DE233110C - - Google Patents

Info

Publication number
DE233110C
DE233110C DENDAT233110D DE233110DA DE233110C DE 233110 C DE233110 C DE 233110C DE NDAT233110 D DENDAT233110 D DE NDAT233110D DE 233110D A DE233110D A DE 233110DA DE 233110 C DE233110 C DE 233110C
Authority
DE
Germany
Prior art keywords
piston
control
rod
membrane
cataract
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.)
Active
Application number
DENDAT233110D
Other languages
German (de)
English (en)
Publication of DE233110C publication Critical patent/DE233110C/de
Active 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

Landscapes

  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Engineering & Computer Science (AREA)
  • Automation & Control Theory (AREA)
  • Fluid-Pressure Circuits (AREA)
DENDAT233110D Active DE233110C (ar)

Publications (1)

Publication Number Publication Date
DE233110C true DE233110C (ar)

Family

ID=493074

Family Applications (1)

Application Number Title Priority Date Filing Date
DENDAT233110D Active DE233110C (ar)

Country Status (1)

Country Link
DE (1) DE233110C (ar)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2586688A (en) * 1948-11-16 1952-02-19 Westinghouse Electric Corp Automatically and manually controlled servomotor for interceptor valve of turbine and reheater apparatus
US2629365A (en) * 1949-03-11 1953-02-24 Union Carbide & Carbon Corp Electropneumatic control system
US2803258A (en) * 1954-06-16 1957-08-20 Bristol Company Disposable pilot valve
US2836153A (en) * 1954-08-24 1958-05-27 Bristol Company Pilot valve
US3389641A (en) * 1966-10-24 1968-06-25 United Aircraft Corp Hydraulic control mechanism with hydraulic delayed reset
US3389640A (en) * 1966-08-31 1968-06-25 United Aircraft Corp Hydraulic control mechanism having viscosity independent restoring mechanism

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2586688A (en) * 1948-11-16 1952-02-19 Westinghouse Electric Corp Automatically and manually controlled servomotor for interceptor valve of turbine and reheater apparatus
US2629365A (en) * 1949-03-11 1953-02-24 Union Carbide & Carbon Corp Electropneumatic control system
US2803258A (en) * 1954-06-16 1957-08-20 Bristol Company Disposable pilot valve
US2836153A (en) * 1954-08-24 1958-05-27 Bristol Company Pilot valve
US3389640A (en) * 1966-08-31 1968-06-25 United Aircraft Corp Hydraulic control mechanism having viscosity independent restoring mechanism
US3389641A (en) * 1966-10-24 1968-06-25 United Aircraft Corp Hydraulic control mechanism with hydraulic delayed reset

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