GB603283A - Improvements in or relating to internal combustion turbine power plants - Google Patents
Improvements in or relating to internal combustion turbine power plantsInfo
- Publication number
- GB603283A GB603283A GB1855447A GB1855447A GB603283A GB 603283 A GB603283 A GB 603283A GB 1855447 A GB1855447 A GB 1855447A GB 1855447 A GB1855447 A GB 1855447A GB 603283 A GB603283 A GB 603283A
- Authority
- GB
- United Kingdom
- Prior art keywords
- turbine
- relating
- internal combustion
- power plants
- turbine power
- 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 1
- 235000013175 Crataegus laevigata Nutrition 0.000 abstract 1
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
- 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
-
- 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
- F02C3/10—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor with another turbine driving an output shaft but not driving the compressor
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
603,283. Gas turbine plant for aircraft. POWER JETS (RESEARCH & DEVELOPMENT), Ltd., and HAWTHORNE, W. R. June 27, 1946, No. 18554/47. Drawings to Specification. [Class 110 (iii)] A gas turbine plant comprising a h.p. compressor driven by a h.p. turbine and a l.p. compressor driven by a l.p. turbine differs from that described in Specification 602,584 in that the air-screw shaft is directly connected to the l.p. turbine shaft and speed-reduction gear, if any, for the airscrew is located forwardly of the h.p. turbine. The turbine exhaust may be led to a propulsion jet.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1855447A GB603283A (en) | 1946-06-27 | 1946-06-27 | Improvements in or relating to internal combustion turbine power plants |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1855447A GB603283A (en) | 1946-06-27 | 1946-06-27 | Improvements in or relating to internal combustion turbine power plants |
Publications (1)
Publication Number | Publication Date |
---|---|
GB603283A true GB603283A (en) | 1948-06-11 |
Family
ID=10114436
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1855447A Expired GB603283A (en) | 1946-06-27 | 1946-06-27 | Improvements in or relating to internal combustion turbine power plants |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB603283A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0395497A1 (en) * | 1989-04-26 | 1990-10-31 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" | Counter rotating prop-fan engine |
US9644537B2 (en) | 2013-03-14 | 2017-05-09 | United Technologies Corporation | Free stream intake with particle separator for reverse core engine |
FR3061241A1 (en) * | 2016-12-23 | 2018-06-29 | Safran Aircraft Engines | REVERSE FLOW TURBOPROPULSER |
EP3572638B1 (en) * | 2016-07-19 | 2020-12-23 | Pratt & Whitney Canada Corp. | Turboprop engine |
-
1946
- 1946-06-27 GB GB1855447A patent/GB603283A/en not_active Expired
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0395497A1 (en) * | 1989-04-26 | 1990-10-31 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" | Counter rotating prop-fan engine |
FR2646473A1 (en) * | 1989-04-26 | 1990-11-02 | Snecma | ENGINE WITH TRACTRIC CONTROTOTATIVE BLOWERS |
US5105618A (en) * | 1989-04-26 | 1992-04-21 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation "S.N.E.C.M.A." | Counterrotating fan engine |
US9644537B2 (en) | 2013-03-14 | 2017-05-09 | United Technologies Corporation | Free stream intake with particle separator for reverse core engine |
EP3572638B1 (en) * | 2016-07-19 | 2020-12-23 | Pratt & Whitney Canada Corp. | Turboprop engine |
FR3061241A1 (en) * | 2016-12-23 | 2018-06-29 | Safran Aircraft Engines | REVERSE FLOW TURBOPROPULSER |
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