阅读说明：本技术 飞行器的流动本体及飞行器 (Flow body of aircraft and aircraft ) 是由 彼得·克罗伊策 于 2019-07-26 设计创作，主要内容包括：一种飞行器的流动本体(10),包括：流动表面(11),所述流动表面在所述飞行器的飞行期间暴露于气流中,所述流动表面(11)在所述飞行器的飞行期间产生至少一个湍流空气流的区域(24),至少一个穿孔区域,所述至少一个穿孔区域包括延伸穿过所述流动表面(11)的多个开口(32),集流腔(14),所述集流腔被定位在所述流动表面(11)的内部、与所述开口(32)处于流体连通,以及至少一个抽吸管(28),所述抽吸管具有第一端部(27)和第二端部(29),所述第一端部(27)与所述集流腔(14)处于流体连通,所述第二端部(29)包括抽吸开口(20)、并且安排在所述至少一个湍流空气流的区域(24)中,其中,所述抽吸开口(20)被适配成用于当在飞行期间所述流动表面(11)暴露于气流时在所述至少一个抽吸管(28)中引起抽吸,由此引起穿过所述多个开口(32)的空气流。本发明提供一种具有改善的空气流的流动本体(10)。(A flow body (10) of an aircraft, comprising: a flow surface (11) exposed to an airflow during flight of the aircraft, the flow surface (11) generating at least one region (24) of turbulent airflow during flight of the aircraft, at least one perforated region comprising a plurality of openings (32) extending through the flow surface (11), a manifold (14) positioned inside the flow surface (11) in fluid communication with the openings (32), and at least one suction duct (28) having a first end (27) and a second end (29), the first end (27) being in fluid communication with the manifold (14), the second end (29) comprising a suction opening (20) and being arranged in the at least one region (24) of turbulent airflow, wherein the suction opening (20) is adapted for inducing suction in the at least one suction duct (28) when the flow surface (11) is exposed to an airflow during flight, thereby inducing an airflow through the plurality of openings (32). The invention provides a flow body (10) with improved air flow.)