GB734810A - A pneumatically actuated governor for regulating fuel flow to an internal combustionengine - Google Patents
A pneumatically actuated governor for regulating fuel flow to an internal combustionengineInfo
- Publication number
- GB734810A GB734810A GB10552/53A GB1055253A GB734810A GB 734810 A GB734810 A GB 734810A GB 10552/53 A GB10552/53 A GB 10552/53A GB 1055253 A GB1055253 A GB 1055253A GB 734810 A GB734810 A GB 734810A
- Authority
- GB
- United Kingdom
- Prior art keywords
- valve
- bellows
- diaphragm
- stem
- passage
- 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
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D3/00—Controlling low-pressure fuel injection, i.e. where the fuel-air mixture containing fuel thus injected will be substantially compressed by the compression stroke of the engine, by means other than controlling only an injection pump
- F02D3/02—Controlling low-pressure fuel injection, i.e. where the fuel-air mixture containing fuel thus injected will be substantially compressed by the compression stroke of the engine, by means other than controlling only an injection pump with continuous injection or continuous flow upstream of the injection nozzle
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- High-Pressure Fuel Injection Pump Control (AREA)
Abstract
734,810. Gas turbine plant. GARRETT CORPORATION. April 17, 1953 [May 2, 1952], No. 10552/53. Class 110 (3). [Also in Group XXIX] A pneumatically-actuated governor for controlling the fuel supply to a gas turbine engine in dependence on the ratio of the pressures on opposite sides of the engine compressor and also on the ambient air temperature comprises a casing 26 having a chamber divided into two compartments 27, 50 by a movable wall such as the flexible diaphragm 49, a valve 33 operatively connected to the movable wall and adapted to control a passage 25 connecting the compartment 27 on one side of the wall with a fluid-pressure actuated fuel control means V, and means such as the bellows 53 for modifying the actuation of the valve 33 by the movable wall in response to changes in the ambient barometric pressure and temperature. The turbine T has a combustion chamber 10 supplied with air by the compressor C and with fuel by a nozzle 11 supplied by a pump P. The compartment 27 is exposed to the outlet pressure of the compressor by a pipe 40 and the compartment 50 is open at atmospheric pressure through a port 51. The fuel pump P has a by-pass 12 regulated by a diaphragm-actuated by-pass valve 23 controlled by the valve 33. The control chamber 19 of the by-pass valve 23 communicates by the passage 25 and a restriction 30 with a passage 29. A recess 28 below the restriction 30 communicates with a vent passage 31 adjustable by a metering valve 32. The bellows 53 comprises inner and outer walls, the space between which is charged with air or other suitable medium to detect also changes in the atmospheric temperature. The head 54 of the bellows is exposed to atmospheric pressure and is loaded by a spring 64 which can be adjusted by a ring 65 screwed into an openended sleeve 66. The sleeve is clamped in spaced relation to the end cover 48 by screws 67. The valve 33 is opened against a spring by a screw-threaded stem 55 which is adjustably connected to the diaphragm 49 and to the head 54 of the bellows.' Thus by slackening a nut 59, the stem 55 may be rotated in a nut 56 clamped to the diaphragm 49 so that the central area of the diaphragm is raised or lowered and the effective area of the diaphragm decreased or increased. The stem 55 may be raised or lowered to alter its position with reference to the valve 33 by rotation of a nut 61 mounted in the bellows head 54. The interior of the bellows is open to atmospheric pressure through the clearance 58 between the end cover 48 and the stem 55. A single-walled bellows may be used in some cases.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US734810XA | 1952-05-02 | 1952-05-02 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB734810A true GB734810A (en) | 1955-08-10 |
Family
ID=22113941
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB10552/53A Expired GB734810A (en) | 1952-05-02 | 1953-04-17 | A pneumatically actuated governor for regulating fuel flow to an internal combustionengine |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB734810A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3791399A (en) * | 1971-03-16 | 1974-02-12 | Gachot Jean | Pressure regulators for compressed-air circuits |
-
1953
- 1953-04-17 GB GB10552/53A patent/GB734810A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3791399A (en) * | 1971-03-16 | 1974-02-12 | Gachot Jean | Pressure regulators for compressed-air circuits |
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