GB2626545A - Active throttle arrangement and control system - Google Patents
Active throttle arrangement and control system Download PDFInfo
- 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
Links
- 125000004122 cyclic group Chemical group 0.000 abstract 1
- 238000004804 winding Methods 0.000 abstract 1
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.
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)
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 |
-
2023
- 2023-01-25 GB GB2301049.9A patent/GB2626545A/en active Pending
Patent Citations (3)
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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