Aircraft model with auxiliary leveling blade control system
A control system and auxiliary balance technology, which is applied in the field of model aircraft with auxiliary balance blade control system, can solve problems such as difficulties, operator and airframe safety threats, and achieve the effect of ensuring safe use and smooth flight movement.
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[0019] refer to figure 1 , which illustrates the disassembly of an embodiment of the present invention; refer to figure 2 , illustrating a schematic assembly of an embodiment; refer to image 3 , illustrates a bottom view of the blade fixing device of an embodiment; in this embodiment, the self-balancing headstock device includes an aircraft drive shaft 1, a rotating block 11, a rotating block bearing 111, a rotating block strip groove 112, a cylinder Pin 113, fixed through hole 114, rotating device 2, a pair of main blades 20, main blade bolts 201, main blade nuts 202, a pair of balance blades 21, balance blade bolts 211, balance blade nuts 212, balance rods 22, balance rods Bearing 221, blade fixing device 23, blade fixing device slot 231, vertical through hole 232, horizontal through hole 233, counterweight sleeve 24, hexagon socket bolt 241, "ten" shaped frame 25 that forms an acute angle with the horizontal plane, balance baseball shape Overcoat 26, spherical overcoat ...
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