GB797025A - Air pressure regulating and shut-off valve - Google Patents
Air pressure regulating and shut-off valveInfo
- Publication number
- GB797025A GB797025A GB1883/56A GB188356A GB797025A GB 797025 A GB797025 A GB 797025A GB 1883/56 A GB1883/56 A GB 1883/56A GB 188356 A GB188356 A GB 188356A GB 797025 A GB797025 A GB 797025A
- Authority
- GB
- United Kingdom
- Prior art keywords
- valve
- piston
- pressure
- line
- bellows
- 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
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16K—VALVES; TAPS; COCKS; ACTUATING-FLOATS; DEVICES FOR VENTING OR AERATING
- F16K31/00—Actuating devices; Operating means; Releasing devices
- F16K31/12—Actuating devices; Operating means; Releasing devices actuated by fluid
- F16K31/42—Actuating devices; Operating means; Releasing devices actuated by fluid by means of electrically-actuated members in the supply or discharge conduits of the fluid motor
-
- 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
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/26—Starting; Ignition
- F02C7/268—Starting drives for the rotor, acting directly on the rotor of the gas turbine to be started
- F02C7/275—Mechanical drives
- F02C7/277—Mechanical drives the starter being a separate turbine
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- Fluid-Driven Valves (AREA)
- Actuator (AREA)
Abstract
797,025. Fluid-pressure servomotor-control systems. BENDIX AVIATION CORPORATION. Jan. 19, 1956 [March 24, 1955], No. 1883/56. Class 135. Energization of a solenoid valve 26 closes a branch line 25 from a main duct 2 to an outer bellows 28, the inner bellows 32 being both coupled to the latter and normally at atmospheric pressure, and vents the bellows conduit 27 whereupon they collapse and move a piston valve 21 to the right, thus opening the top of a cylinder 15 to atmosphere via a port 17 and admitting air from line 25 upstream of the valve 26 to the bottom of the cylinder through a port 19, so elevating a spring-loaded piston 8, which through a piston-rod 12 and linkage 9, 10, opens a butterfly valve 7 in the duct 2 and allows air to flow to a starter turbine 4. The cylinder 15 has a dashpot 20. As the pressure builds up it effects a leftward movement of the inner bellows 32, after traversing a line 35, until the piston valve 21 is returned to the position shown, closing both ports 17, 19; at the same time the piston spring 16, which normally keeps the butterfly valve closed, progressively returns the latter towards the closed position until the desired flow to the turbine is attained. If the pressure in the line increases beyond this value the bellows 32 moves the piston valve to the left of the neutral position, thus venting the lower part of the cylinder 15 and admitting pressure air to the top thereof, so forcing the piston 8 downwards and further closing the butterfly valve 7 to reduce the pressure of air supplied to the turbine. As the pressure in line 35 changes, the piston valve will oscillate over ports 17, 19 to regulate the air pressure supplied to the turbine. Should line 35 break, excessive air pressure downstream of the butterfly valve 7 will act over a line 36 to move a piston 37 against a spring 38 and supply the inner bellows 32 via a channel 39. Upon de-energizing the valve 26 the outer bellows 28, connected to line 25, moves the pilot valve to cause downward movement of the piston 8, so closing the butterfly valve.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US797025XA | 1955-03-24 | 1955-03-24 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB797025A true GB797025A (en) | 1958-06-25 |
Family
ID=22152237
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1883/56A Expired GB797025A (en) | 1955-03-24 | 1956-01-19 | Air pressure regulating and shut-off valve |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB797025A (en) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2158616A (en) * | 1984-05-10 | 1985-11-13 | Anthony Charles Robert Johnson | Hydraulic operated pressure reducing valve |
FR2607189A1 (en) * | 1986-11-20 | 1988-05-27 | Snecma | DEVICE FOR CONTROLLING AN AIRCRAFT TURBOMACHINE STARTING VALVE |
CN104533631A (en) * | 2014-12-03 | 2015-04-22 | 中国航空工业集团公司金城南京机电液压工程研究中心 | Air turbine starter turbine class-front pressure restriction apparatus |
EP2434130A3 (en) * | 2010-09-22 | 2015-06-24 | Hamilton Sundstrand Corporation | Turbine starter valve |
CN110440041A (en) * | 2019-08-28 | 2019-11-12 | 西北工业大学 | One kind can rapid cut-off butterfly valves formula pressure-regulating device |
-
1956
- 1956-01-19 GB GB1883/56A patent/GB797025A/en not_active Expired
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2158616A (en) * | 1984-05-10 | 1985-11-13 | Anthony Charles Robert Johnson | Hydraulic operated pressure reducing valve |
FR2607189A1 (en) * | 1986-11-20 | 1988-05-27 | Snecma | DEVICE FOR CONTROLLING AN AIRCRAFT TURBOMACHINE STARTING VALVE |
EP0270443A1 (en) * | 1986-11-20 | 1988-06-08 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" | Regulating device for the starting valve of a turbo starter for an aircraft engine |
US4805873A (en) * | 1986-11-20 | 1989-02-21 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation "S.N.E.C.M.A." | Control device for a starter valve of a turbine aero-engine |
EP2434130A3 (en) * | 2010-09-22 | 2015-06-24 | Hamilton Sundstrand Corporation | Turbine starter valve |
CN104533631A (en) * | 2014-12-03 | 2015-04-22 | 中国航空工业集团公司金城南京机电液压工程研究中心 | Air turbine starter turbine class-front pressure restriction apparatus |
CN110440041A (en) * | 2019-08-28 | 2019-11-12 | 西北工业大学 | One kind can rapid cut-off butterfly valves formula pressure-regulating device |
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