Cylindrical unmanned aerial vehicle
An unmanned aerial vehicle and a barrel-type technology, applied in the field of aircraft, can solve the problems of poor flight aerodynamic stability, short flight time, complex service life, etc., and achieve the effects of good aerodynamic characteristics, small space occupation, and simple operation.
Inactive Publication Date: 2020-03-10
西安毫米波光子科技有限公司
View PDF4 Cites 5 Cited by
- Summary
- Abstract
- Description
- Claims
- Application Information
AI Technical Summary
Problems solved by technology
However, the existing folding-wing UAV automatically unfolds its wings after take-off, but this deployment method is limited by the launch mechanism and the operation is complicated and the service life is short, which will also greatly increase the preparation time before the UAV launch. The barrel-launched UAV in the technology has a shorter flight time
The existing folding-wing UAV wings are simply unable to adapt to various harsh conditions, and the flight aerodynamic stability is poor
Method used
the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
View moreImage
Smart Image Click on the blue labels to locate them in the text.
Smart ImageViewing Examples
Examples
Experimental program
Comparison scheme
Effect test
Embodiment Construction
[0024] In order to enable those skilled in the art to better understand the technical solution of the present invention, the barrel drone of the present invention will be further described in detail below in conjunction with the accompanying drawings and specific embodiments.
[0025] Such as Figure 1-7 As shown, it includes a fuselage 1, an upper wing 2, a lower wing 3, a V-shaped tail 4, a power assembly 5, and a foldable propeller assembly 6.
[0026] Wherein the fuselage 1 is a cylindrical structure, the bottom and top of the fuselage are cut flat to form the folded upper wing 2 and the lower wing 3, and the left and right sides of the fuselage tail are obliquely cut for storing the folded The V-tail 4.
[0027] Further, the upper wing 2 includes an upper wing left section 7 and an upper wing right section 8, and the lower wing 3 includes a lower wing left section 9 and a lower wing right section 10 , lower wing left aileron 11, lower wing right aileron 12; wherein when...
the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to View More PUM
Login to View More Abstract
The invention relates to a cylindrical unmanned aerial vehicle. The cylindrical unmanned aerial vehicle comprises a vehicle body, upper wings, lower wings, a V-shaped empennage, a power assembly and afoldable propeller assembly. By means of the layout of the upper wings and the lower wings and the arrangement of the V-shaped empennage, the cylindrical unmanned aerial vehicle can adapt to multipleclimates and severe conditions and has the advantage that the cruising state aerodynamic characteristic is good. Meanwhile, by means of the folding setting of the wings, the corresponding wings are arranged at the bottom, the top and the tail of the vehicle body, and therefore the barrel-held state of the cylindrical unmanned aerial vehicle can be small in occupied space and light in weight, thecylindrical unmanned aerial vehicle can be carried on the back of a single soldier and can also be launched in a cluster mode, and the operation is easy.
Description
technical field [0001] The invention relates to the technical field of aircraft, in particular to a barrel-type unmanned aerial vehicle. Background technique [0002] The folding wing UAV is a kind of UAV with foldable wings, which can fold all parts through the folding mechanism, effectively reduce the space size, and realize the launch or delivery of various weapon platforms. Folding-wing UAVs can perform single or multiple tasks such as reconnaissance and damage assessment, communication relay, target indication, and precision strikes through the organic combination of ammunition technology. It has low cost, high cost ratio, small size, and strong stealth capabilities. Features. [0003] Most of the existing folding-wing UAVs only have foldable wings for storage. Before take-off, the wings are unfolded to take off like fixed-wing aircraft. space advantage. However, the existing folding-wing UAV automatically unfolds its wings after take-off, but this deployment method ...
Claims
the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to View More Application Information
Patent Timeline
Login to View More Patent Type & Authority Applications(China)
IPC IPC(8): B64C1/30B64C1/00B64C3/00
CPCB64C1/00B64C1/30B64C3/00
Inventor 岑宇辉周梦娇周浩君孙天韵张海云
Owner 西安毫米波光子科技有限公司