CN215728906U

CN215728906U - Weather detection unmanned aerial vehicle

Info

Publication number: CN215728906U
Application number: CN202022721704.1U
Authority: CN
Inventors: 郑诗盈; 胡程超; 郭天一; 谢杰杰
Original assignee: Individual
Current assignee: Individual
Priority date: 2020-11-23
Filing date: 2020-11-23
Publication date: 2022-02-01
Anticipated expiration: 2030-11-23

Abstract

The utility model relates to the field of unmanned aerial vehicles, and discloses a meteorological detection unmanned aerial vehicle which comprises a body shell, a rotating motor, a camera device and a meteorological analyzer, wherein the side edge of the body shell is fixedly connected with a support frame, four groups of support frames are mutually symmetrical, one end of each of the four groups of support frames is fixedly connected with the body shell, the other end of each support frame is fixedly connected with a protection plate, one side of each support frame, which is close to the protection plate, is provided with a groove, the groove is internally and slidably connected with the rotating motor, the output end of the rotating motor is fixedly connected with a propeller, the shell at the lower end of the rotating motor is slidably connected with the groove, and the bottom end of the groove is fixedly connected with a spring. This meteorological detection unmanned aerial vehicle through rotating there being the space between motor lower extreme and the support frame, and installs the spring in the space, to engine body shell's influence when improving the screw and rotate, reduces the vibration, and the increase buffering reduces the impact force to screw and motor when descending, utilizes the combination increase buffering of slider spout and push rod.

Description

Weather detection unmanned aerial vehicle

Technical Field

The utility model relates to the field of unmanned aerial vehicles, in particular to a meteorological detection unmanned aerial vehicle.

Background

Drones tend to be more suitable for tasks that are too "fool, dirty, or dangerous" than are manned aircraft. Unmanned aerial vehicles can be classified into military and civil applications according to the application field. For military use, unmanned aerial vehicles divide into reconnaissance aircraft and target drone. In the civil aspect, the unmanned aerial vehicle + the industry application is really just needed by the unmanned aerial vehicle; at present at the aerial photography, agriculture, plant protection, miniature autodyne, express delivery transportation, disaster relief, observe wild animal, control infectious disease, survey and drawing, news report, electric power is patrolled and examined, relief of disaster, the film and television is shot, make the application in fields such as romantic, great expansion unmanned aerial vehicle's own usage, developed country is also actively expanding the industry and is using and developing unmanned aerial vehicle technique, see from current structure, general unmanned aerial vehicle is used for the meteorological survey time measuring, because meteorological analyzer is difficult to dismantle, make the structure inconvenient, unable change equipment, and the rotatory vibration that comes of unmanned aerial vehicle screw causes the influence to the organism and reduces life cycle.

Therefore, a meteorological detection unmanned aerial vehicle is designed.

SUMMERY OF THE UTILITY MODEL

Aiming at the defects of the prior art, the utility model provides a meteorological detection unmanned aerial vehicle, which solves the problems that the structure is inconvenient, equipment cannot be replaced, and the vibration caused by the rotation of a propeller of the unmanned aerial vehicle affects the body and reduces the service cycle.

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

the utility model provides a meteorological detection unmanned aerial vehicle, includes engine body shell, rotates motor, camera device and meteorological analyzer, engine body shell side fixedly connected with support frame, four groups the mutual symmetry of support frame, four groups support frame one end fixed connection engine body shell, and support frame other end fixed connection backplate, one side that the support frame is close to the backplate is seted up flutedly, sliding connection has the rotation motor in the recess, rotate motor output end fixed connection screw, and rotate in the motor lower extreme shell sliding connection recess, recess bottom end fixedly connected with spring, the one end fixed connection recess bottom inner wall of spring, and the bottom shell of spring other end fixed connection rotation motor.

Further, the spout has been seted up to the spring both sides, and is two sets of sliding connection has the slider on the spout, slider bottom sliding connection is on the spout, and rotates the one end of connecting the push rod through the pivot in the slider upper end, and the push rod other end passes through bolt fixed connection and rotates motor bottom shell.

Further, a notch is formed in the middle of the upper end face of the engine body shell, one end of the connecting rod is installed at the notch of the engine body shell, and the other end of the connecting rod is provided with the meteorological analyzer.

Further, an opening is formed in the opening of the machine body shell, a clamping block is connected to the inside of the opening in a sliding mode, one end of the clamping block is fixedly connected with one end of the elastic piece, the other end of the elastic piece is fixedly connected with the opening and is far away from the inner wall of one side of the clamping block, a clamping groove is formed in the position, corresponding to the opening, of the connecting rod, and the clamping block is clamped with the clamping groove in a corresponding mode.

Furthermore, the fixture block is of a trapezoidal structure, the trapezoidal surfaces of the fixture blocks are opposite, the connecting rod is of a cylindrical structure, and the inclined surface of the clamping groove on the connecting rod, which corresponds to the fixture block, is also of an inclined structure.

Furthermore, a hole groove is formed in one side of the engine body shell, a camera device is installed at the position of the hole groove, and the two sides of the camera device are rotatably connected with the engine body shell.

The utility model has the beneficial effects that:

1. the utility model discloses a, through rotating there being the space between motor lower extreme and the support frame, and install the spring in the space, to engine body shell's influence when improving the screw and rotate, reduce the vibration, the increase buffering reduces the impact force to screw and motor when descending, utilizes the combination increase buffering of slider spout and push rod.

2. The utility model discloses a, utilize the backplate to support, and be connected with the connecting rod on the engine body shell, and the connecting rod passes through the fixture block joint with the opening part, realizes that meteorological analyzer conveniently dismantles and takes, and the fixture block is the slope trapezium structure simultaneously, and just two sets of fixture blocks place on the contrary, utilizes the swivelling joint pole to make the fixture block shrink connecting rod that can release, utilizes the shell fragment to recoil to fix the connecting rod.

Drawings

FIG. 1 is a schematic structural view of the present invention;

FIG. 2 is a schematic view of a groove structure according to the present invention;

FIG. 3 is an enlarged view of the structure at A in FIG. 1;

FIG. 4 is a schematic cross-sectional view of a connecting rod according to the present invention;

fig. 5 is a schematic diagram of a fixture block structure according to the present invention.

In the figure: 1. a body housing; 2. a support frame; 3. a propeller; 4. a guard plate; 5. a camera device; 6. a connecting rod; 7. a spring; 8. a weather analyzer; 9. rotating the motor; 10. a card slot; 11. a spring plate; 12. an opening; 13. a clamping block; 14. a groove; 15. a slider; 16. a chute; 17. a rotating shaft; 18. a push rod.

Detailed Description

In order to make the objects, technical solutions and advantages of the embodiments of the present invention clearer, the technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are some, but not all, embodiments of the present invention. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.

Referring to FIGS. 1-5: the utility model provides a meteorological detection unmanned aerial vehicle, including engine body shell 1, rotate motor 9, camera device 5 and

meteorological analyzer

8, 1 side fixedly connected with support frame 2 of engine body shell, 2 mutual symmetries of four group's support frames, 2 one end fixed connection engine body shells 1 of four group's support frames, and 2 other ends fixed connection backplate 4 of support frame, support frame 2 is close to one side of backplate 4 and sets up fluted 14, sliding connection has rotation motor 9 in the recess 14, rotate motor 9 output end fixed connection screw 3, and rotate in the motor 9 lower extreme shell sliding

connection recess

14, 14 bottom fixed connection of recess has

spring

7, 14 bottom inner walls of one end fixed connection recess of spring 7, and the bottom shell of spring 7 other end fixed connection rotation motor 9, utilize spring 7 to kick-back the increase buffering.

Wherein, the spout 16 has been seted up to spring 7 both sides, and sliding connection has slider 15 on two sets of spouts 16, and slider 15 bottom sliding connection is on

spout

16, and 15 upper ends of slider rotate the one end of connecting push rod 18 through pivot 17, and the push rod 18 other end passes through bolt fixed connection and rotates motor 9 bottom shell, utilizes the slip between slider 15 and the spout 16 to drive push rod 18 increase buffering.

Wherein, the notch has been seted up to engine body shell 1 up end intermediate position, and engine body shell 1's notch department installs the one end of connecting rod 6, and the connecting rod 6 other end installs meteorological analyzer 8, utilizes meteorological analyzer 8 to survey high altitude weather.

Wherein, the inside opening 12 of having seted up of the notch of engine body shell 1, and the inside sliding connection of opening 12 has fixture block 13, the one end of fixture block 13 one end fixed connection shell fragment 11, and one side inner wall that fixture block 13 was kept away from to the other end fixed connection opening 12 of shell fragment 11, and draw-in groove 10 has been seted up to connecting rod 6 and opening 12 corresponding position, and fixture block 13 and the mutual joint that corresponds of draw-in groove 10 block connecting rod 6, conveniently dismantle and take.

Wherein, fixture block 13 is the trapezium structure, and two sets of fixture block 13 trapezoidal surfaces are opposite, and connecting rod 6 is cylindrical structure, and the inclined plane that draw-in groove 10 on connecting rod 6 corresponds fixture block 13 also is the slope structure, utilizes the convenient dismantlement of fixture block 13 structure.

Wherein, the hole groove has been seted up to engine body shell 1 one side, and hole groove department installs camera device 5, and camera device 5 both sides are rotated and are connected engine body shell 1, make things convenient for unmanned aerial vehicle to carry out the high altitude and survey.

In conclusion, when the propeller landing device is used, a gap is formed between the lower end of the rotating motor 9 and the support frame 2, and the spring 7 is arranged in the gap, so that the influence of the rotation of the propeller 3 on the machine body shell 1 is improved, the vibration is reduced, the impact force on the propeller 3 and the motor is reduced by increasing the buffer when the propeller landing device lands, and the buffer is increased by the combination of the sliding chute 16 of the sliding block 15 and the push rod 18; utilize backplate 4 to support, and be connected with connecting rod 6 on engine body shell 1, and connecting rod 6 and opening 12 department pass through fixture block 13 joint, realize that meteorological analyzer 8 conveniently dismantles and take, and fixture block 13 is the slope trapezium structure simultaneously, and two sets of fixture blocks 13 are placed on the contrary, utilize swivelling joint pole 6 to make fixture block 13 shrink connecting rod 6 that can release, utilize shell fragment 11 to recoil to fix connecting rod 6.

The above examples are only intended to illustrate the technical solution of the present invention, but not to limit it; although the present invention has been described in detail with reference to the foregoing embodiments, it will be understood by those of ordinary skill in the art that: the technical solutions described in the foregoing embodiments may still be modified, or some technical features may be equivalently replaced; and such modifications or substitutions do not depart from the spirit and scope of the corresponding technical solutions of the embodiments of the present invention.

Claims

1. The utility model provides a meteorological detection unmanned aerial vehicle, includes engine body shell (1), rotating electrical machines (9), camera device (5) and meteorological analyzer (8), its characterized in that: engine body shell (1) side fixedly connected with support frame (2), four groups the mutual symmetry of support frame (2), four groups support frame (2) one end fixed connection engine body shell (1), and support frame (2) other end fixed connection backplate (4), one side that support frame (2) are close to backplate (4) is seted up fluted (14), sliding connection has rotation motor (9) in recess (14), rotate motor (9) output fixed connection screw (3), and rotate in motor (9) lower extreme shell sliding connection recess (14), recess (14) bottom fixedly connected with spring (7), the one end fixed connection recess (14) bottom inner wall of spring (7), and the bottom shell of spring (7) other end fixed connection rotation motor (9).

2. The weather detection unmanned aerial vehicle of claim 1, wherein: spout (16), two sets of have been seted up to spring (7) both sides sliding connection has slider (15) on spout (16), slider (15) bottom sliding connection is on spout (16), and rotates the one end of connecting push rod (18) through pivot (17) in slider (15) upper end, and the push rod (18) other end passes through bolt fixed connection and rotates motor (9) bottom shell.

3. The weather detection unmanned aerial vehicle of claim 1, wherein: the notch has been seted up to engine body shell (1) up end intermediate position, and the notch department of engine body shell (1) installs the one end of connecting rod (6), and meteorological analyzer (8) are installed to the connecting rod (6) other end.

4. The weather detection unmanned aerial vehicle of claim 1, wherein: opening (12) have been seted up to engine body shell (1) notch inside, and opening (12) inside sliding connection has fixture block (13), the one end of fixture block (13) one end fixed connection shell fragment (11), and one side inner wall of fixture block (13) is kept away from in other end fixed connection opening (12) of shell fragment (11), fixture block (13) and draw-in groove (10) correspond the joint each other, draw-in groove (10) are seted up on connecting rod (6) and are corresponded with opening (12) position.

5. The weather detection unmanned aerial vehicle of claim 4, wherein: the clamping blocks (13) are of a trapezoidal structure, the trapezoidal surfaces of the two groups of clamping blocks (13) are opposite, the connecting rod (6) is of a cylindrical structure, and the inclined surface, corresponding to the clamping blocks (13), of the clamping groove (10) in the connecting rod (6) is also of an inclined structure.

6. The weather detection unmanned aerial vehicle of claim 1, wherein: a hole groove is formed in one side of the engine body shell (1), a camera device (5) is installed at the position of the hole groove, and the two sides of the camera device (5) are connected with the engine body shell (1) in a rotating mode.