The invention describes a helicopter (1) comprising: a tail boom (7); a vertical tail (8) protruding from the tail boom (7); the horizontal empennage (9) is arranged at the tail beam (7) and is transverse to the vertical empennage (8); at least one of the vertical tail (8) and the horizontal tail (9) defines a first aerodynamic surface (10, 11) generating a first aerodynamic force; at least one first element (20, 90) transverse to the first aerodynamic surface (10, 11); and a second aerodynamic surface (21, 92) generating a second aerodynamic force, the second aerodynamic surface being connected to the first element (20, 90), facing and spaced apart from the first aerodynamic surface (10, 11); the second aerodynamic surface (21, 92) is spaced apart from the other of the vertical tail (8) and the horizontal tail (9).
本发明描述了一种直升机(1),其包括:尾梁(7);从尾梁(7)突出的垂直尾翼(8);以及设置在尾梁(7)处并横向于垂直尾翼(8)的水平尾翼(9);垂直尾翼(8)和水平尾翼(9)中的至少一个限定产生第一空气动力的第一空气动力学表面(10、11);横向于第一空气动力学表面(10、11)的至少一个第一元件(20、90);以及产生第二空气动力的第二空气动力学表面(21、92),该第二空气动力学表面与第一元件(20、90)连接,面对第一空气动力学表面(10、11)并且与该第一空气动力学表面间隔开;第二空气动力学表面(21、92)与垂直尾翼(8)和水平尾翼(9)中的另一个间隔开。
Helicopter, helicopter kit and associated reconfiguration method
直升机、直升机套件及相关联的重新配置方法
2022-10-14
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
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