Low-rotating-speed double-layer propcopter


  • Inventors: HUANG CHUNSHUI
  • Assignees: 黄春水
  • Publication Date: August 14, 2013
  • Publication Number: CN-203127143-U


The utility model discloses a low-rotating-speed double-layer propcopter which comprises a stander and two layers of propellers, wherein the propellers are arranged on the stander through a center shaft; the two layers of propellers are respectively an upper propeller and a lower propeller; the rotating direction of the upper propeller is opposite to that of the lower propeller; each of the upper propeller and the lower propeller comprises two blades; the two blades are respectively symmetrically arranged on two sides of the center shaft through connection rods; concave structures are arranged on the lower surfaces of the blades; when the load weight is 200 kilograms, the sum of areas of the corresponding four blades is 6-15 square meters; and the blades are 1.8-2.5 meters long and 0.6-1.5 meters wide. The low-rotating-speed double-layer propcopter has the advantages that the rotating speed of the large-blade propellers is lower, the abrasion to accessories is lower, the service life is longer, and the fault rate is lowe; the utilization rate of engine power is improved; by adoption of the smaller-size engine, the low-rotating-speed double-layer propcopter is lighter in mass, lower in cost and higher in market prospect; and energy can be better saved.




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Cited By (3)

    Publication numberPublication dateAssigneeTitle
    CN-103072689-AMay 01, 2013黄春水Low-rotating-speed double-layer propcopter
    CN-103072689-BApril 13, 2016黄春水低转速双层螺旋桨直升机
    CN-105539830-AMay 04, 2016歌尔科技有限公司Air vehicle