GB2196910B - Actuator system for a control surface on an aircraft wing - Google Patents

Actuator system for a control surface on an aircraft wing

Info

Publication number
GB2196910B
GB2196910B GB8623492A GB8623492A GB2196910B GB 2196910 B GB2196910 B GB 2196910B GB 8623492 A GB8623492 A GB 8623492A GB 8623492 A GB8623492 A GB 8623492A GB 2196910 B GB2196910 B GB 2196910B
Authority
GB
United Kingdom
Prior art keywords
control surface
actuator system
aircraft wing
wing
aircraft
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 - Lifetime
Application number
GB8623492A
Other versions
GB8623492D0 (en
GB2196910A (en
Inventor
Philip Hudson
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.)
ZF International UK Ltd
Original Assignee
Lucas Industries 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
Application filed by Lucas Industries Ltd filed Critical Lucas Industries Ltd
Priority to GB8623492A priority Critical patent/GB2196910B/en
Publication of GB8623492D0 publication Critical patent/GB8623492D0/en
Publication of GB2196910A publication Critical patent/GB2196910A/en
Application granted granted Critical
Publication of GB2196910B publication Critical patent/GB2196910B/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • 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
    • B64C13/38—Transmitting means with power amplification
    • B64C13/50—Transmitting means with power amplification using electrical energy
    • B64C13/505—Transmitting means with power amplification using electrical energy having duplication or stand-by provisions

Landscapes

  • Engineering & Computer Science (AREA)
  • Automation & Control Theory (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Actuator (AREA)
GB8623492A 1986-09-30 1986-09-30 Actuator system for a control surface on an aircraft wing Expired - Lifetime GB2196910B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB8623492A GB2196910B (en) 1986-09-30 1986-09-30 Actuator system for a control surface on an aircraft wing

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB8623492A GB2196910B (en) 1986-09-30 1986-09-30 Actuator system for a control surface on an aircraft wing

Publications (3)

Publication Number Publication Date
GB8623492D0 GB8623492D0 (en) 1986-11-05
GB2196910A GB2196910A (en) 1988-05-11
GB2196910B true GB2196910B (en) 1990-02-14

Family

ID=10605027

Family Applications (1)

Application Number Title Priority Date Filing Date
GB8623492A Expired - Lifetime GB2196910B (en) 1986-09-30 1986-09-30 Actuator system for a control surface on an aircraft wing

Country Status (1)

Country Link
GB (1) GB2196910B (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2787759B1 (en) * 1998-12-28 2001-03-16 Aerospatiale METHOD AND SYSTEM FOR CONTROLLING A GOVERNOR OF AN AIRCRAFT OPERATED BY MULTIPLE HYDRAULIC CYLINDERS AND MODULAR POWER
CN106741865B (en) * 2016-11-30 2019-03-08 中国航空工业集团公司沈阳飞机设计研究所 A kind of airplane servo actuating system hydraulic control method

Also Published As

Publication number Publication date
GB8623492D0 (en) 1986-11-05
GB2196910A (en) 1988-05-11

Similar Documents

Publication Publication Date Title
GB2196588B (en) Rudder control arrangement for aircraft
GB2216860B (en) Helicopter control systems
GB2196589B (en) Aircraft elevator control system
DE3462866D1 (en) Aircraft flight control system
GB2158405B (en) Position and control system for helicopter blade actuation
IL76953A0 (en) Aircraft airfoil camber automatic control system
EP0179209A3 (en) Automatic cancellation device for control force errors for aircraft, particulary helicopters
EP0125088A3 (en) Flight control systems for helicopters
EP0263247A3 (en) Flight control system
EP0261056A3 (en) Collective control system for a helicopter
EP0219816A3 (en) Aircraft flying control systems
GB2211635B (en) Control system for synchrophasing aircraft propellers
DE3760445D1 (en) Control system for a moving aerodynamic surface of an aircraft
EP0297304A3 (en) Slat actuating system for aircraft wing
IL84785A0 (en) Flight control optimization system for multi-control surface aircraft
GB2237899B (en) Automated approach speed control for an airplane
GB2159476B (en) A control mechanism for an aircraft
EP0272058A3 (en) Helicopter flight control systems
GB2095002B (en) Actuator system for a control surface of an aircraft
GB2167551B (en) A ventilating arrangement for an aircraft galley
DE3173391D1 (en) Actuation system for a control surface of an aircraft
GB2172861B (en) Aileron for an airplane wing
GB8905631D0 (en) Jettisonable aerodynamic control surface
GB2196910B (en) Actuator system for a control surface on an aircraft wing
GB2208631B (en) Aircraft precision approach control system

Legal Events

Date Code Title Description
732E Amendments to the register in respect of changes of name or changes affecting rights (sect. 32/1977)
PCNP Patent ceased through non-payment of renewal fee

Effective date: 20050930