FR1602870A - - Google Patents
Info
- Publication number
- FR1602870A FR1602870A FR38880A FR1602870DA FR1602870A FR 1602870 A FR1602870 A FR 1602870A FR 38880 A FR38880 A FR 38880A FR 1602870D A FR1602870D A FR 1602870DA FR 1602870 A FR1602870 A FR 1602870A
- 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
- 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
- F02K1/54—Nozzles having means for reversing jet thrust
- F02K1/64—Reversing fan flow
- F02K1/68—Reversers mounted on the engine housing downstream of the fan exhaust section
-
- 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
-
- 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
- F02K3/06—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 with front fan
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)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US37966964A | 1964-07-01 | 1964-07-01 | |
| FR38880 | 1965-11-18 | ||
| US66654667A | 1967-08-31 | 1967-08-31 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| FR1602870A true FR1602870A (fr) | 1971-02-08 |
Family
ID=27242734
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| FR38880A Expired FR1602870A (fr) | 1964-07-01 | 1965-11-18 |
Country Status (4)
| Country | Link |
|---|---|
| US (1) | US3533237A (fr) |
| DE (1) | DE1526812C3 (fr) |
| FR (1) | FR1602870A (fr) |
| GB (1) | GB1211192A (fr) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2477100A1 (fr) * | 1980-03-03 | 1981-09-04 | Gen Electric | Systeme d'ejection d'air de dilution de moteur a turbosoufflante |
Families Citing this family (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4314681A (en) * | 1979-08-31 | 1982-02-09 | General Electric Company | Drag-reducing component |
| GB2061389B (en) * | 1979-10-23 | 1983-05-18 | Rolls Royce | Rod installation for a gas turbine engine |
| US4410150A (en) * | 1980-03-03 | 1983-10-18 | General Electric Company | Drag-reducing nacelle |
| US4799633A (en) * | 1982-10-29 | 1989-01-24 | General Electric Company | Laminar flow necelle |
| AU555526B2 (en) * | 1982-10-29 | 1986-09-25 | General Electric Company | Aircraft engine nacelle |
| FR2926536B1 (fr) * | 2008-01-23 | 2010-07-30 | Snecma | Accrochage d'un systeme propulsif a un element de structure d'un aeronef |
| US9840917B2 (en) * | 2011-12-13 | 2017-12-12 | United Technologies Corporation | Stator vane shroud having an offset |
Family Cites Families (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3095166A (en) * | 1963-06-25 | briggs | ||
| US2416389A (en) * | 1942-06-17 | 1947-02-25 | Armstrong Siddeley Motors Ltd | Torque balancing of jet propulsion turbine plant |
| US3036431A (en) * | 1959-09-08 | 1962-05-29 | Boeing Co | Thrust reverser for jet engines |
| FR1271544A (fr) * | 1960-07-11 | 1961-09-15 | Nord Aviation | Combiné turboréacteur-statoréacteur |
| FR1325056A (fr) * | 1962-03-15 | 1963-04-26 | Nord Aviation | Perfectionnements aux combinés turboréacteur-statoréacteur |
| US3241313A (en) * | 1963-09-18 | 1966-03-22 | Gen Electric | Thrust deflector |
-
1965
- 1965-06-25 GB GB27143/65A patent/GB1211192A/en not_active Expired
- 1965-06-30 DE DE1526812A patent/DE1526812C3/de not_active Expired
- 1965-11-18 FR FR38880A patent/FR1602870A/fr not_active Expired
-
1967
- 1967-08-31 US US666546A patent/US3533237A/en not_active Expired - Lifetime
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2477100A1 (fr) * | 1980-03-03 | 1981-09-04 | Gen Electric | Systeme d'ejection d'air de dilution de moteur a turbosoufflante |
Also Published As
| Publication number | Publication date |
|---|---|
| GB1211192A (en) | 1970-11-04 |
| US3533237A (en) | 1970-10-13 |
| DE1526812B2 (de) | 1978-02-02 |
| DE1526812A1 (de) | 1971-01-14 |
| DE1526812C3 (de) | 1978-09-28 |