Integrated control system for aircraft with V-shaped empennage
A control system and aircraft technology, applied in the field of control systems, can solve the problems of inconvenient control, complex control system structure, large cabin space, etc., and achieve the effects of weight reduction, simple control system, and small size
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[0041] Hereinafter, preferred embodiments of the present invention are given in conjunction with the drawings to illustrate the technical solutions of the present invention in detail.
[0042] Such as Figure 2 to Figure 5 As shown, the integrated V-tail aircraft control system provided by the present invention includes a cross section rotatably connected to the body of the aircraft. Type shaft 1 for fixing The bracket 13 of the type shaft 1; two handles 2 movably arranged at both ends of the shaft 1 and used to drive the shaft 1 to rotate synchronously along the axis OO. At the same time, the two handles 2 can also be left and right in the plane where the cross section of the shaft 1 is located. Swing right. Among them, when the two handles 2 rotate along the axis O-O or swing left and right in the plane where the cross section of the shaft 1 is located, they can both act synchronously.
[0043] In order to control the aircraft's V-tail 8 for elevation or direction deflection c...
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