GB2007303B - By-pass gas turbine engines - Google Patents
By-pass gas turbine enginesInfo
- Publication number
- GB2007303B GB2007303B GB7841808A GB7841808A GB2007303B GB 2007303 B GB2007303 B GB 2007303B GB 7841808 A GB7841808 A GB 7841808A GB 7841808 A GB7841808 A GB 7841808A GB 2007303 B GB2007303 B GB 2007303B
- Authority
- GB
- United Kingdom
- Prior art keywords
- gas turbine
- turbine engines
- pass gas
- pass
- engines
- 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
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
- F02K1/38—Introducing air inside the jet
- F02K1/386—Introducing air inside the jet mixing devices in the jet pipe, e.g. for mixing primary and secondary flow
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2270/00—Control
- F05D2270/01—Purpose of the control system
- F05D2270/17—Purpose of the control system to control boundary layer
- F05D2270/173—Purpose of the control system to control boundary layer by the Coanda effect
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Exhaust Silencers (AREA)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB7841808A GB2007303B (en) | 1977-11-04 | 1978-10-24 | By-pass gas turbine engines |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB4597677 | 1977-11-04 | ||
GB7841808A GB2007303B (en) | 1977-11-04 | 1978-10-24 | By-pass gas turbine engines |
Publications (2)
Publication Number | Publication Date |
---|---|
GB2007303A GB2007303A (en) | 1979-05-16 |
GB2007303B true GB2007303B (en) | 1982-04-07 |
Family
ID=26265706
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB7841808A Expired GB2007303B (en) | 1977-11-04 | 1978-10-24 | By-pass gas turbine engines |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB2007303B (en) |
Families Citing this family (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4265646A (en) * | 1979-10-01 | 1981-05-05 | General Electric Company | Foreign particle separator system |
US4284170A (en) * | 1979-10-22 | 1981-08-18 | United Technologies Corporation | Gas turbine noise suppressor |
GB2082259B (en) * | 1980-08-15 | 1984-03-07 | Rolls Royce | Exhaust flow mixers and nozzles |
GB2146702B (en) * | 1983-09-14 | 1987-12-23 | Rolls Royce | Exhaust mixer for turbofan aeroengine |
GB2149456B (en) * | 1983-11-08 | 1987-07-29 | Rolls Royce | Exhaust mixing in turbofan aeroengines |
-
1978
- 1978-10-24 GB GB7841808A patent/GB2007303B/en not_active Expired
Also Published As
Publication number | Publication date |
---|---|
GB2007303A (en) | 1979-05-16 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PCNP | Patent ceased through non-payment of renewal fee |