DE69217254D1 - Linearbetätiger für ein abblasventil - Google Patents
Linearbetätiger für ein abblasventilInfo
- Publication number
- DE69217254D1 DE69217254D1 DE69217254T DE69217254T DE69217254D1 DE 69217254 D1 DE69217254 D1 DE 69217254D1 DE 69217254 T DE69217254 T DE 69217254T DE 69217254 T DE69217254 T DE 69217254T DE 69217254 D1 DE69217254 D1 DE 69217254D1
- Authority
- DE
- Germany
- Prior art keywords
- blow
- valve
- linear actuator
- actuator
- linear
- 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
- 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
-
- 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
- F04D27/0223—Control schemes therefor
Landscapes
- Engineering & Computer Science (AREA)
- Life Sciences & Earth Sciences (AREA)
- Sustainable Development (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Control Of Turbines (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US07/830,047 US5216877A (en) | 1992-01-31 | 1992-01-31 | Linear actuator for a bleed valve |
PCT/US1992/010102 WO1993015322A1 (en) | 1992-01-31 | 1992-11-23 | Linear actuator for a bleed valve |
Publications (2)
Publication Number | Publication Date |
---|---|
DE69217254D1 true DE69217254D1 (de) | 1997-03-13 |
DE69217254T2 DE69217254T2 (de) | 1997-06-12 |
Family
ID=25256190
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE69217254T Expired - Fee Related DE69217254T2 (de) | 1992-01-31 | 1992-11-23 | Linearbetätiger für ein abblasventil |
Country Status (5)
Country | Link |
---|---|
US (1) | US5216877A (de) |
EP (1) | EP0656996B1 (de) |
JP (1) | JPH07503297A (de) |
DE (1) | DE69217254T2 (de) |
WO (1) | WO1993015322A1 (de) |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6560967B1 (en) | 1998-05-29 | 2003-05-13 | Jeffrey Mark Cohen | Method and apparatus for use with a gas fueled combustor |
US6974306B2 (en) * | 2003-07-28 | 2005-12-13 | Pratt & Whitney Canada Corp. | Blade inlet cooling flow deflector apparatus and method |
US7069728B2 (en) * | 2003-07-29 | 2006-07-04 | Pratt & Whitney Canada Corp. | Multi-position BOV actuator |
US11168578B2 (en) * | 2018-09-11 | 2021-11-09 | Pratt & Whitney Canada Corp. | System for adjusting a variable position vane in an aircraft engine |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2958457A (en) * | 1959-05-26 | 1960-11-01 | Samuel S Fox | Gradual bleed control |
US3172259A (en) * | 1962-03-02 | 1965-03-09 | Avco Corp | Variable geometry control for gas turbine engines |
US3646753A (en) * | 1970-04-28 | 1972-03-07 | United Aircraft Corp | Engine compressor bleed control system |
US3994617A (en) * | 1972-09-15 | 1976-11-30 | The Bendix Corporation | Control apparatus particularly for a plurality of compressor bleed valves of a gas turbine engine |
US3849021A (en) * | 1973-04-02 | 1974-11-19 | Bendix Corp | Compressor geometry control apparatus for gas turbine engine |
GB1469511A (en) * | 1973-07-05 | 1977-04-06 | Lucas Industries Ltd | Fluid pressure operated actuator device |
US4251985A (en) * | 1979-07-17 | 1981-02-24 | General Motors Corporation | Bleed valve control circuit |
US5072578A (en) * | 1989-12-14 | 1991-12-17 | Allied-Signal Inc. | Acceleration override means for a fuel control |
-
1992
- 1992-01-31 US US07/830,047 patent/US5216877A/en not_active Expired - Fee Related
- 1992-11-23 EP EP93900634A patent/EP0656996B1/de not_active Expired - Lifetime
- 1992-11-23 DE DE69217254T patent/DE69217254T2/de not_active Expired - Fee Related
- 1992-11-23 JP JP5513186A patent/JPH07503297A/ja active Pending
- 1992-11-23 WO PCT/US1992/010102 patent/WO1993015322A1/en active IP Right Grant
Also Published As
Publication number | Publication date |
---|---|
JPH07503297A (ja) | 1995-04-06 |
EP0656996B1 (de) | 1997-01-29 |
DE69217254T2 (de) | 1997-06-12 |
EP0656996A1 (de) | 1995-06-14 |
WO1993015322A1 (en) | 1993-08-05 |
US5216877A (en) | 1993-06-08 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition | ||
8339 | Ceased/non-payment of the annual fee |