GB601170A - Improvements in internal combustion turbine plant for propulsion - Google Patents
Improvements in internal combustion turbine plant for propulsionInfo
- Publication number
- GB601170A GB601170A GB1655345A GB1655345A GB601170A GB 601170 A GB601170 A GB 601170A GB 1655345 A GB1655345 A GB 1655345A GB 1655345 A GB1655345 A GB 1655345A GB 601170 A GB601170 A GB 601170A
- Authority
- GB
- United Kingdom
- Prior art keywords
- turbine
- ducts
- plant
- airscrew
- stage
- 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 abstract 3
- 239000007789 gas Substances 0.000 abstract 3
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
- F02K1/78—Other construction of jet pipes
-
- 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
- F02C3/067—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 having counter-rotating rotors
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
601,170. Propelling ships and aircraft. SMITH, D. M., and METROPOLITANVICKERS ELECTRICAL CO., Ltd. June 28, 1945, No. 16553. [Classes 4 and 114] [Also in Group XXVI] In a gas turbine plant comprising an axial flow compressor 1, an annular combustion chamber or group of annularly arranged combustion chambers 2, a turbine 4 driving the compressor 1 and a two-stage turbine 8, 9 in axial alignment and in which each stage of the turbine 8, 9 is direct coupled to an element of a contra-rotational pusher airscrew 10, 11, the exhaust ducts 15 finally leaving the power turbine are flared with respect to the plant axis so that either the hot gases will mix with the external air and flow therewith through the airscrew or said ducts have a large radial component so that the gases flow outside the peripheries of the airscrews. There may be provided more than two ducts 15, which may be annularly distributed around the axis. The ducts 15 are preferably of streamline form.
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB601170A true GB601170A (en) | 1948-04-29 |
Family
ID=1732383
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB1655345A Expired GB601170A (en) | 1945-06-28 | Improvements in internal combustion turbine plant for propulsion |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB601170A (en) |
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE963203C (en) * | 1952-05-06 | 1957-05-02 | Alfred Buechi | Propeller turbine engine |
| US2912823A (en) * | 1955-11-25 | 1959-11-17 | Gen Electric | Gas turbine engine with free turbine power take-off |
| GB2117054A (en) * | 1982-02-17 | 1983-10-05 | Rolls Royce | Aircraft propulsion engine having a rear mounted propfan |
| GB2138507A (en) * | 1983-04-22 | 1984-10-24 | Rolls Royce | Mounting end exhausting in turbo-propellor aircraft engines |
| US4789304A (en) * | 1987-09-03 | 1988-12-06 | United Technologies Corporation | Insulated propeller blade |
| FR2622637A1 (en) * | 1987-10-22 | 1989-05-05 | United Technologies Corp | EXHAUST NOZZLE FOR A PROPULSIVE PROPELLER PROPULSION DEVICE |
| US5197855A (en) * | 1991-07-01 | 1993-03-30 | United Technologies Corporation | Engine exhaust/blade interaction noise suppression |
| WO2011107320A1 (en) | 2010-03-03 | 2011-09-09 | Rolls-Royce Plc | Flow mixer and corresponding gas turbine engine |
-
1945
- 1945-06-28 GB GB1655345A patent/GB601170A/en not_active Expired
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE963203C (en) * | 1952-05-06 | 1957-05-02 | Alfred Buechi | Propeller turbine engine |
| US2912823A (en) * | 1955-11-25 | 1959-11-17 | Gen Electric | Gas turbine engine with free turbine power take-off |
| GB2117054A (en) * | 1982-02-17 | 1983-10-05 | Rolls Royce | Aircraft propulsion engine having a rear mounted propfan |
| US4488399A (en) * | 1982-02-17 | 1984-12-18 | Rolls-Royce Limited | Propfan aircraft propulsion engine |
| GB2138507A (en) * | 1983-04-22 | 1984-10-24 | Rolls Royce | Mounting end exhausting in turbo-propellor aircraft engines |
| US4789304A (en) * | 1987-09-03 | 1988-12-06 | United Technologies Corporation | Insulated propeller blade |
| FR2622637A1 (en) * | 1987-10-22 | 1989-05-05 | United Technologies Corp | EXHAUST NOZZLE FOR A PROPULSIVE PROPELLER PROPULSION DEVICE |
| US4864820A (en) * | 1987-10-22 | 1989-09-12 | United Technologies Corporation | Exhaust nozzle |
| US5197855A (en) * | 1991-07-01 | 1993-03-30 | United Technologies Corporation | Engine exhaust/blade interaction noise suppression |
| WO2011107320A1 (en) | 2010-03-03 | 2011-09-09 | Rolls-Royce Plc | Flow mixer and corresponding gas turbine engine |
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