GB510300A - Improvements in servo-assisted control systems - Google Patents
Improvements in servo-assisted control systemsInfo
- Publication number
- GB510300A GB510300A GB24175/38A GB2417538A GB510300A GB 510300 A GB510300 A GB 510300A GB 24175/38 A GB24175/38 A GB 24175/38A GB 2417538 A GB2417538 A GB 2417538A GB 510300 A GB510300 A GB 510300A
- Authority
- GB
- United Kingdom
- Prior art keywords
- lever
- power device
- control
- joystick
- valves
- 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
Links
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
- F15B9/12—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 both the controlling element and the servomotor control the same member influencing a fluid passage and are connected to that member by means of a differential gearing
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B62—LAND VEHICLES FOR TRAVELLING OTHERWISE THAN ON RAILS
- B62D—MOTOR VEHICLES; TRAILERS
- B62D5/00—Power-assisted or power-driven steering
- B62D5/06—Power-assisted or power-driven steering fluid, i.e. using a pressurised fluid for most or all the force required for steering a vehicle
- B62D5/20—Power-assisted or power-driven steering fluid, i.e. using a pressurised fluid for most or all the force required for steering a vehicle specially adapted for particular type of steering gear or particular application
- B62D5/24—Power-assisted or power-driven steering fluid, i.e. using a pressurised fluid for most or all the force required for steering a vehicle specially adapted for particular type of steering gear or particular application for worm type
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63H—MARINE PROPULSION OR STEERING
- B63H25/00—Steering; Slowing-down otherwise than by use of propulsive elements; Dynamic anchoring, i.e. positioning vessels by means of main or auxiliary propulsive elements
- B63H25/06—Steering by rudders
- B63H25/08—Steering gear
- B63H25/14—Steering gear power assisted; power driven, i.e. using steering engine
- B63H25/26—Steering engines
- B63H25/28—Steering engines of fluid type
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
- B64C13/24—Transmitting means
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/40—Weight reduction
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Combustion & Propulsion (AREA)
- Automation & Control Theory (AREA)
- Chemical & Material Sciences (AREA)
- Ocean & Marine Engineering (AREA)
- Transportation (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Control Devices (AREA)
- Servomotors (AREA)
- Mechanically-Actuated Valves (AREA)
- Fluid-Pressure Circuits (AREA)
Abstract
510,300. Fluid-pressure servomotor-control systems. SPLADIS SOC. POUR L'APPLICATION D'INVENTIONS SCIENTIFIQUES. Aug. 16, 1938, No. 24175. Convention. date, May 30. [Class 135] A servo-assisted control mechanism for controlling the steering or stabilisation of air, land, or water-craft comprises a valve device 13, Fig. 2, which is adapted to be actuated, to control the pressure of liquid supplied from pumps 24, 24<1> to the two sides of a power device 23, by, a control member such as the joystick 14 of an aircraft. The joystick is connected to one end of a floating lever 12, the other end of which is connected to both the power device and the operating rod 19 of the rudder. Intermediate its length the lever 12 is connected to one end of a lever 5 of the valve device 13, which is shown in detail in Fig. 3, which lever is pivoted at B<1> and its other end arranged between two valve members 3, 3<1>. These valves control the flows from branch conduits leading from the pump supplies to the two ends of the power device so as to vary the pressures on the two sides of the power piston 22. Manual effort applied to the joystick 14 reacts back upon the lever 5 to move one of the valves' 3, 3<1> in a closing direction against the pressure developed thereby and open the other a corresponding amount to bring the power device 23 into operation to assist in the actuation of the rudder. The pressure difference developed. in the power device is thus proportional, to the effort applied by the operator and the movement of the power device provides a " follow-up " to restore the valves 3, 3<1> to their neutral positions. In the event of failure of the liquid pressure supply the operator can assume complete manual control. Movement of the joystick 14 in a perpendicular direction operates in a similar manner through a servo-assisted mechanism to control the transverse equilibrium of the craft. In this case however, instead of the floating-lever system 12 for actuating the valves 3, 3' a differential gear train 37 is employed as shown in detail in Fig. 8 in connection with a vehicle steering gear. Manual rotation of the shaft 28 by the driver is transmitted to the steering worm wheel 33 through a pinion 27, planet pinions 29a, 29b in a casing 34, and a pinion 30 on a shaft 31. The manual effort reacts against the casing 34, a limited movement of which is adapted to actuate the lever 5 of a valve device 13, as previously described, to bring a power device into operation to drive the shaft 31 and wormwheel 33 to assist the manual effort and provide a "followup" by restoring the casing 34 to a neutral position.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CH205713T | 1938-05-30 | ||
GB11136/39A GB527716A (en) | 1938-05-30 | 1939-04-12 | Improvements in servo-assisted control systems |
Publications (1)
Publication Number | Publication Date |
---|---|
GB510300A true GB510300A (en) | 1939-07-31 |
Family
ID=25724215
Family Applications (3)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB24175/38A Expired GB510300A (en) | 1938-05-30 | 1938-08-16 | Improvements in servo-assisted control systems |
GB32572/38A Expired GB510304A (en) | 1938-05-30 | 1938-11-09 | Improvements in servo-assisted control systems |
GB11136/39A Expired GB527716A (en) | 1938-05-30 | 1939-04-12 | Improvements in servo-assisted control systems |
Family Applications After (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB32572/38A Expired GB510304A (en) | 1938-05-30 | 1938-11-09 | Improvements in servo-assisted control systems |
GB11136/39A Expired GB527716A (en) | 1938-05-30 | 1939-04-12 | Improvements in servo-assisted control systems |
Country Status (2)
Country | Link |
---|---|
CH (1) | CH205713A (en) |
GB (3) | GB510300A (en) |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2650669A (en) * | 1949-05-02 | 1953-09-01 | Gemmer Mfg Co | Manual and hydraulic power actuated steering gear |
DE951977C (en) * | 1955-05-01 | 1956-11-08 | Zahnradfabrik Friedrichshafen | Steering gear, especially for motor vehicles, with an auxiliary power device that supports manual actuation |
CN111572787B (en) * | 2020-05-07 | 2022-05-03 | 南通大学 | Unmanned aerial vehicle self-balancing device based on planetary gear speed change and balancing method thereof |
-
1938
- 1938-05-30 CH CH205713D patent/CH205713A/en unknown
- 1938-08-16 GB GB24175/38A patent/GB510300A/en not_active Expired
- 1938-11-09 GB GB32572/38A patent/GB510304A/en not_active Expired
-
1939
- 1939-04-12 GB GB11136/39A patent/GB527716A/en not_active Expired
Also Published As
Publication number | Publication date |
---|---|
GB527716A (en) | 1940-10-15 |
GB510304A (en) | 1939-07-31 |
CH205713A (en) | 1939-06-30 |
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