FR2392239B1 - - Google Patents
Info
- Publication number
- FR2392239B1 FR2392239B1 FR7626938A FR7626938A FR2392239B1 FR 2392239 B1 FR2392239 B1 FR 2392239B1 FR 7626938 A FR7626938 A FR 7626938A FR 7626938 A FR7626938 A FR 7626938A FR 2392239 B1 FR2392239 B1 FR 2392239B1
- Authority
- FR
- France
- 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
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
-
- 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
- F02K3/077—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 the plant being of the multiple flow type, i.e. having three or more flows
-
- 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
- F02K3/12—Plants including a gas turbine driving a compressor or a ducted fan characterised by having more than one gas turbine
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)
- Testing Of Engines (AREA)
Priority Applications (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR7626938A FR2392239A1 (fr) | 1976-08-30 | 1976-08-30 | Systeme de propulsion pour avion supersonique |
| GB34470/77A GB1534625A (en) | 1976-08-30 | 1977-08-17 | Gas turbine jet propulsion units for supersonic aircraft |
| US05/827,704 US4183211A (en) | 1976-08-30 | 1977-08-25 | Propulsion system for supersonic aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR7626938A FR2392239A1 (fr) | 1976-08-30 | 1976-08-30 | Systeme de propulsion pour avion supersonique |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| FR2392239A1 FR2392239A1 (fr) | 1978-12-22 |
| FR2392239B1 true FR2392239B1 (US08080257-20111220-C00005.png) | 1979-09-07 |
Family
ID=9177449
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| FR7626938A Granted FR2392239A1 (fr) | 1976-08-30 | 1976-08-30 | Systeme de propulsion pour avion supersonique |
Country Status (3)
| Country | Link |
|---|---|
| US (1) | US4183211A (US08080257-20111220-C00005.png) |
| FR (1) | FR2392239A1 (US08080257-20111220-C00005.png) |
| GB (1) | GB1534625A (US08080257-20111220-C00005.png) |
Families Citing this family (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2513697A1 (fr) * | 1981-09-25 | 1983-04-01 | Snecma | Moteur de propulsion, notamment pour avion supersonique |
| DE4012103C1 (en) * | 1990-04-14 | 1991-07-25 | Karl Dipl.-Ing. 2742 Gnarrenburg De Kastens | Hypersonic aircraft reaction drive - has flow tube with frontal air entry slot and trough at trailing end |
| JP3120113B1 (ja) * | 1999-11-10 | 2000-12-25 | 科学技術庁航空宇宙技術研究所長 | 高速航空機用ジェットエンジン |
| CA2329555A1 (en) * | 2000-12-22 | 2002-06-22 | Jose Albero | Main propulsion engine system integrated with secondary power unit |
| AU2002250133A1 (en) * | 2001-02-16 | 2002-09-04 | Hamilton Sundstrand Corporation | Improved aircraft system architecture |
| FR2875855B1 (fr) * | 2004-09-27 | 2006-12-22 | Snecma Moteurs Sa | Turboreacteur avec un bras monobloc de raccord de servitudes et le bras monobloc de raccord de servitudes |
| US8844266B1 (en) * | 2011-10-03 | 2014-09-30 | Florida Turbine Technologies, Inc. | Variable bypass ratio augmented gas turbine engine |
| US9222409B2 (en) * | 2012-03-15 | 2015-12-29 | United Technologies Corporation | Aerospace engine with augmenting turbojet |
| DE102016118779A1 (de) * | 2016-10-04 | 2018-04-05 | Rolls-Royce Deutschland Ltd & Co Kg | Turbofan-Triebwerk für ein ziviles Überschallflugzeug |
| US10677264B2 (en) | 2016-10-14 | 2020-06-09 | General Electric Company | Supersonic single-stage turbofan engine |
| US10683806B2 (en) | 2017-01-05 | 2020-06-16 | General Electric Company | Protected core inlet with reduced capture area |
Family Cites Families (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3677012A (en) * | 1962-05-31 | 1972-07-18 | Gen Electric | Composite cycle turbomachinery |
| US3659422A (en) * | 1966-11-04 | 1972-05-02 | North American Rockwell | Method and apparatus for aircraft propulsion |
| US3841091A (en) * | 1973-05-21 | 1974-10-15 | Gen Electric | Multi-mission tandem propulsion system |
| US4033119A (en) * | 1973-09-06 | 1977-07-05 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Dual cycle aircraft turbine engine |
| US4054030A (en) * | 1976-04-29 | 1977-10-18 | General Motors Corporation | Variable cycle gas turbine engine |
-
1976
- 1976-08-30 FR FR7626938A patent/FR2392239A1/fr active Granted
-
1977
- 1977-08-17 GB GB34470/77A patent/GB1534625A/en not_active Expired
- 1977-08-25 US US05/827,704 patent/US4183211A/en not_active Expired - Lifetime
Also Published As
| Publication number | Publication date |
|---|---|
| US4183211A (en) | 1980-01-15 |
| FR2392239A1 (fr) | 1978-12-22 |
| GB1534625A (en) | 1978-12-06 |
Similar Documents
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| ST | Notification of lapse |