DE278689C - - Google Patents
Info
- 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
Links
- 239000012530 fluid Substances 0.000 claims description 14
- 230000001276 controlling effect Effects 0.000 claims description 10
- 230000002776 aggregation Effects 0.000 claims 1
- 238000004220 aggregation Methods 0.000 claims 1
- 239000007788 liquid Substances 0.000 description 7
- 230000000694 effects Effects 0.000 description 5
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 3
- 210000003414 Extremities Anatomy 0.000 description 2
- 230000000875 corresponding Effects 0.000 description 2
- 230000000295 complement Effects 0.000 description 1
- 239000007789 gas Substances 0.000 description 1
- 239000012528 membrane Substances 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000006011 modification reaction Methods 0.000 description 1
- 230000001105 regulatory Effects 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
- F15B—SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
- F15B9/00—Servomotors 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
- F15B9/02—Servomotors 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
- F15B9/08—Servomotors 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
- F15B9/10—Servomotors 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)
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)
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 |
-
0
- DE DENDAT278689D patent/DE278689C/de active Active
Cited By (8)
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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