GB807918A - Control systems for aircraft - Google Patents

Control systems for aircraft

Info

Publication number
GB807918A
GB807918A GB21925/55A GB2192555A GB807918A GB 807918 A GB807918 A GB 807918A GB 21925/55 A GB21925/55 A GB 21925/55A GB 2192555 A GB2192555 A GB 2192555A GB 807918 A GB807918 A GB 807918A
Authority
GB
United Kingdom
Prior art keywords
aircraft
yieldable
control
coupling
july
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
GB21925/55A
Inventor
Ruben Hadekel
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 Ltd
Original Assignee
Sperry Gyroscope Co Ltd
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
Priority claimed from GB7783/54A external-priority patent/GB803572A/en
Application filed by Sperry Gyroscope Co Ltd filed Critical Sperry Gyroscope Co Ltd
Priority to GB21925/55A priority Critical patent/GB807918A/en
Priority to DES49766A priority patent/DE1111026B/en
Publication of GB807918A publication Critical patent/GB807918A/en
Expired legal-status Critical Current

Links

Classifications

    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/0055—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements
    • G05D1/0061—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements for transition from automatic pilot to manual pilot and vice versa
    • 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

Landscapes

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

Abstract

807,918. Automatic control systems for aircraft SPERRY GYROSCOPE CO. Ltd. July 12, 1956 [July 29, 1955], No. 21925/55. Addition to 803,572. Drawings to Specification. Class 38 (4). [Also in Groups XXXIII and XXIX] In a system, as in the parent Specification, in in which a main hydraulic servomotor actuating a control surface of an aircraft may be automatically or manually controlled through an electrical control system, or manually controlled through a mechanical control system, a spring- loaded yieldable coupling is added between the manual controller and the artificial feel device associated with it so that, if sufficient force is applied to the manual controller during electric automatic control, the coupling yields and opens a switch to change over the system to mechanical control. This yieldable coupling is additional to that provided in the parent Specification which requires more force to operate it since the artificial feel device must be operated with it. The switches associated with the two yieldable couplings are connected in series. The switch associated with the additional yieldable coupling is shorted during electric manual control to prevent changeover. Specification 803,574 is referred to.
GB21925/55A 1954-03-17 1955-07-29 Control systems for aircraft Expired GB807918A (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
GB21925/55A GB807918A (en) 1954-03-17 1955-07-29 Control systems for aircraft
DES49766A DE1111026B (en) 1954-03-17 1956-07-28 Safety device in flight control systems for switching from automatic to manual control

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB7783/54A GB803572A (en) 1954-03-17 1954-03-17 Control systems for aircraft
GB21925/55A GB807918A (en) 1954-03-17 1955-07-29 Control systems for aircraft

Publications (1)

Publication Number Publication Date
GB807918A true GB807918A (en) 1959-01-21

Family

ID=37192512

Family Applications (1)

Application Number Title Priority Date Filing Date
GB21925/55A Expired GB807918A (en) 1954-03-17 1955-07-29 Control systems for aircraft

Country Status (2)

Country Link
DE (1) DE1111026B (en)
GB (1) GB807918A (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2947005B1 (en) * 2014-05-20 2018-07-04 Mecaer Aviation Group S.p.A. Aircraft hybrid flight control system

Also Published As

Publication number Publication date
DE1111026B (en) 1961-07-13
DE1111026C2 (en) 1962-02-01

Similar Documents

Publication Publication Date Title
GB807918A (en) Control systems for aircraft
GB803577A (en) Control systems for aircraft
GB931662A (en) Aircraft flight control system
GB803574A (en) Control systems for aircraft
CA480433A (en) Navigational control system
CA482572A (en) Safety control device for disconnecting switch
CA626339A (en) Two stage clutch control system
CA602362A (en) Hydraulic supply system for an aeronautical propeller or the like
JPS52133484A (en) Operation test system for remote supervision control system
CA488801A (en) Hydraulic control systems
CA443394A (en) Hydraulic remote control system
CA440483A (en) Hydraulic remote control system
CA499640A (en) Power operated tool with automatic control valve system
CA604088A (en) Coupling means for a switch unit
CA442814A (en) Hydraulic control system emergency device
CA445394A (en) Control means for power transmission system
CA480454A (en) Fluid line coupling for hydraulic control system
CA444451A (en) Hydraulic control system
CA442815A (en) Hydraulic control system
CA487004A (en) Pump control system
CA623005A (en) Electric control system for fluid operated actuators
CA486611A (en) Heating system control
CA484909A (en) Power system control
AU270842B2 (en) Ducting system for environmental control
AU833252A (en) Improvements in automatic craft control systems