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aircraft

An aircraft and shaft technology, applied in the field of flight, can solve the problems of aircraft rollover, difficult operation, misalignment, etc., and achieve the effect of high safety factor, convenient steering, and avoiding rollover

Active Publication Date: 2016-07-13
CHINA HANGFA SOUTH IND CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, this approach is more difficult to achieve in operation, and, because the direction of the force of the counterweight to the aircraft is opposite to the direction of the force provided by the lifting device of the aircraft itself, and does not overlap, it is also easy to cause the aircraft to roll over and reduce the weight of the aircraft. factor of safety
In addition, the steering of the aircraft also needs to be realized by moving the counterweight, so the steering of the aircraft is more difficult

Method used

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Embodiment Construction

[0020] It should be noted that the embodiments in the application and the features in the embodiments can be combined with each other if there is no conflict. Hereinafter, the present invention will be described in detail with reference to the drawings and in conjunction with the embodiments.

[0021] Such as figure 1 As shown, in this embodiment, the aircraft includes a main body 10 and two lifting devices 20. Two lifting devices 20 are arranged on the main body 10, and the two lifting devices 20 are arranged at intervals perpendicular to the advancing direction of the main body 10.

[0022] With the aircraft of this embodiment, since the main body 10 is provided with two spaced lifting devices 20, the left or right turn of the aircraft can be achieved by controlling the lifting force of the lifting device 20 to the main body 10. Specifically, the lifting force of the lifting device 20 on the left side on the main body 10 is greater than the lifting force of the lifting device 2...

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Abstract

The invention provides an aircraft, comprising a main body (10), and the aircraft further includes: two lifting devices (20), arranged on the main body (10), and the two lifting devices (20) advance vertically to the main body (10). The interval setting in the direction. The aircraft of the invention has a higher safety factor.

Description

Technical field [0001] The present invention relates to the field of flight technology, in particular to an aircraft. Background technique [0002] At present, in order to prevent the aircraft from rolling during flight, that is to say, to prevent the aircraft from rolling sideways, the method adopted is to change the position of the center of gravity of the aircraft, for example, move the counterweight set on the aircraft, when the aircraft is going to the left When rolling over, when the counterweight is moved to the left side of the aircraft, the left side of the aircraft moves down and the right side of the aircraft moves up at the same time. This prevents the left side of the aircraft from rolling; when the aircraft wants to roll to the right, when the counterweight moves To the right side of the aircraft, the right side of the aircraft moves down, while the left side of the aircraft moves up, so as to prevent the aircraft from rolling over. However, this approach is more d...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64C27/82
Inventor 王梅梅易翔农斌刘丽莎程辉王琳
Owner CHINA HANGFA SOUTH IND CO LTD
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