Longitudinally crossed dual-rotor helicopter

An unmanned helicopter, vertically crossed technology, applied in the field of vertically crossed double-rotor unmanned helicopters, can solve the problem of small tail rotor power consumption, etc., and achieve the effect of large vertical center of gravity, small flight resistance and large lift

Active Publication Date: 2014-10-15
杨克伟
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  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

[0003] The present invention provides a longitudinal intersecting twin-rotor unmanned he

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  • Longitudinally crossed dual-rotor helicopter
  • Longitudinally crossed dual-rotor helicopter
  • Longitudinally crossed dual-rotor helicopter

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[0015] The embodiments of the present invention will be described in detail below with reference to the accompanying drawings, but the present invention can be implemented in a variety of different ways defined and covered by the claims.

[0016] Please refer to Figure 1 to Figure 3 , The present invention provides a longitudinally crossed dual-rotor unmanned helicopter, including: a first bevel gear 3, two first steering gears 7, two shafts 32, two propeller parts, two operating mechanisms and two transmissions A transmission mechanism with the same structure; the transmission mechanism includes a second bevel gear 4, a third bevel gear 5 and a fourth bevel gear 6, wherein the second bevel gear 4 meshes with the first bevel gear 3, and the second bevel gear 4 and the third bevel gear The bevel gear 5 is drivingly connected, and the third bevel gear 5 is engaged with the fourth bevel gear 6; the two transmission mechanisms are respectively arranged on both sides of the first bev...

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Abstract

The invention provides a longitudinally crossed dual-rotor helicopter. The longitudinally crossed dual-rotor helicopter comprises a first bevel gear, two first steering engines, two shafts, two propeller parts, two operating mechanisms, and two transmission mechanisms with the same transmission structure; each transmission mechanism comprises a second bevel gear, a third bevel gear and a fourth bevel gear, wherein the second bevel gear is engaged with the first bevel gear and in drive connection with the third bevel gear, and the third bevel gear is engaged with the fourth bevel gear; the two transmission mechanisms are arranged at the two sides of the first bevel gear, respectively; the fourth bevel gears of the two transmission mechanisms are corresponding connected with the two shafts one to one, and the two shafts are opposite in rotation direction; the two propeller parts are mounted at the top ends of the two shafts, respectively; the first steering engines are in drive connection with the propeller parts by use of the operating mechanisms, respectively.

Description

Technical field [0001] The invention relates to the field of helicopters, in particular to a longitudinal cross-type dual-rotor unmanned helicopter. Background technique [0002] In the direct generator in the prior art, as the main propeller rotates to generate lift, it also produces a reaction force opposite to the propeller rotation. In order to overcome this reaction force, a small tail slurry is required. The small tail slurry is powered by the engine to make the small tail The rotation of the propeller produces a pulling force that is opposite to the direction of rotation of the main propeller, which keeps the helicopter body from rotating, while the small tail propeller consumes a certain amount of power, which is a weak part of the helicopter. Summary of the invention [0003] The present invention provides a longitudinal cross-type dual-rotor unmanned helicopter to solve the problem of power consumption for small tail rotors in the prior art. [0004] In order to solve the...

Claims

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Application Information

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IPC IPC(8): B64C27/08
Inventor 杨克伟
Owner 杨克伟
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