BE732591A - - Google Patents
Info
- Publication number
- BE732591A BE732591A BE732591DA BE732591A BE 732591 A BE732591 A BE 732591A BE 732591D A BE732591D A BE 732591DA BE 732591 A BE732591 A BE 732591A
- Authority
- BE
- Belgium
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
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
- F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
- F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
- F02K3/075—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type controlling flow ratio between flows
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- 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)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Supercharger (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US71694368A | 1968-03-28 | 1968-03-28 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| BE732591A true BE732591A (enExample) | 1969-10-16 |
Family
ID=24880076
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| BE732591D BE732591A (enExample) | 1968-03-28 | 1969-05-06 |
Country Status (7)
| Country | Link |
|---|---|
| US (1) | US3508403A (enExample) |
| AU (1) | AU458204B2 (enExample) |
| BE (1) | BE732591A (enExample) |
| CH (1) | CH496169A (enExample) |
| DE (1) | DE1919035A1 (enExample) |
| FR (1) | FR2041560A5 (enExample) |
| GB (1) | GB1270434A (enExample) |
Families Citing this family (17)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR1592652A (enExample) * | 1968-11-08 | 1970-05-19 | ||
| US4335573A (en) * | 1970-09-02 | 1982-06-22 | General Electric Company | Gas turbine engine mixer |
| US5483793A (en) * | 1970-09-02 | 1996-01-16 | General Electric Company | Infrared radiation suppression device |
| US4030291A (en) * | 1976-01-02 | 1977-06-21 | General Electric Company | Thrust reverser for a gas turbofan engine |
| US4117671A (en) * | 1976-12-30 | 1978-10-03 | The Boeing Company | Noise suppressing exhaust mixer assembly for ducted-fan, turbojet engine |
| US4335801A (en) * | 1980-12-15 | 1982-06-22 | The Boeing Company | Noise suppressing nozzle |
| FR2513697A1 (fr) * | 1981-09-25 | 1983-04-01 | Snecma | Moteur de propulsion, notamment pour avion supersonique |
| GB2209054B (en) * | 1987-08-26 | 1992-04-15 | Rolls Royce Plc | Gas turbine nozzles |
| US5826424A (en) * | 1992-04-16 | 1998-10-27 | Klees; Garry W. | Turbine bypass engines |
| US5261229A (en) * | 1992-08-03 | 1993-11-16 | General Electric Company | Noise-suppressed exhaust nozzles for jet engines |
| US5381655A (en) * | 1993-05-10 | 1995-01-17 | General Electric Company | Admission mixing duct assembly |
| US5758488A (en) * | 1993-05-11 | 1998-06-02 | Roderick Thomson | Core flow expansion chamber device system for reduction of jet turbine engine noise |
| FR2858999B1 (fr) * | 2003-08-18 | 2005-11-11 | Snecma Moteurs | Turbomachine pour aeronef a emissions de bruit reduites |
| US7114323B2 (en) * | 2004-03-05 | 2006-10-03 | United Technologies Corporation | Jet exhaust noise reduction system and method |
| US7353647B2 (en) * | 2004-05-13 | 2008-04-08 | General Electric Company | Methods and apparatus for assembling gas turbine engines |
| GB0603285D0 (en) | 2006-02-18 | 2006-03-29 | Rolls Royce Plc | A gas turbine engine |
| DE102008024022A1 (de) * | 2008-05-16 | 2009-11-19 | Rolls-Royce Deutschland Ltd & Co Kg | Gasturbinentriebwerk, insbesondere Flugtriebwerk |
Family Cites Families (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3118276A (en) * | 1964-01-21 | Gas turbine engines | ||
| US2529973A (en) * | 1946-05-29 | 1950-11-14 | Rateau Soc | Arrangement for the starting of two shaft gas turbine propelling means chiefly on board of aircraft |
| US2978865A (en) * | 1956-02-06 | 1961-04-11 | Curtiss Wright Corp | Turbo fan exhaust mixing device |
| US2929203A (en) * | 1956-08-31 | 1960-03-22 | Westinghouse Electric Corp | Afterburning bypass aviation turbojet engine |
| US2999672A (en) * | 1958-04-09 | 1961-09-12 | Curtiss Wright Corp | Fluid mixing apparatus |
| US3048376A (en) * | 1958-04-09 | 1962-08-07 | Curtiss Wright Corp | Fluid mixing apparatus |
| GB918778A (en) * | 1959-06-23 | 1963-02-20 | Rolls Royce | Improvements in or relating to gas-turbine engines |
| GB945862A (en) * | 1961-08-18 | 1964-01-08 | Rolls Royce | Gas turbine by-pass engines |
-
1968
- 1968-03-28 US US716943A patent/US3508403A/en not_active Expired - Lifetime
-
1969
- 1969-04-14 AU AU53437/69A patent/AU458204B2/en not_active Expired
- 1969-04-15 GB GB09238/69A patent/GB1270434A/en not_active Expired
- 1969-04-15 DE DE19691919035 patent/DE1919035A1/de active Pending
- 1969-04-16 CH CH578169A patent/CH496169A/de not_active IP Right Cessation
- 1969-04-29 FR FR6913687A patent/FR2041560A5/fr not_active Expired
- 1969-05-06 BE BE732591D patent/BE732591A/xx unknown
Also Published As
| Publication number | Publication date |
|---|---|
| DE1919035A1 (de) | 1970-11-05 |
| CH496169A (de) | 1970-09-15 |
| US3508403A (en) | 1970-04-28 |
| GB1270434A (en) | 1972-04-12 |
| AU458204B2 (en) | 1975-01-30 |
| AU5343769A (en) | 1970-10-22 |
| FR2041560A5 (enExample) | 1971-01-29 |