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FR2986829B1 - Piece de support de turbomachine a structure hybride - Google Patents

Piece de support de turbomachine a structure hybride

Info

Publication number
FR2986829B1
FR2986829B1 FR1251198A FR1251198A FR2986829B1 FR 2986829 B1 FR2986829 B1 FR 2986829B1 FR 1251198 A FR1251198 A FR 1251198A FR 1251198 A FR1251198 A FR 1251198A FR 2986829 B1 FR2986829 B1 FR 2986829B1
Authority
FR
France
Prior art keywords
support piece
hybrid structure
turbomachine support
turbomachine
hybrid
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
FR1251198A
Other languages
English (en)
Other versions
FR2986829A1 (fr
Inventor
Robin Mandel
Wouter Balk
Nicolas Christian Raymond Leblond
Jean-Yves Picart
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
Safran SA
Original Assignee
Safran SA
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 SA, SNECMA SAS filed Critical Safran SA
Priority to FR1251198A priority Critical patent/FR2986829B1/fr
Priority to US14/377,644 priority patent/US20150021455A1/en
Priority to PCT/FR2013/050239 priority patent/WO2013117853A1/fr
Priority to GB1413896.0A priority patent/GB2513274A/en
Publication of FR2986829A1 publication Critical patent/FR2986829A1/fr
Application granted granted Critical
Publication of FR2986829B1 publication Critical patent/FR2986829B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • 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
    • F02C7/32—Arrangement, mounting, or driving, of auxiliaries
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16L—PIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
    • F16L3/00—Supports for pipes, cables or protective tubing, e.g. hangers, holders, clamps, cleats, clips, brackets
    • F16L3/08—Supports for pipes, cables or protective tubing, e.g. hangers, holders, clamps, cleats, clips, brackets substantially surrounding the pipe, cable or protective tubing
    • F16L3/12—Supports for pipes, cables or protective tubing, e.g. hangers, holders, clamps, cleats, clips, brackets substantially surrounding the pipe, cable or protective tubing comprising a member substantially surrounding the pipe, cable or protective tubing
    • F16L3/123—Supports for pipes, cables or protective tubing, e.g. hangers, holders, clamps, cleats, clips, brackets substantially surrounding the pipe, cable or protective tubing comprising a member substantially surrounding the pipe, cable or protective tubing and extending along the attachment surface
    • 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
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/28—Supporting or mounting arrangements, e.g. for turbine casing
    • 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
    • F02C7/24—Heat or noise insulation
    • F02C7/25—Fire protection or prevention
    • 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
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/60—Properties or characteristics given to material by treatment or manufacturing
    • F05D2300/603—Composites; e.g. fibre-reinforced

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR1251198A 2012-02-09 2012-02-09 Piece de support de turbomachine a structure hybride Active FR2986829B1 (fr)

Priority Applications (4)

Application Number Priority Date Filing Date Title
FR1251198A FR2986829B1 (fr) 2012-02-09 2012-02-09 Piece de support de turbomachine a structure hybride
US14/377,644 US20150021455A1 (en) 2012-02-09 2013-02-05 Turbine engine support part of hybrid structure
PCT/FR2013/050239 WO2013117853A1 (fr) 2012-02-09 2013-02-05 Pièce de support de turbomachine a structure hybride
GB1413896.0A GB2513274A (en) 2012-02-09 2013-02-05 Turbomachine supporting part having a hybrid structure

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1251198A FR2986829B1 (fr) 2012-02-09 2012-02-09 Piece de support de turbomachine a structure hybride

Publications (2)

Publication Number Publication Date
FR2986829A1 FR2986829A1 (fr) 2013-08-16
FR2986829B1 true FR2986829B1 (fr) 2014-03-21

Family

ID=47754824

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1251198A Active FR2986829B1 (fr) 2012-02-09 2012-02-09 Piece de support de turbomachine a structure hybride

Country Status (4)

Country Link
US (1) US20150021455A1 (fr)
FR (1) FR2986829B1 (fr)
GB (1) GB2513274A (fr)
WO (1) WO2013117853A1 (fr)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10202869B2 (en) * 2013-08-22 2019-02-12 United Technologies Corporation Connection for a fairing in a mid-turbine frame of a gas turbine engine
KR102195891B1 (ko) * 2015-05-29 2020-12-28 코오롱인더스트리 주식회사 연료 전지용 캐소드 촉매층, 이의 제조 방법 및 이를 포함하는 연료 전지용 막-전극 어셈블리
US10690267B2 (en) * 2018-07-16 2020-06-23 Raytheon Technologies Corporation Adjustable holding assembly

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2922733A (en) * 1955-02-04 1960-01-26 Richard A Henning Cushion liner for a clamp operable at extreme temperatures
ATE199107T1 (de) * 1997-06-14 2001-02-15 Hilti Ag Einlage für eine rohrschelle
US8104736B2 (en) * 2005-12-01 2012-01-31 Hamilton Sundstrand Corporation Gas turbine engine auxiliary component mount
FR2905981B1 (fr) * 2006-09-15 2008-10-24 Renault Sas Support de turbocompresseur
CN200965140Y (zh) * 2006-10-23 2007-10-24 余雪萍 强化支架
US8201309B1 (en) * 2007-07-30 2012-06-19 Franta John E Attachment hardware
FR2944850B1 (fr) * 2009-04-24 2014-12-26 Snecma Support monobloc d'equipements en aeronautique.
FR2952853B1 (fr) * 2009-11-25 2012-01-13 Corima Roue composite, notamment pour un cycle, et procede de fabrication d'une telle roue
FR2978809B1 (fr) * 2011-08-05 2013-09-06 Safran Ferrure et procede et outillage pour sa production
US20130119191A1 (en) * 2011-11-10 2013-05-16 General Electric Company Load-bearing structures for aircraft engines and processes therefor

Also Published As

Publication number Publication date
WO2013117853A1 (fr) 2013-08-15
GB201413896D0 (en) 2014-09-17
FR2986829A1 (fr) 2013-08-16
US20150021455A1 (en) 2015-01-22
GB2513274A (en) 2014-10-22

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Legal Events

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PLFP Fee payment

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CD Change of name or company name

Owner name: SAFRAN, FR

Effective date: 20170719

Owner name: SAFRAN AIRCRAFT ENGINES, FR

Effective date: 20170719

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Year of fee payment: 9

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