GB662867A - Improvements relating to gas turbine power plants - Google Patents
Improvements relating to gas turbine power plantsInfo
- Publication number
- GB662867A GB662867A GB868649A GB868649A GB662867A GB 662867 A GB662867 A GB 662867A GB 868649 A GB868649 A GB 868649A GB 868649 A GB868649 A GB 868649A GB 662867 A GB662867 A GB 662867A
- Authority
- GB
- United Kingdom
- Prior art keywords
- turbine
- valves
- valve
- exhaust
- air
- 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
- 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)
- Supercharger (AREA)
- Control Of Throttle Valves Provided In The Intake System Or In The Exhaust System (AREA)
Abstract
662,867. Gas turbine plant. POWER JETS (RESEARCH & DEVELOPMENT). Ltd. March 16, 1950 [March 30, 1949], No. 8686/49. Class 110(iii) [Also in Group XXXI] A gas turbine plant of the kind having a gas generator set comprising a compressor, a combustion system and a compressor driving turbine and an independently rotatable radial-vane centripetal flow turbine for delivering external power has means, operative when the power turbine is overdriven, to permit the relief of working fluid from the power turbine and means to effect a reverse flow of fluid through the power turbine to produce a braking effect. The plant shown comprises a compressor 1, a combustion chamber 2, a compressordriving turbine 4 and a power turbine 5 of the radial-vane centripetal flow type connected to the propelling wheels 6 of a vehicle. The exhaust of the turbine 5 is led through a heat exchanger 7 for preheating the air supply to the combustion chamber. When the turbine 5 is overdriven from the propelling wheels, its rotor will suck air from its exhaust and deliver it into its inlet volute. To divert this air and the exhaust gas from the turbine 4, a valve system 13, 15, is provided. The valve 13 connects the exhaust gas from the turbine 4 and the air from the turbine 5 to the byepass 14. The valve 15 connects the duct 14 to the heat-exchanger 7 and also prevents the exhaust travelling upstream. If desired, the valve 13 may be replaced by two valves 13, 13a, the former being used for the exhaust gases from the turbine 4 and the latter for the air from the turibne 5. A valve 16 which allows the turbine 5 to suck air from the atmosphere is also provided. These valves are operated by a speed governor 19 operated by the cage of a differential gear 18 interconnecting the two turbines, 4, 5. An interlock connection 19b is provided between the throttle 3 and the governor 19 to allow operation of the latter only when the throttle is in the idling position. In a modification these valves are operated solely by the throttle lever when the latter is moved, in the closing direction, past the idling position. In a further modification, the governor 19 is dispensed with, and a reduction or reversing gear provided between the turbine 5 and the differential gear. In this case, the valves are made to open by the differential turning in a particular direction when the turbine 4 is idling. In another modification, the differential gear is dispensed with and the valves operated by a governor driven by the turbine 5 so long as the throttle is in the idling position.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB868649A GB662867A (en) | 1949-03-30 | 1949-03-30 | Improvements relating to gas turbine power plants |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB868649A GB662867A (en) | 1949-03-30 | 1949-03-30 | Improvements relating to gas turbine power plants |
Publications (1)
Publication Number | Publication Date |
---|---|
GB662867A true GB662867A (en) | 1951-12-12 |
Family
ID=9857278
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB868649A Expired GB662867A (en) | 1949-03-30 | 1949-03-30 | Improvements relating to gas turbine power plants |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB662867A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2906092A (en) * | 1955-02-10 | 1959-09-29 | Haltenberger Jules | Gas turbine engine with exhaust heat recovery |
US3236311A (en) * | 1962-10-01 | 1966-02-22 | Bristol Siddeley Engines Ltd | Vertical lift power plants for aircraft |
US3280552A (en) * | 1963-12-26 | 1966-10-25 | Albert G Vath | Gas turbine engines and method of operating the same |
-
1949
- 1949-03-30 GB GB868649A patent/GB662867A/en not_active Expired
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2906092A (en) * | 1955-02-10 | 1959-09-29 | Haltenberger Jules | Gas turbine engine with exhaust heat recovery |
US3236311A (en) * | 1962-10-01 | 1966-02-22 | Bristol Siddeley Engines Ltd | Vertical lift power plants for aircraft |
US3280552A (en) * | 1963-12-26 | 1966-10-25 | Albert G Vath | Gas turbine engines and method of operating the same |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US3054257A (en) | Gas turbine power plant for vehicles | |
GB1308399A (en) | Gas turbine type engines | |
GB1278903A (en) | Turbocharger system for internal combustion engine | |
GB754856A (en) | Improvements relating to the air cooling of gas turbines | |
GB1231668A (en) | ||
GB662867A (en) | Improvements relating to gas turbine power plants | |
JPS57200618A (en) | Turbo super charger mechanism | |
GB925984A (en) | Method and apparatus for controlling speed of engine turbochargers | |
US3893292A (en) | Power turbine deceleration control | |
GB538022A (en) | Improvements in the propulsion of aircraft | |
GB1486741A (en) | Power plant | |
GB746377A (en) | Improvements in or relating to gas turbine installations | |
GB617856A (en) | Improvements relating to vehicle propulsion | |
GB819489A (en) | Improvements in differentially connected twin turbine power plant | |
GB701503A (en) | Improvements relating to gas turbine power plant | |
JPS5481406A (en) | Turbine control system | |
GB652048A (en) | Improvements relating to exhaust driven turbines on reciprocating internal combustion engines | |
GB985702A (en) | Gas turbine engine | |
GB716811A (en) | Improvements in gas turbines for the propulsion of vehicles, particularly locomotives | |
GB1162939A (en) | Improvements relating to Gas-Turbine Engines for Driving Vehicles | |
GB778690A (en) | Improvements relating to power producing equipment incorporating gas turbine plant | |
GB640799A (en) | Auxiliary gas turbine set for aircraft with cabin supercharging | |
US2434160A (en) | Reversible turbine arrangement for | |
GB363325A (en) | A method and means for supplying an engine or generator with fluid under pressure | |
GB711789A (en) | Improvements in or relating to gas-turbine power plants |