FR2081027A1 - - Google Patents
Info
- Publication number
- FR2081027A1 FR2081027A1 FR7109324A FR7109324A FR2081027A1 FR 2081027 A1 FR2081027 A1 FR 2081027A1 FR 7109324 A FR7109324 A FR 7109324A FR 7109324 A FR7109324 A FR 7109324A FR 2081027 A1 FR2081027 A1 FR 2081027A1
- 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.)
- Granted
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
- F02K1/76—Control or regulation of thrust reversers
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- 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
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
- F02C7/042—Air intakes for gas-turbine plants or jet-propulsion plants having variable geometry
-
- 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
- F02K1/70—Reversing fan flow using thrust reverser flaps or doors mounted on the fan housing
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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)
- Physics & Mathematics (AREA)
- Geometry (AREA)
- Control Of Turbines (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB8164/70A GB1249609A (en) | 1970-02-20 | 1970-02-20 | Powerplant comprising a gas turbine engine |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| FR2081027A1 true FR2081027A1 (OSRAM) | 1971-11-26 |
| FR2081027B1 FR2081027B1 (OSRAM) | 1975-08-22 |
Family
ID=9846998
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| FR7109324A Expired FR2081027B1 (OSRAM) | 1970-02-20 | 1971-03-17 |
Country Status (2)
| Country | Link |
|---|---|
| FR (1) | FR2081027B1 (OSRAM) |
| GB (1) | GB1249609A (OSRAM) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR3123946A1 (fr) * | 2021-06-13 | 2022-12-16 | Safran Aircraft Engines | Entrée d’air d’ensemble propulsif d’aéronef comprenant des organes mobiles pour favoriser une phase d’inversion de poussée et procédé d’utilisation d’une telle entrée d’air |
Citations (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3019600A (en) * | 1959-08-03 | 1962-02-06 | United Aircraft Corp | Turbo-fan engine thrust reverser |
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1970
- 1970-02-20 GB GB8164/70A patent/GB1249609A/en not_active Expired
-
1971
- 1971-03-17 FR FR7109324A patent/FR2081027B1/fr not_active Expired
Patent Citations (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3019600A (en) * | 1959-08-03 | 1962-02-06 | United Aircraft Corp | Turbo-fan engine thrust reverser |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR3123946A1 (fr) * | 2021-06-13 | 2022-12-16 | Safran Aircraft Engines | Entrée d’air d’ensemble propulsif d’aéronef comprenant des organes mobiles pour favoriser une phase d’inversion de poussée et procédé d’utilisation d’une telle entrée d’air |
| WO2022263203A1 (fr) * | 2021-06-13 | 2022-12-22 | Safran Aircraft Engines | Entrée d'air d'ensemble propulsif d'aéronef comprenant des organes mobiles pour favoriser une phase d'inversion de poussée et procédé d'utilisation d'une telle entrée d'air |
| US12234790B2 (en) | 2021-06-13 | 2025-02-25 | Safran Aircraft Engines | Air inlet for an aircraft propulsion unit comprising mobile members for promoting a thrust reversal phase, and method for using such an air inlet |
Also Published As
| Publication number | Publication date |
|---|---|
| GB1249609A (en) | 1971-10-13 |
| FR2081027B1 (OSRAM) | 1975-08-22 |
Similar Documents
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| TP | Transmission of property | ||
| ST | Notification of lapse |