Military unmanned aerial vehicle fault protection device
A fail-safe and unmanned aerial vehicle technology, which is applied in the direction of motor vehicles, aircraft landers, transportation and packaging, etc. It can solve the problems of easy damage on both sides or the bottom of the fuselage, damage to the drone fuselage, and low disassembly efficiency. Achieve good protection effect, wide application range, and ensure complete effect
Inactive Publication Date: 2021-02-05
安徽徽光智能科技有限责任公司
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Problems solved by technology
[0004] The purpose of the present invention is to provide a military UAV fault protection device to solve the problem that the existing military UAVs in the above background technology will fail due to external force impact or their own factors. The machine body is damaged, and the two sides or the bottom of the machine body are easily damaged, and the installation positions required by different bodies are also different, but most of them are locked by bolts. This kind of installation method is relatively easy to operate. It is cumbersome and the efficiency of disassembly and assembly is relatively low
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[0027] The following will clearly and completely describe the technical solutions in the embodiments of the present invention with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only some, not all, embodiments of the present invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.
[0028] see Figure 1-6 , the embodiment provided by the present invention: a military UAV fault protection device, including a warehouse body 1 and a control panel 14, the bottom of the warehouse body 1 is provided with a rubber air bag 2, and the middle position of the inner bottom of the warehouse body 1 is provided with a screw thread Rod 15, and the threaded rod 15 runs through the middle of the top of the bin body 1 and extends to the outside of the bin b...
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The invention discloses a military unmanned aerial vehicle fault protection device which comprises a bin body and a control panel, a rubber air bag is arranged at the bottom of the bin body, a threaded rod is arranged in the middle of the bottom in the bin body, and the threaded rod penetrates through the middle of the top of the bin body and extends to the exterior of the bin body; the bottom ofthe outer side of the threaded rod is sleeved with a driven gear, sleeves B are arranged at the bottoms of the two sides of the bin body, racks are arranged in the sleeves B, mounting bases are symmetrically arranged on the two sides of the top in the bin body, gears are arranged in the mounting bases, and the gears are engaged with the racks, the two sets of racks and the mounting base are located at the two ends in the bin body correspondingly. Through mutual cooperation of the servo motor, the driving gear, the driven gear, the threaded rod, the internal thread sleeve, the hinge plate and the sleeve A, the fixing plate is driven to disassemble and assemble the unmanned aerial vehicle base body, disassembly and assembly by an operator are facilitated, and the operation efficiency is improved.
Description
technical field [0001] The invention relates to the technical field of military unmanned aerial vehicles, in particular to a military unmanned aerial vehicle fault protection device. Background technique [0002] Military drones are unmanned aircraft controlled by remote control equipment or self-contained programs. According to their control methods, they are mainly divided into three types: radio remote control, automatic program control and comprehensive control; Widely used, the research and development of UAVs has made breakthrough progress, and has frequently appeared in several local wars, and has repeatedly made military exploits, and has been highly praised by military personnel from various countries; [0003] Existing military drones will fail due to external force impact or their own factors. The impact force of external force impact will cause damage to the body of the drone. The sides or the bottom of the body are very prone to damage, and different body needs ...
Claims
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IPC IPC(8): B64C39/02B64D45/04B64D45/06
CPCB64C39/02B64D45/04B64D45/06
Inventor 裴忠军严伍琼刘志高
Owner 安徽徽光智能科技有限责任公司