CN209870763U - Unmanned aerial vehicle carries interference nacelle constructional device - Google Patents
Unmanned aerial vehicle carries interference nacelle constructional device Download PDFInfo
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- CN209870763U CN209870763U CN201920610520.2U CN201920610520U CN209870763U CN 209870763 U CN209870763 U CN 209870763U CN 201920610520 U CN201920610520 U CN 201920610520U CN 209870763 U CN209870763 U CN 209870763U
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- heat dissipation
- aerial vehicle
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Abstract
The utility model discloses an unmanned aerial vehicle carries interference nacelle constructional device, including heat dissipation housing and antenna, the heat dissipation housing comprises housing main part, heat dissipation mounting bracket and bottom apron, and the antenna sets up in one side of housing main part, and the antenna passes through bolt fixed connection with the heat dissipation housing, the air intake has been seted up to the both sides of housing main part surface, the side-mounting of housing main part has unmanned aerial vehicle to connect the socket, and the heat dissipation mounting bracket imbeds in the inside of housing main part, and the adjacent side of heat dissipation mounting bracket is equipped with the fan, and the fan passes through bolt fixed connection with the housing main part, and the fan is connected socket electric connection with unmanned aerial vehicle, and the bottom apron sets up in the bottom of housing main part, and heat dissipation mounting bracket and bottom apron welded fastening. The method has the advantages of improving the heat dispersion of the interference pod and improving the endurance of the interference emission equipment.
Description
Technical Field
The utility model relates to a nacelle technical field specifically says a unmanned aerial vehicle carries interference nacelle constructional device.
Background
Electronic warfare plays an increasingly important role in the present warfare, and the electronic interference technology is one of the important components in electronic warfare, is an important measure for preventing or destroying acquisition, transmission and utilization of electromagnetic information of enemies, and is a 'soft killing' means of aggressive electronic warfare. The electronic interference is electromagnetic waves which are consciously emitted, forwarded or reflected with specific performance so as to disturb, deceive and suppress enemy military electronic information systems and weapon guidance control systems and enable the enemy military electronic information systems and weapon guidance control systems not to work normally. The unmanned aerial vehicle-mounted interference pod is hung at the lower part of an unmanned aerial vehicle body, the pod is operated and commanded on the ground to emit specific electromagnetic waves to a target region so as to interfere with a deception enemy radar and an electronic information system, and power supply of the interference pod is provided by the unmanned aerial vehicle. However, the heat dissipation performance of the existing interference pod is poor, and the endurance of the interference emission equipment is negatively influenced.
SUMMERY OF THE UTILITY MODEL
Therefore, in order to solve the above-mentioned not enough, the utility model provides an unmanned aerial vehicle carries interference nacelle constructional device herein has the advantage that improves interference nacelle heat dispersion, promotes the continuation of the journey of interference emission equipment.
The utility model discloses a realize like this, construct an unmanned aerial vehicle and carry interference nacelle constructional device, including heat dissipation housing and antenna, the heat dissipation housing is by the housing main part, heat dissipation mounting bracket and bottom apron constitute, the antenna sets up in one side of housing main part, the antenna passes through bolt fixed connection with the heat dissipation housing, the air intake has been seted up to the both sides of housing main part surface, the side-mounting of housing main part has unmanned aerial vehicle to connect the socket, the heat dissipation mounting bracket imbeds in the inside of housing main part, the adjacent side of heat dissipation mounting bracket is equipped with the fan, the fan passes through bolt fixed connection with the housing main part, fan and unmanned aerial vehicle connection socket electric connection, the bottom apron sets up in the bottom of housing main part, heat dissipation mounting bracket and bottom apron welded fastening, and.
Furthermore, the heat dissipation mounting frame is of a rectangular frame structure, 2 heat dissipation toothed sheets are arranged in the middle of the interior of the heat dissipation mounting frame, the interference device is selected according to the function, demand or cost budget, and other factors, the interference device is mounted on the heat dissipation mounting frame through screws and is ensured to be in contact with the heat dissipation toothed sheets during mounting, heat dissipation silica gel is required to be coated between the interference device and the heat dissipation toothed sheets, then the antenna and the unmanned aerial vehicle connecting socket are connected with the interference device, finally the heat dissipation mounting frame is mounted in the heat dissipation cover, screws are driven into the bottom cover plate to complete mounting, air inlets are formed in two sides of the outer surface of the cover main body, the heat generated by the work of the interference device is absorbed by the heat dissipation toothed sheets during the flight of the unmanned aerial vehicle, air is filled into the heat dissipation toothed sheets to reduce the temperature of the heat dissipation toothed sheets depending on the flight speed, and meanwhile, the fan is used for exhausting air flow from the, through the passive heat dissipation mode with the initiative like this, the radiating efficiency has been improved by a wide margin, and adopts such rectangle frame construction erection equipment of heat dissipation mounting bracket for the inside interior baffle that does not have of heat dissipation housing has also made things convenient for the wiring of connecting wire.
Furthermore, the air inlet is provided with a louver type groove, and the louver type design is adopted, so that air can be introduced into the nacelle on one hand, and water drops can be prevented from entering the nacelle on the other hand.
Further, unmanned aerial vehicle connection socket adopts 20 core aviation sockets. The unmanned aerial vehicle is connected through the unmanned aerial vehicle connecting socket, and the unmanned aerial vehicle supplies power and inputs control signals to the internal equipment of the nacelle.
Furthermore, the top of the cover main body is provided with a hoisting groove. The nacelle is mounted to the belly of the unmanned aerial vehicle by using a hoisting piece through the set hoisting groove.
The utility model discloses an improvement provides an unmanned aerial vehicle carries interference nacelle constructional device here, compares with current unmanned aerial vehicle carries interference nacelle constructional device, has following advantage: have and improve the advantage that disturbs nacelle heat dispersion, promote the continuation of the journey of interference emission equipment, the concrete embodiment is:
the method has the advantages that: the heat dissipation mounting frame is of a rectangular frame structure, 2 heat dissipation toothed sheets are arranged in the middle of the interior of the heat dissipation mounting frame, the corresponding type equipment is selected according to the consideration of functions, requirements or cost budget, the interference equipment is mounted on the heat dissipation mounting frame through screws and is ensured to be in contact with the heat dissipation toothed sheets during mounting, heat dissipation silica gel is required to be coated between the interference equipment and the heat dissipation toothed sheets, then the antenna and an unmanned aerial vehicle connecting socket are connected with the interference equipment, finally the heat dissipation mounting frame is mounted in a heat dissipation cover, screws are driven into a bottom cover plate to complete mounting, air inlets are formed in two sides of the outer surface of the cover main body, the heat generated by the operation of the interference equipment is absorbed by the heat dissipation toothed sheets during the flight of the unmanned aerial vehicle, the air is filled into the heat dissipation toothed sheets to reduce the temperature of the heat dissipation toothed sheets depending on the flight speed, and meanwhile, the air flow generated by the air exhausted, through the passive heat dissipation mode with the initiative like this, the radiating efficiency has been improved by a wide margin, and adopts such rectangle frame construction erection equipment of heat dissipation mounting bracket for the inside interior baffle that does not have of heat dissipation housing has also made things convenient for the wiring of connecting wire.
Drawings
Fig. 1 is a schematic structural diagram of an unmanned aerial vehicle-mounted interference pod structure device of the invention;
fig. 2 is an exploded view of the structure of the interference pod for the unmanned aerial vehicle.
Sequence numbers shown in the figures: antenna 1, heat dissipation housing 2, housing main part 3, fan 4, unmanned aerial vehicle connection socket 5, air intake 6, hoist and mount groove 7, heat dissipation mounting bracket 8, heat dissipation tooth piece 9 and bottom apron 10.
Detailed Description
The present invention will be described in detail below with reference to the accompanying drawings, wherein the technical solutions in the embodiments of the present invention are clearly and completely described, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments of the present invention, all other embodiments obtained by those skilled in the art without creative efforts belong to the protection scope of the present invention; furthermore, the terms "first," "second," "third," "upper, lower, left, right," and the like are used for descriptive purposes only and are not to be construed as indicating or implying relative importance. Meanwhile, in the description of the present invention, unless otherwise explicitly specified or limited, the terms "connected" and "connected" should be interpreted broadly, and may be, for example, fixedly connected, detachably connected, or integrally connected; the connection can be mechanical connection or electrical connection; may be directly connected or indirectly connected through an intermediate. The specific meaning of the above terms in the present invention can be understood in specific cases to those skilled in the art.
The utility model provides an unmanned aerial vehicle carries interference nacelle constructional device through the improvement here, as shown in the attached drawing of the specification, can be implemented as follows; including heat dissipation housing 2 and antenna 1, heat dissipation housing 2 is by housing main part 3, heat dissipation mounting bracket 8 and bottom apron 10 constitute, antenna 1 sets up in one side of housing main part 3, antenna 1 passes through bolt fixed connection with heat dissipation housing 2, air intake 6 has been seted up to the both sides of housing main part 3 surface, the side-mounting of housing main part 3 has unmanned aerial vehicle connection socket 5, heat dissipation mounting bracket 8 imbeds in the inside of housing main part 3, heat dissipation mounting bracket 8's adjacent side is equipped with fan 4, fan 4 passes through bolt fixed connection with housing main part 3, fan 4 is connected 5 electric connection with unmanned aerial vehicle, bottom apron 10 sets up in housing main part 3's bottom plate, heat dissipation mounting bracket 8 and bottom apron 10 welded fastening, and bottom apron 10 passes through screw fixed connection with housing main part 3.
In the utility model, the heat dissipation mounting rack 8 is a rectangular frame structure, 2 heat dissipation teeth 9 are arranged at the middle position inside the heat dissipation mounting rack 8, the interference device is selected according to the function, demand or cost budget, the interference device is arranged on the heat dissipation mounting rack 8 through screws, and ensures that the interference device is contacted with the heat dissipation teeth 9 when in installation, heat dissipation silica gel is coated between the interference device and the heat dissipation teeth 9, then the antenna 1 and the unmanned aerial vehicle connecting socket 5 are connected with the interference device, finally the heat dissipation mounting rack 8 is arranged in the heat dissipation cover 2, screws are driven into the bottom cover plate 10 to complete installation, because the air inlets 6 are arranged at the two sides of the outer surface of the cover main body 3, the heat generated by the work of the interference device is absorbed by the heat dissipation teeth 9 during the flight process of the unmanned aerial vehicle, the air is filled into the heat dissipation teeth 9 by the flight speed to reduce the temperature of the heat dissipation teeth 9, meanwhile, the fan 4 is used for exhausting air at the end part to generate airflow to carry out heat dissipation of the low-heat-dissipation tooth piece 9 together, the heat dissipation efficiency is greatly improved through the passive and active heat dissipation mode, and the rectangular frame structure mounting equipment such as the heat dissipation mounting frame 8 is adopted, so that the heat dissipation cover 2 is not provided with an inner partition plate inside, and the wiring of a connecting wire is facilitated;
the air inlet 6 is a louver type slot, and a louver type design is adopted, so that air can be introduced into the nacelle on one hand, and water drops can be prevented from entering the nacelle on the other hand; the unmanned aerial vehicle connecting socket 5 adopts a 20-core aviation socket. The unmanned aerial vehicle is connected with the unmanned aerial vehicle through the arranged unmanned aerial vehicle connecting socket 5, and the unmanned aerial vehicle is used for supplying power and inputting control signals to the internal equipment of the nacelle; the top of the cover body 3 is provided with a hoisting groove 7. The pod is mounted to the belly position of the drone using a sling through the provided sling slot 7.
The working principle of the unmanned aerial vehicle-mounted interference pod structure device is as follows: the pod is installed to the belly position of the unmanned aerial vehicle by using a hoisting piece through an arranged hoisting groove 7, the pod is connected with the unmanned aerial vehicle through an unmanned aerial vehicle connecting socket 5, the unmanned aerial vehicle is used for power supply and control signal input of equipment in the pod, please refer to fig. 2, a heat dissipation mounting frame 8 is of a rectangular frame structure, 2 heat dissipation toothed sheets 9 are arranged at the middle position in the heat dissipation mounting frame 8, interference equipment selects corresponding type equipment according to the factors such as functions, requirements or cost budget, the interference equipment is installed on the heat dissipation mounting frame 8 through screws and is ensured to be in contact with the heat dissipation toothed sheets 9 during installation, heat dissipation silica gel is required to be coated between the interference equipment and the heat dissipation toothed sheets 9, then the antenna 1 and the unmanned aerial vehicle connecting socket 5 are connected with the interference equipment, and finally the heat dissipation mounting frame 8 is installed in the heat dissipation cover 2, screws are driven into a bottom cover plate, because the air inlet 6 has been seted up to the both sides of covering 3 surfaces of cover main part, the unmanned aerial vehicle carries the flight in-process, absorb the heat that the work of interference ware equipment produced by heat dissipation tine 9, the speed that relies on the flight makes the air pour into through air inlet 6 and reduces heat dissipation tine 9 temperature, simultaneously at the tip by fan 4 extraction air produce the air current together carry out the heat dissipation of low heat dissipation tine 9, through the heat dissipation mode of adding the initiative passively like this, the radiating efficiency has been improved by a wide margin, and adopt the installation equipment of such rectangular frame structure of heat dissipation mounting bracket 8, make 2 inside no inner partition boards of heat dissipation housing, the wiring of connecting wire has also been made things convenient for.
In conclusion; unmanned aerial vehicle carries interference nacelle constructional device compares with current unmanned aerial vehicle carries interference nacelle constructional device, has the advantage that improves interference nacelle heat dispersion, promotes the continuation of the journey of interference emission equipment.
The previous description of the disclosed embodiments is provided to enable any person skilled in the art to make or use the present invention. Various modifications to these embodiments will be readily apparent to those skilled in the art, and the generic principles defined herein may be applied to other embodiments without departing from the spirit or scope of the invention. Thus, the present invention is not intended to be limited to the embodiments shown herein but is to be accorded the widest scope consistent with the principles and novel features disclosed herein.
Claims (5)
1. The utility model provides an unmanned aerial vehicle carries interference nacelle constructional device, includes heat dissipation housing (2) and antenna (1), its characterized in that: the heat dissipation cover (2) is composed of a cover main body (3), a heat dissipation mounting frame (8) and a bottom cover plate (10), the antenna (1) is arranged on one side of the cover main body (3), the antenna (1) is fixedly connected with the heat dissipation cover (2) through bolts, air inlets (6) are formed in two sides of the outer surface of the cover main body (3), an unmanned aerial vehicle connection socket (5) is installed on the side surface of the cover main body (3), the heat dissipation mounting frame (8) is embedded in the cover main body (3), a fan (4) is arranged on the adjacent side of the heat dissipation mounting frame (8), the fan (4) is fixedly connected with the cover main body (3) through bolts, the fan (4) is electrically connected with the unmanned aerial vehicle connection socket (5), the bottom cover plate (10) is arranged at the bottom of the cover main body (3), and the heat dissipation mounting frame (8) is fixedly welded with the bottom cover plate, and the bottom cover plate (10) is fixedly connected with the cover body (3) through screws.
2. The structure device of the unmanned aerial vehicle-mounted interference pod as claimed in claim 1, wherein: the heat dissipation mounting rack (8) is of a rectangular frame structure, and 2 heat dissipation tooth sheets (9) are arranged in the middle of the interior of the heat dissipation mounting rack (8).
3. The structure device of the unmanned aerial vehicle-mounted interference pod as claimed in claim 1, wherein: the air inlet (6) is provided with a shutter type slot.
4. The structure device of the unmanned aerial vehicle-mounted interference pod as claimed in claim 1, wherein: unmanned aerial vehicle connecting socket (5) adopt 20 core aviation sockets.
5. The structure device of the unmanned aerial vehicle-mounted interference pod as claimed in claim 1, wherein: the top of the cover main body (3) is provided with a hoisting groove (7).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920610520.2U CN209870763U (en) | 2019-04-29 | 2019-04-29 | Unmanned aerial vehicle carries interference nacelle constructional device |
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|---|---|---|---|
| CN201920610520.2U CN209870763U (en) | 2019-04-29 | 2019-04-29 | Unmanned aerial vehicle carries interference nacelle constructional device |
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| CN209870763U true CN209870763U (en) | 2019-12-31 |
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| CN201920610520.2U Active CN209870763U (en) | 2019-04-29 | 2019-04-29 | Unmanned aerial vehicle carries interference nacelle constructional device |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111288851A (en) * | 2020-03-27 | 2020-06-16 | 中交遥感天域科技江苏有限公司 | Multi-frequency omnidirectional unmanned aerial vehicle control equipment system |
| CN112469252A (en) * | 2020-12-11 | 2021-03-09 | 无锡职业技术学院 | Efficient cooling assembly suitable for micro-miniature photoelectric pod electronic unit |
-
2019
- 2019-04-29 CN CN201920610520.2U patent/CN209870763U/en active Active
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111288851A (en) * | 2020-03-27 | 2020-06-16 | 中交遥感天域科技江苏有限公司 | Multi-frequency omnidirectional unmanned aerial vehicle control equipment system |
| CN111288851B (en) * | 2020-03-27 | 2022-06-10 | 中交遥感天域科技江苏有限公司 | Multi-frequency omnidirectional unmanned aerial vehicle control equipment system |
| CN112469252A (en) * | 2020-12-11 | 2021-03-09 | 无锡职业技术学院 | Efficient cooling assembly suitable for micro-miniature photoelectric pod electronic unit |
| CN112469252B (en) * | 2020-12-11 | 2023-01-24 | 无锡职业技术学院 | Efficient cooling assembly suitable for micro-miniature photoelectric pod electronic unit |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| PE01 | Entry into force of the registration of the contract for pledge of patent right | ||
| PE01 | Entry into force of the registration of the contract for pledge of patent right |
Denomination of utility model: A kind of unmanned aerial vehicle jamming pod structure device Effective date of registration: 20220809 Granted publication date: 20191231 Pledgee: Xi'an innovation financing Company limited by guarantee Pledgor: Xi'an Ruiao Electromagnetic Environment Technology Co.,Ltd. Registration number: Y2022610000475 |
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| PC01 | Cancellation of the registration of the contract for pledge of patent right | ||
| PC01 | Cancellation of the registration of the contract for pledge of patent right |
Date of cancellation: 20230706 Granted publication date: 20191231 Pledgee: Xi'an innovation financing Company limited by guarantee Pledgor: Xi'an Ruiao Electromagnetic Environment Technology Co.,Ltd. Registration number: Y2022610000475 |
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| PE01 | Entry into force of the registration of the contract for pledge of patent right | ||
| PE01 | Entry into force of the registration of the contract for pledge of patent right |
Denomination of utility model: A Structural Device for Unmanned Aerial Vehicle Jamming Pod Effective date of registration: 20230719 Granted publication date: 20191231 Pledgee: Xi'an innovation financing Company limited by guarantee Pledgor: Xi'an Ruiao Electromagnetic Environment Technology Co.,Ltd. Registration number: Y2023610000597 |