The invention belongs to the technical field of helicopter design, and particularly relates to a method for determining the flight performance of a helicopter through test flight data. The method comprises the following steps: obtaining power required for hovering according to hovering test flight data; according to the variable-height level flight test flight data, determining the level flight required power, and in the variable-height level flight process, keeping the conversion weight of the helicopter unchanged by adjusting the flight height; determining the climbing efficiency according to the sawtooth climbing test flight data, and determining the climbing required power; engine installation loss is determined according to hovering, level flight and climbing test flight data, and therefore the available power of the helicopter is determined; and determining the flight performance according to the required power and the available power of the helicopter in the states of hovering, level flight and climbing.
本发明属于直升机设计技术领域,尤其涉及一种通过试飞数据确定直升机飞行性能的方法。所述方法包括:根据悬停试飞数据得到悬停需用功率;根据变高度平飞试飞数据,确定平飞需用功率,在所述变高度平飞过程中,通过调整飞行高度保持直升机换算重量不变;根据锯齿爬升试飞数据确定爬升效率,确定爬升需用功率;根据悬停、平飞、爬升试飞数据确定发动机安装损失,从而确定直升机可用功率;根据悬停、平飞、爬升状态下的直升机需用功率和可用功率,确定飞行性能。
Method for determining flight performance of helicopter through test flight data
一种通过试飞数据确定直升机飞行性能的方法
2025-02-18
Patent
Electronic Resource
Chinese
IPC: | B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen |
Helicopter flight test instrumentation
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