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Composite wing aviation aircraft and flight control method thereof

A flight control and aircraft technology, applied in the field of aviation flight, can solve the problems of low coordination operation quality, unsatisfactory effect, and inability to capture the navigation route, so as to facilitate real-time shooting of the navigation environment, reduce the flight height, and have good buffering and guiding performance. Effect

Inactive Publication Date: 2019-09-17
邓欣奇
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] In the existing technology, the quality of the cooperation between the various electrical components inside the compound wing aircraft is low. Its electrical components are powered, thereby effectively saving electricity; during the flight, the environment of the flight route cannot be captured

Method used

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  • Composite wing aviation aircraft and flight control method thereof
  • Composite wing aviation aircraft and flight control method thereof
  • Composite wing aviation aircraft and flight control method thereof

Examples

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Embodiment Construction

[0032] In order to make the purpose, technical solutions and advantages of the present invention clearer, the present invention will be further described in detail below in conjunction with the accompanying drawings. Obviously, the described embodiments are only some of the embodiments of the present invention, rather than all of them. 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.

[0033] The terms "first", "second", "third", "fourth", "fifth", "sixth", "seventh" and "Eighth" and the like, if present, are used to distinguish similar items and are not necessarily used to describe a particular order or sequence. It is to be understood that the data so used are interchangeable under appropriate circumstances such that the embodiments of the invention described herein are, for example, capable of practice in sequences...

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PUM

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Abstract

The invention discloses a composite wing aviation aircraft and a flight control method thereof, and belongs to the technical field of aviation flight. The composite wing aviation aircraft comprises a casing, a control device, and a main flight device, a secondary flight device, an energy storage device, a driving recorder and a shock absorption device, wherein the control device is arranged inside the casing, the main flight device is inserted to the upper part of the casing, the secondary flight device is inserted in one end of the casing, the energy storage device is connected to the upper left surface of the casing in a buckled mode, the driving recorder is inserted into the lower left surface of the casing in a spiral mode, and the shock absorption device is welded to the lower surface of the casing. The control device correspondingly comprises a host machine, a controller, a processor, a wireless transceiver module and a circuit board. According to the composite wing aviation aircraft and the flight control method thereof, the transmission of signals between a remote controller and the aircraft is facilitated through the control device, the main flight device and the secondary flight device are arranged, it is beneficial to controlling the flight state of the aircraft, the energy storage device is arranged to make full use of outdoor solar energy, a more environmentally friendly mode is achieved, and the driving recorder is detachably connected obliquely with the lower part of the casing so as to facilitate observation of the flight environment of the aircraft.

Description

technical field [0001] The invention relates to the technical field of aviation flight, in particular to a compound wing aircraft and a flight control method thereof. Background technique [0002] With the development of general aviation, there are more and more styles of aircraft, and the society's demand for air vehicles is increasing, and the application range is becoming wider and wider, such as: aerial photography, agriculture, forestry and plant protection, police inspection, power inspection , geological exploration, battlefield reconnaissance, special reconnaissance, material transportation, sea and air joint search and other fields. However, existing general-purpose aircraft generally include several types of aircraft such as fixed-wing, helicopter, multi-rotor and tilt-rotor. [0003] In the existing technology, the quality of the cooperation between the various electrical components inside the compound wing aircraft is low. Its electrical components supply energ...

Claims

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Application Information

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IPC IPC(8): B64C27/26B64D27/24B64D47/00
CPCB64C27/26B64D27/24B64D47/00B64D27/353Y02T50/50
Inventor 邓欣奇
Owner 邓欣奇
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