The invention relates to a method for mounting a vortex generator (32) on a pneumatic wall (30) of an aircraft, characterized in that it comprises, prior to the step of assembling the vortex generator (32) and the pneumatic wall (30), a step of providing at least one gasket (52) interposed between a base (40) of the vortex generator (32) and the pneumatic wall (30), said gasket (52) comprising a first face (52.1) and a second face (52.2), the first surface is oriented towards the pneumatic wall (30) during operation and is shaped to fit an inner surface (30.2) of the pneumatic wall (30), and the second surface is oriented towards the base (40) during operation and is shaped to fit an upper surface (44.1, 46.1) of a wing (44, 46) of the base (40). This solution allows the vortex generator (32) to be manufactured without taking into account the radian of the pneumatic wall (30). The invention also relates to an aircraft comprising at least one vortex generator mounted in this way.
本发明涉及一种将涡流发生器(32)安装在飞行器的气动壁(30)上的安装方法,其特点在于,该方法在组装涡流发生器(32)和气动壁(30)的步骤之前包括设置插设在涡流发生器(32)的底座(40)和气动壁(30)之间的至少一个垫片(52)的步骤,所述垫片(52)包括第一面(52.1)和第二面(52.2),第一面在运行时朝气动壁(30)定向、且其形状适配气动壁(30)的内表面(30.2),第二面在运行时朝底座(40)定向、且其形状适配底座(40)的翼部(44、46)的上表面(44.1、46.1)。该方案允许制造涡流发生器(32)而无需考虑气动壁(30)的弧度。本发明还涉及包括以这种方式安装的至少一个涡流发生器的飞行器。
Method for mounting vortex generator on pneumatic wall of aircraft and aircraft comprising vortex generator so mounted
用于将涡流发生器安装在飞行器的气动壁上的方法及包括如此安装的涡流发生器的飞行器
2024-04-12
Patent
Electronic Resource
Chinese
European Patent Office | 2024
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