FR3125139B1 - DEVICE FOR CONTROLLING A MECHANICAL ENERGY VARIATION ORGAN OF AN AIRCRAFT AND ASSOCIATED METHOD - Google Patents
DEVICE FOR CONTROLLING A MECHANICAL ENERGY VARIATION ORGAN OF AN AIRCRAFT AND ASSOCIATED METHOD Download PDFInfo
- Publication number
- FR3125139B1 FR3125139B1 FR2107283A FR2107283A FR3125139B1 FR 3125139 B1 FR3125139 B1 FR 3125139B1 FR 2107283 A FR2107283 A FR 2107283A FR 2107283 A FR2107283 A FR 2107283A FR 3125139 B1 FR3125139 B1 FR 3125139B1
- Authority
- FR
- France
- Prior art keywords
- lever
- aircraft
- controlling
- movement
- mechanical energy
- 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
Links
- 210000000056 organ Anatomy 0.000 title 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D31/00—Power plant control systems; Arrangement of power plant control systems in aircraft
- B64D31/02—Initiating means
- B64D31/04—Initiating means actuated personally
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- User Interface Of Digital Computer (AREA)
- Mechanical Control Devices (AREA)
Abstract
Dispositif de commande d’un organe de variation d’énergie mécanique d’un aéronef et procédé associé Le dispositif de commande (10) comprend un support (14) et au moins une manette (16) montée mobile sur le support (14) dans deux sens de déplacement selon une direction de déplacement (D) entre une pluralité de positions dont une position stratégique, le dispositif (10) comprenant en outre un système (18) de génération de force sur la manette (16) configuré de sorte que, lorsque la manette (16) est à proximité de la position stratégique, le système (18) est propre à appliquer une force de sollicitation de la manette (16) vers la position stratégique dans chaque sens de déplacement. Lorsque la manette (16) reste dans la position stratégique pendant une durée supérieure à une temporisation prédéfinie, le système (18) est propre à cesser d’appliquer la force de sollicitation dans au moins un sens de déplacement. Figure pour l'abrégé : Figure 1Device for controlling a mechanical energy variation member of an aircraft and associated method The control device (10) comprises a support (14) and at least one lever (16) movably mounted on the support (14) in two directions of movement in a direction of movement (D) between a plurality of positions including a strategic position, the device (10) further comprising a system (18) for generating force on the lever (16) configured so that, when the lever (16) is close to the strategic position, the system (18) is able to apply a biasing force from the lever (16) towards the strategic position in each direction of movement. When the lever (16) remains in the strategic position for a duration greater than a predefined time delay, the system (18) is able to stop applying the biasing force in at least one direction of movement. Figure for abstract: Figure 1
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR2107283A FR3125139B1 (en) | 2021-07-06 | 2021-07-06 | DEVICE FOR CONTROLLING A MECHANICAL ENERGY VARIATION ORGAN OF AN AIRCRAFT AND ASSOCIATED METHOD |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR2107283A FR3125139B1 (en) | 2021-07-06 | 2021-07-06 | DEVICE FOR CONTROLLING A MECHANICAL ENERGY VARIATION ORGAN OF AN AIRCRAFT AND ASSOCIATED METHOD |
FR2107283 | 2021-07-06 |
Publications (2)
Publication Number | Publication Date |
---|---|
FR3125139A1 FR3125139A1 (en) | 2023-01-13 |
FR3125139B1 true FR3125139B1 (en) | 2024-05-31 |
Family
ID=78820901
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR2107283A Active FR3125139B1 (en) | 2021-07-06 | 2021-07-06 | DEVICE FOR CONTROLLING A MECHANICAL ENERGY VARIATION ORGAN OF AN AIRCRAFT AND ASSOCIATED METHOD |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR3125139B1 (en) |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2892835B1 (en) * | 2005-10-28 | 2008-01-18 | Airbus France Sas | MOTOR-REGIME CONTROL DEVICE, MOTOR-REGIME CONTROL METHOD AND AIRCRAFT COMPRISING SUCH A DEVICE |
FR3022356B1 (en) * | 2014-06-16 | 2018-03-02 | Thales | METHOD AND DEVICE FOR GENERATING AT LEAST ONE SETPOINT AMONG A FLIGHT CONTROL SET, A MOTOR CONTROL SET AND AN AIRCRAFT GUIDANCE SET, COMPUTER PROGRAM PRODUCT AND ASSOCIATED AIRCRAFT |
FR3058806B1 (en) | 2016-11-14 | 2019-01-25 | Dassault Aviation | DEVICE FOR MANAGING THE MECHANICAL ENERGY OF AN AIRCRAFT, HAVING A FORCE APPLICATION SYSTEM ON A CONTROL KNOB, AIRCRAFT AND ASSOCIATED METHOD |
US10967953B2 (en) * | 2017-12-11 | 2021-04-06 | The Boeing Company | Combined active stick and control boost actuator system |
EP3650354B1 (en) * | 2018-11-12 | 2021-11-03 | Ratier-Figeac SAS | Thrust control assembly |
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2021
- 2021-07-06 FR FR2107283A patent/FR3125139B1/en active Active
Also Published As
Publication number | Publication date |
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FR3125139A1 (en) | 2023-01-13 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PLFP | Fee payment |
Year of fee payment: 2 |
|
PLSC | Publication of the preliminary search report |
Effective date: 20230113 |
|
PLFP | Fee payment |
Year of fee payment: 3 |
|
PLFP | Fee payment |
Year of fee payment: 4 |