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 systems

Info

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
Application number
GB14149/48A
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Publication of GB669308A publication Critical patent/GB669308A/en
Expired legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05DSYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D13/00Control of linear speed; Control of angular speed; Control of acceleration or deceleration, e.g. of a prime mover
    • G05D13/02Details
    • G05D13/06Details 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.
GB14149/48A 1947-06-28 1948-05-25 Improvements in or relating to damping devices for governors of hydraulic apparatus or systems Expired GB669308A (en)

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)

* Cited by examiner, † Cited by third party
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

Cited By (1)

* Cited by examiner, † Cited by third party
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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