Fuselage protection device and protection method of unmanned aerial vehicle
A protective device and UAV technology, which is applied to aircraft indicating devices, aircraft parts, transportation and packaging, etc. It can solve problems such as crashes and UAVs losing their flight capabilities, and achieve the effect of reducing the risk of being damaged
Inactive Publication Date: 2022-07-08
江苏云端智能科技有限公司
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Problems solved by technology
[0004] In view of this, the object of the present invention is to propose a fuselage protection device and a protection method for a UAV, so as to solve the problem that the UAV will easily lose its flying ability and eventually crash after the wing of the UAV is hit.
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[0026] In order to make the objectives, technical solutions and advantages of the present invention more clearly understood, the present invention will be further described in detail below with reference to specific embodiments and accompanying drawings.
[0027] It should be noted that, unless otherwise defined, the technical terms or scientific terms used in the embodiments of the present invention shall be the usual meanings understood by those with ordinary skills in the field to which the present invention belongs. The terms "first," "second," and similar terms used herein do not denote any order, quantity, or importance, but are merely used to distinguish different components. "Comprises" or "comprising" and similar words mean that the elements or things appearing before the word encompass the elements or things recited after the word and their equivalents, but do not exclude other elements or things. Words like "connected" or "connected" are not limited to physical or m...
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The invention relates to the technical field of unmanned aerial vehicle protection, in particular to an unmanned aerial vehicle fuselage protection device and method.The unmanned aerial vehicle fuselage protection device comprises an unmanned aerial vehicle body, a fuselage is arranged in the middle of the unmanned aerial vehicle body, first supports are arranged on the peripheral side of the fuselage at equal intervals, the first supports are provided with wings, and arc-shaped connecting plates located on one sides of the wings are arranged at the ends of the first supports; a first arc-shaped sliding groove is formed in the outer side of the arc-shaped connecting plate, a first arc-shaped sliding block is slidably connected into the first arc-shaped sliding groove, the first arc-shaped sliding block is connected with an arc-shaped anti-collision plate parallel to the arc-shaped connecting plate through a connecting frame, a first rack is connected to the bottom of the first arc-shaped sliding block, and arc-shaped protective cover pieces are arranged on the two sides of the first arc-shaped sliding groove correspondingly. The arc-shaped protective cover piece comprises an outer arc-shaped telescopic cylinder located on one side of the arc-shaped connecting plate, and an inner arc-shaped telescopic cylinder is slidably connected into the outer arc-shaped telescopic cylinder. According to the unmanned aerial vehicle, the wings can be protected more comprehensively, and the risk that the unmanned aerial vehicle body is damaged after being impacted is reduced.
Description
technical field [0001] The invention relates to the technical field of drone protection, in particular to a fuselage protection device and a protection method for a drone. Background technique [0002] UAVs are easily damaged by external influences during flight. [0003] For example, the patent with the application number of CN202021650570.2, an anti-collision and collision avoidance device for unmanned aerial vehicle operation, including a drone main body, the drone main body is provided with a plurality of wings, and two adjacent wings of the drone main body are provided An anti-collision and collision-avoidance structure is arranged between them, and the anti-collision and collision-avoidance structure includes a baffle set on the wing of the main body of the drone. The side of the board away from the main body of the drone is provided with a center jack, and an anti-collision rod is inserted and fixed in the center jack, one end of the anti-collision rod protrudes from...
Claims
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Login to View More IPC IPC(8): B64D45/00
CPCB64D45/00B64U30/20B64U10/10Y02T50/40
Inventor 林俊武李超罗帅
Owner 江苏云端智能科技有限公司