CN214930628U - Bottom over-and-under type meteorological unmanned aerial vehicle - Google Patents

Bottom over-and-under type meteorological unmanned aerial vehicle Download PDF

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Publication number
CN214930628U
CN214930628U CN202121773572.5U CN202121773572U CN214930628U CN 214930628 U CN214930628 U CN 214930628U CN 202121773572 U CN202121773572 U CN 202121773572U CN 214930628 U CN214930628 U CN 214930628U
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China
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cavity
meteorological
movable rod
unmanned aerial
gear
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CN202121773572.5U
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Chinese (zh)
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王大军
胡盼伟
张磊
张毅
黄志飞
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Anhui Weiyuan Intelligent Technology Co.,Ltd.
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Wuhu Weiyuan Intelligent Technology Co ltd
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Abstract

The utility model provides a bottom lifting type meteorological unmanned aerial vehicle, which relates to the technical field of unmanned aerial vehicles, and comprises a body, wings, impellers and installation cavities, wherein the wings are arranged outside the body, the impellers are installed above the wings, a plurality of installation cavities are arranged on two sides below the body, a connecting rod is arranged below the installation cavities, a first buffer mechanism is arranged inside the installation cavities, a movable rod is meshed with a transmission gear through teeth, and limiting mechanisms are arranged on the front side and the rear side of the movable rod; the utility model discloses be provided with elevating system in the inside of cavity, utilize elevating system's servo motor, drive gear, movable rod and stop gear mutually support, can drive meteorological sensor and remove, convenient regulation meteorological sensor's position for meteorological sensor more accuracy when detecting, thereby improved the accuracy of this unmanned aerial vehicle when using greatly.

Description

Bottom over-and-under type meteorological unmanned aerial vehicle
Technical Field
The utility model relates to an unmanned air vehicle technique field especially relates to a bottom over-and-under type meteorological unmanned aerial vehicle.
Background
Unmanned aerial vehicle, called unmanned aerial vehicle for short, is an unmanned aerial vehicle operated by radio remote control equipment and a self-contained program control device, and is a general name of unmanned aerial vehicles in practice, and the unmanned aerial vehicle is used in many fields, wherein the meteorological unmanned aerial vehicle is particularly important when detecting meteorological phenomena;
meteorological unmanned aerial vehicle need use meteorological sensor when surveying the weather, but meteorological sensor of current meteorological unmanned aerial vehicle fixes in unmanned aerial vehicle's bottom, and inconvenient operation that goes up and down to meteorological sensor, and then lead to inconvenient more accurate detect meteorological data, consequently the utility model provides a bottom over-and-under type meteorological unmanned aerial vehicle is with the problem of solving existence among the prior art.
SUMMERY OF THE UTILITY MODEL
To the above problem, the utility model provides a bottom over-and-under type meteorological unmanned aerial vehicle, this bottom over-and-under type meteorological unmanned aerial vehicle is provided with elevating system in the inside of cavity, utilizes the mutually supporting of elevating system's servo motor, drive gear, movable rod and stop gear, can drive meteorological sensor and remove, and convenient regulation meteorological sensor's position for meteorological sensor more accuracy when detecting, thereby improved the accuracy of this unmanned aerial vehicle when using greatly.
For realizing the purpose of the utility model, the utility model discloses a following technical scheme realizes: the utility model provides a bottom over-and-under type meteorological unmanned aerial vehicle, includes organism, wing, impeller and installation cavity, the outside of organism sets up the wing, the impeller is installed to the top of wing, the both sides of organism below are provided with a plurality of installation cavities, the below of installation cavity is provided with the connecting rod, the inside of installation cavity is provided with first buffer gear, the cavity is installed to the below of organism, the inside of cavity is provided with elevating system, elevating system's below installation meteorological sensor.
Elevating system includes servo motor, drive gear, movable rod and stop gear, servo motor install in the front side of cavity, drive gear install in the inside of cavity, servo motor's output with drive gear's one end is connected, the movable rod install in the inside of cavity, the below of movable rod with meteorological sensor's top is connected, one side of movable rod is provided with tooth, the movable rod pass through tooth with drive gear meshes, the front side and the rear side of movable rod all are provided with stop gear.
The further improvement lies in that: stop gear includes gag lever post and stop collar, the gag lever post install in inside front side and the rear side of cavity, the cover is equipped with the stop collar on the gag lever post, one side of stop collar with the movable rod is connected.
The further improvement lies in that: first buffer gear includes expanding spring and mounting panel, expanding spring install in the inside of installation cavity, the mounting panel is installed to expanding spring's one end, the opposite side of mounting panel with the one end of connecting rod is connected.
The further improvement lies in that: the installation cavity is provided with four, four the installation cavity is in the below symmetric distribution of organism, it is adjacent the below of connecting rod is equipped with the sill bar, the internally mounted of sill bar has second buffer gear.
The further improvement lies in that: the second buffer mechanism comprises a return spring, a clamping block and a movable block, the return spring is symmetrically installed in the bottom rod, the clamping block is installed at one end of the return spring, the movable block is arranged in the bottom rod, and the upper portion of the movable block is connected with the bottom end of the connecting rod.
The utility model discloses beneficial effect:
1. the utility model discloses be provided with elevating system in the inside of cavity, utilize elevating system's servo motor, drive gear, movable rod and stop gear mutually support, can drive meteorological sensor and remove, convenient regulation meteorological sensor's position for meteorological sensor more accuracy when detecting, thereby improved the accuracy of this unmanned aerial vehicle when using greatly.
2. The utility model discloses the inside of installation cavity is provided with first buffer gear, utilizes mutually supporting of first buffer gear's expanding spring and mounting panel for the connecting rod can stretch out and draw back in the inside of installation cavity, and the impact force that causes when slowing down the unmanned aerial vehicle whereabouts makes unmanned aerial vehicle safer when using.
3. The utility model discloses the inside of sill bar is provided with second buffer gear, utilizes mutually supporting of second buffer gear's reset spring, fixture block and movable block for the impact force that this unmanned aerial vehicle received when descending is less, makes this unmanned aerial vehicle safer when using.
Drawings
Fig. 1 is a schematic structural diagram of the present invention.
Fig. 2 is a schematic front view of the cross-sectional structure of the present invention.
Fig. 3 is a schematic side view of the cross-sectional structure of the present invention.
Fig. 4 is an enlarged partial cross-sectional view of the utility model at a in fig. 1.
Wherein: 1. a body; 2. an airfoil; 3. an impeller; 4. a mounting cavity; 5. a connecting rod; 6. a cavity; 7. a meteorological sensor; 8. a servo motor; 9. a transmission gear; 10. a movable rod; 11. a limiting rod; 12. a limiting sleeve; 13. a tension spring; 14. mounting a plate; 15. a bottom bar; 16. a return spring; 17. a clamping block; 18. a movable block.
Detailed Description
In order to deepen the understanding of the present invention, the following embodiments will be combined to make the present invention do further details, and the present embodiment is only used for explaining the present invention, and does not constitute the limitation of the protection scope of the present invention.
Example one
According to fig. 1-4, this embodiment provides a bottom over-and-under type meteorological unmanned aerial vehicle, including organism 1, wing 2, impeller 3 and installation cavity 4, the outside of organism 1 sets up wing 2, impeller 3 is installed to the top of wing 2, the both sides of organism 1 below are provided with a plurality of installation cavities 4, the below of installation cavity 4 is provided with connecting rod 5, the inside of installation cavity 4 is provided with first buffer gear, cavity 6 is installed to the below of organism 1, the inside of cavity 6 is provided with elevating system, elevating system's below installation meteorological sensor 7.
The lifting mechanism comprises a servo motor 8, a transmission gear 9, a movable rod 10 and a limiting mechanism, the servo motor 8 is installed on the front side of the cavity 6, the transmission gear 9 is installed inside the cavity 6, the output end of the servo motor 8 is connected with one end of the transmission gear 9, the movable rod 10 is installed inside the cavity 6, the lower portion of the movable rod 10 is connected with the upper portion of the meteorological sensor 7, one side of the movable rod 10 is provided with teeth, the movable rod 10 is meshed with the transmission gear 9 through the teeth, the limiting mechanisms are arranged on the front side and the rear side of the movable rod 10, the impeller 3 is started to drive the machine body 1 to fly, then the servo motor 8 is started to drive the transmission gear 9 to rotate, so that the movable rod 10 is driven to move, and the meteorological sensor 7 is moved out of the cavity 6, and detecting weather.
Stop gear includes gag lever post 11 and stop collar 12, gag lever post 11 install in the inside front side and the rear side of cavity 6, the cover is equipped with stop collar 12 on the gag lever post 11, one side of stop collar 12 with movable rod 10 is connected, utilizes the cooperation of gag lever post 11 and stop collar 12, and is spacing to movable rod 10.
First buffer gear includes expanding spring 13 and mounting panel 14, expanding spring 13 install in the inside of installation cavity 4, mounting panel 14 is installed to expanding spring 13's one end, mounting panel 14's opposite side with the one end of connecting rod 5 is connected, and mounting panel 14 receives the impact force of connecting rod 5, utilizes expanding spring 13 to drive mounting panel 14 and stretches out and draws back, alleviates impact force.
Example two
According to fig. 1-4, the embodiment provides a bottom lifting type meteorological unmanned aerial vehicle, which comprises a body 1, wings 2, impellers 3 and mounting cavities 4, wherein the wings 2 are arranged on the outer side of the body 1, the impellers 3 are mounted above the wings 2, a plurality of mounting cavities 4 are arranged on two sides of the lower portion of the body 1, connecting rods 5 are arranged below the mounting cavities 4, a first buffer mechanism is arranged inside the mounting cavities 4, a cavity 6 is mounted below the body 1, a lifting mechanism is arranged inside the cavity 6, and a meteorological sensor 7 is mounted below the lifting mechanism;
the lifting mechanism comprises a servo motor 8, a transmission gear 9, a movable rod 10 and a limiting mechanism, the servo motor 8 is installed on the front side of the cavity 6, the transmission gear 9 is installed inside the cavity 6, the output end of the servo motor 8 is connected with one end of the transmission gear 9, the movable rod 10 is installed inside the cavity 6, the lower portion of the movable rod 10 is connected with the upper portion of the meteorological sensor 7, one side of the movable rod 10 is provided with teeth, the movable rod 10 is meshed with the transmission gear 9 through the teeth, the limiting mechanisms are arranged on the front side and the rear side of the movable rod 10, the impeller 3 is started to drive the machine body 1 to fly, then the servo motor 8 is started to drive the transmission gear 9 to rotate, so that the movable rod 10 is driven to move, and the meteorological sensor 7 is moved out of the cavity 6, and detecting weather.
Stop gear includes gag lever post 11 and stop collar 12, gag lever post 11 install in the inside front side and the rear side of cavity 6, the cover is equipped with stop collar 12 on the gag lever post 11, one side of stop collar 12 with movable rod 10 is connected, utilizes the cooperation of gag lever post 11 and stop collar 12, and is spacing to movable rod 10.
Installation cavity 4 is provided with four, four installation cavity 4 is in the below symmetric distribution of organism 1 has improved the stability when unmanned aerial vehicle descends, and is adjacent the below of connecting rod 5 is equipped with sill bar 15, the internally mounted of sill bar 15 has second buffer gear, utilizes the impact force that second buffer gear received when descending to unmanned aerial vehicle to alleviate.
First buffer gear includes expanding spring 13 and mounting panel 14, expanding spring 13 install in the inside of installation cavity 4, mounting panel 14 is installed to expanding spring 13's one end, mounting panel 14's opposite side with the one end of connecting rod 5 is connected, and mounting panel 14 receives the impact force of connecting rod 5, utilizes expanding spring 13 to drive mounting panel 14 and stretches out and draws back, alleviates impact force.
The second buffer gear includes reset spring 16, fixture block 17 and movable block 18, reset spring 16 symmetry is installed in the inside of sill bar 15, fixture block 17 is installed to reset spring 16's one end, the inside of sill bar 15 is provided with movable block 18, movable block 18's top with the bottom of connecting rod 5 is connected, and movable block 18 receives downward impact force, utilizes reset spring 16 to drive fixture block 17 and stretches out and draws back, alleviates the impact force that movable block 18 received.
During the use, the staff starts impeller 3 and drives organism 1 and flies, then start servo motor 8 and drive gear 9 and rotate, the event drives movable rod 10 and removes, remove meteorological sensor 7 from the inside of cavity 6, detect meteorology, drive movable rod 10 through drive gear 9 and remove to different heights, detect the environment of co-altitude, after finishing detecting, start servo motor 8, make its reversal, withdraw meteorological sensor 7 to the inside of cavity 6, when unmanned aerial vehicle descends, connecting rod 5 receives the effect of impact force under expanding spring 13 and reset spring 16's dual function, can protect organism 1, carry out dual shock attenuation to organism 1, security when reinforcing unmanned aerial vehicle uses.
The utility model discloses a be provided with elevating system in the inside of cavity 6, utilize the mutually supporting of elevating system's servo motor 8, drive gear 9, movable rod 10 and stop gear, can drive meteorological sensor 7 and remove, the convenient position of adjusting meteorological sensor 7 makes meteorological sensor 7 more accurate when detecting, thereby has improved the accuracy of this unmanned aerial vehicle when using greatly the utility model discloses the inside of installation cavity 4 is provided with first buffer gear, utilizes the mutually supporting of first buffer gear's expanding spring 13 and mounting panel 14, makes connecting rod 5 can stretch out and draw back in the inside of installation cavity 4, slows down the impact force that causes when unmanned aerial vehicle falls, thereby makes unmanned aerial vehicle safer when using; the utility model discloses be provided with second buffer gear in the inside of sill bar 15, utilize mutually supporting of second buffer gear's reset spring 16, fixture block 17 and movable block 18 for the impact force that this unmanned aerial vehicle received when descending is less, makes this unmanned aerial vehicle safer when using.
The foregoing illustrates and describes the principles, general features, and advantages of the present invention. It will be understood by those skilled in the art that the present invention is not limited to the above embodiments, and that the foregoing embodiments and descriptions are provided only to illustrate the principles of the present invention without departing from the spirit and scope of the present invention. The scope of the invention is defined by the appended claims and equivalents thereof.

Claims (6)

1. The utility model provides a bottom over-and-under type meteorological unmanned aerial vehicle, includes organism (1), wing (2), impeller (3) and installation cavity (4), its characterized in that: the outside of organism (1) sets up wing (2), impeller (3) are installed to the top of wing (2), the both sides of organism (1) below are provided with a plurality of installation cavity (4), the below of installation cavity (4) is provided with connecting rod (5), the inside of installation cavity (4) is provided with a buffer gear, cavity (6) are installed to the below of organism (1), the inside of cavity (6) is provided with elevating system, meteorological sensor (7) are installed to elevating system's below.
2. The overhead meteorological drone of claim 1, wherein: elevating system includes servo motor (8), drive gear (9), movable rod (10) and stop gear, servo motor (8) install in the front side of cavity (6), drive gear (9) install in the inside of cavity (6), servo motor's (8) output with the one end of drive gear (9) is connected, movable rod (10) install in the inside of cavity (6), the below of movable rod (10) with the top of meteorological sensor (7) is connected, one side of movable rod (10) is provided with the tooth, movable rod (10) through the tooth with drive gear (9) meshing, the front side and the rear side of movable rod (10) all are provided with stop gear.
3. The overhead meteorological drone of claim 2, wherein: stop gear includes gag lever post (11) and stop collar (12), gag lever post (11) install in cavity (6) inside front side and rear side, the cover is equipped with stop collar (12) on gag lever post (11), one side of stop collar (12) with movable rod (10) are connected.
4. The overhead meteorological drone of claim 1, wherein: first buffer gear includes expanding spring (13) and mounting panel (14), expanding spring (13) install in the inside of installation cavity (4), mounting panel (14) are installed to the one end of expanding spring (13), the one end of connecting rod (5) with mounting panel (14) bottom plate is connected.
5. The overhead meteorological drone of claim 1, wherein: installation cavity (4) are provided with four, four installation cavity (4) are in the below symmetric distribution of organism (1), and are adjacent the below of connecting rod (5) is equipped with sill bar (15), the internally mounted of sill bar (15) has second buffer gear.
6. The overhead meteorological drone of claim 5, wherein: the second buffer mechanism comprises a return spring (16), a clamping block (17) and a movable block (18), the return spring (16) is symmetrically installed in the bottom rod (15), the clamping block (17) is installed at one end of the return spring (16), the movable block (18) is arranged in the bottom rod (15), and the top of the movable block (18) is connected with the bottom end of the connecting rod (5).
CN202121773572.5U 2021-08-02 2021-08-02 Bottom over-and-under type meteorological unmanned aerial vehicle Active CN214930628U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202121773572.5U CN214930628U (en) 2021-08-02 2021-08-02 Bottom over-and-under type meteorological unmanned aerial vehicle

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202121773572.5U CN214930628U (en) 2021-08-02 2021-08-02 Bottom over-and-under type meteorological unmanned aerial vehicle

Publications (1)

Publication Number Publication Date
CN214930628U true CN214930628U (en) 2021-11-30

Family

ID=79068116

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202121773572.5U Active CN214930628U (en) 2021-08-02 2021-08-02 Bottom over-and-under type meteorological unmanned aerial vehicle

Country Status (1)

Country Link
CN (1) CN214930628U (en)

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Address after: 241000 building 27, Wuhu navigation Innovation Park, Beihang, Xinwu Avenue, Wanhe Town, Wuhu County, Wuhu City, Anhui Province

Patentee after: Anhui Weiyuan Intelligent Technology Co.,Ltd.

Address before: 241000 building 27, Wuhu navigation Innovation Park, Beihang, Xinwu Avenue, Wanhe Town, Wuhu County, Wuhu City, Anhui Province

Patentee before: Wuhu Weiyuan Intelligent Technology Co.,Ltd.