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Novel aircraft and aircraft system

An aircraft, a new type of technology, applied in the field of flight, can solve the problems of all-terrain takeoff and landing, incomplete shooting scenes, prone to crashes, etc., and achieve the effects of increased flight speed, improved flight flexibility, and convenient manipulation

Pending Publication Date: 2017-12-08
汤新哲 +2
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0008] The purpose of the present invention is to provide a new type of aircraft and aircraft system, so as to alleviate the technical problems in the prior art that the shooting scenes are not comprehensive, the flight in complex space is prone to crash, and the technical problems of all-terrain take-off and landing

Method used

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Embodiment Construction

[0044] The technical solutions of the present invention will be clearly and completely described below in conjunction with the accompanying drawings. Apparently, the described embodiments are some of the embodiments of the present invention, but not 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.

[0045] In the description of the present invention, it should be noted that the terms "center", "upper", "lower", "left", "right", "vertical", "horizontal", "inner", "outer" etc. The indicated orientation or positional relationship is based on the orientation or positional relationship shown in the drawings, and is only for the convenience of describing the present invention and simplifying the description, rather than indicating or implying that the referred device or element must have a specific orientation, ...

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Abstract

The invention provides a novel aircraft and an aircraft system, and relates to the technical field of flight. The novel aircraft comprises a fuselage, a pitch-control motor, a roll control motor, a transverse adjusting mechanism, two longitudinal adjusting mechanisms and a four-propeller-supporting-wing adjusting dual-output-shaft motor. The two longitudinal adjusting mechanisms are symmetrically arranged on the two sides of the fuselage. The pitch-control motor is arranged on the longitudinal adjusting mechanisms to control movement of the longitudinal adjusting mechanisms. The roll control motor is arranged on the fuselage and connected with the longitudinal adjusting mechanisms through the transverse adjusting mechanism. The transverse adjusting mechanism controls the longitudinal adjusting mechanisms to move in the transverse direction of the aircraft. Two output shafts of the four-propeller-supporting-wing adjusting dual-output-shaft motor are in transmission connection with four propeller supporting wings to control axial movement of the propeller supporting wings. According to the novel aircraft, the technical problems that a shooting scene is not comprehensive, the aircraft crashes easily in a complex space, and the aircraft takes off and lands on all terrains are solved.

Description

technical field [0001] The invention relates to the technical field of flight, in particular to a novel aircraft and an aircraft system. Background technique [0002] Multi-rotor drones have the characteristics of vertical take-off and landing, hovering in the air, take-off and landing without a runway, maneuverability and ultra-low altitude flight, etc., which make them have incomparable advantages over fixed-wing drones and have a wide range of application prospects. In terms of civilian use, drones can be used in agricultural plant protection, power line inspection, environmental air detection, traffic detection, water resource detection, aerial photography and disaster relief. In terms of military use, it can be used in mission reconnaissance, as a target drone, air relay, air / ground strike and jamming, electronic countermeasures and other fields. [0003] With the continuous development of UAVs in various fields, the tasks it performs are more diverse and complex. In ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C1/06B64C1/30B64C27/08
CPCB64C1/061B64C1/30B64C27/08B64U10/10B64U50/19B64U2101/30B64U2201/20
Inventor 汤新哲马博昊韩云飞
Owner 汤新哲
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