GB515290A - Improvements in or relating to control systems for dirigible craft - Google Patents

Improvements in or relating to control systems for dirigible craft

Info

Publication number
GB515290A
GB515290A GB17917/38A GB1791738A GB515290A GB 515290 A GB515290 A GB 515290A GB 17917/38 A GB17917/38 A GB 17917/38A GB 1791738 A GB1791738 A GB 1791738A GB 515290 A GB515290 A GB 515290A
Authority
GB
United Kingdom
Prior art keywords
pressure
servo
motor
movement
valve
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
Application number
GB17917/38A
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Sperry Gyroscope Co Inc
Original Assignee
Sperry Gyroscope Co Inc
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Sperry Gyroscope Co Inc filed Critical Sperry Gyroscope Co Inc
Publication of GB515290A publication Critical patent/GB515290A/en
Expired legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05DSYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/08Control of attitude, i.e. control of roll, pitch, or yaw
    • G05D1/0808Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)

Abstract

515,290. Auomatic pilots. SPERRY GYROSCOPE CO., Inc. June 16, 1938, No. 17917. Convention date, June 19, 1937. [Class 135] A control system for a control surface of a craft such as an aircraft rudder comprises a servo-motor operating under the control of remote valve means, whereby the surface is moved in accordance with the forces operating on the valve means, and means for directly applying fluid pressure, arising from back pressure on the control surface, to the valve means in opposition to the controlling forces acting thereon, whereby the movement of the control surface is limited. Movement of the craft with respect to a gyroscopic direction indicator 1 causes a semi-circular plate 5 to vary diametrically opposite openings 6, 7 connected respectively to diaphragm chambers 17<1>, 17 and the differential pressure acting on the diaphragms 40<1>, 40 displaces a rod 18 carrying piston valves 19, 20, 21. The valves 19. 21 cover inlet ports 25, 26 for pressure fluid introduced through a pipe 24 and displacement of the valve rod 18 uncovers one or other of the ports 25, 26 to put it intocommunication with one or other of pipes 28, 29 leading to a servo-motor 30, the pipe 29, 28 not so used being connected by movement of the valve 20 with a return pipe 27. A rate-of-turn indicator 11 is coupled in parallel with the direction indicator 1 to co-operate in actuating the valves, cocks 15, 15<1>, 16, 16<1> being provided to determine the relative effectiveness of the indicators. The servo-motor 30 controls a rudder &c. R and the increased resistance of the rudder as it moves further from its normal position builds up pressure in the servo-motor, this pressure acting back. through the conduit 28, 29 to open a ball valve 34 in a passage 33, 35 leading behind the adjacent piston 19, 21 to check further movement of the servo-motor. A bellows communicating with the passage 35 acts as a pressure accumulator to prolong the opposition pressure.
GB17917/38A 1937-06-19 1938-06-16 Improvements in or relating to control systems for dirigible craft Expired GB515290A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US515290XA 1937-06-19 1937-06-19

Publications (1)

Publication Number Publication Date
GB515290A true GB515290A (en) 1939-11-30

Family

ID=21971875

Family Applications (1)

Application Number Title Priority Date Filing Date
GB17917/38A Expired GB515290A (en) 1937-06-19 1938-06-16 Improvements in or relating to control systems for dirigible craft

Country Status (1)

Country Link
GB (1) GB515290A (en)

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