FR1339601A - Perfectionnement aux réacteurs à double flux - Google Patents
Perfectionnement aux réacteurs à double fluxInfo
- Publication number
- FR1339601A FR1339601A FR906141A FR906141A FR1339601A FR 1339601 A FR1339601 A FR 1339601A FR 906141 A FR906141 A FR 906141A FR 906141 A FR906141 A FR 906141A FR 1339601 A FR1339601 A FR 1339601A
- Authority
- FR
- France
- Prior art keywords
- improvement
- reactors
- bypass
- bypass reactors
- 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
- F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
- F02K3/08—Plants including a gas turbine driving a compressor or a ducted fan with supplementary heating of the working fluid; Control thereof
- F02K3/105—Heating the by-pass flow
- F02K3/11—Heating the by-pass flow by means of burners or combustion chambers
-
- 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
- F02K3/08—Plants including a gas turbine driving a compressor or a ducted fan with supplementary heating of the working fluid; Control thereof
- F02K3/10—Plants including a gas turbine driving a compressor or a ducted fan with supplementary heating of the working fluid; Control thereof by after-burners
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Engine Equipment That Uses Special Cycles (AREA)
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR906141A FR1339601A (fr) | 1962-08-04 | 1962-08-04 | Perfectionnement aux réacteurs à double flux |
US298607A US3204404A (en) | 1962-08-04 | 1963-07-30 | Double flow jet-engines |
GB30491/63A GB1028296A (en) | 1962-08-04 | 1963-08-01 | Improvements in or relating to by-pass turbojets |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR906141A FR1339601A (fr) | 1962-08-04 | 1962-08-04 | Perfectionnement aux réacteurs à double flux |
Publications (1)
Publication Number | Publication Date |
---|---|
FR1339601A true FR1339601A (fr) | 1963-10-11 |
Family
ID=8784645
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR906141A Expired FR1339601A (fr) | 1962-08-04 | 1962-08-04 | Perfectionnement aux réacteurs à double flux |
Country Status (3)
Country | Link |
---|---|
US (1) | US3204404A (fr) |
FR (1) | FR1339601A (fr) |
GB (1) | GB1028296A (fr) |
Families Citing this family (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1126163A (en) * | 1967-06-16 | 1968-09-05 | Rolls Royce | Gas turbine by-pass engine |
US3630029A (en) * | 1970-01-14 | 1971-12-28 | Lucas Industries Ltd | Fuel controls for reheat systems of gas turbine engines |
US4244183A (en) * | 1978-04-27 | 1981-01-13 | United Technologies Corporation | Control means for an augmentor for a gas turbine engine |
DE3543908C1 (de) * | 1985-12-12 | 1987-01-29 | Mtu Muenchen Gmbh | Einrichtung zur Steuerung der Brennstoffzufuhr zum Nachbrenner eines Nebenstrom-Gasturbinenstrahltriebwerkes |
DE4324794C2 (de) * | 1993-07-23 | 1997-10-16 | Alexander Schaefer | Düsenantrieb |
GB2610568A (en) | 2021-09-08 | 2023-03-15 | Rolls Royce Plc | An improved gas turbine engine |
GB2610565A (en) | 2021-09-08 | 2023-03-15 | Rolls Royce Plc | An improved gas turbine engine |
GB2610570A (en) * | 2021-09-08 | 2023-03-15 | Rolls Royce Plc | An improved gas turbine engine |
GB2610567A (en) | 2021-09-08 | 2023-03-15 | Rolls Royce Plc | An improved gas turbine engine |
GB2610572A (en) | 2021-09-08 | 2023-03-15 | Rolls Royce Plc | An improved gas turbine engine |
GB2610569A (en) | 2021-09-08 | 2023-03-15 | Rolls Royce Plc | An improved gas turbine engine |
Family Cites Families (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2955414A (en) * | 1957-09-03 | 1960-10-11 | United Aircraft Corp | Combined power plant |
US3054254A (en) * | 1959-01-27 | 1962-09-18 | United Aircraft Corp | Turbofan afterburner fuel control improvement |
-
1962
- 1962-08-04 FR FR906141A patent/FR1339601A/fr not_active Expired
-
1963
- 1963-07-30 US US298607A patent/US3204404A/en not_active Expired - Lifetime
- 1963-08-01 GB GB30491/63A patent/GB1028296A/en not_active Expired
Also Published As
Publication number | Publication date |
---|---|
GB1028296A (en) | 1966-05-04 |
US3204404A (en) | 1965-09-07 |
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