FR918317A - Exhaust gas turbo blower feeding a high speed internal combustion engine - Google Patents
Exhaust gas turbo blower feeding a high speed internal combustion engineInfo
- Publication number
- FR918317A FR918317A FR918317DA FR918317A FR 918317 A FR918317 A FR 918317A FR 918317D A FR918317D A FR 918317DA FR 918317 A FR918317 A FR 918317A
- Authority
- FR
- France
- Prior art keywords
- exhaust gas
- combustion engine
- internal combustion
- high speed
- turbo blower
- 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
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D17/00—Regulating or controlling by varying flow
- F01D17/10—Final actuators
- F01D17/12—Final actuators arranged in stator parts
- F01D17/18—Final actuators arranged in stator parts varying effective number of nozzles or guide conduits, e.g. sequentially operable valves for steam turbines
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D17/00—Regulating or controlling by varying flow
- F01D17/10—Final actuators
- F01D17/12—Final actuators arranged in stator parts
- F01D17/14—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits
- F01D17/141—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of shiftable members or valves obturating part of the flow path
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D27/00—Control, e.g. regulation, of pumps, pumping installations or pumping systems specially adapted for elastic fluids
- F04D27/007—Conjoint control of two or more different functions
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2250/00—Geometry
- F05D2250/40—Movement of components
- F05D2250/41—Movement of components with one degree of freedom
- F05D2250/411—Movement of components with one degree of freedom in rotation
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR918317T | 1945-08-10 |
Publications (1)
Publication Number | Publication Date |
---|---|
FR918317A true FR918317A (en) | 1947-02-05 |
Family
ID=9424358
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR918317D Expired FR918317A (en) | 1945-08-10 | 1945-08-10 | Exhaust gas turbo blower feeding a high speed internal combustion engine |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR918317A (en) |
Cited By (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2705590A (en) * | 1949-10-28 | 1955-04-05 | Rolls Royce | Multi-stage axial-flow compressors with adjustable pitch stator blades |
DE1056428B (en) * | 1953-06-09 | 1959-04-30 | Laval Steam Turbine Company De | Method for regulating an internal combustion engine with an exhaust gas turbocharger |
US2933236A (en) * | 1955-12-09 | 1960-04-19 | Power Jets Res & Dev Ltd | Rotary dynamic compressors |
US2935295A (en) * | 1951-01-26 | 1960-05-03 | Thompson Ramo Wooldridge Inc | Throttle configuration varying apparatus and control means therefor |
US3173241A (en) * | 1955-08-29 | 1965-03-16 | Laval Turbine | Turbocharger involving a centripetal turbine |
EP0056669A1 (en) * | 1981-01-21 | 1982-07-28 | ATELIERS DE CONSTRUCTIONS ELECTRIQUES DE CHARLEROI (ACEC) Société Anonyme | Turbine with variable inlet section |
FR2545153A1 (en) * | 1983-04-29 | 1984-11-02 | Microturbo Sa | Improved centripetal turbine |
EP0419871A1 (en) * | 1989-09-29 | 1991-04-03 | React Energy Ltd. | Turbine |
CN110185631A (en) * | 2019-04-18 | 2019-08-30 | 西安热工研究院有限公司 | The symmetrical overcritical working medium closed centrifugal compressor set of partial admission and method |
-
1945
- 1945-08-10 FR FR918317D patent/FR918317A/en not_active Expired
Cited By (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2705590A (en) * | 1949-10-28 | 1955-04-05 | Rolls Royce | Multi-stage axial-flow compressors with adjustable pitch stator blades |
US2935295A (en) * | 1951-01-26 | 1960-05-03 | Thompson Ramo Wooldridge Inc | Throttle configuration varying apparatus and control means therefor |
DE1056428B (en) * | 1953-06-09 | 1959-04-30 | Laval Steam Turbine Company De | Method for regulating an internal combustion engine with an exhaust gas turbocharger |
US3173241A (en) * | 1955-08-29 | 1965-03-16 | Laval Turbine | Turbocharger involving a centripetal turbine |
US2933236A (en) * | 1955-12-09 | 1960-04-19 | Power Jets Res & Dev Ltd | Rotary dynamic compressors |
EP0056669A1 (en) * | 1981-01-21 | 1982-07-28 | ATELIERS DE CONSTRUCTIONS ELECTRIQUES DE CHARLEROI (ACEC) Société Anonyme | Turbine with variable inlet section |
EP0056569A1 (en) * | 1981-01-21 | 1982-07-28 | ATELIERS DE CONSTRUCTIONS ELECTRIQUES DE CHARLEROI (ACEC) Société Anonyme | Turbine with variable inlet section |
FR2545153A1 (en) * | 1983-04-29 | 1984-11-02 | Microturbo Sa | Improved centripetal turbine |
EP0419871A1 (en) * | 1989-09-29 | 1991-04-03 | React Energy Ltd. | Turbine |
CN110185631A (en) * | 2019-04-18 | 2019-08-30 | 西安热工研究院有限公司 | The symmetrical overcritical working medium closed centrifugal compressor set of partial admission and method |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
FR918317A (en) | Exhaust gas turbo blower feeding a high speed internal combustion engine | |
FR1039357A (en) | Fuel nozzle for air-cooled internal combustion engines | |
FR1053105A (en) | Injection internal combustion engine with a supply blower driven by an exhaust gas turbine | |
FR996589A (en) | Improvement in ignition of internal combustion engines | |
FR911142A (en) | Scavenging internal combustion engine driven by an exhaust gas turbine | |
FR934813A (en) | Internal combustion engine | |
FR919930A (en) | Exhaust turbo-blower internal combustion engine | |
FR947832A (en) | Internal combustion engine | |
FR997221A (en) | Improvement in internal combustion engines | |
FR1030063A (en) | Internal combustion engine, including diesel engine powered by an exhaust gas turbocharger | |
FR1006398A (en) | Air-cooled internal combustion engine | |
FR55958E (en) | Rotary internal combustion engine | |
FR931895A (en) | Air-cooled internal combustion engine | |
FR925431A (en) | Air-cooled internal combustion engine | |
FR1067466A (en) | Internal combustion engine with compressor | |
FR933387A (en) | Internal combustion engine | |
FR1027345A (en) | Air-cooled injection internal combustion engine | |
FR916641A (en) | Rotary internal combustion engine | |
FR1043094A (en) | Air-cooled internal combustion engine | |
CH252885A (en) | Ignition device for four-stroke internal combustion engines. | |
FR933612A (en) | Thermal engine, especially internal combustion | |
FR950774A (en) | Internal combustion engine | |
FR995259A (en) | Air-cooled internal combustion engine | |
FR927108A (en) | Internal combustion engine with rotor | |
FR919280A (en) | Rotary internal combustion engine |