GB500840A - - Google Patents

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Publication number
GB500840A
GB500840A GB500840DA GB500840A GB 500840 A GB500840 A GB 500840A GB 500840D A GB500840D A GB 500840DA GB 500840 A GB500840 A GB 500840A
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GB
United Kingdom
Prior art keywords
recesses
servomotor
gyroscope
opposed
march
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.)
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Publication of GB500840A publication Critical patent/GB500840A/en
Active legal-status Critical Current

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  • Actuator (AREA)

Abstract

500,840. Fluid-pressure servomoters. AGA-BALTIC RADIO AKTIEBOLAG. March 17, 1938, No. 8282. Convention date, March 19, 1937. [Class 135] A servomotor device controlled by a gyroscope driven by liquid or gaseous pressure medium and sus ponded in gimbals co axial with the servomotor has the gyroscope and power device driven by the same pressure medium which passes through a hollow gimbal ring to the control mechanism and thence to the power device. In the form shown an oscillating vane motor has diametrically opposed vanes 8 working in semi-cylindrical chambers. An extension 15 of the hub carries a pulley 17 adapted to be connected to the part operated while an extension 16 carries a movable ported seat 18 for the control valve. The rotary disc control valve has a pair of supply ports 26, 26<1> and a pair of exhaust recesses 27, 27<1> which ports and recesses co-operate with arcuate recesses in the seat opposed recesses being coupled together and to opposed working chambers. The actuating fluid is supplied through a pipe 22 and hollow gimbal ring 3 of a controlling gyroscope 1 to a chamber 24 formed in the valve member. The Specification as open to inspection under Sect. 91 states that the servomotor may be operated under the control of temperature, pressure, volume, &c. This subjectmatter does not appear in the Specification as accepted.
GB500840D Active GB500840A (en)

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GB500840A true GB500840A (en)

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ID=1747467

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Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2446335A (en) * 1945-06-29 1948-08-03 Niles Bement Pond Co Control apparatus for internalcombustion engines
US2642885A (en) * 1947-06-07 1953-06-23 Elmer C Wade Gyroscopic valve control for hydraulic circuits
US3066653A (en) * 1960-02-08 1962-12-04 Thompson Ramo Wooldridge Inc Hot gas servo system
US3417667A (en) * 1965-11-10 1968-12-24 Fujitsu Ltd Oil pressure torque amplifier
US4056041A (en) * 1974-08-02 1977-11-01 Abex Corporation Control system for axial piston fluid energy translating device
US4646621A (en) * 1983-05-20 1987-03-03 Matsushita Electric Industrial Co., Ltd. Hydraulic servo actuator

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2446335A (en) * 1945-06-29 1948-08-03 Niles Bement Pond Co Control apparatus for internalcombustion engines
US2642885A (en) * 1947-06-07 1953-06-23 Elmer C Wade Gyroscopic valve control for hydraulic circuits
US3066653A (en) * 1960-02-08 1962-12-04 Thompson Ramo Wooldridge Inc Hot gas servo system
US3417667A (en) * 1965-11-10 1968-12-24 Fujitsu Ltd Oil pressure torque amplifier
US4056041A (en) * 1974-08-02 1977-11-01 Abex Corporation Control system for axial piston fluid energy translating device
US4646621A (en) * 1983-05-20 1987-03-03 Matsushita Electric Industrial Co., Ltd. Hydraulic servo actuator

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