UA84680C2 - турбовентиляторный двигатель и опора для распределения служебных магистралей - Google Patents
турбовентиляторный двигатель и опора для распределения служебных магистралейInfo
- Publication number
- UA84680C2 UA84680C2 UAA200500227A UAA200500227A UA84680C2 UA 84680 C2 UA84680 C2 UA 84680C2 UA A200500227 A UAA200500227 A UA A200500227A UA A200500227 A UAA200500227 A UA A200500227A UA 84680 C2 UA84680 C2 UA 84680C2
- Authority
- UA
- Ukraine
- Prior art keywords
- service conduits
- turbofan engine
- distribution support
- housing
- conduits
- Prior art date
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)
Abstract
Изобретение касается турбовентиляторного двигателя, который содержит внешний корпус (11), поддерживаемый кронштейном (12), внутренний корпус (34), который находится напротив корпуса (11), и служебные магистрали (38). Вдоль оси кронштейна (12) сформирована опора (35) для деления служебных магистралей на внутреннем корпусе (34), которая содержит первую опорную подушку (36) для приема служебных магистралей с внешней стороны внутреннего корпуса (34).
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 |
---|---|
UA84680C2 true UA84680C2 (ru) | 2008-11-25 |
Family
ID=34586488
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
UAA200500227A UA84680C2 (ru) | 2004-01-12 | 2005-01-10 | турбовентиляторный двигатель и опора для распределения служебных магистралей |
Country Status (10)
Country | Link |
---|---|
US (1) | US7506499B2 (ru) |
EP (1) | EP1553262B1 (ru) |
JP (1) | JP4081090B2 (ru) |
CN (1) | CN100447397C (ru) |
CA (1) | CA2492171C (ru) |
DE (1) | DE602005009982D1 (ru) |
ES (1) | ES2315820T3 (ru) |
FR (1) | FR2865002B1 (ru) |
RU (1) | RU2365777C2 (ru) |
UA (1) | UA84680C2 (ru) |
Families Citing this family (27)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2004011521A1 (ja) * | 2002-07-29 | 2004-02-05 | Sumitomo Chemical Company, Limited | 熱硬化性樹脂組成物及び接着性フィルム |
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 |
US9478896B2 (en) | 2011-12-22 | 2016-10-25 | Rolls-Royce Plc | Electrical connectors |
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 |
EP2900956B1 (en) * | 2012-09-26 | 2019-11-20 | United Technologies Corporation | Gas turbine engine comprising a seal assembly for a static structure thereof |
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)
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 |
AU2002311751A1 (en) * | 2001-01-10 | 2002-10-15 | Alliant Techsystems Inc. | Fiber-reinforced rocket motor insulation |
FR2842565B1 (fr) * | 2002-07-17 | 2005-01-28 | Snecma Moteurs | Demarreur-generateur integre pour turbomachine |
-
2004
- 2004-01-12 FR FR0400222A patent/FR2865002B1/fr not_active Expired - Fee Related
-
2005
- 2005-01-10 CA CA2492171A patent/CA2492171C/fr active Active
- 2005-01-10 UA UAA200500227A patent/UA84680C2/ru unknown
- 2005-01-10 US US11/030,971 patent/US7506499B2/en active Active
- 2005-01-11 JP JP2005003401A patent/JP4081090B2/ja active Active
- 2005-01-11 ES ES05300012T patent/ES2315820T3/es active Active
- 2005-01-11 DE DE602005009982T patent/DE602005009982D1/de active Active
- 2005-01-11 EP EP05300012A patent/EP1553262B1/fr active Active
- 2005-01-11 RU RU2005100179/06A patent/RU2365777C2/ru active
- 2005-01-12 CN CNB2005100041623A patent/CN100447397C/zh active Active
Also Published As
Publication number | Publication date |
---|---|
RU2365777C2 (ru) | 2009-08-27 |
CA2492171C (fr) | 2012-05-01 |
CA2492171A1 (fr) | 2005-07-12 |
EP1553262A1 (fr) | 2005-07-13 |
CN100447397C (zh) | 2008-12-31 |
FR2865002A1 (fr) | 2005-07-15 |
JP4081090B2 (ja) | 2008-04-23 |
ES2315820T3 (es) | 2009-04-01 |
JP2005201267A (ja) | 2005-07-28 |
US7506499B2 (en) | 2009-03-24 |
RU2005100179A (ru) | 2006-06-20 |
FR2865002B1 (fr) | 2006-05-05 |
DE602005009982D1 (de) | 2008-11-13 |
US20050247042A1 (en) | 2005-11-10 |
CN1661201A (zh) | 2005-08-31 |
EP1553262B1 (fr) | 2008-10-01 |
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