CN208915414U - A kind of unmanned plane shell with sealed heat-dissipating and filter function - Google Patents
A kind of unmanned plane shell with sealed heat-dissipating and filter function Download PDFInfo
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- CN208915414U CN208915414U CN201821579911.4U CN201821579911U CN208915414U CN 208915414 U CN208915414 U CN 208915414U CN 201821579911 U CN201821579911 U CN 201821579911U CN 208915414 U CN208915414 U CN 208915414U
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- cover
- wall
- fuselage
- fixedly connected
- dissipating
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Abstract
The utility model relates to air vehicle technique fields, and disclose a kind of unmanned plane shell with sealed heat-dissipating and filter function, including fuselage, cover is provided at the top of the fuselage, the first seal groove is offered at the top of the fuselage, the inner wall of first seal groove is fixedly connected with the first sealing ring, and the inside of the cover offers catch basin.The unmanned plane shell with sealed heat-dissipating and filter function, pass through setting screwed pipe and threaded hole, cover can be screwed in fuselage, during the installation process, cover squeezes the first sealing ring, to achieve the effect that internal and extraneous sealing, pass through the catch basin of setting, connecting tube and shape cooling tube, water cooling can be carried out to the unmanned machine host of bottom, and bottom is provided with cooling device, unmanned machine host can be carried out air-cooled, two cooling devices are all installed on cover, it can be regarded as entirety with cover, heat radiation sealed effect is all very good, the person of being convenient to use uses.
Description
Technical field
The utility model relates to air vehicle technique field, specially a kind of unmanned plane with sealed heat-dissipating and filter function
Shell.
Background technique
UAV is not carried people to fly using what radio robot and the presetting apparatus provided for oneself manipulated
Device, unmanned plane are actually the general designation of unmanned vehicle, domestic and international unmanned plane the relevant technologies rapid development, UAV system
Many kinds of, purposes is wide and distinct characteristics, causes it in size, quality, voyage, endurance, flying height, flying speed and task
There is larger difference Deng various aspects, due to the diversity of unmanned plane, different classification methods is had for different considering: by winged
The classification of row platform configuration, unmanned plane can be divided into fixed-wing unmanned plane, rotor wing unmanned aerial vehicle, unmanned airship, umbrella wing unmanned plane and flapping wing
Unmanned plane etc..
Since UAV has great significance to Future Air Combat, each main military country, the world all step up into
The development work of row UAV, however there is sealing and ask with what heat dissipation contradicted in unmanned plane shell currently on the market
Topic, sealing effect is good to be not easy to coexist with good heat dissipation effect, and it is necessary to have filter functions for unmanned plane internal wiring complexity, so
It is proposed a kind of unmanned plane shell with sealed heat-dissipating and filter function to solve the above problems.
Utility model content
(1) the technical issues of solving
In view of the deficiencies of the prior art, the utility model provides a kind of unmanned plane with sealed heat-dissipating and filter function
Shell has the advantages of sealed heat-dissipating and filter function, and the unmanned plane shell solved currently on the market has sealing and heat dissipation
The problem of contradicting, sealing effect is good to be not easy to coexist with good heat dissipation effect, and it is necessary to have filtering for unmanned plane internal wiring complexity
The problem of function.
(2) technical solution
For the purpose for realizing above-mentioned sealed heat-dissipating and filter function, the utility model is provided the following technical solutions: a kind of tool
There are the unmanned plane shell of sealed heat-dissipating and filter function, including fuselage, cover is provided at the top of the fuselage, the fuselage
Top offers the first seal groove, and the inner wall of first seal groove is fixedly connected with the first sealing ring, the inside of the cover
Catch basin is offered, the bottom of the cover is communicated with equally distributed connecting tube, top and the catch basin phase of the connecting tube
Connection, the outer wall of the connecting tube offer the second seal groove, and the inner wall of second seal groove is fixedly connected with the second sealing
Circle, the fuselage are internally provided with annular cooling conduit, and the top of the annular cooling conduit is connected with connecting tube, the cover
Bottom be fixedly connected with screwed pipe, offer threaded hole at the top of the fuselage, the inner wall and screwed pipe spiral shell of the threaded hole
Line connection, the bottom of the cover are fixedly installed with cooling device, the bottom of the cover and bottom for being located at cooling device is solid
Surely it is connected with protective cover, the bottom of the protective cover offers equally distributed through-hole, and the inner wall of the screwed pipe is fixedly connected
There is equally distributed pull rod, the bottom end of the pull rod is fixedly connected with clip, and the inner wall and annular cooling conduit of the clip are clamped,
The inner bottom wall of the fuselage is fixedly installed with unmanned machine host, the inner bottom wall of the fuselage and left side for being located at unmanned machine host is solid
Dingan County is equipped with filter.
Preferably, the output end of the filter is electrically connected with the input terminal of unmanned machine host, the right side of filter and nothing
There are gaps between man-machine host.
Preferably, the cooling device includes motor, motor connecting rod, shaft and fan, and the outer wall of motor is fixedly connected
Have equally distributed motor connecting rod, the opposite one end of motor connecting rod is fixedly connected with cover, the output shaft of motor with turn
Axis is fixedly connected, and the outer wall of shaft is fixedly connected with fan.
Preferably, the protective cover is hemispherical cover, and there are gaps between the inner wall and fan of protective cover.
Preferably, the top of first sealing ring is contacted with the bottom of cover, the outer wall and storage of second sealing ring
The inner wall of sink contacts.
Preferably, there are gaps between the bottom of the annular cooling conduit and unmanned machine host, and annular cooling conduit is outer
Diameter is less than the outer diameter of screwed pipe.
(3) beneficial effect
Compared with prior art, the utility model provides outside a kind of unmanned plane with sealed heat-dissipating and filter function
Shell, have it is following the utility model has the advantages that
1, the unmanned plane shell with sealed heat-dissipating and filter function can be by machine by setting screwed pipe and threaded hole
Lid screws in fuselage, and during the installation process, cover squeezes the first sealing ring, to achieve the effect that inside is sealed with extraneous, leads to
Catch basin, connecting tube and the shape cooling tube of setting are crossed, water cooling can be carried out to the unmanned machine host of bottom, and bottom is provided with cooling
Device, can be air-cooled to the progress of unmanned machine host, and two cooling devices are all installed on cover, can regard it as with cover
Whole, heat radiation sealed effect is all very good, and the person of being convenient to use uses.
2, unmanned plane shell with sealed heat-dissipating and filter function, by the way that filter, filter and unmanned plane is arranged
Host electrical connection, can make the circuit of unmanned plane host complex obtain the signal of required frequency, reached the function of filtering, facilitated
User uses.
Detailed description of the invention
Fig. 1 is the utility model structure front view；
Fig. 2 is the utility model fuselage cross-sectional view.
In figure: 1 fuselage, 2 covers, 3 first seal grooves, 4 first sealing rings, 5 catch basins, 6 connecting tubes, 7 second seal grooves,
8 second sealing rings, 9 annular cooling conduits, 10 screwed pipes, 11 threaded holes, 12 cooling devices, 13 protective covers, 14 through-holes, 15 pull rods,
16 clips, 17 unmanned machine hosts, 18 filters.
Specific embodiment
The following will be combined with the drawings in the embodiments of the present invention, carries out the technical scheme in the embodiment of the utility model
Clearly and completely describe, it is clear that the described embodiments are only a part of the embodiments of the utility model, rather than whole
Embodiment.Based on the embodiments of the present invention, those of ordinary skill in the art are without making creative work
Every other embodiment obtained, fall within the protection scope of the utility model.
A kind of unmanned plane shell with sealed heat-dissipating and filter function referring to FIG. 1-2, including fuselage 1, fuselage 1
Top is provided with cover 2, and the top of fuselage 1 offers the first seal groove 3, and the inner wall of the first seal groove 3 is fixedly connected with first
The top of sealing ring 4, the first sealing ring 4 is contacted with the bottom of cover 2, and the inner wall of the outer wall and catch basin 5 of the second sealing ring 8 connects
Touching, the inside of cover 2 offer catch basin 5, and the bottom of cover 2 is communicated with equally distributed connecting tube 6, the top of connecting tube 6
It is connected with catch basin 5, the outer wall of connecting tube 6 offers the second seal groove 7, and the inner wall of the second seal groove 7 is fixedly connected with
Two sealing rings 8, fuselage 1 are internally provided with annular cooling conduit 9, deposit between the bottom of annular cooling conduit 9 and unmanned machine host 17
In gap, and the outer diameter of annular cooling conduit 9 is less than the outer diameter of screwed pipe 10, and the top of annular cooling conduit 9 is connected with connecting tube 6
Logical, the bottom of cover 2 is fixedly connected with screwed pipe 10, by setting screwed pipe 10 and threaded hole 11, cover 2 can be screwed in fuselage
In 1, during the installation process, cover 2 squeezes the first sealing ring 4, to achieve the effect that internal and extraneous sealing, passes through setting
Catch basin 5, connecting tube 6 and shape cooling tube 9 can carry out water cooling to the unmanned machine host 17 of bottom, and bottom is provided with cooling dress
12 are set, unmanned machine host 17 can be carried out air-cooled, two cooling devices 12 are all installed on the cover 2, can see it with cover 2
An entirety is done, heat radiation sealed effect is all very good, and the person of being convenient to use uses, and the top of fuselage 1 offers threaded hole 11, spiral shell
The inner wall of pit 11 is threadedly coupled with screwed pipe 10, and the bottom of cover 2 is fixedly installed with cooling device 12, and cooling device 12 includes
Motor, motor connecting rod, shaft and fan, the outer wall of motor are fixedly connected with equally distributed motor connecting rod, motor connection
The opposite one end of bar is fixedly connected with cover 2, and the output shaft of motor is fixedly connected with shaft, and outer wall and the fan of shaft are fixed
Connection, the bottom of cover 2 and the bottom for being located at cooling device 12 are fixedly connected with protective cover 13, and protective cover 13 is hemispherical cover,
And there are gap between the inner wall and fan of protective cover 13, the bottom of protective cover 13 offers equally distributed through-hole 14, screw thread
The inner wall of pipe 10 is fixedly connected with equally distributed pull rod 15, and the bottom end of pull rod 15 is fixedly connected with clip 16, clip 16 it is interior
Wall and annular cooling conduit 9 are clamped, and the inner bottom wall of fuselage 1 is fixedly installed with unmanned machine host 17, the inner bottom wall of fuselage 1 and are located at nothing
The left side of man-machine host 17 is fixedly installed with filter 18, and the model of filter 18 can be ME-966-2.5, is filtered by setting
Device 18, filter 18 are electrically connected with unmanned machine host 17, and the complicated circuit of unmanned machine host 17 can be made to obtain the letter of required frequency
Number, reach the function of filtering, the person of being convenient to use uses, the input terminal electricity of the output end of filter 18 and unmanned machine host 17
Connection, there are gaps between the right side of filter 18 and unmanned machine host 17.
When in use, by setting screwed pipe 10 and threaded hole 11, cover 2 can be screwed in fuselage 1, in installation process
In, cover 2 squeezes the first sealing ring 4, to achieve the effect that internal and extraneous sealing, passes through the catch basin 5 of setting, connecting tube
6 and shape cooling tube 9, water cooling can be carried out to the unmanned machine host 17 of bottom, and bottom is provided with cooling device 12, it can be to unmanned plane
Host 17 carries out air-cooled, and two cooling devices 12 are all installed on the cover 2, can regard it as entirety with cover 2, are radiated
Sealing effect is all very good, and by the way that filter 18 is arranged, filter 18 is electrically connected with unmanned machine host 17, can make unmanned machine host
17 complicated circuits obtain the signal of required frequency, have reached the function of filtering, and the person of being convenient to use uses.
In conclusion this has the unmanned plane shell of sealed heat-dissipating and filter function, pass through setting screwed pipe 10 and screw thread
Hole 11 can screw in cover 2 in fuselage 1, and during the installation process, cover 2 squeezes the first sealing ring 4, to reach internal and outer
The effect of boundary's sealing can carry out the unmanned machine host 17 of bottom by the catch basin 5 of setting, connecting tube 6 and shape cooling tube 9
Water cooling, and bottom is provided with cooling device 12, can carry out unmanned machine host 17 air-cooled, and two cooling devices 12 are all mounted in
On cover 2, it can be regarded as entirety with cover 2, heat radiation sealed effect is all very good, and the person of being convenient to use uses.
Also, by setting filter 18, filter 18 is electrically connected with unmanned machine host 17, and unmanned machine host 17 can be made multiple
Miscellaneous circuit obtains the signal of required frequency, has reached the function of filtering, and the person of being convenient to use uses.
It should be noted that the terms "include", "comprise" or its any other variant are intended to the packet of nonexcludability
Contain, so that the process, method, article or equipment for including a series of elements not only includes those elements, but also including
Other elements that are not explicitly listed, or further include for elements inherent to such a process, method, article, or device.
In the absence of more restrictions, the element limited by sentence "including a ...", it is not excluded that including the element
Process, method, article or equipment in there is also other identical elements.
While there has been shown and described that the embodiments of the present invention, for the ordinary skill in the art,
It is understood that these embodiments can be carried out with a variety of variations in the case where not departing from the principles of the present invention and spirit, repaired
Change, replacement and variant, the scope of the utility model is defined by the appended claims and the equivalents thereof.
Claims (6)
1. a kind of unmanned plane shell with sealed heat-dissipating and filter function, including fuselage (1), it is characterised in that: the fuselage
(1) it is provided at the top of cover (2), is offered the first seal groove (3) at the top of the fuselage (1), first seal groove (3)
Inner wall be fixedly connected with the first sealing ring (4), the inside of the cover (2) offers catch basin (5), the cover (2)
Bottom is communicated with equally distributed connecting tube (6), and the top of the connecting tube (6) is connected with catch basin (5), the connecting tube
(6) outer wall offers the second seal groove (7), and the inner wall of second seal groove (7) is fixedly connected with the second sealing ring (8),
The fuselage (1) is internally provided with annular cooling conduit (9), and the top of the annular cooling conduit (9) is connected with connecting tube (6)
Logical, the bottom of the cover (2) is fixedly connected with screwed pipe (10), offers threaded hole (11), institute at the top of the fuselage (1)
The inner wall for stating threaded hole (11) is threadedly coupled with screwed pipe (10), and the bottom of the cover (2) is fixedly installed with cooling device
(12), the bottom of the cover (2) and be located at cooling device (12) bottom be fixedly connected with protective cover (13), the protective cover
(13) bottom offers equally distributed through-hole (14), and the inner wall of the screwed pipe (10) is fixedly connected with equally distributed drawing
The bottom end of bar (15), the pull rod (15) is fixedly connected with clip (16), the inner wall of the clip (16) and annular cooling conduit (9)
Clamping, the inner bottom wall of the fuselage (1) is fixedly installed with unmanned machine host (17), the inner bottom wall of the fuselage (1) and is located at nothing
Filter (18) are fixedly installed on the left of man-machine host (17).
2. a kind of unmanned plane shell with sealed heat-dissipating and filter function according to claim 1, it is characterised in that: institute
The output end for stating filter (18) is electrically connected with the input terminal of unmanned machine host (17), the right side of filter (18) and unmanned owner
There are gaps between machine (17).
3. a kind of unmanned plane shell with sealed heat-dissipating and filter function according to claim 1, it is characterised in that: institute
Stating cooling device (12) includes motor, motor connecting rod, shaft and fan, and the outer wall of motor is fixedly connected with equally distributed horse
Up to connecting rod, the opposite one end of motor connecting rod is fixedly connected with cover (2), and the output shaft of motor is fixedly connected with shaft,
The outer wall of shaft is fixedly connected with fan.
4. a kind of unmanned plane shell with sealed heat-dissipating and filter function according to claim 1, it is characterised in that: institute
Stating protective cover (13) is hemispherical cover, and there are gaps between the inner wall and fan of protective cover (13).
5. a kind of unmanned plane shell with sealed heat-dissipating and filter function according to claim 1, it is characterised in that: institute
The top for stating the first sealing ring (4) is contacted with the bottom of cover (2), outer wall and catch basin (5) of second sealing ring (8)
Inner wall contact.
6. a kind of unmanned plane shell with sealed heat-dissipating and filter function according to claim 1, it is characterised in that: institute
It states between the bottom of annular cooling conduit (9) and unmanned machine host (17) there are gap, and the outer diameter of annular cooling conduit (9) is less than spiral shell
The outer diameter of line pipe (10).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821579911.4U CN208915414U (en) | 2018-09-27 | 2018-09-27 | A kind of unmanned plane shell with sealed heat-dissipating and filter function |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821579911.4U CN208915414U (en) | 2018-09-27 | 2018-09-27 | A kind of unmanned plane shell with sealed heat-dissipating and filter function |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208915414U true CN208915414U (en) | 2019-05-31 |
Family
ID=66707176
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821579911.4U Expired - Fee Related CN208915414U (en) | 2018-09-27 | 2018-09-27 | A kind of unmanned plane shell with sealed heat-dissipating and filter function |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208915414U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110943270A (en) * | 2019-11-15 | 2020-03-31 | 深圳市安达工业设计有限公司 | Superconducting filter convenient to heat dissipation |
| CN111740298A (en) * | 2020-06-22 | 2020-10-02 | 中国科学院长春光学精密机械与物理研究所 | Aviation laser |
| CN114096466A (en) * | 2020-04-30 | 2022-02-25 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle |
-
2018
- 2018-09-27 CN CN201821579911.4U patent/CN208915414U/en not_active Expired - Fee Related
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110943270A (en) * | 2019-11-15 | 2020-03-31 | 深圳市安达工业设计有限公司 | Superconducting filter convenient to heat dissipation |
| CN110943270B (en) * | 2019-11-15 | 2021-02-09 | 苏州莫得克精密科技有限公司 | Superconducting filter convenient to heat dissipation |
| CN114096466A (en) * | 2020-04-30 | 2022-02-25 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle |
| CN111740298A (en) * | 2020-06-22 | 2020-10-02 | 中国科学院长春光学精密机械与物理研究所 | Aviation laser |
| CN111740298B (en) * | 2020-06-22 | 2021-09-03 | 中国科学院长春光学精密机械与物理研究所 | Aviation laser |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20190531 Termination date: 20210927 |