DE602005009982D1 - Verteilungsträger der Dienstrohre eines Mantelstromtriebwerks - Google Patents

Verteilungsträger der Dienstrohre eines Mantelstromtriebwerks

Info

Publication number
DE602005009982D1
DE602005009982D1 DE602005009982T DE602005009982T DE602005009982D1 DE 602005009982 D1 DE602005009982 D1 DE 602005009982D1 DE 602005009982 T DE602005009982 T DE 602005009982T DE 602005009982 T DE602005009982 T DE 602005009982T DE 602005009982 D1 DE602005009982 D1 DE 602005009982D1
Authority
DE
Germany
Prior art keywords
turbofan engine
service pipes
distribution carrier
carrier
distribution
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
DE602005009982T
Other languages
English (en)
Inventor
Jeremy Fert
Georges Mazeaud
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 DE602005009982D1 publication Critical patent/DE602005009982D1/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
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Automatic Cycles, And Cycles In General (AREA)
DE602005009982T 2004-01-12 2005-01-11 Verteilungsträger der Dienstrohre eines Mantelstromtriebwerks Active DE602005009982D1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0400222A FR2865002B1 (fr) 2004-01-12 2004-01-12 Turboreacteur a double flux comprenant un support de distribution de servitudes et le support de distribution de servitudes.

Publications (1)

Publication Number Publication Date
DE602005009982D1 true DE602005009982D1 (de) 2008-11-13

Family

ID=34586488

Family Applications (1)

Application Number Title Priority Date Filing Date
DE602005009982T Active DE602005009982D1 (de) 2004-01-12 2005-01-11 Verteilungsträger der Dienstrohre eines Mantelstromtriebwerks

Country Status (10)

Country Link
US (1) US7506499B2 (de)
EP (1) EP1553262B1 (de)
JP (1) JP4081090B2 (de)
CN (1) CN100447397C (de)
CA (1) CA2492171C (de)
DE (1) DE602005009982D1 (de)
ES (1) ES2315820T3 (de)
FR (1) FR2865002B1 (de)
RU (1) RU2365777C2 (de)
UA (1) UA84680C2 (de)

Families Citing this family (27)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR20050026063A (ko) * 2002-07-29 2005-03-14 스미또모 가가꾸 가부시키가이샤 열경화성 수지 조성물 및 접착성 필름
US20060032974A1 (en) * 2004-08-16 2006-02-16 Honeywell International Inc. Modular installation kit for auxiliary power unit
FR2875855B1 (fr) * 2004-09-27 2006-12-22 Snecma Moteurs Sa Turboreacteur avec un bras monobloc de raccord de servitudes et le bras monobloc de raccord de servitudes
FR2920195B1 (fr) * 2007-08-23 2009-11-20 Snecma Turbomachine a double flux a reduction de bruit de jet
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
FR2928961B1 (fr) * 2008-03-19 2015-11-13 Snecma Distributeur sectorise pour une turbomachine.
FR2930592B1 (fr) * 2008-04-24 2010-04-30 Snecma Distributeur de turbine pour une turbomachine
US20100238270A1 (en) * 2009-03-20 2010-09-23 Intrepid Management Group, Inc. Endoscopic apparatus and method for producing via a holographic optical element an autostereoscopic 3-d image
US8753075B2 (en) 2010-07-20 2014-06-17 Rolls-Royce Corporation Fan case assembly and method
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
US9478896B2 (en) 2011-12-22 2016-10-25 Rolls-Royce Plc Electrical connectors
GB2497809B (en) * 2011-12-22 2014-03-12 Rolls Royce Plc Method of servicing a gas turbine engine
CA2881774C (en) 2012-09-26 2017-10-24 United Technologies Corporation Seal assembly for a static structure of a gas turbine engine
FR2999651B1 (fr) 2012-12-18 2015-01-16 Snecma Extension de carter intermediaire a conception amelioree
FR3005992B1 (fr) * 2013-05-24 2015-05-22 Snecma Dispositif de passage de servitudes pour une turbomachine
FR3011584B1 (fr) * 2013-10-04 2018-02-23 Safran Aircraft Engines Extension de carter intermediaire
FR3015625B1 (fr) * 2013-12-20 2015-12-11 Snecma Bras de guidage d'elements de forme allongee, en particulier pour une turbomachine
FR3034465B1 (fr) * 2015-04-03 2017-05-05 Snecma Turbomoteur comportant deux flux de ventilation distincts
CN105715316B (zh) * 2016-01-26 2017-06-27 北京航空航天大学 一种带倒z字形支板的简易排气框架
FR3051840B1 (fr) * 2016-05-31 2020-01-10 Safran Aircraft Engines Carter intermediaire de turbomachine, equipee d'une piece d'etancheite a interface bras/virole
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
RU2642991C1 (ru) * 2017-04-19 2018-01-29 Публичное акционерное общество "ОДК-Уфимское моторостроительное производственное объединение" (ПАО "ОДК-УМПО") Клапанный узел канала перепуска компрессора
US10641115B2 (en) * 2017-08-29 2020-05-05 United Technologies Corporation Segmented conduit with airfoil geometry
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
FR3086003B1 (fr) * 2018-09-17 2020-12-25 Safran Aircraft Engines Systeme de distribution d'un fluide primaire et d'un fluide secondaire
FR3123942B1 (fr) * 2021-06-09 2024-02-09 Safran Aircraft Engines Support de carenage incurvé d’un bras structural de turbomachine

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3826088A (en) * 1973-02-01 1974-07-30 Gen Electric Gas turbine engine augmenter cooling liner stabilizers and supports
US4577891A (en) * 1983-10-27 1986-03-25 The United States Of America As Represented By The Secretary Of The Air Force Torque limiting collar
US4987736A (en) * 1988-12-14 1991-01-29 General Electric Company Lightweight gas turbine engine frame with free-floating heat shield
US5174110A (en) * 1991-10-17 1992-12-29 United Technologies Corporation Utility conduit enclosure for turbine engine
US5292227A (en) * 1992-12-10 1994-03-08 General Electric Company Turbine frame
US5746574A (en) * 1997-05-27 1998-05-05 General Electric Company Low profile fluid joint
DE19726392A1 (de) * 1997-06-21 1998-12-24 Bosch Gmbh Robert Gemischabgabevorrichtung
US6125627A (en) * 1998-08-11 2000-10-03 Allison Advanced Development Company Method and apparatus for spraying fuel within a gas turbine engine
EP1373386B1 (de) * 2001-01-10 2006-08-16 Alliant Techsystems Inc. Faserverstärkte isolierung für raketenmotoren
FR2842565B1 (fr) * 2002-07-17 2005-01-28 Snecma Moteurs Demarreur-generateur integre pour turbomachine

Also Published As

Publication number Publication date
US20050247042A1 (en) 2005-11-10
EP1553262A1 (de) 2005-07-13
FR2865002B1 (fr) 2006-05-05
FR2865002A1 (fr) 2005-07-15
JP2005201267A (ja) 2005-07-28
CN1661201A (zh) 2005-08-31
US7506499B2 (en) 2009-03-24
CA2492171A1 (fr) 2005-07-12
RU2005100179A (ru) 2006-06-20
EP1553262B1 (de) 2008-10-01
ES2315820T3 (es) 2009-04-01
RU2365777C2 (ru) 2009-08-27
JP4081090B2 (ja) 2008-04-23
CN100447397C (zh) 2008-12-31
UA84680C2 (ru) 2008-11-25
CA2492171C (fr) 2012-05-01

Similar Documents

Publication Publication Date Title
DE602005009982D1 (de) Verteilungsträger der Dienstrohre eines Mantelstromtriebwerks
NO20070239L (no) System for a vaske en gassturbinmotor
DE602005004447D1 (de) Manschettendichtung für Turbinenleitschaufeln
DE602005007391D1 (de) Gasturbinentriebwerk
DE602005014079D1 (de) Auswuchtvorrichtung für Gasturbinentriebwerke
DE602005003759D1 (de) Gegenläufiges Turbinentriebwerk
DK2054593T3 (da) Forkammer til en gasmotor
GB2427654B (en) Gas turbine engine
GB2473578B (en) Gas turbine engine system
DE602005007297D1 (de) Turbine eines Gasturbinentriebwerks
DE602005000026D1 (de) Dichtungsanordnung für die Hochdruckturbine einer Turbomaschine
GB2436128B (en) Gas turbine engine
GB0406174D0 (en) Turbine engine arrangement
DK1903188T3 (da) Gasturbine
GB2443194B (en) Gas turbine engine
DE602005012168D1 (de) Gasturbine mit einem System zur Schalldämpfung
EP1924762A4 (de) Turbomotorverbrennungssysteme
DE602005014314D1 (de) Auswuchtvorrichtung für Gasturbinentriebwerke
EP1745213A4 (de) Druckflüssigkeitsbetriebener turbinenmotor
DE602007007384D1 (de) Zentralkörper der Schubdüse eines Turbinentriebwerks
GB0401189D0 (en) Turbine engine arrangements
DE602006020376D1 (de) ugehörige Gasturbine
DE602005001231D1 (de) Verriegelungsmittel für Gasturbinentriebwerke
GB2414430B (en) Method for coating gas turbine engine components
DE602005002290D1 (de) Kraftstoffschlauch

Legal Events

Date Code Title Description
8364 No opposition during term of opposition