GB604304A - Improvements in automatic devices for controlling the pressure in flying suits designed to prevent "black-out" in aircraft pilots - Google Patents
Improvements in automatic devices for controlling the pressure in flying suits designed to prevent "black-out" in aircraft pilotsInfo
- Publication number
- GB604304A GB604304A GB2020945A GB2020945A GB604304A GB 604304 A GB604304 A GB 604304A GB 2020945 A GB2020945 A GB 2020945A GB 2020945 A GB2020945 A GB 2020945A GB 604304 A GB604304 A GB 604304A
- Authority
- GB
- United Kingdom
- Prior art keywords
- valve
- piston
- spring
- suit
- aircraft
- 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
- F16K1/00—Lift valves or globe valves, i.e. cut-off apparatus with closure members having at least a component of their opening and closing motion perpendicular to the closing faces
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Safety Valves (AREA)
- Control Of Fluid Pressure (AREA)
Abstract
604,304. Valves. HYMATIC ENGINEERING CO., Ltd., (formerly HEYWOOD COMPRESSOR CO., Ltd.), JAY, J. B., and HUNT, J. A. Aug. 7, 1945, No. 20209. [Class 135] A valve for controlling automatically the inflation of a flying suit to prevent blackout of the pilot when making sharp turns or pulling out of a dive, comprises a casing a having an inlet o connected to the compressed air system of the aircraft and an outlet p to the flying suit, and a double-beat valve n of, e.g. moulded rubber, as described in Specification 597,103, [Group XI], and mounted on a spring-loaded carrier m, the.opening of which is controlled by a piston c carrying a weight b and secured to a rod d supported by a spring e itself supported by a spring-loaded piston f. Normally, the weight is held against the valve cover h by the springs, but when the acceleration of the aircraft normal to the direction of flight reaches, say, 2g, the piston c is moved against the springs until it contacts with and opens the valve n. The air pressure on the piston f reduces the upward thrust on the valve carrier m and thus permits rapid opening of the valve. Upon reduction of the acceleration, the valve closes and air is permitted to flow from the suit to the atmosphere through ports a<SP>1</SP>, c<SP>1</SP> in the casing and the piston c respectively. The valve is provided with a test push-button i.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2020945A GB604304A (en) | 1945-08-07 | 1945-08-07 | Improvements in automatic devices for controlling the pressure in flying suits designed to prevent "black-out" in aircraft pilots |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2020945A GB604304A (en) | 1945-08-07 | 1945-08-07 | Improvements in automatic devices for controlling the pressure in flying suits designed to prevent "black-out" in aircraft pilots |
Publications (1)
Publication Number | Publication Date |
---|---|
GB604304A true GB604304A (en) | 1948-07-01 |
Family
ID=10142225
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB2020945A Expired GB604304A (en) | 1945-08-07 | 1945-08-07 | Improvements in automatic devices for controlling the pressure in flying suits designed to prevent "black-out" in aircraft pilots |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB604304A (en) |
Cited By (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2620813A (en) * | 1950-12-22 | 1952-12-09 | Chloride Electrical Storage Co | Selector mechanism |
US2654381A (en) * | 1947-06-20 | 1953-10-06 | Hobbs Transmission Ltd | Variable-ratio power transmitting apparatus |
US2676601A (en) * | 1951-05-29 | 1954-04-27 | Dunlop Rubber Co | Fluid pressure valve |
US2683001A (en) * | 1951-04-30 | 1954-07-06 | Bendix Aviat Corp | Acceleration responsive fluid pressure distribution control system |
US2748786A (en) * | 1950-07-14 | 1956-06-05 | Isreeli Jack | Pressure-control apparatus for anti-g suits |
US2753881A (en) * | 1951-09-14 | 1956-07-10 | Bendix Aviat Corp | G responsive valve |
US2789556A (en) * | 1953-05-11 | 1957-04-23 | Clark | Valve and system for the protection of aircraft occupants |
US2823687A (en) * | 1951-05-26 | 1958-02-18 | Aro Equipment Corp | Valve structure |
US3100495A (en) * | 1960-11-21 | 1963-08-13 | Bendix Corp | Vibration resistant acceleration activated valve |
US3152047A (en) * | 1958-08-22 | 1964-10-06 | Commissariat Energie Atomique | Liquid moderated nuclear reactors subject to varying movements |
-
1945
- 1945-08-07 GB GB2020945A patent/GB604304A/en not_active Expired
Cited By (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2654381A (en) * | 1947-06-20 | 1953-10-06 | Hobbs Transmission Ltd | Variable-ratio power transmitting apparatus |
US2748786A (en) * | 1950-07-14 | 1956-06-05 | Isreeli Jack | Pressure-control apparatus for anti-g suits |
US2620813A (en) * | 1950-12-22 | 1952-12-09 | Chloride Electrical Storage Co | Selector mechanism |
US2683001A (en) * | 1951-04-30 | 1954-07-06 | Bendix Aviat Corp | Acceleration responsive fluid pressure distribution control system |
US2823687A (en) * | 1951-05-26 | 1958-02-18 | Aro Equipment Corp | Valve structure |
US2676601A (en) * | 1951-05-29 | 1954-04-27 | Dunlop Rubber Co | Fluid pressure valve |
US2753881A (en) * | 1951-09-14 | 1956-07-10 | Bendix Aviat Corp | G responsive valve |
US2789556A (en) * | 1953-05-11 | 1957-04-23 | Clark | Valve and system for the protection of aircraft occupants |
US3152047A (en) * | 1958-08-22 | 1964-10-06 | Commissariat Energie Atomique | Liquid moderated nuclear reactors subject to varying movements |
US3100495A (en) * | 1960-11-21 | 1963-08-13 | Bendix Corp | Vibration resistant acceleration activated valve |
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