DE602005003294D1 - Turbinenstrahltriebwerk mit einem einteiligen Arm zur Verbindung von Hilfskomponenten - Google Patents

Turbinenstrahltriebwerk mit einem einteiligen Arm zur Verbindung von Hilfskomponenten

Info

Publication number
DE602005003294D1
DE602005003294D1 DE602005003294T DE602005003294T DE602005003294D1 DE 602005003294 D1 DE602005003294 D1 DE 602005003294D1 DE 602005003294 T DE602005003294 T DE 602005003294T DE 602005003294 T DE602005003294 T DE 602005003294T DE 602005003294 D1 DE602005003294 D1 DE 602005003294D1
Authority
DE
Germany
Prior art keywords
jet engine
auxiliary components
turbine jet
connecting auxiliary
piece arm
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
DE602005003294T
Other languages
English (en)
Other versions
DE602005003294T2 (de
Inventor
Johnny Letache
Pierre Gagneux
Lionel Jean Lefranc
Joseph Taglialavore
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
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 SNECMA SAS filed Critical SNECMA SAS
Publication of DE602005003294D1 publication Critical patent/DE602005003294D1/de
Application granted granted Critical
Publication of DE602005003294T2 publication Critical patent/DE602005003294T2/de
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • 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
    • F01D25/16—Arrangement of bearings; Supporting or mounting bearings in casings
    • F01D25/162—Bearing supports
    • 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
    • F01D9/00—Stators
    • F01D9/06—Fluid supply conduits to nozzles or the like
    • F01D9/065—Fluid supply or removal conduits traversing the working fluid flow, e.g. for lubrication-, cooling-, or sealing fluids
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
    • F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Cylinder Crankcases Of Internal Combustion Engines (AREA)
DE602005003294T 2004-09-27 2005-09-26 Turbinenstrahltriebwerk mit einem einteiligen Arm zur Verbindung von Hilfskomponenten Active DE602005003294T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0452174A FR2875855B1 (fr) 2004-09-27 2004-09-27 Turboreacteur avec un bras monobloc de raccord de servitudes et le bras monobloc de raccord de servitudes
FR0452174 2004-09-27

Publications (2)

Publication Number Publication Date
DE602005003294D1 true DE602005003294D1 (de) 2007-12-27
DE602005003294T2 DE602005003294T2 (de) 2008-09-11

Family

ID=34952105

Family Applications (1)

Application Number Title Priority Date Filing Date
DE602005003294T Active DE602005003294T2 (de) 2004-09-27 2005-09-26 Turbinenstrahltriebwerk mit einem einteiligen Arm zur Verbindung von Hilfskomponenten

Country Status (8)

Country Link
US (1) US7661272B2 (de)
EP (1) EP1640591B1 (de)
JP (1) JP2006097680A (de)
CN (1) CN100560958C (de)
CA (1) CA2520464C (de)
DE (1) DE602005003294T2 (de)
FR (1) FR2875855B1 (de)
RU (1) RU2358137C2 (de)

Families Citing this family (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2925120B1 (fr) * 2007-12-18 2010-02-19 Snecma Extension de carter intermediaire pour turboreacteur d'aeronef, comprenant une rainure annulaire sectorisee de reception des capots de nacelle
FR2936556B1 (fr) * 2008-09-30 2015-07-24 Snecma Systeme de commande d'equipements a geometrie variable d'une turbomachine, notamment par guignols.
CH703309A1 (de) 2010-06-10 2011-12-15 Alstom Technology Ltd Abgasgehäuse für eine gasturbine sowie verfahren zum herstellen eines solchen abgasgehäuses.
US20130042630A1 (en) * 2011-08-19 2013-02-21 United Technologies Corporation Gas turbine engine accessory mount
GB2498006B (en) 2011-12-22 2014-07-09 Rolls Royce Plc Gas turbine engine systems
GB2497807B (en) 2011-12-22 2014-09-10 Rolls Royce Plc Electrical harness
GB2497809B (en) * 2011-12-22 2014-03-12 Rolls Royce Plc Method of servicing a gas turbine engine
US9478896B2 (en) 2011-12-22 2016-10-25 Rolls-Royce Plc Electrical connectors
FR3001498B1 (fr) * 2013-01-30 2015-02-27 Snecma Partie fixe de recepteur de turbomachine comprenant un ensemble de maintien en position de servitudes a l'interieur d'un arbre creux fixe
GB201306482D0 (en) * 2013-04-10 2013-05-22 Rolls Royce Plc Mounting arrangement
FR3005992B1 (fr) * 2013-05-24 2015-05-22 Snecma Dispositif de passage de servitudes pour une turbomachine
FR3015625B1 (fr) * 2013-12-20 2015-12-11 Snecma Bras de guidage d'elements de forme allongee, en particulier pour une turbomachine
JP6118721B2 (ja) * 2013-12-20 2017-04-19 株式会社Ihi ファンケース及びファンケースの製造方法
FR3051014B1 (fr) * 2016-05-09 2018-05-18 Safran Aircraft Engines Ensemble pour turbomachine comprenant un distributeur, un element de structure de turbomachine, et un dispositif de fixation
FR3052488B1 (fr) * 2016-06-14 2018-05-25 Safran Aircraft Engines Carter d'echappement de turbomachine
DE102016215030A1 (de) * 2016-08-11 2018-02-15 Rolls-Royce Deutschland Ltd & Co Kg Turbofan-Triebwerk mit einer im Sekundärstromkanal liegenden und ein separates Abschlusselement aufweisenden Verkleidung
US10727656B2 (en) * 2017-11-08 2020-07-28 Raytheon Technologies Corporation Igniter cable conduit for gas turbine engine
US11230995B2 (en) 2017-11-08 2022-01-25 Raytheon Technologies Corporation Cable conduit for turbine engine bypass
FR3077846B1 (fr) * 2018-02-14 2020-03-13 Safran Aircraft Engines Virole exterieure de carter intermediaire pour turbomachine d'aeronef a double flux, comprenant des dispositifs ameliores d'etancheite a l'air et de resistance au feu
GB201820505D0 (en) * 2018-12-17 2019-01-30 Rolls Royce Connector system
FR3096743B1 (fr) * 2019-05-28 2021-05-07 Safran Aircraft Engines Paroi coupe-feu et procédé d’ouverture de celle-ci
FR3117173A1 (fr) 2020-12-09 2022-06-10 Safran Aircraft Engines Ensemble propulsif d’aéronef et procédé d’adaptation d’un ensemble propulsif

Family Cites Families (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2392239A1 (fr) * 1976-08-30 1978-12-22 Snecma Systeme de propulsion pour avion supersonique
JPS58107948U (ja) * 1982-01-19 1983-07-22 井関農機株式会社 油圧取出部の構造
US4618419A (en) * 1984-07-19 1986-10-21 Clive Hollinshead Liquid storage tank moisture filter
FR2631386A1 (fr) * 1988-05-11 1989-11-17 Snecma Turbomachine comportant une grille d'entree incorporant des tubes de passage d'huile
US4987736A (en) * 1988-12-14 1991-01-29 General Electric Company Lightweight gas turbine engine frame with free-floating heat shield
US5136837A (en) * 1990-03-06 1992-08-11 General Electric Company Aircraft engine starter integrated boundary bleed system
US5174110A (en) * 1991-10-17 1992-12-29 United Technologies Corporation Utility conduit enclosure for turbine engine
EP0550126A1 (de) * 1992-01-02 1993-07-07 General Electric Company Hitzeschild für Nachbrenner
US5292227A (en) * 1992-12-10 1994-03-08 General Electric Company Turbine frame
DE4404879C2 (de) * 1994-02-17 1997-04-10 Technoflow Tube Systems Gmbh Werkmäßig vorgefertigtes Fluidleitungssystem, welches zur Montage in ein Kraftfahrzeug im Zuge der automatischen Bandfertigung von typisierten Kraftfahrzeugen eingerichtet ist
CA2160647C (en) * 1995-10-16 2002-05-28 Thomas William Garay Helical bearing anchor catcher
JP3129658B2 (ja) * 1996-04-26 2001-01-31 本田技研工業株式会社 自動車の加圧燃料配管構造およびその配管漏れ検査方法
JPH10118219A (ja) * 1996-08-28 1998-05-12 Mitsui Chem Inc スプリンクラー用配管と、その施工法
US5746574A (en) * 1997-05-27 1998-05-05 General Electric Company Low profile fluid joint
US6439841B1 (en) * 2000-04-29 2002-08-27 General Electric Company Turbine frame assembly
US6358001B1 (en) * 2000-04-29 2002-03-19 General Electric Company Turbine frame assembly
JP4611512B2 (ja) * 2000-12-19 2011-01-12 本田技研工業株式会社 航空機用ガスタービン・エンジンのファンダクト構造
DE10148874C2 (de) * 2001-10-04 2003-12-24 Siemens Ag Düseneinrichtung, insbesondere zur Kraftstoffeinspritzung
US7370467B2 (en) * 2003-07-29 2008-05-13 Pratt & Whitney Canada Corp. Turbofan case and method of making
FR2865002B1 (fr) * 2004-01-12 2006-05-05 Snecma Moteurs Turboreacteur a double flux comprenant un support de distribution de servitudes et le support de distribution de servitudes.

Also Published As

Publication number Publication date
RU2005129854A (ru) 2007-04-10
RU2358137C2 (ru) 2009-06-10
EP1640591A1 (de) 2006-03-29
CN100560958C (zh) 2009-11-18
FR2875855B1 (fr) 2006-12-22
US7661272B2 (en) 2010-02-16
CN1782346A (zh) 2006-06-07
DE602005003294T2 (de) 2008-09-11
CA2520464A1 (fr) 2006-03-27
US20070234706A1 (en) 2007-10-11
FR2875855A1 (fr) 2006-03-31
CA2520464C (fr) 2012-04-03
JP2006097680A (ja) 2006-04-13
EP1640591B1 (de) 2007-11-14

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