BE468782A - - Google Patents
Info
- Publication number
- BE468782A BE468782A BE468782DA BE468782A BE 468782 A BE468782 A BE 468782A BE 468782D A BE468782D A BE 468782DA BE 468782 A BE468782 A BE 468782A
- Authority
- BE
- Belgium
Links
Classifications
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- 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
- F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas- turbine plants for special use
- F02C6/20—Adaptations of gas-turbine plants for driving vehicles
- F02C6/206—Adaptations of gas-turbine plants for driving vehicles the vehicles being airscrew driven
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- 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
- F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
- F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
- F02K3/062—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type with aft fan
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- 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
- F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
- F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
- F02K3/072—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type with counter-rotating, e.g. fan rotors
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB47242A GB586557A (en) | 1942-01-12 | 1942-01-12 | Improvements in internal combustion turbine plant for propulsion |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| BE468782A true BE468782A (pt) |
Family
ID=9704953
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| BE468782D BE468782A (pt) | 1942-01-12 |
Country Status (4)
| Country | Link |
|---|---|
| BE (1) | BE468782A (pt) |
| ES (1) | ES175239A1 (pt) |
| FR (1) | FR942481A (pt) |
| GB (1) | GB586557A (pt) |
Families Citing this family (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3381475A (en) * | 1965-06-28 | 1968-05-07 | Bristol Siddeley Engines Ltd | Jet propulsion engines |
| GB2117054B (en) * | 1982-02-17 | 1985-01-30 | Rolls Royce | Aircraft propulsion engine having a rear mounted propfan |
| GB2173863B (en) * | 1985-04-17 | 1989-07-19 | Rolls Royce Plc | A propeller module for an aero gas turbine engine |
| US4815273A (en) * | 1985-12-31 | 1989-03-28 | Peter Rudolph | Single propeller turboprop propulsion apparatus |
| US4817382A (en) * | 1985-12-31 | 1989-04-04 | The Boeing Company | Turboprop propulsion apparatus |
| GB2209575A (en) * | 1987-09-05 | 1989-05-17 | Rolls Royce Plc | A gearbox arrangement for driving contra-rotating multi-bladed rotors |
| US4936748A (en) * | 1988-11-28 | 1990-06-26 | General Electric Company | Auxiliary power source in an unducted fan gas turbine engine |
| US5108259A (en) * | 1988-12-19 | 1992-04-28 | General Electric Company | Flexible connector for use in aircraft |
| US5010729A (en) * | 1989-01-03 | 1991-04-30 | General Electric Company | Geared counterrotating turbine/fan propulsion system |
| FR2940247B1 (fr) * | 2008-12-19 | 2011-01-21 | Snecma | Systeme d'helices contrarotatives entrainees par un train epicycloidal offrant une repartition de couple equilibree entre les deux helices |
| FR2948921A1 (fr) * | 2009-11-25 | 2011-02-11 | Snecma | Systeme d'helices contrarotatives comprenant des moyens ameliores d'equilibrage de couple |
| FR2955085B1 (fr) * | 2010-01-08 | 2011-12-23 | Snecma | Systeme d'helices contrarotatives pour turbomachine d'aeronef |
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0
- BE BE468782D patent/BE468782A/xx unknown
-
1942
- 1942-01-12 GB GB47242A patent/GB586557A/en not_active Expired
-
1946
- 1946-08-28 FR FR942481D patent/FR942481A/fr not_active Expired
- 1946-10-09 ES ES175239A patent/ES175239A1/es not_active Expired
Also Published As
| Publication number | Publication date |
|---|---|
| ES175239A1 (es) | 1946-11-16 |
| GB586557A (en) | 1947-03-24 |
| FR942481A (fr) | 1949-02-09 |