FR685830A - Turbine à combustion continue - Google Patents
Turbine à combustion continueInfo
- Publication number
- FR685830A FR685830A FR685830DA FR685830A FR 685830 A FR685830 A FR 685830A FR 685830D A FR685830D A FR 685830DA FR 685830 A FR685830 A FR 685830A
- Authority
- FR
- France
- Prior art keywords
- combustion turbine
- continuous combustion
- continuous
- turbine
- combustion
- 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
- 238000002485 combustion reaction Methods 0.000 title 1
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
- F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
- F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
- F02C3/045—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor having compressor and turbine passages in a single rotor-module
-
- 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
- F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
- F02C3/34—Gas-turbine plants characterised by the use of combustion products as the working fluid with recycling of part of the working fluid, i.e. semi-closed cycles with combustion products in the closed part of the cycle
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Life Sciences & Earth Sciences (AREA)
- Sustainable Development (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR685830T | 1929-11-30 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| FR685830A true FR685830A (fr) | 1930-07-17 |
Family
ID=9025203
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| FR685830D Expired FR685830A (fr) | 1929-11-30 | 1929-11-30 | Turbine à combustion continue |
Country Status (1)
| Country | Link |
|---|---|
| FR (1) | FR685830A (fr) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2595505A (en) * | 1946-04-20 | 1952-05-06 | Continental Aviat & Engineerin | Coaxial combustion products generator, turbine, and compressor |
| US2632998A (en) * | 1946-08-03 | 1953-03-31 | Lewis D Burch | Multiple stage rotary translation engine |
| US2648492A (en) * | 1945-05-14 | 1953-08-11 | Edward A Stalker | Gas turbine incorporating compressor |
| US2692476A (en) * | 1950-11-13 | 1954-10-26 | Boeing Co | Gas turbine engine air starting motor constituting air supply mechanism |
| US2749023A (en) * | 1952-02-18 | 1956-06-05 | Bristol Aeroplane Co Ltd | Gas turbine engines |
-
1929
- 1929-11-30 FR FR685830D patent/FR685830A/fr not_active Expired
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2648492A (en) * | 1945-05-14 | 1953-08-11 | Edward A Stalker | Gas turbine incorporating compressor |
| US2595505A (en) * | 1946-04-20 | 1952-05-06 | Continental Aviat & Engineerin | Coaxial combustion products generator, turbine, and compressor |
| US2632998A (en) * | 1946-08-03 | 1953-03-31 | Lewis D Burch | Multiple stage rotary translation engine |
| US2692476A (en) * | 1950-11-13 | 1954-10-26 | Boeing Co | Gas turbine engine air starting motor constituting air supply mechanism |
| US2749023A (en) * | 1952-02-18 | 1956-06-05 | Bristol Aeroplane Co Ltd | Gas turbine engines |
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