FR3045012B1 - Mat d'accrochage d'une turbomachine muni d'un element de protection thermique - Google Patents

Mat d'accrochage d'une turbomachine muni d'un element de protection thermique

Info

Publication number
FR3045012B1
FR3045012B1 FR1562179A FR1562179A FR3045012B1 FR 3045012 B1 FR3045012 B1 FR 3045012B1 FR 1562179 A FR1562179 A FR 1562179A FR 1562179 A FR1562179 A FR 1562179A FR 3045012 B1 FR3045012 B1 FR 3045012B1
Authority
FR
France
Prior art keywords
turbomachine
protection element
thermal protection
mat
attaching
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
FR1562179A
Other languages
English (en)
Other versions
FR3045012A1 (fr
Inventor
Yann Queau
Camille Chaper
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 FR1562179A priority Critical patent/FR3045012B1/fr
Priority to CN201611118466.7A priority patent/CN107010235A/zh
Priority to US15/375,474 priority patent/US20170166317A1/en
Publication of FR3045012A1 publication Critical patent/FR3045012A1/fr
Application granted granted Critical
Publication of FR3045012B1 publication Critical patent/FR3045012B1/fr
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • 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
    • B64C—AEROPLANES; HELICOPTERS
    • B64C23/00—Influencing air flow over aircraft surfaces, not otherwise provided for
    • B64C23/06—Influencing air flow over aircraft surfaces, not otherwise provided for by generating vortices
    • 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
    • B64D27/16—Aircraft characterised by the type or position of power plants of jet type
    • B64D27/18—Aircraft characterised by the type or position of power plants of jet 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
    • 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
    • B64D27/402—Arrangements for mounting power plants in aircraft comprising box like supporting frames, e.g. pylons or arrangements for embracing the power plant
    • 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
    • B64D29/02—Power-plant nacelles, fairings or cowlings associated with 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
    • B64D33/00—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/04—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of exhaust outlets or jet pipes
    • 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
    • Y02T50/10—Drag reduction

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Connection Of Plates (AREA)
FR1562179A 2015-12-11 2015-12-11 Mat d'accrochage d'une turbomachine muni d'un element de protection thermique Expired - Fee Related FR3045012B1 (fr)

Priority Applications (3)

Application Number Priority Date Filing Date Title
FR1562179A FR3045012B1 (fr) 2015-12-11 2015-12-11 Mat d'accrochage d'une turbomachine muni d'un element de protection thermique
CN201611118466.7A CN107010235A (zh) 2015-12-11 2016-12-07 用于涡轮机的设置有热保护元件的支承挂架
US15/375,474 US20170166317A1 (en) 2015-12-11 2016-12-12 Support pylon for a turbomachine, provided with a thermal protection element

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1562179A FR3045012B1 (fr) 2015-12-11 2015-12-11 Mat d'accrochage d'une turbomachine muni d'un element de protection thermique

Publications (2)

Publication Number Publication Date
FR3045012A1 FR3045012A1 (fr) 2017-06-16
FR3045012B1 true FR3045012B1 (fr) 2017-12-08

Family

ID=55361736

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1562179A Expired - Fee Related FR3045012B1 (fr) 2015-12-11 2015-12-11 Mat d'accrochage d'une turbomachine muni d'un element de protection thermique

Country Status (3)

Country Link
US (1) US20170166317A1 (fr)
CN (1) CN107010235A (fr)
FR (1) FR3045012B1 (fr)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2578447A (en) * 2018-10-26 2020-05-13 Airbus Operations Ltd Aircraft assembly with a hot-air exhaust outlet
GB2591471A (en) * 2020-01-28 2021-08-04 Airbus Operations Ltd Flow control device actuation
FR3121428B1 (fr) * 2021-04-02 2025-07-11 Airbus Operations Sas Mât réacteur d’aéronef comportant un ensemble mobile de capots

Family Cites Families (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6427948B1 (en) * 2000-10-30 2002-08-06 Michael Campbell Controllable vortex generator
US7802752B2 (en) * 2002-03-20 2010-09-28 The Regents Of The University Of California Jet engine noise suppressor
BRPI0613492A2 (pt) * 2005-06-30 2011-01-11 Bell Helicopter Textron Inc gerador de vórtice retrátil
WO2007077620A1 (fr) * 2005-12-28 2007-07-12 National University Corporation Nagoya University Generateur de tourbillon intelligent, et aeronef, bateaux, et machines rotative associes
FR2905930B1 (fr) * 2006-09-18 2009-05-15 Airbus France Sa Generateur de tourbillon en sortie de gaz chauds
US7753316B2 (en) * 2007-04-27 2010-07-13 The Boeing Company Deployable flap edge fence
AU2009243923B2 (en) * 2008-05-07 2015-04-30 Entecho Pty Ltd Fluid dynamic device with thrust control shroud
US8087617B2 (en) * 2008-08-15 2012-01-03 The Boeing Company Retractable nacelle chine
DE102009003084B4 (de) * 2009-05-13 2013-03-14 Airbus Operations Gmbh Verkleidung für eine Auftriebshilfe
FR2952349B1 (fr) * 2009-11-06 2012-02-17 Airbus Operations Sas Procede de fabrication d'un mat reacteur equipe d'un generateur de tourbillons
FR2956855B1 (fr) * 2010-02-26 2012-07-27 Snecma Dispositif de reduction du bruit de paroi sur les pylones des turboreacteurs
US20130255796A1 (en) * 2012-03-30 2013-10-03 General Electric Company Flow-control device, component having a flow-control device, and method of producing a flow-control device
US9080820B2 (en) * 2012-05-22 2015-07-14 The Boeing Company Heat dissipation switch
US9493228B2 (en) * 2012-11-28 2016-11-15 The Boeing Company High heat transfer rate reusable thermal protection system
US10290879B2 (en) * 2012-12-05 2019-05-14 Intelligent Energy Limited Microvalve
US9638176B2 (en) * 2013-05-10 2017-05-02 The Boeing Company Vortex generator using shape memory alloys
FR3009339B1 (fr) * 2013-07-30 2018-01-26 Safran Aircraft Engines Turbomachine comprenant un dispositif de refroidissement du pylone
US9277789B2 (en) * 2013-09-10 2016-03-08 Texas Instruments Incorporated Current, temperature or electromagnetic field actuated fasteners
US9789956B2 (en) * 2014-09-19 2017-10-17 The Boeing Company Vortex generators responsive to ambient conditions

Also Published As

Publication number Publication date
FR3045012A1 (fr) 2017-06-16
CN107010235A (zh) 2017-08-04
US20170166317A1 (en) 2017-06-15

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