209B1 (fr) 2010-04-27 2010-04-27 Mat de support de turbomachine pour aeronef

Country Status (2)

Country Link
US (1) US8714477B2 (fr)
FR (1) FR2959209B1 (fr)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20110182723A1 (en) * 2010-01-26 2011-07-28 Airbus Operations (S.A.S) Turbomachine aircraft propeller
FR2968634B1 (fr) * 2010-12-08 2013-08-02 Snecma Pylone de fixation d'un moteur d'aeronef a helices propulsives non carenees
EP2789518B9 (fr) * 2011-12-09 2019-12-25 Mitsubishi Electric Corporation Dispositif de refroidissement pour dispositif sous-plancher pour véhicule
CA2918320C (fr) 2013-07-26 2018-05-15 Mra Systems, Inc. Mat d'accrochage de moteur pour aeronef
US10907500B2 (en) * 2015-02-06 2021-02-02 Raytheon Technologies Corporation Heat exchanger system with spatially varied additively manufactured heat transfer surfaces
FR3037318B1 (fr) * 2015-06-15 2017-06-30 Snecma Ensemble propulsif pour aeronef comprenant un turboreacteur a soufflante non carenee et un pylone d'accrochage
FR3050781A1 (fr) * 2016-04-27 2017-11-03 Airbus Operations Sas Dispositif de reduction des perturbations aerodynamiques dans le sillage d'un profil aerodynamique par soufflage a repartition variable a l'extrados et l'intrados
FR3050721B1 (fr) * 2016-04-28 2018-04-13 Airbus Operations Ensemble moteur pour aeronef comprenant un bord d'attaque de mat integre a une rangee annulaire d'aubes directrices de sortie non carenees
FR3097257B1 (fr) * 2019-06-17 2021-07-02 Sogeclair Sa Echangeur thermique de refroidissement d'un moteur propulsif d'aéronef.

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR748657A (fr) * 1932-03-30 1933-07-07 Aeronautique Soc Gen Perfectionnements aux radiateurs d'ailes
US3783935A (en) * 1972-05-30 1974-01-08 United Aircraft Prod Surface cooler
US5156353A (en) 1987-04-13 1992-10-20 General Electric Company Aircraft pylon
US5149018A (en) * 1990-05-17 1992-09-22 The Boeing Company Cooling system for a hypersonic aircraft
US5123242A (en) * 1990-07-30 1992-06-23 General Electric Company Precooling heat exchange arrangement integral with mounting structure fairing of gas turbine engine
FR2742479B1 (fr) * 1995-12-13 1998-01-16 Snecma Dispositif de refroidissement d'un turbomoteur sur aeronef
FR2839948B1 (fr) * 2002-05-22 2004-12-17 Airbus France Echangeur pour circuit de conditionnement d'air d'aeronef et ensemble de propulsion integrant un tel echangeur
GB2413366B (en) * 2004-04-24 2006-09-13 Rolls Royce Plc Engine.
FR2889298B1 (fr) * 2005-07-28 2010-11-26 Airbus France Echangeur thermique, ensemble propulseur, et aeronef comportant un tel ensemble propulseur
FR2891248B1 (fr) * 2005-09-28 2009-05-01 Airbus France Sas Ensemble moteur pour aeronef comprenant un moteur ainsi qu'un mat d'accrochage d'un tel moteur
GB2473651B (en) * 2009-09-21 2011-08-31 Rolls Royce Plc Gas turbine aircraft engines and operation thereof
FR2951436B1 (fr) * 2009-10-15 2011-12-09 Airbus Operations Sas Mat d'accrochage de turbomoteur d'aeronef a canalisations d'air chaud concentriques
EP2472067B1 (fr) * 2010-12-31 2013-09-25 Techspace Aero S.A. Intégration d'un échangeur de chaleur surfacique avec débit d'air régulé dans un moteur d'avion

Also Published As

Publication number Publication date
FR2959209A1 (fr) 2011-10-28
US20110315813A1 (en) 2011-12-29
US8714477B2 (en) 2014-05-06

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