DE278689C - - Google Patents

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Publication number
DE278689C
DE278689C DENDAT278689D DE278689DA DE278689C DE 278689 C DE278689 C DE 278689C DE NDAT278689 D DENDAT278689 D DE NDAT278689D DE 278689D A DE278689D A DE 278689DA DE 278689 C DE278689 C DE 278689C
Authority
DE
Germany
Prior art keywords
pressure
controlling
controlled
fluid
piston
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
DENDAT278689D
Other languages
German (de)
English (en)
Publication of DE278689C publication Critical patent/DE278689C/de
Active legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F15FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
    • F15BSYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
    • F15B9/00Servomotors with follow-up action, e.g. obtained by feed-back control, i.e. in which the position of the actuated member conforms with that of the controlling member
    • F15B9/02Servomotors with follow-up action, e.g. obtained by feed-back control, i.e. in which the position of the actuated member conforms with that of the controlling member with servomotors of the reciprocatable or oscillatable type
    • F15B9/08Servomotors with follow-up action, e.g. obtained by feed-back control, i.e. in which the position of the actuated member conforms with that of the controlling member with servomotors of the reciprocatable or oscillatable type controlled by valves affecting the fluid feed or the fluid outlet of the servomotor
    • F15B9/10Servomotors with follow-up action, e.g. obtained by feed-back control, i.e. in which the position of the actuated member conforms with that of the controlling member with servomotors of the reciprocatable or oscillatable type controlled by valves affecting the fluid feed or the fluid outlet of the servomotor in which the controlling element and the servomotor each controls a separate member, these members influencing different fluid passages or the same passage

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Fluid-Pressure Circuits (AREA)
DENDAT278689D Active DE278689C (pt)

Publications (1)

Publication Number Publication Date
DE278689C true DE278689C (pt)

Family

ID=534666

Family Applications (1)

Application Number Title Priority Date Filing Date
DENDAT278689D Active DE278689C (pt)

Country Status (1)

Country Link
DE (1) DE278689C (pt)

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2969640A (en) * 1953-08-25 1961-01-31 Solar Aircraft Co Pressure ratio sensing, indicating, and controlling apparatus
US2981058A (en) * 1955-09-16 1961-04-25 Solar Aircraft Co Multiple pressure sensing, indicating and control apparatus
US2986929A (en) * 1957-04-22 1961-06-06 Solar Aircraft Co Pressure ratio indicator and controller for variable area nozzle
US3014493A (en) * 1957-12-31 1961-12-26 United Aircraft Corp High temperature pneumatic actuator
US3028096A (en) * 1959-03-20 1962-04-03 United Aircraft Corp Temperature control valve
US3042058A (en) * 1957-02-22 1962-07-03 Sarl Rech S Etudes Production High output differential electromagnetic valve
US3047234A (en) * 1958-02-28 1962-07-31 Fortier Andre Pneumatically operated control devices
US3083695A (en) * 1958-07-30 1963-04-02 Thompson Ramo Wooldridge Inc Control actuator mechanism

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2969640A (en) * 1953-08-25 1961-01-31 Solar Aircraft Co Pressure ratio sensing, indicating, and controlling apparatus
US2981058A (en) * 1955-09-16 1961-04-25 Solar Aircraft Co Multiple pressure sensing, indicating and control apparatus
US3042058A (en) * 1957-02-22 1962-07-03 Sarl Rech S Etudes Production High output differential electromagnetic valve
US2986929A (en) * 1957-04-22 1961-06-06 Solar Aircraft Co Pressure ratio indicator and controller for variable area nozzle
US3014493A (en) * 1957-12-31 1961-12-26 United Aircraft Corp High temperature pneumatic actuator
US3047234A (en) * 1958-02-28 1962-07-31 Fortier Andre Pneumatically operated control devices
US3083695A (en) * 1958-07-30 1963-04-02 Thompson Ramo Wooldridge Inc Control actuator mechanism
US3028096A (en) * 1959-03-20 1962-04-03 United Aircraft Corp Temperature control valve

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