aircraft

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...

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

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