CN212022958U

CN212022958U - Hybrid unmanned aerial vehicle

Info

Publication number: CN212022958U
Application number: CN202020728430.6U
Authority: CN
Inventors: 竺铝涛
Original assignee: Hangzhou Tanpu New Material Technology Co ltd; Zhejiang University of Technology ZJUT
Current assignee: Hangzhou Tanpu New Material Technology Co ltd; Zhejiang University of Technology ZJUT
Priority date: 2020-05-07
Filing date: 2020-05-07
Publication date: 2020-11-27
Anticipated expiration: 2030-05-07

Abstract

The utility model discloses an unmanned aerial vehicle that oil electricity mixes, including the unmanned aerial vehicle body, the unmanned aerial vehicle body includes unmanned aerial vehicle wing, and unmanned aerial vehicle wing top outer wall sets up the guiding gutter that four to six equidistance distribute, the top outer wall of unmanned aerial vehicle body has the spoiler through the screw connection, and all there is folding support frame in the four corners department of unmanned aerial vehicle body bottom outer wall through the screw connection, folding support frame includes the fixed block, and the bottom outer wall of fixed block has slewing mechanism through the screw connection, and slewing mechanism is including rotating the motor, and there is the bracing piece through the coupling joint in the one end of rotating the motor output shaft. The utility model discloses when unmanned aerial vehicle flies, the effectual air resistance that produces when having reduced unmanned aerial vehicle and traveling at a high speed of spoiler of afterbody, on the other hand folding support frame is with the bracing piece jack-up, meets with the contact surface of air when reducing the flight, reduces the windage, has improved unmanned aerial vehicle's flying speed, has also reduced the consumption speed of energy.

Description

Hybrid unmanned aerial vehicle

Technical Field

The utility model relates to an unmanned air vehicle technique field especially relates to an unmanned aerial vehicle that oil electricity mixes.

Background

An unmanned plane is called an unmanned plane for short, and is called a UAV (unmanned aerial vehicle) in English, and the unmanned plane is an unmanned plane operated by utilizing a radio remote control device and a self-contained program control device, or is completely or intermittently and autonomously operated by an on-board computer.

Hybrid unmanned aerial vehicle of oil electricity that exists on the market at present is by fuel and electric power hybrid drive, has both solved electric unmanned aerial vehicle's power difference, and the problem of continuation of the journey is short, has also solved the high shortcoming of fuel unmanned aerial vehicle consumption, but hybrid unmanned aerial vehicle of oil electricity when flight, the fuselage still can produce very big windage, and these windages not only can reduce unmanned aerial vehicle's airspeed, also can accelerate the consumption speed of energy.

Disclosure of Invention

The utility model aims at solving the shortcoming that exists among the prior art, and the unmanned aerial vehicle that a proposed oil-electricity mixes.

In order to achieve the above purpose, the utility model adopts the following technical scheme:

the utility model provides an unmanned aerial vehicle that oil and electricity mixes, includes the unmanned aerial vehicle body, the unmanned aerial vehicle body includes unmanned aerial vehicle wing, and unmanned wing top outer wall sets up four to six equidistance distribution's guiding gutter, the top outer wall of unmanned aerial vehicle body has the spoiler through the screw connection, and all there is folding support frame in the four corners department of unmanned aerial vehicle body bottom outer wall through the screw connection.

Further, the folding support frame includes the fixed block, and the bottom outer wall of fixed block has slewing mechanism through screw connection, and slewing mechanism includes the rotation motor, and the one end of rotating the motor output shaft has the bracing piece through the coupling joint.

Further, the spoiler is located the positive center of unmanned aerial vehicle body.

Further, the bottom of the unmanned aerial vehicle body is provided with a rectangular clamping groove, and the specification of the rectangular clamping groove is matched with that of the supporting rod.

Furthermore, the unmanned aerial vehicle wing is obliquely arranged, and the inclination angle of the unmanned aerial vehicle wing is ten to fifteen degrees.

Further, there is the ultrasonic wave to drive bird mechanism unmanned aerial vehicle body bottom outer wall through the screw connection, and the ultrasonic wave drives bird mechanism and includes solar cell panel and fixed plate, there is heat energy sensor one side outer wall on fixed plate top through the screw connection, there is the controller opposite side outer wall on fixed plate top through rivet connection, the controller includes display screen and control button, there is ultrasonic transducer solar cell panel bottom outer wall through the screw connection, there is the power one side inner wall that bird mechanism bottom was driven to the ultrasonic wave through the screw connection.

The utility model has the advantages that:

1. this an unmanned aerial vehicle for oil-electricity mixture, through being provided with spoiler and folding support frame, when unmanned aerial vehicle flies, the effectual air resistance that produces when having reduced unmanned aerial vehicle and traveling at a high speed of the spoiler of afterbody, on the other hand folding support frame is with the bracing piece jack-up, meets with the contact surface of air when reducing the flight, reduces the windage, has improved unmanned aerial vehicle's flying speed, has also reduced the consumption speed of energy.

2. This an unmanned aerial vehicle for oil electricity mixes drives bird mechanism through being provided with the ultrasonic wave, and when unmanned aerial vehicle when flight in the air, the ultrasonic wave drives bird mechanism and passes through heat energy sensor response birds, and the rethread ultrasonic wave is with birds expulsion, and the phenomenon of having avoided unmanned aerial vehicle collision birds damage takes place.

The part not related in the device all is the same with prior art or can adopt prior art to realize, and the device design structure is reasonable, and convenient to use satisfies people's user demand.

Drawings

Fig. 1 is a schematic perspective view of the overall structure of a hybrid unmanned aerial vehicle according to the present invention;

fig. 2 is a schematic structural view of an ultrasonic bird-repelling mechanism of the hybrid oil-electric unmanned aerial vehicle provided by the utility model;

fig. 3 is the utility model provides an unmanned aerial vehicle's that oil and electricity mixes overall structure elevation.

Fig. 4 is the utility model provides a hybrid unmanned aerial vehicle's folding support frame structure schematic diagram.

In the figure: the unmanned aerial vehicle comprises an unmanned aerial vehicle body 1, a diversion trench 2, a spoiler 3, an ultrasonic bird repelling mechanism 4, a folding support frame 5, an unmanned aerial vehicle wing 6, a display screen 7, a solar cell panel 8, an ultrasonic transducer 9, a thermal energy sensor 10, a fixing plate 11, a power supply 12, a controller 13, a control button 14, a fixing block 15, a rotating mechanism 16 and a support rod 17.

Detailed Description

The technical solution of the present patent will be described in further detail with reference to the following embodiments.

Reference will now be made in detail to embodiments of the present patent, examples of which are illustrated in the accompanying drawings, wherein like or similar reference numerals refer to the same or similar elements or elements having the same or similar function throughout. The embodiments described below with reference to the drawings are exemplary only for the purpose of explaining the present patent and are not to be construed as limiting the present patent.

In the description of this patent, it is to be understood that the terms "center," "upper," "lower," "front," "rear," "left," "right," "vertical," "horizontal," "top," "bottom," "inner," "outer," and the like are used in the orientations and positional relationships indicated in the drawings for the convenience of describing the patent and for the simplicity of description, and are not intended to indicate or imply that the referenced devices or elements must have a particular orientation, be constructed and operated in a particular orientation, and are not to be considered limiting of the patent.

In the description of this patent, it is noted that unless otherwise specifically stated or limited, the terms "mounted," "connected," and "disposed" are to be construed broadly and can include, for example, fixedly connected, disposed, detachably connected, disposed, or integrally connected and disposed. The specific meaning of the above terms in this patent may be understood by those of ordinary skill in the art as appropriate.

Example 1

Referring to fig. 1-4, an unmanned aerial vehicle that oil and electricity mixes, including unmanned aerial vehicle body 1, unmanned aerial vehicle body 1 includes unmanned aerial vehicle wing 6, and four to six equidistance distribution's guiding gutter 2 is seted up to 6 top outer walls of unmanned aerial vehicle wing, and the top outer wall of unmanned aerial vehicle body 1 has spoiler 3 through the screw connection, and the four corners department of 1 bottom outer wall of unmanned aerial vehicle body all has folding support frame 5 through the screw connection.

The utility model discloses in, folding support frame 5 includes fixed block 15, and the bottom outer wall of fixed block 15 has slewing mechanism 16 through screw connection, and slewing mechanism 16 is including rotating the motor, and there is bracing piece 17 in the one end of rotating the motor output shaft through the coupling joint.

The utility model discloses in, spoiler 3 is located the positive center of unmanned aerial vehicle body 1.

The utility model discloses in, the rectangle draw-in groove has been seted up to 1 bottom of unmanned aerial vehicle body, and the specification of rectangle draw-in groove and the specification looks adaptation of bracing piece 17.

The utility model discloses in, unmanned aerial vehicle wing 6 is the slope setting, and 6 inclination of unmanned aerial vehicle wing are ten to fifteen degrees.

The working principle is as follows: when unmanned aerial vehicle flies, the folding support frame 5 of unmanned aerial vehicle body 1 packs up bracing piece 17 through slewing mechanism 16's effect, reduces the area of contact with the air, and when flying fast, the air current can flow along with guiding gutter 2 on streamlined unmanned aerial vehicle wing 6, is derived softly by the spoiler 3 of afterbody, accomplishes the process that unmanned aerial vehicle flies.

Example 2

Referring to fig. 2, an unmanned aerial vehicle that oil electricity mixes, this embodiment compares in embodiment 1, still include that 1 bottom outer wall of unmanned aerial vehicle body has the ultrasonic wave to drive bird mechanism 4 through screw connection, and the ultrasonic wave drives bird mechanism 4 and includes solar cell panel 8 and fixed plate 11, there is heat energy sensor 10 one side outer wall on fixed plate 11 top through screw connection, there is controller 13 opposite side outer wall on fixed plate 11 top through rivet connection, controller 13 includes display screen 7 and

control button

14, 8 bottom outer walls of solar cell panel have ultrasonic transducer 9 through screw connection, there is power 12 one side inner wall that the ultrasonic wave drives bird mechanism 4 bottom through screw connection.

The working principle is as follows: at unmanned aerial vehicle flight in-process, the heat energy sensor 10 that the bird mechanism 4 was driven to the ultrasonic wave senses being close to in the bird, urges ultrasonic transducer 9 to send the ultrasonic wave of expulsion birds by power 12, when sunshine is sufficient, can also produce the electric energy through solar cell panel 8 and store in power 12.

The above, only be the concrete implementation of the preferred embodiment of the present invention, but the protection scope of the present invention is not limited thereto, and any person skilled in the art is in the technical scope of the present invention, according to the technical solution of the present invention and the utility model, the concept of which is equivalent to replace or change, should be covered within the protection scope of the present invention.

Claims

1. The utility model provides an unmanned aerial vehicle that oil electricity mixes, includes unmanned aerial vehicle body (1), its characterized in that, unmanned aerial vehicle body (1) is including unmanned aerial vehicle wing (6), and unmanned aerial vehicle wing (6) top outer wall sets up four to six guiding gutter (2) that the equidistance distributes, there is spoiler (3) top outer wall of unmanned aerial vehicle body (1) through the screw connection, and all there is folding support frame (5) in the four corners department of unmanned aerial vehicle body (1) bottom outer wall through screw connection.

2. The hybrid unmanned aerial vehicle of claim 1, wherein the folding support frame (5) comprises a fixing block (15), a rotating mechanism (16) is connected to the outer wall of the bottom of the fixing block (15) through a screw, the rotating mechanism (16) comprises a rotating motor, and one end of an output shaft of the rotating motor is connected with a support rod (17) through a coupling.

3. A hybrid drone according to claim 1, characterised in that the spoiler (3) is located in the centre of the drone body (1).

4. The hybrid unmanned aerial vehicle of claim 1, wherein a rectangular clamping groove is formed in the bottom of the unmanned aerial vehicle body (1), and the specification of the rectangular clamping groove is matched with that of the support rod (17).

5. A hybrid unmanned aerial vehicle according to claim 1, wherein the unmanned aerial vehicle wing (6) is inclined, and the angle of inclination of the unmanned aerial vehicle wing (6) is ten to fifteen degrees.

6. The hybrid unmanned aerial vehicle of oil and electricity of claim 1, characterized in that, there is the ultrasonic wave to drive bird mechanism (4) on the outer wall of unmanned aerial vehicle body (1) bottom through screw connection, and the ultrasonic wave drives bird mechanism (4) and includes solar cell panel (8) and fixed plate (11), there is heat energy sensor (10) on one side outer wall on fixed plate (11) top through screw connection, there is controller (13) on the other side outer wall on fixed plate (11) top through rivet connection, controller (13) include display screen (7) and control button (14), there is ultrasonic transducer (9) on the outer wall of solar cell panel (8) bottom through screw connection, there is power (12) on one side inner wall of ultrasonic wave drive bird mechanism (4) bottom through screw connection.