GB2578204B - High-lift system for an aircraft - Google Patents

High-lift system for an aircraft Download PDF

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Publication number
GB2578204B
GB2578204B GB1912256.3A GB201912256A GB2578204B GB 2578204 B GB2578204 B GB 2578204B GB 201912256 A GB201912256 A GB 201912256A GB 2578204 B GB2578204 B GB 2578204B
Authority
GB
United Kingdom
Prior art keywords
aircraft
lift system
lift
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.)
Active
Application number
GB1912256.3A
Other versions
GB2578204A (en
GB201912256D0 (en
Inventor
Schievelbusch Bernd
Kohlöffel Christian
Trenkle Christian
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.)
Liebherr Aerospace Lindenberg GmbH
Original Assignee
Liebherr Aerospace Lindenberg GmbH
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 Liebherr Aerospace Lindenberg GmbH filed Critical Liebherr Aerospace Lindenberg GmbH
Publication of GB201912256D0 publication Critical patent/GB201912256D0/en
Publication of GB2578204A publication Critical patent/GB2578204A/en
Application granted granted Critical
Publication of GB2578204B publication Critical patent/GB2578204B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C13/00Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
    • B64C13/24Transmitting means
    • B64C13/38Transmitting means with power amplification
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C13/00Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
    • B64C13/24Transmitting means
    • B64C13/38Transmitting means with power amplification
    • B64C13/40Transmitting means with power amplification using fluid pressure
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C13/00Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
    • B64C13/24Transmitting means
    • B64C13/38Transmitting means with power amplification
    • B64C13/50Transmitting means with power amplification using electrical energy
GB1912256.3A 2018-09-07 2019-08-27 High-lift system for an aircraft Active GB2578204B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE102018121856.7A DE102018121856A1 (en) 2018-09-07 2018-09-07 High lift system for an aircraft

Publications (3)

Publication Number Publication Date
GB201912256D0 GB201912256D0 (en) 2019-10-09
GB2578204A GB2578204A (en) 2020-04-22
GB2578204B true GB2578204B (en) 2022-09-14

Family

ID=68108814

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1912256.3A Active GB2578204B (en) 2018-09-07 2019-08-27 High-lift system for an aircraft

Country Status (3)

Country Link
DE (1) DE102018121856A1 (en)
FR (1) FR3085665B1 (en)
GB (1) GB2578204B (en)

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5082208A (en) * 1989-09-29 1992-01-21 The Boeing Company System and method for controlling an aircraft flight control member
EP2727831A1 (en) * 2012-10-30 2014-05-07 Airbus Operations GmbH Method for transferring hydraulic power between two hydraulic systems in an aircraft, use of a power control unit and drive system in an aircraft
EP3549859A1 (en) * 2018-04-06 2019-10-09 Goodrich Actuation Systems Limited Hydraulic power drive unit

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH07112836B2 (en) * 1991-06-14 1995-12-06 富士重工業株式会社 Aircraft hydraulic steering system
EP3037346B1 (en) * 2014-12-22 2018-10-24 Airbus Operations GmbH Method for testing a component in a high lift system of an aircraft

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5082208A (en) * 1989-09-29 1992-01-21 The Boeing Company System and method for controlling an aircraft flight control member
EP2727831A1 (en) * 2012-10-30 2014-05-07 Airbus Operations GmbH Method for transferring hydraulic power between two hydraulic systems in an aircraft, use of a power control unit and drive system in an aircraft
EP3549859A1 (en) * 2018-04-06 2019-10-09 Goodrich Actuation Systems Limited Hydraulic power drive unit

Also Published As

Publication number Publication date
GB2578204A (en) 2020-04-22
FR3085665A1 (en) 2020-03-13
DE102018121856A1 (en) 2020-03-12
GB201912256D0 (en) 2019-10-09
FR3085665B1 (en) 2022-04-22

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