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aircraft

A technology of aircraft and fuselage, which is applied in the field of aircraft, and can solve problems such as insufficient flexibility of aircraft pitching or steering performance

Active Publication Date: 2020-11-24
ZHUHAI PANLEI INTELLIGENT TECH CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0007] In view of the problem that the pitching or steering performance of the above-mentioned existing aircraft is not flexible enough, the purpose of the present invention is to provide an aircraft with high flexibility in pitching or steering performance

Method used

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Embodiment Construction

[0023] The aircraft of the present invention will be described in detail below in conjunction with the accompanying drawings.

[0024] see Figure 1-9 , respectively show perspective views of the aircraft of the present invention in different implementations and different viewing angles from different angles and assembled states.

[0025] see Figure 1~6 , shows an aircraft 100 according to a first embodiment of the present invention. It is an aircraft in the form of a glider. Its composition includes a fuselage 101 , a main wing 102 , a V-shaped tail 103 , a V-shaped tail rudder 104 and a ducted propeller 114 . The structure of the aircraft 100 is basically the same as that of the existing glider. For example, its main wing 102 is fixed on the front part of the fuselage 101 along its central axis, and the main wing 102 is provided with an aileron 102A. The propeller 114 is suspended vertically below the main wing 102 . The axial direction of the central axis of the fusel...

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Abstract

The invention relates to an aircraft which comprises an aircraft body, a main wing, an empennage and a telescopic device. The axial direction of the central axis of the aircraft body is parallel to the advancing direction of the aircraft. The main wing is fixed at the front end of the middle of the aircraft body along the central axis direction of the aircraft body. The telescopic device comprises a driving motor, a threaded rod and a sleeve in one of the composition formations; the driving motor is fixed in the belly of the aircraft body; one end of the threaded rod is connected with the driving motor, and the other end of the threaded rod rotatably stretches into the sleeve; the end, opposite to the stretching end of the threaded rod, of the sleeve is fixedly provided with the empennage; the sleeve is simultaneously fixed in the radial direction and in the circumferential direction and slidably installed in the belly of the aircraft body in the axial direction. The aircraft can change of the rotational inertia of the aircraft in flying, and then the excellent steering maneuverability can be obtained.

Description

technical field [0001] The present invention relates to an aircraft, especially an aircraft capable of flying in the atmosphere. Background technique [0002] An aircraft is an aircraft manufactured and controlled by humans that can fly in the atmosphere. They rely on the static buoyancy of the air or the aerodynamic force generated by the relative motion of the air to lift into the air. [0003] Common aircraft include balloons, gliders, airships, airplanes, helicopters, and quadcopters. [0004] Among them, a glider refers to a fixed-wing aircraft that is heavier than air and does not rely on a power plant to fly. After taking off, it only relies on the reaction force of the air acting on its lifting surface to carry out free flight. Generally speaking, the glider does not have a power plant, but there are also powered gliders equipped with a power plant. A powered glider is equipped with a small auxiliary power unit for self-flight. [0005] The structure of a modern...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64C31/024B64C5/12
Inventor 何春旺
Owner ZHUHAI PANLEI INTELLIGENT TECH CO LTD
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