Airplane with composite power wings

A composite and powered wing technology, applied in the aviation field, can solve the problems of flight altitude, flight speed and maximum take-off weight, etc., and achieve the effect of small size, large lift, and low development and production costs

Inactive Publication Date: 2013-11-06
陈海生
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Although the rotary-wing aircraft has good flexibility and loose requirements on the environment for take-off and landing, there are problems such as relatively small flying height, flying speed and maximum take-off weight. More than 30 tons, the flight altitude does not exceed 5,000 meters, and the flight speed does not exceed 600 km / h

Method used

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Embodiment Construction

[0014] The composite power wing aircraft of the present invention is realized in this way, and is described in detail below in conjunction with the accompanying drawings.

[0015] See Figure 1 ~ Figure 3 , the composite power wing aircraft is made up of: composite power wing 1, body 2, horizontal direction control rudder 3, body movement engine 4, wing movement engine 5, control cabin 6 and wing fixing bracket 7, body 2 adopts jet According to the body structure of the type aircraft, the horizontal direction control rudder 3, the body motion engine 4 and the control cabin 6 are arranged in the body 2, and the composite power wing 1 is in the shape of a disc, and is fixed on the On the left and right sides of the body 2, the wing motion engine 5 is arranged under the composite power wing 1.

[0016] Control the number of revolutions of the wing motion engine 5, control the motion state in the vertical direction and the size of the lift force by the wing control system arrange...

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PUM

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Abstract

The invention relates to an airplane with composite power wings. The airplane is characterized by being composed of the composite power wings, an airplane body, a horizontal direction control rudder, an airplane body motion engine, wing motion engines, a control cabin and wing fixing supports. The airplane body is in the structure of an airplane body of a jet airplane. The horizontal direction control rudder, the airplane body motion engine and the control cabin are arranged in the airplane body. The composite power wings are in the shapes of disks and are fixed on the left side and the right side of the airplane body through the wing fixing supports extending out of the airplane body, and the wing motion engines are arranged on the lower surfaces of the composite power wings. The airplane overcomes contradictions of airplanes with fixed wings and rotating wings in aspects of the aerodynamics including lifting force, resisting force and disturbing force; has a large lifting force and a small body form on the condition of the same geometric dimensions and is not limited in aspects of take-off and landing conditions; is simple in structure and low in development and production cost; can take off and land vertically and can hover; can be used for developing airplanes and transportation and emergency equipment with many varieties, many specifications and many purposes.

Description

technical field [0001] The invention belongs to the technical field of aviation and relates to a novel aircraft, in particular to a composite power wing aircraft. Background technique [0002] The wing is a key component of the aircraft and one of the determining factors of the aircraft's carrying capacity. Modern aircraft can be roughly divided into two categories: fixed-wing aircraft and rotary-wing aircraft. Although the fixed-wing aircraft has the characteristics of high flying height, fast speed and large carrying capacity, its large size and heavy weight limit the flexibility and carrying capacity of the aircraft, and its use is restricted due to its harsh take-off and landing conditions scope. According to relevant information, the current largest aircraft in the world has a take-off weight of about 600 tons. The maximum take-off weight of the Yun-20 transport aircraft developed by my country is 220 tons. Such a large aircraft can only take off and land at a few air...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C39/06B64C27/26
Inventor 陈海生陈泰安
Owner 陈海生
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