GB2626545A - Active throttle arrangement and control system - Google Patents

Active throttle arrangement and control system Download PDF

Info

Publication number
GB2626545A
GB2626545A GB2301049.9A GB202301049A GB2626545A GB 2626545 A GB2626545 A GB 2626545A GB 202301049 A GB202301049 A GB 202301049A GB 2626545 A GB2626545 A GB 2626545A
Authority
GB
United Kingdom
Prior art keywords
gearbox
body casing
motor body
control system
assembly
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.)
Pending
Application number
GB2301049.9A
Other versions
GB202301049D0 (en
Inventor
Edward Cater Marcus
Mark Dee Justin
David Hollands Robert
Paul Mihr Jonathan
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.)
BAE Systems PLC
Original Assignee
BAE Systems PLC
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 BAE Systems PLC filed Critical BAE Systems PLC
Priority to GB2301049.9A priority Critical patent/GB2626545A/en
Publication of GB202301049D0 publication Critical patent/GB202301049D0/en
Publication of GB2626545A publication Critical patent/GB2626545A/en
Pending legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02D—CONTROLLING COMBUSTION ENGINES
    • F02D11/00—Arrangements for, or adaptations to, non-automatic engine control initiation means, e.g. operator initiated
    • F02D11/06—Arrangements for, or adaptations to, non-automatic engine control initiation means, e.g. operator initiated characterised by non-mechanical control linkages, e.g. fluid control linkages or by control linkages with power drive or assistance
    • F02D11/10—Arrangements for, or adaptations to, non-automatic engine control initiation means, e.g. operator initiated characterised by non-mechanical control linkages, e.g. fluid control linkages or by control linkages with power drive or assistance of the electric type
    • F02D11/105—Arrangements for, or adaptations to, non-automatic engine control initiation means, e.g. operator initiated characterised by non-mechanical control linkages, e.g. fluid control linkages or by control linkages with power drive or assistance of the electric type characterised by the function converting demand to actuation, e.g. a map indicating relations between an accelerator pedal position and throttle valve opening or target engine torque
    • 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
    • B64C13/02—Initiating means
    • B64C13/04—Initiating means actuated personally
    • B64C13/042—Initiating means actuated personally operated by hand
    • 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
    • B64C13/02—Initiating means
    • B64C13/04—Initiating means actuated personally
    • B64C13/042—Initiating means actuated personally operated by hand
    • B64C13/0421—Initiating means actuated personally operated by hand control sticks for primary flight controls
    • 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
    • B64C13/02—Initiating means
    • B64C13/04—Initiating means actuated personally
    • B64C13/042—Initiating means actuated personally operated by hand
    • B64C13/0423—Initiating means actuated personally operated by hand yokes or steering wheels for primary flight controls
    • 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
    • B64C13/02—Initiating means
    • B64C13/04—Initiating means actuated personally
    • B64C13/042—Initiating means actuated personally operated by hand
    • B64C13/0425—Initiating means actuated personally operated by hand for actuating trailing or leading edge flaps, air brakes or spoilers

Landscapes

  • Engineering & Computer Science (AREA)
  • Automation & Control Theory (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Throttle Valves Provided In The Intake System Or In The Exhaust System (AREA)

Abstract

An assembly 900 (e.g. a throttle, active stick, cyclics) comprising an actuator assembly 912 comprising a motor body casing 920, and a gearbox 904, and a lever 903 connected to an output stage of the gearbox 906. The assembly further comprises trunnion bearings 922, 924 configured to mount the motor body casing to a chassis (fig.10, 1002) and a link 914 configured to connect the motor body casing to the chassis, wherein the link comprises a force sensor, thus eliminating the need for a dynamic wire connection. The lever may comprise a grip. The actuator assembly may comprise motor windings and a resolver area positioned either side of the gearbox.
GB2301049.9A 2023-01-25 2023-01-25 Active throttle arrangement and control system Pending GB2626545A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB2301049.9A GB2626545A (en) 2023-01-25 2023-01-25 Active throttle arrangement and control system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2301049.9A GB2626545A (en) 2023-01-25 2023-01-25 Active throttle arrangement and control system

Publications (2)

Publication Number Publication Date
GB202301049D0 GB202301049D0 (en) 2023-03-08
GB2626545A true GB2626545A (en) 2024-07-31

Family

ID=85383221

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2301049.9A Pending GB2626545A (en) 2023-01-25 2023-01-25 Active throttle arrangement and control system

Country Status (1)

Country Link
GB (1) GB2626545A (en)

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20190176997A1 (en) * 2017-12-13 2019-06-13 Safe Flight Instrument Corporation Aircraft torque control device
US20210371083A1 (en) * 2018-10-15 2021-12-02 Safe Flight lnstrument Corporation Aircraft torque control device
US20220063794A1 (en) * 2018-12-28 2022-03-03 Safran Electronics & Defense Force application device for a control stick of an aircraft

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20190176997A1 (en) * 2017-12-13 2019-06-13 Safe Flight Instrument Corporation Aircraft torque control device
US20210371083A1 (en) * 2018-10-15 2021-12-02 Safe Flight lnstrument Corporation Aircraft torque control device
US20220063794A1 (en) * 2018-12-28 2022-03-03 Safran Electronics & Defense Force application device for a control stick of an aircraft

Also Published As

Publication number Publication date
GB202301049D0 (en) 2023-03-08

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