FR2866079B1 - Diffuseur pour turboreacteur - Google Patents
Diffuseur pour turboreacteurInfo
- Publication number
- FR2866079B1 FR2866079B1 FR0401084A FR0401084A FR2866079B1 FR 2866079 B1 FR2866079 B1 FR 2866079B1 FR 0401084 A FR0401084 A FR 0401084A FR 0401084 A FR0401084 A FR 0401084A FR 2866079 B1 FR2866079 B1 FR 2866079B1
- Authority
- FR
- France
- Prior art keywords
- turboreactor
- diffuser
- 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 - Lifetime
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/40—Casings; Connections of working fluid
- F04D29/52—Casings; Connections of working fluid for axial pumps
- F04D29/54—Fluid-guiding means, e.g. diffusers
- F04D29/541—Specially adapted for elastic fluid pumps
- F04D29/542—Bladed diffusers
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
- F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
- F23R3/60—Support structures; Attaching or mounting means
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
- F05B2230/00—Manufacture
- F05B2230/60—Assembly methods
- F05B2230/604—Assembly methods using positioning or alignment devices for aligning or centering, e.g. pins
- F05B2230/606—Assembly methods using positioning or alignment devices for aligning or centering, e.g. pins using maintaining alignment while permitting differential dilatation
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Priority Applications (8)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0401084A FR2866079B1 (fr) | 2004-02-05 | 2004-02-05 | Diffuseur pour turboreacteur |
EP05290094A EP1561998B1 (fr) | 2004-02-05 | 2005-01-14 | Diffuseur pour turboréacteur |
ES05290094T ES2382552T3 (es) | 2004-02-05 | 2005-01-14 | Difusor para turborreactor |
US11/039,887 US7197882B2 (en) | 2004-02-05 | 2005-01-24 | Turbojet diffuser |
JP2005016575A JP2005220904A (ja) | 2004-02-05 | 2005-01-25 | ターボジェットディフューザ |
CA2494943A CA2494943C (fr) | 2004-02-05 | 2005-01-31 | Diffuseur pour turboreacteur |
CN200510006289.9A CN1651735A (zh) | 2004-02-05 | 2005-02-02 | 涡轮喷气发动机扩压器 |
RU2005102776/06A RU2365762C2 (ru) | 2004-02-05 | 2005-02-04 | Диффузор турбореактивного двигателя и турбореактивный двигатель |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0401084A FR2866079B1 (fr) | 2004-02-05 | 2004-02-05 | Diffuseur pour turboreacteur |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2866079A1 FR2866079A1 (fr) | 2005-08-12 |
FR2866079B1 true FR2866079B1 (fr) | 2006-03-17 |
Family
ID=34673895
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR0401084A Expired - Lifetime FR2866079B1 (fr) | 2004-02-05 | 2004-02-05 | Diffuseur pour turboreacteur |
Country Status (8)
Country | Link |
---|---|
US (1) | US7197882B2 (fr) |
EP (1) | EP1561998B1 (fr) |
JP (1) | JP2005220904A (fr) |
CN (1) | CN1651735A (fr) |
CA (1) | CA2494943C (fr) |
ES (1) | ES2382552T3 (fr) |
FR (1) | FR2866079B1 (fr) |
RU (1) | RU2365762C2 (fr) |
Families Citing this family (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2415749B (en) * | 2004-07-02 | 2009-10-07 | Demag Delaval Ind Turbomachine | A gas turbine engine including an exhaust duct comprising a diffuser for diffusing the exhaust gas produced by the engine |
US20110176917A1 (en) * | 2004-07-02 | 2011-07-21 | Brian Haller | Exhaust Gas Diffuser Wall Contouring |
FR2920525B1 (fr) * | 2007-08-31 | 2014-06-13 | Snecma | Separateur pour alimentation de l'air de refroidissement d'une turbine |
FR2925109B1 (fr) * | 2007-12-14 | 2015-05-15 | Snecma | Module de turbomachine muni d'un dispositif d'amelioration des jeux radiaux |
FR2942267B1 (fr) * | 2009-02-19 | 2011-05-06 | Turbomeca | Temoin d'erosion pour roue de compresseur |
US8534076B2 (en) * | 2009-06-09 | 2013-09-17 | Honeywell Internationl Inc. | Combustor-turbine seal interface for gas turbine engine |
US8388307B2 (en) * | 2009-07-21 | 2013-03-05 | Honeywell International Inc. | Turbine nozzle assembly including radially-compliant spring member for gas turbine engine |
US20150241067A1 (en) * | 2012-09-26 | 2015-08-27 | United Technologies Corporation | Fastened joint for a tangential on board injector |
US11732892B2 (en) | 2013-08-14 | 2023-08-22 | General Electric Company | Gas turbomachine diffuser assembly with radial flow splitters |
US10533437B2 (en) * | 2013-11-04 | 2020-01-14 | United Technologies Corporation | Inner diffuser case for a gas turbine engine |
CN105716114B (zh) * | 2014-12-04 | 2018-05-08 | 中国航空工业集团公司沈阳发动机设计研究所 | 一种可拆换的矩形扩压器 |
CN106226056A (zh) * | 2016-08-12 | 2016-12-14 | 中国航空工业集团公司沈阳发动机设计研究所 | 一种扩压器 |
CN107339712B (zh) * | 2017-06-13 | 2020-03-24 | 中国航发湖南动力机械研究所 | 径向流燃烧室扩压器及燃气轮机 |
CN113983494B (zh) * | 2021-09-22 | 2022-10-21 | 南京航空航天大学 | 一种扩压比智能可调的燃气轮机主燃烧室多通道扩压器 |
CN114412594B (zh) * | 2022-01-25 | 2024-08-23 | 中国联合重型燃气轮机技术有限公司 | 一种重型燃气轮机壳体结构 |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB589541A (en) * | 1941-09-22 | 1947-06-24 | Hayne Constant | Improvements in axial flow turbines, compressors and the like |
US5165850A (en) * | 1991-07-15 | 1992-11-24 | General Electric Company | Compressor discharge flowpath |
FR2706534B1 (fr) * | 1993-06-10 | 1995-07-21 | Snecma | Diffuseur-séparateur multiflux avec redresseur intégré pour turboréacteur. |
FR2794816B1 (fr) * | 1999-06-10 | 2001-07-06 | Snecma | Stator de compresseur a haute pression |
US6651439B2 (en) * | 2001-01-12 | 2003-11-25 | General Electric Co. | Methods and apparatus for supplying air to turbine engine combustors |
-
2004
- 2004-02-05 FR FR0401084A patent/FR2866079B1/fr not_active Expired - Lifetime
-
2005
- 2005-01-14 ES ES05290094T patent/ES2382552T3/es active Active
- 2005-01-14 EP EP05290094A patent/EP1561998B1/fr active Active
- 2005-01-24 US US11/039,887 patent/US7197882B2/en active Active
- 2005-01-25 JP JP2005016575A patent/JP2005220904A/ja not_active Withdrawn
- 2005-01-31 CA CA2494943A patent/CA2494943C/fr active Active
- 2005-02-02 CN CN200510006289.9A patent/CN1651735A/zh active Pending
- 2005-02-04 RU RU2005102776/06A patent/RU2365762C2/ru active
Also Published As
Publication number | Publication date |
---|---|
CA2494943A1 (fr) | 2005-08-05 |
JP2005220904A (ja) | 2005-08-18 |
US7197882B2 (en) | 2007-04-03 |
EP1561998A1 (fr) | 2005-08-10 |
RU2005102776A (ru) | 2006-07-10 |
CA2494943C (fr) | 2012-04-24 |
US20050172632A1 (en) | 2005-08-11 |
ES2382552T3 (es) | 2012-06-11 |
RU2365762C2 (ru) | 2009-08-27 |
CN1651735A (zh) | 2005-08-10 |
FR2866079A1 (fr) | 2005-08-12 |
EP1561998B1 (fr) | 2012-03-07 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
CD | Change of name or company name | ||
PLFP | Fee payment |
Year of fee payment: 13 |
|
PLFP | Fee payment |
Year of fee payment: 14 |
|
PLFP | Fee payment |
Year of fee payment: 15 |
|
CD | Change of name or company name |
Owner name: SAFRAN AIRCRAFT ENGINES, FR Effective date: 20170719 |
|
PLFP | Fee payment |
Year of fee payment: 17 |
|
PLFP | Fee payment |
Year of fee payment: 18 |
|
PLFP | Fee payment |
Year of fee payment: 19 |
|
PLFP | Fee payment |
Year of fee payment: 20 |