首页> 外国专利> The directional stabilizer device and a rotor anti - torque carene and inclined, and a tail unit in a 'v' asymmetric and helicopter relates to such a device.

The directional stabilizer device and a rotor anti - torque carene and inclined, and a tail unit in a 'v' asymmetric and helicopter relates to such a device.

机译:方向稳定器装置和旋翼反倾斜和倾斜的转子,以及“ v”形不对称直升机中的尾部单元涉及这种装置。

摘要

The directional and stabilizer device comprises a rotor anti - torque carene7, drives in rotation in a vein transversale9 provided carenage10 in an inclined on the vertical an angle ranging between 0 and 45. / p & & p & it comprises also a tail "- v" fixed to the top of the carenage10, and the two surfaces aerodynamiques15, 16 are extend of asymmetric with respect to the vertical plane passing through the top of the carenage10. The surfaces aerodynamiques15 et16 are incline according to the angular ranges between 0 and 45. / p & & p & application to the equipment of helicopters has a single rotor lift a mechanical drive.
机译:方向性和稳定器装置包括转子抗扭矩保护器,该驱动器在设置为支架10的支架上以垂直方向倾斜的角度在0°和45°之间的角度在静脉横穿中驱动旋转。 & &它也包括固定在支架10顶部的尾部“ -v”,并且空气动力学15、16的两个表面相对于穿过支架10顶部的垂直平面不对称地延伸。表面aerodynamiques15et16根据0到45之间的角度范围倾斜。 & &应用于直升机的设备具有单旋翼升降机械驱动器。

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