Control circuit and control method of electric accelerator, aircraft and storage medium
Control circuit and control method of electric accelerator, aircraft and storage medium
- Neue Suche nach: KE JIE
- Neue Suche nach: ZHANG XU
- Neue Suche nach: JIN CHONGWEN
- Neue Suche nach: WANG PENG
- Neue Suche nach: HE BIHAI
- Neue Suche nach: FENG KUAN
- Neue Suche nach: SANG YICHEN
- Neue Suche nach: KE JIE
- Neue Suche nach: ZHANG XU
- Neue Suche nach: JIN CHONGWEN
- Neue Suche nach: WANG PENG
- Neue Suche nach: HE BIHAI
- Neue Suche nach: FENG KUAN
- Neue Suche nach: SANG YICHEN
The invention provides a control circuit and method for an electric accelerator, an aircraft and a storage medium. The control circuit comprises a first accelerator table power module, a second accelerator table power module, a first angle analyzer and a second angle analyzer. The first accelerator table power supply module and the first angle analyzer are connected in series to form a first branch; the second accelerator table power supply module and the second angle analyzer are connected in series to form a second branch; the first branch circuit is electrically connected between a first aircraft power supply and the electric accelerator; the second branch circuit is electrically connected between a second aircraft power supply and the electric accelerator; wherein the first accelerator table power supply module is electrically connected between the first angle analyzer and the first aircraft power supply; and the second accelerator table power supply module is electrically connected between the second angle analyzer and the second aircraft power supply.
本申请提出一种电动油门的控制电路、控制方法、飞行器及存储介质，所述控制电路包括：第一油门台电源模块、第二油门台电源模块、第一角度解析器以及第二角度解析器；所述第一油门台电源模块与所述第一角度解析器串联以构成第一支路；所述第二油门台电源模块与所述第二角度解析器串联以构成第二支路；所述第一支路电连接在第一飞机电源与所述电动油门之间；所述第二支路电连接在第二飞机电源与所述电动油门之间；其中，所述第一油门台电源模块电连接在所述第一角度解析器与所述第一飞机电源之间；所述第二油门台电源模块电连接在所述第二角度解析器与所述第二飞机电源之间。
Dokumentinformationen
Control circuit and control method of electric accelerator, aircraft and storage medium
电动油门的控制电路、控制方法、飞行器及存储介质
2024-04-12
Patent
Elektronische Ressource
Chinesisch
| IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / H02H EMERGENCY PROTECTIVE CIRCUIT ARRANGEMENTS , Schutzschaltungsanordnungen / H02J CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER , Schaltungsanordnungen oder Systeme für die Abgabe oder Verteilung elektrischer Leistung / H02M APPARATUS FOR CONVERSION BETWEEN AC AND AC, BETWEEN AC AND DC, OR BETWEEN DC AND DC, AND FOR USE WITH MAINS OR SIMILAR POWER SUPPLY SYSTEMS , Anlagen zur Umformung von Wechselstrom in Wechselstrom, von Wechselstrom in Gleichstrom oder umgekehrt, oder von Gleichstrom in Gleichstrom und zur Verwendung in Netzen oder ähnlichen Stromversorgungssystemen |
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