GB781962A - Fuel controls for turbo power plants - Google Patents
Fuel controls for turbo power plantsInfo
- Publication number
- GB781962A GB781962A GB1093056A GB1093056A GB781962A GB 781962 A GB781962 A GB 781962A GB 1093056 A GB1093056 A GB 1093056A GB 1093056 A GB1093056 A GB 1093056A GB 781962 A GB781962 A GB 781962A
- Authority
- GB
- United Kingdom
- Prior art keywords
- power plant
- function
- fuel flow
- valve
- power plants
- 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
- F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
- F02C9/16—Control of working fluid flow
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Control Of Turbines (AREA)
Abstract
781,962. Gas turbine plant. UNITED AIRCRAFT CORPORATION. Jan. 6, 1953, No. 10930/56. Divided out of 781,961. Drawings to Specification. Class 110 (3). [Also in Group XXIX] A fuel control system for a gas turbine power plant includes a fuel flow regulating valve, a power-setting lever, means for metering the fuel flow through the valve as a function of the setting of the lever and a power plant temperature, e.g. the compressor inlet temperature, means for limiting the fuel flow through the valve as a function of power plant speed and a power plant temperature, and means for modifying the effect of either or both of the beforementioned means as a function of a power plant pressure, e.g. compressor delivery pressure. The invention is described with reference to Figs. 1 and 4 of Specification 781,961. Specifications 781,963 and 781,964, [both in Group XXIX], also divided from Specification 781,961 are referred to.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1093056A GB781962A (en) | 1953-01-06 | 1953-01-06 | Fuel controls for turbo power plants |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1093056A GB781962A (en) | 1953-01-06 | 1953-01-06 | Fuel controls for turbo power plants |
Publications (1)
Publication Number | Publication Date |
---|---|
GB781962A true GB781962A (en) | 1957-08-28 |
Family
ID=9976933
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1093056A Expired GB781962A (en) | 1953-01-06 | 1953-01-06 | Fuel controls for turbo power plants |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB781962A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP2236794A1 (en) * | 2009-03-19 | 2010-10-06 | Pratt & Whitney Canada Corp. | Control of gas turbine engine |
-
1953
- 1953-01-06 GB GB1093056A patent/GB781962A/en not_active Expired
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP2236794A1 (en) * | 2009-03-19 | 2010-10-06 | Pratt & Whitney Canada Corp. | Control of gas turbine engine |
US8099227B2 (en) | 2009-03-19 | 2012-01-17 | Pratt & Whitney Canada Corp. | Control of gas turbine engine |
US8538658B2 (en) | 2009-03-19 | 2013-09-17 | Pratt & Whitney Canada Corp. | Control of gas turbine engine |
US8886438B2 (en) | 2009-03-19 | 2014-11-11 | Pratt & Whitney Canada Corp. | Control of gas turbine engine |
US9382849B2 (en) | 2009-03-19 | 2016-07-05 | Pratt & Whitney Canada Corp. | Control of gas turbine engine |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
GB790836A (en) | Improvements in or relating to gas-turbine engine cooling arrangements | |
GB781962A (en) | Fuel controls for turbo power plants | |
GB671379A (en) | Improvements in or relating to fuel systems for gas-turbine aircraft engines | |
GB659569A (en) | Improvements in or relating to lubrication systems for aviation power plants | |
GB729272A (en) | Fuel control system for gas turbines | |
GB616622A (en) | Improvements in or relating to gas-turbines and controlling means therefor | |
GB729300A (en) | Fuel control system for gas turbines | |
GB742270A (en) | Improvements relating to gas-turbine engine fuel systems | |
GB745146A (en) | Fuel feed and power control system for gas turbine engines | |
GB852346A (en) | Improvements in or relating to engine control systems | |
GB827282A (en) | Improvements in or relating to pressure-sensitive control mechanisms | |
GB802923A (en) | Improvements in or relating to fuel supply systems for gas turbine engines | |
GB738895A (en) | Devices for automatically controlling the secondary fuel supply in jet propulsion and other gas turbine engines | |
GB1084957A (en) | Improvements in or relating to turbojets with afterburner and variable area nozzle means | |
GB721459A (en) | Internal combustion turbine power plants | |
GB866461A (en) | A turbo-unit for supplying charging and cooling air for an internal-combustion engine | |
GB710261A (en) | Improvements in or relating to control arrangements for gas turbines and other primemovers | |
GB711846A (en) | Control device for gas turbine aircraft propulsion units | |
GB871474A (en) | A servomotor operated fuel control system for a gas turbine power plant | |
GB837957A (en) | Improvements in or relating to burners | |
GB861761A (en) | Improvements relating to aircraft auxiliary installations | |
GB816553A (en) | Fuel control means for gas turbines | |
GB1067110A (en) | Fuel control apparatus for a gas turbine engine | |
GB1507907A (en) | Fuel supply control apparatus for a gasturbine engine | |
GB714140A (en) | Improvements in or relating to control systems for engines |