GB490978A - Improvements in and relating to the regulation of gas turbines - Google Patents
Improvements in and relating to the regulation of gas turbinesInfo
- Publication number
- GB490978A GB490978A GB30163/37A GB3016337A GB490978A GB 490978 A GB490978 A GB 490978A GB 30163/37 A GB30163/37 A GB 30163/37A GB 3016337 A GB3016337 A GB 3016337A GB 490978 A GB490978 A GB 490978A
- Authority
- GB
- United Kingdom
- Prior art keywords
- pipe
- oil
- compressor
- turbine
- chamber
- 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
Landscapes
- Engine Equipment That Uses Special Cycles (AREA)
Abstract
490,978. Gas turbine plant. AKT.- GES. BROWN, BOVERI, & CIE. Nov. 3, 1937, No. 30163. Convention date, Nov. 3, 1936. [Class 110 (iii)] A gas turbine plant, comprising a turbine Tg driving an electrical generator G and plant auxiliaries, and a second turbine Tc driving a compressor C, has the quantity of fuel supplied to a combustion chamber A regulated in accordance with the speed of the turbine Tg and the outlet air pressure of the compressor C. A pump M supplies fuel to the burner, and a pump P feeds oil to the bearings by way of a pipe U, and oil for controls Z, S, D. A pipe W leads air from the compressor to beneath a diaphragm L, and oil from a pipe N enters a cylinder D and flows through an outlet hole F. The cylinder D and piston T may both be moved axially to control the quantity of oil passing through the hole F. A piston S is under the influence of oil in a pipe J and a spring, to control the quantity of fuel passing to the chamber A. The temperature of the gases leaving the chamber A may be kept constant by means of a mixture regulator comprising two diaphragms X, Y. The spaces on each side of X are connected to opposite sides of a measuring constriction in the pipe E, and the spaces on opposite sides of Y, to a measuring constriction in the air intake pipe of the compressor C.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR490978X | 1936-11-03 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB490978A true GB490978A (en) | 1938-08-24 |
Family
ID=8904409
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB30163/37A Expired GB490978A (en) | 1936-11-03 | 1937-11-03 | Improvements in and relating to the regulation of gas turbines |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB490978A (en) |
Cited By (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2469678A (en) * | 1943-12-18 | 1949-05-10 | Edwin T Wyman | Combination steam and gas turbine |
| US2503048A (en) * | 1945-12-27 | 1950-04-04 | Lucas Ltd Joseph | Means for controlling the flow of liquid fuel to prime movers |
| US2618927A (en) * | 1946-06-25 | 1952-11-25 | Niles Bement Pond Co | Fuel and torque control apparatus for internal-combustion engines |
| US2643514A (en) * | 1948-08-23 | 1953-06-30 | Rolls Royce | Fuel system for gas-turbine engines with means to maintain the fuel supply within desired limits during transient operating conditions |
| US2664151A (en) * | 1947-05-12 | 1953-12-29 | Rolls Royce | Control means for fuel systems of gas turbine engines |
| US2669094A (en) * | 1947-02-01 | 1954-02-16 | Niles Bement Pond Co | Fuel control apparatus for jet engines |
| US2669838A (en) * | 1946-09-13 | 1954-02-23 | Niles Bement Pond Co | Fluid pump control apparatus for internal-combustion turbine engines |
| US2671860A (en) * | 1947-06-26 | 1954-03-09 | Bendix Aviat Corp | Load sensitive fuel governor for gas turbines |
| US2688844A (en) * | 1945-03-05 | 1954-09-14 | Power Jets Res & Dev Ltd | Rotary compressor and its control, and application thereof in combustion turbine power plant |
| US2697909A (en) * | 1946-04-23 | 1954-12-28 | Niles Bement Pond Co | Fuel control for turbojet engines |
| US2700872A (en) * | 1947-01-11 | 1955-02-01 | Niles Bement Pond Co | Fuel control apparatus for internalcombustion engines |
| US2743051A (en) * | 1950-07-03 | 1956-04-24 | Power Jets Res & Dev Ltd | Gas turbine plant |
| DE1097763B (en) * | 1954-03-01 | 1961-01-19 | Bendix Corp | Fuel quantity control system for a gas turbine system working with a compressor |
-
1937
- 1937-11-03 GB GB30163/37A patent/GB490978A/en not_active Expired
Cited By (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2469678A (en) * | 1943-12-18 | 1949-05-10 | Edwin T Wyman | Combination steam and gas turbine |
| US2688844A (en) * | 1945-03-05 | 1954-09-14 | Power Jets Res & Dev Ltd | Rotary compressor and its control, and application thereof in combustion turbine power plant |
| US2503048A (en) * | 1945-12-27 | 1950-04-04 | Lucas Ltd Joseph | Means for controlling the flow of liquid fuel to prime movers |
| US2697909A (en) * | 1946-04-23 | 1954-12-28 | Niles Bement Pond Co | Fuel control for turbojet engines |
| US2618927A (en) * | 1946-06-25 | 1952-11-25 | Niles Bement Pond Co | Fuel and torque control apparatus for internal-combustion engines |
| US2669838A (en) * | 1946-09-13 | 1954-02-23 | Niles Bement Pond Co | Fluid pump control apparatus for internal-combustion turbine engines |
| US2700872A (en) * | 1947-01-11 | 1955-02-01 | Niles Bement Pond Co | Fuel control apparatus for internalcombustion engines |
| US2669094A (en) * | 1947-02-01 | 1954-02-16 | Niles Bement Pond Co | Fuel control apparatus for jet engines |
| US2664151A (en) * | 1947-05-12 | 1953-12-29 | Rolls Royce | Control means for fuel systems of gas turbine engines |
| US2671860A (en) * | 1947-06-26 | 1954-03-09 | Bendix Aviat Corp | Load sensitive fuel governor for gas turbines |
| US2643514A (en) * | 1948-08-23 | 1953-06-30 | Rolls Royce | Fuel system for gas-turbine engines with means to maintain the fuel supply within desired limits during transient operating conditions |
| US2743051A (en) * | 1950-07-03 | 1956-04-24 | Power Jets Res & Dev Ltd | Gas turbine plant |
| DE1097763B (en) * | 1954-03-01 | 1961-01-19 | Bendix Corp | Fuel quantity control system for a gas turbine system working with a compressor |
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