FR331292A - Continuous combustion turbo-engine - Google Patents
Continuous combustion turbo-engineInfo
- Publication number
- FR331292A FR331292A FR331292DA FR331292A FR 331292 A FR331292 A FR 331292A FR 331292D A FR331292D A FR 331292DA FR 331292 A FR331292 A FR 331292A
- Authority
- FR
- France
- Prior art keywords
- engine
- continuous combustion
- combustion turbo
- turbo
- continuous
- 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
- 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
- F02C7/12—Cooling of plants
- F02C7/14—Cooling of plants of fluids in the plant, e.g. lubricant or fuel
-
- 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
- F02C3/32—Inducing air flow by fluid jet, e.g. ejector action
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR331292T | 1903-02-16 |
Publications (1)
Publication Number | Publication Date |
---|---|
FR331292A true FR331292A (en) | 1903-09-03 |
Family
ID=1381013
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR331292D Expired FR331292A (en) | 1903-02-16 | 1903-02-16 | Continuous combustion turbo-engine |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR331292A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2546432A (en) * | 1944-03-20 | 1951-03-27 | Power Jets Res & Dev Ltd | Apparatus for deflecting a fuel jet towards a region of turbulence in a propulsive gaseous stream |
US2692480A (en) * | 1948-05-07 | 1954-10-26 | Onera (Off Nat Aerospatiale) | Supersonic internal circulation combustion chamber, in particular combustion chamber for aircraft jet engines |
US2881588A (en) * | 1948-04-27 | 1959-04-14 | Wilbur H Goss | Injector and method for fuel injection |
US3062482A (en) * | 1952-08-25 | 1962-11-06 | A V Roe Canada Ltd | Gas turbine engined aircraft |
-
1903
- 1903-02-16 FR FR331292D patent/FR331292A/en not_active Expired
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2546432A (en) * | 1944-03-20 | 1951-03-27 | Power Jets Res & Dev Ltd | Apparatus for deflecting a fuel jet towards a region of turbulence in a propulsive gaseous stream |
US2881588A (en) * | 1948-04-27 | 1959-04-14 | Wilbur H Goss | Injector and method for fuel injection |
US2692480A (en) * | 1948-05-07 | 1954-10-26 | Onera (Off Nat Aerospatiale) | Supersonic internal circulation combustion chamber, in particular combustion chamber for aircraft jet engines |
US3062482A (en) * | 1952-08-25 | 1962-11-06 | A V Roe Canada Ltd | Gas turbine engined aircraft |
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