CN220584407U - Be used in radiation detector on unmanned aerial vehicle - Google Patents
Be used in radiation detector on unmanned aerial vehicle Download PDFInfo
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- CN220584407U CN220584407U CN202321821522.9U CN202321821522U CN220584407U CN 220584407 U CN220584407 U CN 220584407U CN 202321821522 U CN202321821522 U CN 202321821522U CN 220584407 U CN220584407 U CN 220584407U
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- unmanned aerial
- aerial vehicle
- radiation detector
- mount pad
- battery
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- 230000005855 radiation Effects 0.000 title claims abstract description 34
- 238000001514 detection method Methods 0.000 abstract description 14
- 238000012423 maintenance Methods 0.000 abstract description 2
- 238000009434 installation Methods 0.000 abstract 1
- 230000007547 defect Effects 0.000 description 2
- 230000000670 limiting effect Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000012544 monitoring process Methods 0.000 description 2
- 238000013459 approach Methods 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000012552 review Methods 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
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Abstract
The utility model discloses a radiation detector for an unmanned aerial vehicle, and belongs to the technical field of radiation detection equipment; the utility model provides a radiation detector for unmanned aerial vehicle, includes the mount pad, battery, industrial computer are installed at the mount pad top, the bottom of mount pad is provided with high-pressure ionization chamber, industrial computer and battery, high-pressure ionization chamber electric connection, the both ends of mount pad are provided with the bandage of being connected with unmanned aerial vehicle's organism respectively, be provided with the regulation knot on the bandage, the four corners position of mount pad is provided with the connecting device who is connected with unmanned aerial vehicle's landing frame, connecting device is including installing the pivot seat on the mount pad, the below of pivot seat is provided with the bracing piece, connect through universal bulb between pivot seat and the bracing piece, be provided with the wiring on the bracing piece; the utility model has the advantages of convenient installation on different unmanned aerial vehicles, convenient disassembly and post maintenance.
Description
Technical Field
The utility model relates to the technical field of radiation detection equipment, in particular to a radiation detector used on an unmanned aerial vehicle.
Background
With the great rise of nuclear and radiation emergency risks, the technology system of upgrading port nuclear and radiation response is not slow. Currently, for nuclear and radiation security detection at ports, a radiation detection system is provided at a gateway, and nuclear and radiation security detection is performed on cargo or containers and the like when a transport vehicle loaded with cargo or containers and the like passes through the gateway.
In the Chinese patent document with the authority of CN217332872U, an emergency radiation detection device based on an unmanned aerial vehicle is provided. According to the utility model, the high-voltage ionization chamber is arranged on the unmanned aerial vehicle, radiation safety monitoring is combined with the unmanned aerial vehicle, remote non-contact nuclear and radiation emergency detection is realized, and continuous detection can be carried out on areas with large area, large scale, large volume and multiple targets such as container stacking sites, large-scale resource cargo yards, ports and wharfs, and the like, so that the defect that a traditional channel type radiation detection system can only detect containers or cargoes passing through the detection system in a vehicle carrying mode is overcome, and monitoring can be realized during stacking; personnel are not required to approach the nuclear and radiation area, and personnel radiation exposure is effectively solved.
However, the utility model has the defects that the unmanned aerial vehicle and the radiation detection device are of an integrated structure, firstly, the unmanned aerial vehicle is inconvenient to disassemble during maintenance, secondly, the unmanned aerial vehicle is used as multi-platform equipment and is widely applied to different industries, besides being used for radiation detection, the unmanned aerial vehicle is also frequently used for aerial photography, transportation and the like, so that the integrated structure is unfavorable for the unmanned aerial vehicle to fully exert various functions and is also unfavorable for the detection device to be conveniently and rapidly equipped on unmanned aerial vehicles of different structures for use.
Disclosure of Invention
The utility model aims to solve the problems that a radiation detection device based on an unmanned aerial vehicle in the prior art is of an integrated structure and is inconvenient to detach, and provides a radiation detector used on the unmanned aerial vehicle.
In order to achieve the above purpose, the present utility model adopts the following technical scheme:
the utility model provides a radiation detector for on unmanned aerial vehicle, includes the mount pad, battery, industrial computer are installed at the mount pad top, the bottom of mount pad is provided with high-pressure ionization chamber, industrial computer and battery, high-pressure ionization chamber electric connection, the both ends of mount pad are provided with the bandage of being connected with unmanned aerial vehicle's organism respectively, be provided with on the bandage and adjust the knot, the four corners position of mount pad is provided with the connecting device who is connected with unmanned aerial vehicle's landing frame.
Further, the connecting device comprises a rotating shaft seat arranged on the mounting seat, a supporting rod is arranged below the rotating shaft seat, the rotating shaft seat is connected with the supporting rod through a universal ball head, and a binding wire is arranged on the supporting rod.
Further, the bracing piece includes the first body of rod, the inside of first body of rod is provided with the wire storage groove of opening downwardly, the inside of wire storage groove is provided with the wiring, the one end and the first body of rod of wiring are connected, the other end and interior bolted connection, be provided with on the lateral wall of the first body of rod with interior bolt complex bolt hole.
Further, the inner bolt is in threaded connection with the opening of the wire storage groove.
Further, a nut is arranged at the bottom of the inner bolt, and an outer bolt with the same specification as the inner bolt is arranged at the bottom of the nut.
Further, connecting device still includes the connecting rod, the connecting rod includes the second body of rod of one end and high pressure ionization chamber fixed connection, the draw-in groove has been seted up to the other end of second body of rod, the cross-section of draw-in groove is the C style of calligraphy, pass through draw-in groove joint between first body of rod and the second body of rod.
Further, the top of mount pad is provided with the battery compartment, the inside of battery compartment is provided with the battery, the top of battery compartment is provided with the spring pad, a plurality of the spring pad evenly distributed is on the top surface of battery compartment.
Compared with the prior art, the utility model provides the radiation detector for the unmanned aerial vehicle, which has the following beneficial effects:
according to the radiation detector used on the unmanned aerial vehicle, the industrial personal computer is powered by the battery box high-voltage ionization chamber to detect radiation during use, the detector is tightly tied at the bottom of the unmanned aerial vehicle body through the binding band before use, the connection device is used for being connected with the landing frame of the unmanned aerial vehicle, the stability of connection is improved, and the radiation detector is suitable for unmanned aerial vehicle bodies of different types through the binding band connection and is convenient to detach.
Additional advantages, objects, and features of the utility model will be set forth in part in the description which follows; and will be apparent to those skilled in the art in part based upon a review of the following; alternatively, the teachings may be directed to practice of the present utility model.
Drawings
FIG. 1 is a schematic diagram of the overall structure of the present utility model;
FIG. 2 is a schematic cross-sectional view of a support bar according to the present utility model;
fig. 3 is an enlarged schematic view of the part a of fig. 1 according to the present utility model.
In the figure:
1. a mounting base; 2. a rotating shaft seat; 3. a battery; 4. a strap; 5. an adjusting buckle; 6. a battery compartment; 7. a spring pad; 8. an industrial personal computer; 9. universal ball head; 10. a support rod; 11. a high-voltage ionization chamber; 12. a connecting rod; 13. a wire storage slot; 14. binding wires; 15. an inner bolt; 16. a screw cap; 17. an outer bolt; 18. bolt holes; 19. a first rod body; 20. a second rod body; 21. a clamping groove.
Detailed Description
The following description of the embodiments of the present utility model will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present utility model, but not all embodiments.
Referring to fig. 1-3, the radiation detector for the unmanned aerial vehicle comprises a mounting seat 1, wherein a battery 3 and an industrial personal computer 8 are arranged at the top of the mounting seat 1, a high-voltage ionization chamber 11 is arranged at the bottom of the mounting seat 1, the industrial personal computer 8 is electrically connected with the battery 3 and the high-voltage ionization chamber 11, in particular, a high-voltage ionization chamber cabin, an industrial personal computer cabin and a battery cabin 6 are connected to the mounting seat 1, the high-voltage ionization chamber 11 is arranged in the high-voltage ionization chamber cabin, the industrial personal computer 8 is arranged in the industrial personal computer cabin, and the battery 3 is arranged in the battery cabin;
the two ends of the mounting seat 1 are respectively provided with four binding bands 4 connected with the unmanned aerial vehicle body, one end of the mounting seat 1 is connected with two binding bands, a male buckle and a female buckle of the male buckle are respectively installed, the binding bands 4 are provided with adjusting buckles 5 for adjusting the lengths of the binding bands 4, the length of the binding bands 4 is adjusted through the adjusting buckles 5 according to the size of the unmanned aerial vehicle body to be installed, the detector is tightly bound on the unmanned aerial vehicle body through the binding bands 4, the four corners of the mounting seat 1 are provided with connecting devices connected with the landing frame of the unmanned aerial vehicle, and the connecting devices are matched with the binding bands 4 to improve the stability of connection;
the connecting device comprises a rotating shaft seat 2 arranged on a mounting seat 1, as shown in fig. 1, a supporting rod 10 is connected below the rotating shaft seat 2, the rotating shaft seat 2 is connected with the supporting rod 10 through a universal ball head 9, a binding wire 14 is arranged on the supporting rod 10, the supporting rod 10 is matched with the rotating shaft seat 2 through the universal ball head 9 to adjust the orientation, and then the supporting rod is bound with a landing frame of the unmanned aerial vehicle to be mounted through the binding wire 14, so that the fixing effect is achieved;
the support rod 10 comprises a first rod body 19, a wire storage groove 13 with a downward opening is formed in the first rod body 19, the wire storage groove 13 is of a tubular structure, a binding wire 14 is arranged in the wire storage groove 13, one end of the binding wire 14 is connected with the first rod body 19, the other end of the binding wire is connected with an inner bolt 15, a bolt hole 18 matched with the inner bolt 15 is formed in the side wall of the first rod body 19, when the support rod 10 and a landing frame of an unmanned aerial vehicle are required to be bound together, the binding wire 14 is tensioned and then wound on the landing frame, and finally the inner bolt 15 is screwed into the bolt hole 18, so that the binding wire 14 is kept in a tense state;
the plurality of bolt holes 18 are formed, the plurality of bolt holes 18 are uniformly distributed along the axial direction of the first rod body 19, and when the binding wires 14 are bound on different types of falling frames, the inner bolts 15 are screwed into the bolt holes 18 at corresponding positions, so that the binding wires 14 can be conveniently tightened;
the inner bolt 15 is in threaded connection with the opening of the wire storage groove 13, so that the binding wire 14 is conveniently stored in the wire storage groove 13, and the leakage of the binding wire 14 is avoided;
the bottom of the inner bolt 15 is connected with a screw cap 16, and the bottom of the screw cap 16 is connected with an outer bolt 17 with the same specification as the inner bolt 15, so that the inner bolt 15 can be screwed by the screw cap 16;
the connecting device further comprises a connecting rod 12, the connecting rod 12 comprises a second rod body 20, one end of the second rod body 20 is fixedly connected with the high-voltage ionization chamber 11, a clamping groove 21 is formed in the other end of the second rod body 20, the cross section of the clamping groove 21 is C-shaped, the first rod body 19 and the second rod body 20 are clamped through the clamping groove 21, and particularly as shown in fig. 3, under the limiting effect of the connecting rod 12, the supporting rod 10 can be used as a falling frame and matched with the binding belt 4, so that the connecting rod is suitable for an unmanned aerial vehicle without the falling frame;
the top of the mounting seat 1 is provided with a battery compartment 6, a battery 3 is arranged in the battery compartment 6, the top of the battery compartment 6 is provided with a spring pad 7, a plurality of spring pads 7 are uniformly distributed on the top surface of the battery compartment 6, when the detector is tightly tied on the body of the unmanned aerial vehicle through a binding belt 4, the spring pad 7 is compressed between the battery compartment 6 and the body for supporting the detector, and the situation that the connection between the body and the detector is unstable due to uneven bottom of the body of the unmanned aerial vehicle is avoided;
in the embodiment, the middle of the spring pad 7 is a spring, two ends of the spring are connected with gaskets, and one gasket is glued or welded with the battery compartment 6;
working principle: before use, the detector is tightly tied at the bottom of the unmanned aerial vehicle body through the binding belt 4, the spring pad 7 provides support, and if the unmanned aerial vehicle to be installed does not fall down to a frame, the supporting rod 10 is clamped and fixed in the clamping groove 21 to serve as the falling down frame; if the unmanned aerial vehicle to be installed is provided with a landing frame, the supporting rod 10 is rotated to the position near the rod body of the nearest landing frame, after the inner bolt 15 is screwed out, the inner bolt 15 is wound and fastened on the landing frame through the binding wire 14, and then the outer bolt 17 is screwed into the bolt hole 18.
The foregoing is only a preferred embodiment of the present utility model, but the scope of the present utility model is not limited thereto, and any person skilled in the art, who is within the scope of the present utility model, should make equivalent substitutions or modifications according to the technical scheme of the present utility model and the inventive concept thereof, and should be covered by the scope of the present utility model.
In the description of the present specification, a description referring to terms "one embodiment," "some embodiments," "examples," "specific examples," or "some examples," etc., means that a particular feature, structure, material, or characteristic described in connection with the embodiment or example is included in at least one embodiment or example of the present utility model. In this specification, schematic representations of the above terms are not necessarily directed to the same embodiment or example. Furthermore, the particular features, structures, materials, or characteristics described may be combined in any suitable manner in any one or more embodiments or examples. Furthermore, the different embodiments or examples described in this specification and the features of the different embodiments or examples may be combined and combined by those skilled in the art without contradiction.
While embodiments of the present utility model have been shown and described above, it will be understood that the above embodiments are illustrative and not to be construed as limiting the utility model, and that variations, modifications, alternatives and variations may be made to the above embodiments by one of ordinary skill in the art within the scope of the utility model.
Claims (7)
1. The utility model provides a radiation detector for on unmanned aerial vehicle, includes mount pad (1), battery (3), industrial computer (8) are installed at mount pad (1) top, the bottom of mount pad (1) is provided with high-voltage battery room (11), industrial computer (8) and battery (3), high-voltage battery room (11) electric connection, the both ends of mount pad (1) are provided with bandage (4) of being connected with unmanned aerial vehicle's organism respectively, be provided with on bandage (4) and adjust knot (5), the four corners position of mount pad (1) is provided with the connecting device who is connected with unmanned aerial vehicle's landing frame.
2. A radiation detector for use in an unmanned aerial vehicle according to claim 1, wherein the connecting means comprises a rotary shaft seat (2) mounted on the mounting seat (1), a support rod (10) is provided below the rotary shaft seat (2), the rotary shaft seat (2) is connected with the support rod (10) through a universal ball head (9), and a binding wire (14) is provided on the support rod (10).
3. A radiation detector for use in an unmanned aerial vehicle according to claim 2, wherein the support bar (10) comprises a first bar body (19), the interior of the first bar body (19) is provided with a slot (13) with a downward opening, the interior of the slot (13) is provided with a binding wire (14), one end of the binding wire (14) is connected with the first bar body (19), the other end is connected with an inner bolt (15), and a bolt hole (18) matched with the inner bolt (15) is arranged on the side wall of the first bar body (19).
4. A radiation detector for use in a unmanned aerial vehicle according to claim 3, wherein the inner bolt (15) is screwed to the opening of the slot (13).
5. A radiation detector for use in an unmanned aerial vehicle according to claim 4, wherein the bottom of the inner bolt (15) is provided with a screw cap (16), and the bottom of the screw cap (16) is provided with an outer bolt (17) of the same gauge as the inner bolt (15).
6. The radiation detector for the unmanned aerial vehicle according to claim 5, wherein the connecting device further comprises a connecting rod (12), the connecting rod (12) comprises a second rod body (20) with one end fixedly connected with the high-voltage ionization chamber (11), a clamping groove (21) is formed in the other end of the second rod body (20), the cross section of the clamping groove (21) is C-shaped, and the first rod body (19) is clamped with the second rod body (20) through the clamping groove (21).
7. A radiation detector for use on an unmanned aerial vehicle according to claim 1, wherein the top of the mount (1) is provided with a battery compartment (6), the interior of the battery compartment (6) is provided with a battery (3), the top of the battery compartment (6) is provided with a spring pad (7), and a plurality of the spring pads (7) are evenly distributed on the top surface of the battery compartment (6).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321821522.9U CN220584407U (en) | 2023-07-12 | 2023-07-12 | Be used in radiation detector on unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321821522.9U CN220584407U (en) | 2023-07-12 | 2023-07-12 | Be used in radiation detector on unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN220584407U true CN220584407U (en) | 2024-03-12 |
Family
ID=90116209
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202321821522.9U Active CN220584407U (en) | 2023-07-12 | 2023-07-12 | Be used in radiation detector on unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN220584407U (en) |
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2023
- 2023-07-12 CN CN202321821522.9U patent/CN220584407U/en active Active
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