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An axial aircraft, symmetrical technology, applied in the field of aircraft, can solve the problems of low efficiency, inability to save itself, and fixed-wing aircraft cannot vertically lift and hover
Active Publication Date: 2017-10-10
CHINA AIRCRAFT MAINTENANCE & ENG
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[0002] The traditional octocopter consumes a lot of energy when cruising, and its stability and safety are poor. When it loses part or all of its power, it is basically unable to save itself; the traditional fixed-wing aircraft cannot vertically lift and hover; Low, low security and stability
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[0009] Now in conjunction with accompanying drawing, the present invention is described in detail: a kind of symmetric octacopter, comprises fuselage 1, left compound wing 2, right compound wing 3, support 4, tail boom 5, empennage axis 6, left lateral empennage 7 , right lateral tail 8, vertical tail 9, landing gear 10, front left rotor 11, front right rotor 12, rear left rotor 13 and rear right rotor 14. The fuselage 1 is equipped with a control system and airborne equipment. The bracket 4 is fixedly connected with the fuselage 1 . The left compound wing 2 and the right compound wing 3 have the same structure, and they are symmetrically installed on the left and right sides of the fuselage 1. The front left rotor 11, the front right rotor 12, the rear left rotor 12 and the rear right rotor 14 have the same structure, and they are respectively symmetrically installed on the left and right sides of the front of the fuselage 1 and the left and right sides of the rear through t...
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Abstract
A symmetrical octocopter belongs to the field of aircraft technology, including a fuselage, a left compound wing, a right compound wing, a bracket, a tail boom, a tail shaft, a left transverse tail, a right transverse tail, a vertical tail, a landing gear, a front Left rotor, front right rotor, rear left rotor and rear right rotor. The front left rotor, the front right rotor, the rear left rotor and the rear right rotor have the same structure, and they are installed on the left and right sides and the rear left and right sides of the fuselage by brackets. The left transverse empennage and the right transverse empennage are respectively symmetrically installed on the left and right sections of the empennage shaft, and the left transverse empennage and the right transverse empennage can deflect up and down around the empennage axis. The left compound wing and the right compound wing have the same structure, they are symmetrically installed on the left and right sides of the fuselage, and they are respectively equipped with two rotors. The flaps of the left compound wing consist of a fixed front flap and a rear flap that is deflectable around the wing axis. The take-off and landing site of the aircraft is not large, it can lift vertically, the generated lift is relatively large, it is safe, stable and flexible.
Description
technical field [0001] A symmetrical octocopter belongs to the technical field of aircraft, in particular to an octocopter. Background technique [0002] The traditional octocopter consumes a lot of energy when cruising, and its stability and safety are poor. When it loses part or all of its power, it is basically unable to save itself; the traditional fixed-wing aircraft cannot vertically lift and hover; Low, security and stability are not high. Contents of the invention [0003] The purpose of the invention is to overcome the above-mentioned shortcomings of traditional hexacopters, fixed-wing aircraft and helicopters, and to invent a highly efficient and safe symmetrical octacopter that can take off and land vertically. [0004] A symmetrical octocopter, comprising a fuselage, a left compound wing, a right compound wing, a bracket, a tail boom, a tail shaft, a left transverse tail, a right transverse tail, a vertical tail, a landing gear, a front left rotor, a front rig...
Claims
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Application Information
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