Unmanned aerial vehicle equipment compartment and unmanned aerial vehicle
A technology for equipment cabins and drones, which is applied to aircraft parts, transportation, and packaging, and can solve the problems of high difficulty in installing airborne equipment, small space for airborne equipment, and low space utilization
Pending Publication Date: 2020-10-23
INST OF ENGINEERING THERMOPHYSICS - CHINESE ACAD OF SCI
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Problems solved by technology
[0007] In view of the equipment layout problems caused by the tight space of the UAV equipment cabin above, as well as the insufficiency of the existing conventional installation schemes, especially the equipment cabin of the supersonic UAV, the space reserved for airborne equipment is small, and the space for airborne equipment is limited. Due to the defects of relatively high installation difficulty and low space utilization rate, the present disclosure provides an unmanned aerial vehicle equipment cabin and an unmanned aerial vehicle, which have the characteristics of high space utilization in the equipment cabin and easy installation of airborne equipment
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[0029] In order to make the purpose, technical solutions and advantages of the present disclosure clearer, the present disclosure will be further described in detail below in conjunction with specific embodiments and with reference to the accompanying drawings.
[0030] It should be understood, however, that these descriptions are exemplary only, and are not intended to limit the scope of the present disclosure. In the following detailed description, for purposes of explanation, numerous specific details are set forth in order to provide a thorough understanding of the embodiments of the present disclosure. It may be evident, however, that one or more embodiments may be practiced without these specific details. Also, in the following description, descriptions of well-known technologies are omitted in order to avoid unnecessarily obscuring the concept of the present disclosure.
[0031] The terminology used herein is for the purpose of describing particular embodiments only, a...
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The invention provides an unmanned aerial vehicle equipment compartment and an unmanned aerial vehicle. The unmanned aerial vehicle equipment compartment comprises a sleeve and an equipment compartment section skin. A plurality of equipment mounting areas are arranged in the sleeve; connecting devices for fixing airborne equipment are arranged in the plurality of equipment mounting areas; the sizeof each equipment mounting area is matched with the airborne equipment installed in the equipment mounting area, the multiple equipment mounting areas are distributed in the inner space of the sleeve, the inner surface of the equipment cabin section skin is attached to the outer surface of the sleeve, and the equipment cabin section skin is connected with the sleeve through a connecting piece. Aplurality of equipment mounting areas are arranged in a three-dimensional mode, the concept of a layer is weakened, emphasis is paid to combination of blocks, and the space of an equipment cabin can be fully utilized through the three-dimensional layout of the equipment mounting areas.
Description
technical field [0001] The present disclosure relates to the field of design and manufacture of unmanned aerial vehicles, in particular to an equipment cabin of an unmanned aerial vehicle and an unmanned aerial vehicle. Background technique [0002] Unmanned aerial vehicle is referred to as "drone", and the English abbreviation is "UAV". In recent years, my country's drone technology has gradually matured, and there are many types of drones, with different shapes, volumes, functions and characteristics. Compared with traditional manned aircraft, it has the advantages of small size, low cost, convenient use, and low requirements on the working environment. In the future, in all walks of life in different fields, the application prospects of drones are very broad. [0003] As an important research and development hotspot in the field of domestic drones, supersonic drones have the characteristics of small aspect ratio, small body volume, small body weight, and high maneuverab...
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IPC IPC(8): B64D47/00
CPCB64D47/00
Inventor 李珂尚栢荣陈万里王文剑凡洪林
Owner INST OF ENGINEERING THERMOPHYSICS - CHINESE ACAD OF SCI