GB587516A - Improvements in or relating to regulating means for gas turbine installations - Google Patents
Improvements in or relating to regulating means for gas turbine installationsInfo
- Publication number
- GB587516A GB587516A GB282443A GB282443A GB587516A GB 587516 A GB587516 A GB 587516A GB 282443 A GB282443 A GB 282443A GB 282443 A GB282443 A GB 282443A GB 587516 A GB587516 A GB 587516A
- Authority
- GB
- United Kingdom
- Prior art keywords
- air
- screws
- rotors
- pump
- oil
- 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
- 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
- F02K1/06—Varying effective area of jet pipe or nozzle
- F02K1/15—Control or regulation
- F02K1/16—Control or regulation conjointly with another control
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Supercharger (AREA)
- Control Of Turbines (AREA)
- Transmission Devices (AREA)
Abstract
587,516. Gas turbines; jet propulsion of aircraft; speed governors. BRISTOL AEROPLANE CO., Ltd., and FORTESCUE, P. Feb. 19, 1943, No. 2824. [Classes 57 and 110 (iii)] [Also in Group XXIX] The gas turbine plant of an aircraft drives one, or, a pair of air-screws and provides a propulsive jet. The turbine comprises two rotors, one of which drives the air compressor and the other the air-screws, and the power taken by the air-screws is governed, by varying the pitch of the blades, to maintain a constant ratio between the speeds of the two rotors. To this end, the turbine rotors drive opposite members of a bevel gear differential and the cage, carrying the planet wheels which rotates when the driven wheels do not rotate equally in opposite directions, is geared to an oil pump 88, Fig. 3. This pump transfers oil from one end to the other of a cylinder containing a valve 83 and consequent movement of this valve admits oil from a pump 77 to one side or other of a piston 74 and empowers the latter to vary the pitch of the air-screw blade 73. Specification 587,558 is referred to.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB282443A GB587516A (en) | 1943-02-19 | 1943-02-19 | Improvements in or relating to regulating means for gas turbine installations |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB282443A GB587516A (en) | 1943-02-19 | 1943-02-19 | Improvements in or relating to regulating means for gas turbine installations |
Publications (1)
Publication Number | Publication Date |
---|---|
GB587516A true GB587516A (en) | 1947-04-29 |
Family
ID=9746628
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB282443A Expired GB587516A (en) | 1943-02-19 | 1943-02-19 | Improvements in or relating to regulating means for gas turbine installations |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB587516A (en) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2590932A (en) * | 1948-06-22 | 1952-04-01 | United Aircraft Corp | Aircraft turbine-propeller control system |
US2605851A (en) * | 1946-11-30 | 1952-08-05 | Chrysler Corp | Air intake for aircraft turbopropeller power plant |
US2619797A (en) * | 1948-01-28 | 1952-12-02 | Rolls Royce | Gas turbine engine driving a propeller |
US2696268A (en) * | 1948-10-05 | 1954-12-07 | Bristol Aeroplane Co Ltd | Control system for gas turbine power plants and variable pitch propellers driven thereby |
US2746246A (en) * | 1952-09-05 | 1956-05-22 | Valota Alessandro | Axial flow gas turbine |
-
1943
- 1943-02-19 GB GB282443A patent/GB587516A/en not_active Expired
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2605851A (en) * | 1946-11-30 | 1952-08-05 | Chrysler Corp | Air intake for aircraft turbopropeller power plant |
US2619797A (en) * | 1948-01-28 | 1952-12-02 | Rolls Royce | Gas turbine engine driving a propeller |
US2590932A (en) * | 1948-06-22 | 1952-04-01 | United Aircraft Corp | Aircraft turbine-propeller control system |
US2696268A (en) * | 1948-10-05 | 1954-12-07 | Bristol Aeroplane Co Ltd | Control system for gas turbine power plants and variable pitch propellers driven thereby |
US2746246A (en) * | 1952-09-05 | 1956-05-22 | Valota Alessandro | Axial flow gas turbine |
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