Multi-rotor aircraft auxiliary flight device

A multi-rotor aircraft and flying device technology, applied in the field of aircraft, can solve the problems of increased engine heat load and poor endurance

Pending Publication Date: 2019-06-14
李明珠
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

[0005] The purpose of the embodiments of the present invention is to provide a multi-rotor aircraft auxiliary flight device to solve the problems of increased heat load and poor endurance of aircraft or drone engines in the prior art

Method used

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  • Multi-rotor aircraft auxiliary flight device
  • Multi-rotor aircraft auxiliary flight device
  • Multi-rotor aircraft auxiliary flight device

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Embodiment Construction

[0058] The implementation mode of the present invention is illustrated by specific specific examples below, and those who are familiar with this technology can easily understand other advantages and effects of the present invention from the contents disclosed in this description. Obviously, the described embodiments are a part of the present invention. , but not all examples. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.

[0059] Terms such as "upper", "lower", "left", "right", and "middle" quoted in this specification are only for the convenience of description, and are not used to limit the scope of the present invention. The change or adjustment of the relative relationship shall also be regarded as the implementable scope of the present invention without substantive change of the technical content.

[0060] Su...

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Abstract

The embodiment of the invention discloses a multi-rotor aircraft auxiliary flight device, and relates to the technical field of aircrafts. The device comprises a first auxiliary wing component, a first driving component, a second auxiliary wing, a second driving component and a unit body; the first auxiliary wing component, the first driving component, the second auxiliary wing and the second driving component are all arranged on the unit body, the first driving component is connected with the first auxiliary wing component through a first regulating component, the axis direction of the firstauxiliary wing component is in the horizontal plane, the second driving component is connected with the second auxiliary wing through a second regulating component, and the axis direction of the second auxiliary wing is in the vertical plane; by additionally arranging the device on the aircraft or an unmanned aerial vehicle, the flight attitude is adjusted at different flight stages of the aircraft or the unmanned aerial vehicle, the duration of flight and the service life of an engine are prolonged, and the failure rate is lowered.

Description

technical field [0001] The invention relates to the technical field of aircraft, in particular to an auxiliary flight device for a multi-rotor aircraft. Background technique [0002] Unmanned aircraft, referred to as "UAV", is an unmanned aircraft controlled by radio remote control equipment and its own program control device. There is no cockpit on board, but equipment such as autopilot and program control device are installed. The personnel on the ground, on the ship, or at the remote control station of the parent aircraft track, locate, remotely control, telemeter and digitally transmit it through radar and other equipment. Widely used in aerial reconnaissance, surveillance, communication, anti-submarine, electronic jamming, etc. [0003] Nowadays, all kinds of traditional large, medium and small, electric, gasoline-powered and hybrid aircraft and drones use the method of instantaneously increasing and decreasing the voltage, current, and fuel supply, thereby instantane...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C27/08B64C27/26
Inventor 李明珠
Owner 李明珠
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