GB669308A - Improvements in or relating to damping devices for governors of hydraulic apparatus or systems - Google Patents
Improvements in or relating to damping devices for governors of hydraulic apparatus or systemsInfo
- Publication number
- GB669308A GB669308A GB14149/48A GB1414948A GB669308A GB 669308 A GB669308 A GB 669308A GB 14149/48 A GB14149/48 A GB 14149/48A GB 1414948 A GB1414948 A GB 1414948A GB 669308 A GB669308 A GB 669308A
- Authority
- GB
- United Kingdom
- Prior art keywords
- piston
- valve
- spring
- chamber
- inlet
- 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
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D13/00—Control of linear speed; Control of angular speed; Control of acceleration or deceleration, e.g. of a prime mover
- G05D13/02—Details
- G05D13/06—Details providing for damping of erratic vibrations in governors
Abstract
669,308. Fluid-actuated valves with dashpots. MARINE, O. May 25, 1948 [June 28, 1947], No. 14149/48. Class 135 [Also in Groups XXVIII and XXXII] A valve comprises a closure member 20 positioned relatively to its seat 19 by a piston 18 subjected to the pressures on opposite sides of a restriction 17 to maintain a constant rate of liquid flow at 16 beyond the restriction. The piston is loaded by a spring 2 and hunting is prevented by a dashpot device comprising a piston valve 4 and a piston 3, the spring acting between the piston and the head 1 of the valve and being initially compressed. The piston is slidable on the valve and in a cylinder 7 which has a connection 5 with the inlet line 15 of the flow controlling valve, and an exhaust connection 6. A liquid filled chamber 8 in the cylinder is connected to the interior of the piston 3 by a passage having a throttle 9. Upward movement of the piston 18 compresses the spring 2 and moves the valve 4 to connect the chamber 8 to exhaust, whereby the piston 3 follows the valve at a speed determined by the throttle 9 to close the valve and return the spring to its initial compression. Downward movement of the piston 18 causes extension of the spring and movement of the valve 4 to connect the chamber 8 to the inlet whereby the piston 3 slowly follows the valve to recompress the spring and cut-off the inlet.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR669308X | 1947-06-28 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB669308A true GB669308A (en) | 1952-04-02 |
Family
ID=9015656
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB14149/48A Expired GB669308A (en) | 1947-06-28 | 1948-05-25 | Improvements in or relating to damping devices for governors of hydraulic apparatus or systems |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB669308A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2982258A (en) * | 1957-06-04 | 1961-05-02 | United Aircraft Corp | Pressure ratio device utilizing a free piston valve for pressure ratio regulation and a servo mechanism coacting therewith to amplify pressure ratio error correction |
-
1948
- 1948-05-25 GB GB14149/48A patent/GB669308A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2982258A (en) * | 1957-06-04 | 1961-05-02 | United Aircraft Corp | Pressure ratio device utilizing a free piston valve for pressure ratio regulation and a servo mechanism coacting therewith to amplify pressure ratio error correction |
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