Aircraft

An aircraft and wing technology, applied in the field of aircraft, can solve the problems of large maintenance and repair workload, short stay time, complex helicopter structure, etc., and achieve the effect of simple structure and improved wind resistance.

Inactive Publication Date: 2013-06-26
厦门同嘉信息科技有限公司
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, the structure of the helicopter is quite complicated, the time to stay...

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Embodiment Construction

[0034] Please check figure 1 and figure 2 , which shows a first embodiment of an aircraft of the present invention. The aircraft 100 includes a single wing 10 and a thrust device 20 . The center of gravity G of the aircraft 100 is located at the inner end of the single wing 10 along the length direction.

[0035] The one-sided wing 10 is used to rotate around the center of gravity G of the aircraft 100 to generate lift. The rear end of the single wing 10 along the width direction is provided with an aileron 11 for controlling the flight direction.

[0036] The thrust device 20 is used to propel the single-sided wing 10 to rotate around the center of gravity G of the aircraft 100 . The thrust device 20 may be a propeller or a jet engine or a rocket launcher or the like. The thrust device 20 is connected to the single-side wing 10 , located at the outer end of the single-side wing 10 along the length direction, and connected to the front end of the single-side wing 10 alon...

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Abstract

The invention discloses an aircraft which comprises a unilateral wing used for rotatablely generating lift force, and a thrust device used for pushing the unilateral wing to rotate around the barycenter of the aircraft, wherein an aileron used for controlling a fly direction is arranged on the unilateral wing; and the thrust device is connected onto the unilateral wing, and the barycenter of the aircraft deviates from the center position of the unilateral wing along the length direction. The unilateral wing rotates around the barycenter of the aircraft to generate the lift force, so that the aircraft can vertically rise. Therefore, the aircraft disclosed by the invention has the advantage of vertical take-off and landing. Meanwhile, according to the aircraft, the lift force of the aircraft is generated by the rotation of the unilateral wing, and the front-and-back as well as the left-and-right fly direction is controlled by the aileron, so that the aircraft has the advantage of being simple in structure. According to the gyroscopic effect generated by the means that the unilateral wing rotates around the barycenter of the aircraft, the wind resistance of the aircraft and the stability of fly can be effectively improved.

Description

technical field [0001] The invention relates to an aircraft. Background technique [0002] Aircraft is the main carrier in the air, mainly including fixed-wing aircraft and helicopters. [0003] Fixed-wing aircraft has the advantages of fast flight speed and high flight efficiency. However, fixed-wing aircraft need to have a long runway for takeoff and landing, and the conditions for takeoff and landing are relatively strict, and they cannot take off and land vertically. [0004] Helicopters can do low-altitude, low-speed and maneuvering flights with a constant nose direction. The most prominent feature is that helicopters have the function of vertical take-off and landing. However, the structure of the helicopter is quite complicated, the time to stay in the air is short, and the workload of maintenance and repair is relatively large. [0005] Therefore, there is currently no aircraft that has both the advantages of fixed-wing aircraft and helicopters. It not only has th...

Claims

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Application Information

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IPC IPC(8): B64C29/00B64C27/02B64C9/00
Inventor 向小宏陈学栋王灵廖志勤
Owner 厦门同嘉信息科技有限公司
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