DE69113209T2 - Abblastruktur eines Verdichters. - Google Patents
Abblastruktur eines Verdichters.Info
- Publication number
- DE69113209T2 DE69113209T2 DE69113209T DE69113209T DE69113209T2 DE 69113209 T2 DE69113209 T2 DE 69113209T2 DE 69113209 T DE69113209 T DE 69113209T DE 69113209 T DE69113209 T DE 69113209T DE 69113209 T2 DE69113209 T2 DE 69113209T2
- Authority
- DE
- Germany
- Prior art keywords
- blow
- compressor
- 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 - Fee Related
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
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D27/00—Control, e.g. regulation, of pumps, pumping installations or pumping systems specially adapted for elastic fluids
- F04D27/02—Surge control
- F04D27/0207—Surge control by bleeding, bypassing or recycling fluids
- F04D27/023—Details or means for fluid extraction
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US61567690A | 1990-11-19 | 1990-11-19 |
Publications (2)
Publication Number | Publication Date |
---|---|
DE69113209D1 DE69113209D1 (de) | 1995-10-26 |
DE69113209T2 true DE69113209T2 (de) | 1996-05-02 |
Family
ID=24466390
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE69113209T Expired - Fee Related DE69113209T2 (de) | 1990-11-19 | 1991-11-13 | Abblastruktur eines Verdichters. |
Country Status (4)
Country | Link |
---|---|
EP (1) | EP0487242B1 (de) |
JP (1) | JP2513954B2 (de) |
CA (1) | CA2048829C (de) |
DE (1) | DE69113209T2 (de) |
Families Citing this family (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US9260974B2 (en) | 2011-12-16 | 2016-02-16 | General Electric Company | System and method for active clearance control |
US9145772B2 (en) | 2012-01-31 | 2015-09-29 | United Technologies Corporation | Compressor disk bleed air scallops |
US9528391B2 (en) | 2012-07-17 | 2016-12-27 | United Technologies Corporation | Gas turbine engine outer case with contoured bleed boss |
JP6000142B2 (ja) * | 2013-01-28 | 2016-09-28 | 三菱重工業株式会社 | 回転機械、及びこれを備えているガスタービン |
EP2803822B1 (de) * | 2013-05-13 | 2019-12-04 | Safran Aero Boosters SA | Luftentnahmesystem aus einer axialen Turbomaschine |
JP6134628B2 (ja) | 2013-10-17 | 2017-05-24 | 三菱重工業株式会社 | 軸流式の圧縮機、及びガスタービン |
GB201518448D0 (en) * | 2015-10-19 | 2015-12-02 | Rolls Royce | Compressor |
CN113847280A (zh) * | 2021-10-10 | 2021-12-28 | 中国航发沈阳发动机研究所 | 一种压气机转子级间引气结构 |
Family Cites Families (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3108767A (en) * | 1960-03-14 | 1963-10-29 | Rolls Royce | By-pass gas turbine engine with air bleed means |
GB936635A (en) * | 1961-04-21 | 1963-09-11 | Rolls Royce | Multi-stage axial-flow compressor |
US3777489A (en) * | 1972-06-01 | 1973-12-11 | Gen Electric | Combustor casing and concentric air bleed structure |
DE2247400C2 (de) * | 1972-09-27 | 1975-01-16 | Motoren- Und Turbinen-Union Muenchen Gmbh, 8000 Muenchen | Vorrichtung zum Abblasen von verdichteter Luft aus einem Verdichter eines Gasturbinenstrahltriebwerks |
JPS5364112A (en) * | 1976-11-19 | 1978-06-08 | Hitachi Ltd | Gas turbine compressor |
US4344282A (en) * | 1980-12-16 | 1982-08-17 | United Technologies Corporation | Compressor bleed system |
US4711084A (en) * | 1981-11-05 | 1987-12-08 | Avco Corporation | Ejector assisted compressor bleed |
US4546605A (en) * | 1983-12-16 | 1985-10-15 | United Technologies Corporation | Heat exchange system |
JPS6124675U (ja) * | 1984-07-17 | 1986-02-14 | 日本電気株式会社 | 耐電圧試験器 |
FR2640685B1 (fr) * | 1988-12-15 | 1991-02-08 | Snecma | Vanne de decharge de compresseur de turboreacteur |
-
1991
- 1991-08-08 CA CA002048829A patent/CA2048829C/en not_active Expired - Fee Related
- 1991-11-13 DE DE69113209T patent/DE69113209T2/de not_active Expired - Fee Related
- 1991-11-13 EP EP91310455A patent/EP0487242B1/de not_active Expired - Lifetime
- 1991-11-14 JP JP3325119A patent/JP2513954B2/ja not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
CA2048829C (en) | 2001-12-18 |
JP2513954B2 (ja) | 1996-07-10 |
JPH04284136A (ja) | 1992-10-08 |
EP0487242B1 (de) | 1995-09-20 |
CA2048829A1 (en) | 1992-05-20 |
DE69113209D1 (de) | 1995-10-26 |
EP0487242A1 (de) | 1992-05-27 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition | ||
8328 | Change in the person/name/address of the agent |
Representative=s name: ROEGER UND KOLLEGEN, 73728 ESSLINGEN |
|
8339 | Ceased/non-payment of the annual fee |