The invention provides a helicopter engine power limiting system which comprises an electromechanical management computer used for calculating the state of an engine; the display dial plate is used for displaying the engine state calculated by the electromechanical management computer; the display dial plate comprises an engine state display area, arc-shaped scale marks and watch hands; the engine state display area is used for displaying the current state of an engine, and the arc-shaped scale marks are used for displaying the total distance of the engine and the safe total distance range of the state of the engine. The pointer is used for calibrating the real-time total distance of the engine. The method has the characteristics of improving the decision-making and operation efficiency of the pilot and the space utilization rate of the display area.
本发明提供一种直升机发动机功率限制系统,包括:机电管理计算机,用于计算发动机状态;显示表盘,用于显示机电管理计算机计算得到的发动机状态;所述的显示表盘包括发动机状态显示区域,弧形刻度线和表针;所述的发动机状态显示区域用于显示当前发动机所处状态,弧形刻度线用于显示发动机总距及发动机所处状态的安全总距范围;表针用于标定发动机实时总距。本发明具有提高飞行员决策和操作效率和显示区域的空间利用率的特点。
Helicopter engine power limiting system
一种直升机发动机功率限制系统
2023-03-07
Patent
Elektronische Ressource
Chinesisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
MULTI-ENGINE HELICOPTER POWER SYSTEM ARCHITECTURE AND CORRESPONDING HELICOPTER
Europäisches Patentamt | 2019
|TWIN ENGINE HELICOPTER POWER REQUIREMENTS
SAE Technical Papers | 1989
Twin Engine Helicopter Power Requirements
SAE Technical Papers | 1997
Undercarriage telescopic limiting device, telescopic limiting method and helicopter undercarriage
Europäisches Patentamt | 2024
|