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Cloud platform structure and its fixing frame, aircraft body and aircraft

An aircraft and fixed frame technology, applied in the field of flight control, can solve the problems of poor connection reliability, inconvenient portability and transportation, difficult disassembly and assembly, etc., and achieve the effect of stable connection effect

Active Publication Date: 2018-06-12
BEIJING XIAOMI MOBILE SOFTWARE CO LTD +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The aircraft body and the gimbal structure in the prior art are designed in an integrated manner, so that the aircraft as a whole needs to occupy a large amount of space, making it inconvenient to carry and transport
[0003] In the related technology, it is proposed to separate the aircraft body and the gimbal structure, that is, the split aircraft, but the aircraft body and the gimbal structure need to be connected and matched by screws, and there are problems such as poor connection reliability and difficult disassembly.

Method used

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  • Cloud platform structure and its fixing frame, aircraft body and aircraft
  • Cloud platform structure and its fixing frame, aircraft body and aircraft
  • Cloud platform structure and its fixing frame, aircraft body and aircraft

Examples

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Embodiment Construction

[0033] Reference will now be made in detail to the exemplary embodiments, examples of which are illustrated in the accompanying drawings. When the following description refers to the accompanying drawings, the same numerals in different drawings refer to the same or similar elements unless otherwise indicated. The implementations described in the following exemplary examples do not represent all implementations consistent with the present disclosure. Rather, they are merely examples of apparatuses and methods consistent with aspects of the present disclosure as recited in the appended claims.

[0034] figure 1 is a schematic diagram of a pan-tilt structure shown according to an exemplary embodiment, such as figure 1 As shown, the pan-tilt structure 1 may include: a pan-tilt body 11 and a fixing frame 12; the bottom of the fixing frame 12 can be fixedly connected to the top of the pan-tilt body 11, such as by screws. By configuring a special fixing frame 12, when the fixing ...

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PUM

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Abstract

The invention relates to a holder structure, a fixing frame thereof, an air vehicle body and an air vehicle. The bottom of the fixing frame can be fixedly connected to the top end of a holder body of the holder structure; a fixing buckle is arranged on one side edge of the top of the fixing frame and can be connected to a preformed clamping groove in the bottom of the air vehicle body in a matched mode; at least one buckle hole is formed in the other side edge, opposite to the side edge, of the fixing frame and can be connected to prearranged lock buckles on the bottom of the air vehicle body in a matched mode. According to the technical scheme, the holder structure and the air vehicle body can be stably and fixedly connected or fast disassembled.

Description

technical field [0001] The present disclosure relates to the technical field of flight control, in particular to a platform structure and its fixing frame, an aircraft body and the aircraft. Background technique [0002] Through the gimbal structure assembled on the aircraft body, the stability and controllability of the aerial photography process can be improved. The aircraft body and the gimbal structure in the prior art are designed in an integrated manner, so that the aircraft as a whole needs to occupy a large amount of space, making it inconvenient to carry and transport. [0003] In the related art, it is proposed to separate the aircraft body and the gimbal structure, that is, the split aircraft, but the aircraft body and the gimbal structure need to be connected and matched by screws, and there are problems such as poor connection reliability and difficult disassembly. Contents of the invention [0004] The present disclosure provides a pan-tilt structure and its...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): F16M13/02G03B17/56B64D47/08
CPCB64D47/08F16M13/02G03B17/561
Inventor 车建明杨容涛伍沧浪蔡炜叶华林贺孟华
Owner BEIJING XIAOMI MOBILE SOFTWARE CO LTD