The invention provides a natural icing comprehensive flight test method, and the method comprises the steps: 1, carrying out the normal function verification of an anti-icing system under a continuous maximum icing condition, and enabling the continuous maximum icing condition to be a layered icing cloud condition; the anti-icing system comprises a wing anti-icing system, a nacelle anti-icing system, a windshield heating system and an icing detection system; 2, anti-icing system failure configuration verification is carried out under the continuous maximum icing condition, and anti-icing system failure comprises single-side wing anti-icing air entraining failure and two-side windshield heating failure; and step 3, flight quality and anti-icing system verification under the continuous maximum icing condition is carried out, wherein the flight quality is aircraft stability and maneuverability of the aircraft.
本申请提供一种自然结冰综合试飞方法,所述方法包括:步骤1:进行连续最大结冰条件下防冰系统正常功能验证,其中,连续最大结冰条件为层状结冰云条件;防冰系统包括机翼防冰系统、短舱防冰系统、风挡加温系统和结冰探测系统;步骤2:进行连续最大结冰条件下防冰系统失效构型验证,其中,防冰系统失效包括单侧机翼防冰引气失效和两侧侧风挡加温失效;步骤3:进行连续最大结冰条件下飞行品质和防冰系统验证,其中飞行品质为飞机的飞机稳定性和操纵性。
Natural icing comprehensive flight test method
一种自然结冰综合试飞方法
2024-04-05
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 |
Napier icing research and flight test organisation
Engineering Index Backfile | 1958
CH148 Icing Flight Test Performance Data Correlation
SAE Technical Papers | 2019
|CH148 Icing Flight Test Performance Data Correlation
British Library Conference Proceedings | 2019
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