GB8623492D0 - Actuator system - Google Patents

Actuator system

Info

Publication number
GB8623492D0
GB8623492D0 GB868623492A GB8623492A GB8623492D0 GB 8623492 D0 GB8623492 D0 GB 8623492D0 GB 868623492 A GB868623492 A GB 868623492A GB 8623492 A GB8623492 A GB 8623492A GB 8623492 D0 GB8623492 D0 GB 8623492D0
Authority
GB
United Kingdom
Prior art keywords
actuator system
actuator
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.)
Granted
Application number
GB868623492A
Other versions
GB2196910A (en
GB2196910B (en
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
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 true GB8623492D0 (en) 1986-11-05
GB2196910A GB2196910A (en) 1988-05-11
GB2196910B 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
GB2196910A (en) 1988-05-11
GB2196910B (en) 1990-02-14

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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