GB2231009B - Diverter valve with bypass duct obturator - Google Patents
Diverter valve with bypass duct obturatorInfo
- Publication number
- GB2231009B GB2231009B GB8521954A GB8521954A GB2231009B GB 2231009 B GB2231009 B GB 2231009B GB 8521954 A GB8521954 A GB 8521954A GB 8521954 A GB8521954 A GB 8521954A GB 2231009 B GB2231009 B GB 2231009B
- Authority
- GB
- United Kingdom
- Prior art keywords
- obturator
- diverter valve
- bypass duct
- diverter
- bypass
- 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
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D13/00—Combinations of two or more machines or engines
- F01D13/02—Working-fluid interconnection of machines or engines
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
- F02C9/16—Control of working fluid flow
- F02C9/18—Control of working fluid flow by bleeding, bypassing or acting on variable working fluid interconnections between turbines or compressors or their stages
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D25/00—Pumping installations or systems
- F04D25/16—Combinations of two or more pumps ; Producing two or more separate gas flows
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US06/820,249 US4979363A (en) | 1984-11-17 | 1985-11-15 | Diverter valve with bypass duct obturator |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB8429106 | 1984-11-17 |
Publications (2)
Publication Number | Publication Date |
---|---|
GB2231009A GB2231009A (en) | 1990-11-07 |
GB2231009B true GB2231009B (en) | 1991-01-23 |
Family
ID=10569887
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB8521954A Expired - Fee Related GB2231009B (en) | 1984-11-17 | 1985-09-04 | Diverter valve with bypass duct obturator |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB2231009B (en) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102004042720A1 (en) * | 2004-03-02 | 2005-11-24 | Braun, Alfons | Multi-stage suction fan with at least two radial fans, in particular for use in a suction dredger |
Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB963406A (en) * | 1961-02-16 | 1964-07-08 | Dornier Werke Gmbh | Aircraft with two or more jet engines arranged symmetrically with respect to the central longitudinal axis of the aircraft |
GB1252077A (en) * | 1969-03-08 | 1971-11-03 |
-
1985
- 1985-09-04 GB GB8521954A patent/GB2231009B/en not_active Expired - Fee Related
Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB963406A (en) * | 1961-02-16 | 1964-07-08 | Dornier Werke Gmbh | Aircraft with two or more jet engines arranged symmetrically with respect to the central longitudinal axis of the aircraft |
GB1252077A (en) * | 1969-03-08 | 1971-11-03 |
Also Published As
Publication number | Publication date |
---|---|
GB2231009A (en) | 1990-11-07 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PCNP | Patent ceased through non-payment of renewal fee |
Effective date: 19930904 |