GB802923A - Improvements in or relating to fuel supply systems for gas turbine engines - Google Patents
Improvements in or relating to fuel supply systems for gas turbine enginesInfo
- Publication number
- GB802923A GB802923A GB35467/55A GB3546755A GB802923A GB 802923 A GB802923 A GB 802923A GB 35467/55 A GB35467/55 A GB 35467/55A GB 3546755 A GB3546755 A GB 3546755A GB 802923 A GB802923 A GB 802923A
- Authority
- GB
- United Kingdom
- Prior art keywords
- speed
- valve
- over
- fuel
- fuelling
- 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)
- Output Control And Ontrol Of Special Type Engine (AREA)
Abstract
802,923. Gas turbine plant; speed governors. HOBSON, Ltd., H. M. Dec. 7, 1956 [Dec. 9, 1955], No. 35467/55. Addition to 712,646. Classes 57 and 110 (3). [Also in Group XXIX] The fuel supply apparatus for gas turbines described in the parent Specification is modified by arranging that the speed governor is adjustable to reduce the controlled speed to a value such that the governor is operative on the metering valve 26 to control the flow of fuel to the engine at a speed below the upper limit of the speed range in which the over-fuelling valve 22 is effective to restrict the fuel flow. To provide adequate pressure to operate the metering valve at the minimum controlled speed, the left-hand side of the servo-piston 27 instead of being connected to the downstream side of the over-fuelling valve 22 is connected by a duct 53 to the inlet side of orifice 23 and hence to the delivery of the engine-driven fuel pump supplying the over-fuelling valve. Adj ustment of the loading spring 19 of the servo-control valve 18 in this case is effected by a leveroperated eccentric 51 which acts through a follower 52 on a lever 20 constituting an abutment for the spring 19.
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB164652A GB712646A (en) | 1952-02-21 | 1952-02-21 | Improvements in or relating to fuel supply systems for gas turbine engines |
GB35467/55A GB802923A (en) | 1952-02-21 | 1955-12-09 | Improvements in or relating to fuel supply systems for gas turbine engines |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB164652A GB712646A (en) | 1952-02-21 | 1952-02-21 | Improvements in or relating to fuel supply systems for gas turbine engines |
GB35467/55A GB802923A (en) | 1952-02-21 | 1955-12-09 | Improvements in or relating to fuel supply systems for gas turbine engines |
Publications (1)
Publication Number | Publication Date |
---|---|
GB802923A true GB802923A (en) | 1958-10-15 |
Family
ID=62529054
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB164652A Expired GB712646A (en) | 1952-02-21 | 1952-02-21 | Improvements in or relating to fuel supply systems for gas turbine engines |
GB35467/55A Expired GB802923A (en) | 1952-02-21 | 1955-12-09 | Improvements in or relating to fuel supply systems for gas turbine engines |
Family Applications Before (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB164652A Expired GB712646A (en) | 1952-02-21 | 1952-02-21 | Improvements in or relating to fuel supply systems for gas turbine engines |
Country Status (1)
Country | Link |
---|---|
GB (2) | GB712646A (en) |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2946188A (en) * | 1954-12-09 | 1960-07-26 | Bendix Aviat Corp | Acceleration scheduling and isochronous governing fuel feed and power control devicefor gas turbine engines |
GB897091A (en) * | 1959-07-20 | 1962-05-23 | Rolls Royce | Gas turbine engine fuel system |
-
1952
- 1952-02-21 GB GB164652A patent/GB712646A/en not_active Expired
-
1955
- 1955-12-09 GB GB35467/55A patent/GB802923A/en not_active Expired
Also Published As
Publication number | Publication date |
---|---|
GB712646A (en) | 1954-07-28 |
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