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Multi-rotor manned vehicle

An aircraft and multi-rotor technology, applied in the field of aircraft, can solve problems such as short range, low load, and complicated control process, and achieve the effect of eliminating rotation deviation and balancing lift force

Inactive Publication Date: 2019-01-18
FOSHAN SHENFENG AVIATION SCI & TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] But because the multi-rotor aircraft in the prior art is mostly driven by batteries, it has problems such as short voyage and low load, and has many limitations and defects in completing manned flight; in order to realize manned flight, those skilled in the art try The multi-rotor aircraft is driven by the engine, but the control process is complicated during the engine drive process, the flight attitude is not easy to control, and the application effect is poor

Method used

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Embodiment 1

[0035] Embodiment 1 of the present invention discloses a multi-rotor manned aircraft, comprising an aircraft main body 1, a power mechanism and two rotor mechanisms 2; the aircraft main body 1 includes a cabin 3 and a control cabin 4, the cabin 3 is used for manning, and the control cabin 4 For installing the power mechanism, the control cabin 4 is installed at the bottom of the engine room 3; the power mechanism includes a generator, the generator is installed in the control cabin 4, and the generator is electrically connected to the rotor mechanism 2; two rotor mechanisms 2 are arranged on the bottom of the control cabin 4 On the side, the two rotor mechanisms 2 are arranged symmetrically with respect to the central axis of the aircraft and at the same time with respect to the center of the aircraft, and the two rotor mechanisms 2 are located on the same plane.

[0036]A multi-rotor manned aircraft disclosed by the present invention can generate sufficient power through the p...

Embodiment 2

[0054] Embodiment 2 of the present invention discloses a multi-rotor manned aircraft, comprising an aircraft main body 1, a power mechanism and three rotor mechanisms 2; the aircraft main body 1 includes a cabin 3 and a control cabin 4, the cabin 3 is used for manning, and the control cabin 4 For installing the power mechanism, the control cabin 4 is installed at the bottom of the engine room 3; the power mechanism includes a generator, the generator is installed in the control cabin 4, and the generator is electrically connected to the rotor mechanism 2; three rotor mechanisms 2 are arranged on the bottom of the control cabin 4 On the side, two of the rotor mechanisms 2 are arranged symmetrically with respect to the central axis of the aircraft, the other rotor mechanism 2 is arranged along the central axis, and the three rotor mechanisms 2 are located on the same plane.

[0055] A multi-rotor manned aircraft disclosed by the present invention can generate sufficient power thr...

Embodiment 3

[0067] Embodiment 3 of the present invention discloses a multi-rotor manned aircraft, comprising an aircraft main body 1, a power mechanism and four rotor mechanisms 2; the aircraft main body 1 includes a cabin 3 and a control cabin 4, the cabin 3 is used for manning, and the control cabin 4 For installing the power mechanism, the control cabin 4 is installed at the bottom of the engine room 3; the power mechanism includes a generator, the generator is installed in the control cabin 4, and the generator is electrically connected to the rotor mechanism 2; the four rotor mechanisms 2 are arranged on the bottom of the control cabin 4 On the side, two rotor mechanisms 2 are arranged symmetrically with respect to the central axis of the aircraft, and the rotor mechanisms 2 are located on the same plane.

[0068]A multi-rotor manned aircraft disclosed by the present invention can generate sufficient power through the power mechanism installed in the control cabin, so as to realize ma...

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PUM

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Abstract

The invention discloses a multi-rotor manned aircraft comprising: an aircraft body, a power mechanism and at least two rotor configurations; the main body of the aircraft comprises a nacelle and a control nacelle, wherein the nacelle is used for carrying people, the control nacelle is used for installing a power mechanism, and the control nacelle is installed at the bottom of the nacelle; the power mechanism comprises a generator, the generator is installed in the control cabin, and the generator is electrically connected with the rotor structure; the rotor structure is arranged on the side ofthe control cabin, and the rotor structure is symmetrically arranged with respect to the central axis of the aircraft. The invention discloses a multi-rotor manned aircraft, which has the characteristics of long life time and high flexibility.

Description

technical field [0001] The present invention relates to the technical field of aircraft, and more specifically relates to a multi-rotor manned aircraft. Background technique [0002] Multi-rotor aircraft is an aircraft with simple structure, flexible control and stable flight attitude. At present, with the development of materials, electronics and computer control technology, multi-rotor aircraft has been widely used in aerial photography, monitoring and other fields. The multi-rotor aircraft can take off and land vertically, hover for a long time, and has strong maneuverability. It has great application in high-altitude rescue, fire fighting, personnel and material transportation under special conditions such as high-rise buildings, facilities, cliffs, rivers, and mountains. Advantage. [0003] But because the multi-rotor aircraft in the prior art is mostly driven by batteries, it has problems such as short voyage and low load, and has many limitations and defects in comp...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C27/08B64C39/02B64C25/62B64D27/24
CPCB64C25/62B64C27/08B64C39/024B64D27/24B64U50/19Y02T50/60
Inventor 王鹏飞王志成
Owner FOSHAN SHENFENG AVIATION SCI & TECH
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