Planetary reducer for coaxial propeller reversing helicopter
A technology of planetary reducer and helicopter, which is applied in the direction of unmanned aircraft, aircraft, rotorcraft, etc., and can solve the problem of inability to realize dual-rotor coaxial reverse rotation
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Embodiment 1
[0024] A planetary reducer for a coaxial anti-propeller helicopter of the present invention comprises an intermediate transmission shaft 12, a first-stage sun gear 1 fixed on the top of the intermediate transmission shaft, a plurality, such as three or four, and the above-mentioned The first-stage planetary gear 2 meshed with the first-stage sun gear, the first-stage ring gear 3 meshed with the first-stage planetary gear, and the connecting frame 6 that fixedly connects the first-stage inner ring gear with the outer shaft , a plurality of secondary planetary gears 4 arranged coaxially with the first-stage planetary gears, the secondary sun gears 4 coaxially arranged above the primary sun gear and meshed with the second-stage planetary gears in a relatively rotatable manner 5. The secondary sun gear is connected to the inner shaft through transmission, and the coaxial upper and lower ends of the primary planetary gear and secondary planetary gear are respectively set up and down...
Embodiment 2
[0031] The lower end of the intermediate transmission shaft is fixedly provided with a bevel gear 11 and a bevel gear shaft 10 matched with the bevel gear, and the power end of the bevel gear shaft is fixedly connected with the engine through a coupling. The lower flange 15 of the bevel gear is arranged on the said intermediate transmission shaft, the upper part of the central hole of the said bevel gear is in interference fit with the said intermediate transmission shaft, and the middle part is in interference fit with the said intermediate transmission shaft. The shaft spline fits, and the lower part transition fits with the intermediate transmission shaft. The shaft intersection angle of the bevel gear and the bevel gear shaft is 80°-90°. That is, the shaft angle of a pair of bevel gears can be 90 degrees or not 90 degrees, so that the input shaft can be inclined in different directions to adapt to different installation positions of the engine; or the output shaft of the r...
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