FR411473A - Turbo-compresseur - Google Patents
Turbo-compresseurInfo
- Publication number
- FR411473A FR411473A FR411473DA FR411473A FR 411473 A FR411473 A FR 411473A FR 411473D A FR411473D A FR 411473DA FR 411473 A FR411473 A FR 411473A
- Authority
- FR
- France
- Prior art keywords
- turbo
- compressor
- 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
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D25/00—Pumping installations or systems
- F04D25/02—Units comprising pumps and their driving means
- F04D25/04—Units comprising pumps and their driving means the pump being fluid-driven
- F04D25/045—Units comprising pumps and their driving means the pump being fluid-driven the pump wheel carrying the fluid driving means, e.g. turbine blades
-
- 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
- F02C3/06—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising only axial stages
- F02C3/073—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising only axial stages the compressor and turbine stages being concentric
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR411473T | 1910-01-11 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| FR411473A true FR411473A (fr) | 1910-06-17 |
Family
ID=1455414
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| FR411473D Expired FR411473A (fr) | 1910-01-11 | 1910-01-11 | Turbo-compresseur |
Country Status (1)
| Country | Link |
|---|---|
| FR (1) | FR411473A (fr) |
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2426008A (en) * | 1944-07-13 | 1947-08-19 | Fairey Aviat Co Ltd | Power unit for aircraft and the like |
| US2429681A (en) * | 1942-02-27 | 1947-10-28 | Griffith Alan Arnold | Thrust balancing construction for turbines, compressors, and the like |
| US2435138A (en) * | 1943-01-15 | 1948-01-27 | Armstrong Siddeley Motors Ltd | Compound internal-combustion turbine plant |
| US2455458A (en) * | 1940-03-02 | 1948-12-07 | Power Jets Res & Dev Ltd | Thrust augmenting device for a system for developing propulsive thrust |
| US2470794A (en) * | 1943-12-20 | 1949-05-24 | Robert E Snyder | In-line fluid pump |
| US2471892A (en) * | 1944-02-14 | 1949-05-31 | Lockheed Aircraft Corp | Reactive propulsion power plant having radial flow compressor and turbine means |
| US2505660A (en) * | 1950-04-25 | Augmentor fob jet propulsion hav | ||
| US2906447A (en) * | 1956-03-30 | 1959-09-29 | Specialties Dev Corp | Inflation equipment |
| US2999631A (en) * | 1958-09-05 | 1961-09-12 | Gen Electric | Dual airfoil |
| EP0021459A1 (fr) * | 1979-04-10 | 1981-01-07 | Hendrik Janus Bakker | Turbo-compresseur entraîné par une turbine |
-
1910
- 1910-01-11 FR FR411473D patent/FR411473A/fr not_active Expired
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2505660A (en) * | 1950-04-25 | Augmentor fob jet propulsion hav | ||
| US2455458A (en) * | 1940-03-02 | 1948-12-07 | Power Jets Res & Dev Ltd | Thrust augmenting device for a system for developing propulsive thrust |
| US2429681A (en) * | 1942-02-27 | 1947-10-28 | Griffith Alan Arnold | Thrust balancing construction for turbines, compressors, and the like |
| US2435138A (en) * | 1943-01-15 | 1948-01-27 | Armstrong Siddeley Motors Ltd | Compound internal-combustion turbine plant |
| US2470794A (en) * | 1943-12-20 | 1949-05-24 | Robert E Snyder | In-line fluid pump |
| US2471892A (en) * | 1944-02-14 | 1949-05-31 | Lockheed Aircraft Corp | Reactive propulsion power plant having radial flow compressor and turbine means |
| US2426008A (en) * | 1944-07-13 | 1947-08-19 | Fairey Aviat Co Ltd | Power unit for aircraft and the like |
| US2906447A (en) * | 1956-03-30 | 1959-09-29 | Specialties Dev Corp | Inflation equipment |
| US2999631A (en) * | 1958-09-05 | 1961-09-12 | Gen Electric | Dual airfoil |
| EP0021459A1 (fr) * | 1979-04-10 | 1981-01-07 | Hendrik Janus Bakker | Turbo-compresseur entraîné par une turbine |
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