The invention discloses a testing device for a rudder wing. The testing device for the rudder wing comprises a base; the heating mechanism is movably mounted on the base and is provided with a heating space for heating a rudder wing; the adjusting mechanism is connected between the base and the heating mechanism, and the adjusting mechanism is configured to adjust the heating distance between the heating mechanism and the rudder wing and/or the heat radiation angle when the rudder wing is heated. According to the test device for the rudder wing, the heating angle and distance can be adjusted according to the shape of the rudder wing surface of the rudder wing, so that the heating uniformity of the rudder wing surface is ensured, the heat utilization rate is improved, the accuracy of a simulation experiment of the rudder wing is improved, and the design reliability of the rudder wing is improved.
本申请公开一种用于舵翼的试验装置,所述用于舵翼的试验装置包括:底座;加热机构,所述加热机构可活动地安装于所述底座且设有用于对舵翼加热的加热空间;调节机构,所述调节机构连接于所述底座和所述加热机构之间,且所述调节机构被配置为调整所述加热机构与所述舵翼之间的加热距离和/或对所述舵翼加热时的热辐射角度。本申请的用于舵翼的试验装置,能够针对舵翼的舵翼面形状调整加热角度和距离,以保证舵翼面的加热均匀性,且利于提高热利用率,进而提高舵翼的模拟实验的准确性,进而提高舵翼的设计可靠性。
Testing device for rudder wing
用于舵翼的试验装置
2025-01-07
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 |
THREE-WING TYPE RUDDER AND SHIP WITH THREE-WING TYPE RUDDER
European Patent Office | 2016
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