CN109084616A - weapon cooling device - Google Patents
weapon cooling device Download PDFInfo
- Publication number
- CN109084616A CN109084616A CN201810978895.4A CN201810978895A CN109084616A CN 109084616 A CN109084616 A CN 109084616A CN 201810978895 A CN201810978895 A CN 201810978895A CN 109084616 A CN109084616 A CN 109084616A
- Authority
- CN
- China
- Prior art keywords
- weapon
- shell
- cooling device
- cooling
- heat
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
- 238000001816 cooling Methods 0.000 title claims abstract description 109
- 239000007788 liquid Substances 0.000 claims abstract description 56
- 238000010438 heat treatment Methods 0.000 claims abstract description 24
- 239000002826 coolant Substances 0.000 claims description 14
- 230000007246 mechanism Effects 0.000 claims description 12
- 238000004378 air conditioning Methods 0.000 claims description 4
- 238000004891 communication Methods 0.000 claims description 2
- 230000004992 fission Effects 0.000 claims 1
- 239000000110 cooling liquid Substances 0.000 abstract description 5
- 230000017525 heat dissipation Effects 0.000 abstract description 3
- 238000010586 diagram Methods 0.000 description 3
- 238000010521 absorption reaction Methods 0.000 description 2
- 238000002485 combustion reaction Methods 0.000 description 2
- 239000003721 gunpowder Substances 0.000 description 2
- 238000009434 installation Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 2
- 230000036760 body temperature Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000008878 coupling Effects 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000008569 process Effects 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41A—FUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
- F41A13/00—Cooling or heating systems; Blowing-through of gun barrels; Ventilating systems
- F41A13/12—Systems for cooling the outer surface of the barrel
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41A—FUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
- F41A13/00—Cooling or heating systems; Blowing-through of gun barrels; Ventilating systems
- F41A13/04—Injecting fluids into barrels or cartridge chambers
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
Abstract
The invention relates to a weapon cooling device which is arranged outside a heating part of a weapon and comprises a shell, a radiating piece and a cooling pipe, wherein the shell is provided with an accommodating cavity, the radiating piece and the cooling pipe are arranged in the accommodating cavity, the radiating piece is communicated with the outside and used for absorbing heat conducted by the heating part of the weapon and exchanging heat with the atmosphere, the cooling pipe is constructed in a way that the radiating piece is arranged adjacently, and cooling liquid exchanging heat with the heating part of the weapon flows in the cooling pipe. According to the weapon cooling device provided by the invention, the heat dissipation part absorbs the heat of the heating part of the weapon and exchanges heat with the atmosphere to cool the heating part of the weapon, and the cooling liquid circulating in the cooling pipe exchanges heat with the heating part of the weapon to cool the gun barrel, so that a double cooling mode of air cooling and liquid cooling is realized, and the cooling effect is better.
Description
Technical field
The present invention relates to technical field of heat exchange, more particularly to a kind of weapon cooling device.
Background technique
In Defence business, gun perhaps the weaponrys such as cannon in the process of running since gunpowder is in gun barrel or big gun
Vigorous combustion and highly exothermic in pipe, increase so as to cause gun barrel or gun tube due to absorbing thermal temperature and generate heat it is serious, sternly
The operational safety performance of weapon is affected again.
Therefore, it is necessary to external cooling devices to cool down to weapon, to reduce the temperature of gun barrel or gun tube, but it is traditional
The bad problem of the generally existing cooling effect of cooling device.
Summary of the invention
Based on this, it is necessary to for the bad problem of cooling effect of traditional cooling device to weapon, provide a kind of cold
But the preferable weapon cooling device of effect.
A kind of weapon cooling device, is installed on outside the heating position of the weapon, including shell, radiating piece and cooling tube,
The shell has accommodating chamber, and the radiating piece and the cooling tube be all set in the accommodating chamber, the radiating piece and outer
Boundary's connection, for absorbing the heat of the heating position conduction of the weapon and carrying out heat exchange, the cooling pipe construction with atmosphere
It is disposed adjacent at radiating piece, and circulation has the coolant liquid that heat exchange is carried out with the heating position of the weapon in the cooling tube.
Weapon cooling device provided by the invention, radiating piece absorb the heat of the heating position of weapon and carry out heat with atmosphere
Exchange is cooled down with the heating position to weapon, and the heating position of the coolant liquid and weapon to circulate in cooling tube carries out hot friendship
It changes and is cooled down with the heating position to weapon, so realize cold " double cold " mode of air cooling liquid feeding, cooling effect is preferable.
In one of the embodiments, the shell have a central axis, the radiating piece include multiple heat-dissipating pipes and
Multiple fins, interval is arranged the multiple heat-dissipating pipe with the centerline axis parallel and between each other, and each fin is equal
It is socketed on outside the multiple heat-dissipating pipe, and the multiple fin is arranged along the central axis interval.
The accommodating chamber has opposite first end and second end along the central axis in one of the embodiments,
The cooling tube is repeatedly bent from the first end to the second end with U-shaped turn-back shape, is set with forming multiple intervals
The row set.
The shell is semi-circular or annular in one of the embodiments, the radiating piece and the cooling tube it is outer
Shape of the shape with the shell matches.
The both ends of the cooling tube are respectively provided with for the inlet of feed liquor and for going out liquid in one of the embodiments,
Liquid outlet.
The weapon cooling device further includes liquid storage mechanism in one of the embodiments, the inlet and it is described go out
Liquid mouth is connected to the liquid storage mechanism.
The liquid storage mechanism includes one of liquid reserve tank or soldier's air-conditioning in one of the embodiments,.
The radiating piece cooling tube is arranged far from the heating position of the weapon in one of the embodiments,.
The shell includes the first half-shell and the second half-shell of split settings in one of the embodiments, and described first
Half-shell connect to define to form the accommodating chamber with second half-shell.
The first heat transfer hole and the second heat transfer hole are offered on the shell in one of the embodiments, described first passes
Hot hole and it is described second heat transfer Kong Junyu described in accommodating chamber connection, it is described first heat transfer hole be opened in the shell close to the force
One end of the heating position of device, second heat transfer hole are opened in one end of heating position of the shell far from the weapon.
The weapon cooling device further includes fastener in one of the embodiments, and the fastener is for being arranged in
The shell is the weapon cooling device to be fixedly connected with the weapon.
Detailed description of the invention
The installation diagram for the weapon cooling device that Fig. 1 one embodiment of the invention provides；
Fig. 2 is that weapon cooling device provided in Fig. 1 is assemblied in the structure chart on weapon；
Fig. 3 is the exploded view of weapon cooling device provided in Fig. 1；
Fig. 4 be another embodiment of the present invention provides weapon cooling device structural schematic diagram；
Fig. 5 is the structural schematic diagram for the weapon cooling device that further embodiment of this invention provides.
Specific embodiment
To facilitate the understanding of the present invention, a more comprehensive description of the invention is given in the following sections with reference to the relevant attached drawings.In attached drawing
Give presently preferred embodiments of the present invention.But the invention can be realized in many different forms, however it is not limited to this paper institute
The embodiment of description.On the contrary, purpose of providing these embodiments is keeps the understanding to the disclosure more thorough
Comprehensively.
It should be noted that it can directly on the other element when element is referred to as " being fixed on " another element
Or there may also be elements placed in the middle.When an element is considered as " connection " another element, it, which can be, is directly connected to
To another element or it may be simultaneously present centering elements.Term as used herein " vertical ", " horizontal ", " left side ",
" right side " and similar statement are for illustrative purposes only.
Unless otherwise defined, all technical and scientific terms used herein and belong to technical field of the invention
The normally understood meaning of technical staff is identical.Term as used herein in the specification of the present invention is intended merely to description tool
The purpose of the embodiment of body, it is not intended that in the limitation present invention.Term " and or " used herein includes one or more phases
Any and all combinations of the listed item of pass.
Refering to fig. 1, one embodiment of the invention provides a kind of weapon cooling device 100, for cooling down weapon, specifically, under
Face is described in detail weapon cooling device 100 provided by the invention as gun using the weapon.It is understood that
In other embodiments, above-mentioned weapon is also other national defence weapons, such as cannon, is not limited thereto.
Referring to Fig.2, gun have main body and gun barrel a, gun barrel a connect with main body, gunpowder vigorous combustion and big in gun barrel a
Heat release is measured, therefore the gun barrel a of gun is the heating position of gun, in order to cool down gun, which is installed on rifle
Outside the gun barrel a of branch.
Refering to Fig. 3, specifically, weapon cooling device 100 includes shell 10, radiating piece 20 and cooling tube 30, and weapon is cooling
Device 100 is installed on outside the gun barrel a of gun by shell 10, and shell 10 has accommodating chamber, and radiating piece 20 and cooling tube 30 are all provided with
It is placed in accommodating chamber and radiating piece 20 is disposed adjacent with cooling tube 30, radiating piece 20 is in communication with the outside, for absorbing the heat of gun barrel a
It measures and carries out heat exchange with atmosphere, circulation has coolant liquid (such as water) to carry out heat exchange with gun barrel a in cooling tube 30.
Weapon cooling device 100 provided in an embodiment of the present invention, when being installed on gun barrel a, radiating piece 20 absorbs gun barrel a's
Heat simultaneously carries out heat exchange with atmosphere to cool down to gun barrel a, and the coolant liquid and gun barrel a that circulate in cooling tube 30 carry out heat
Exchange so realizes cold " double cold " mode of air cooling liquid feeding to cool down to gun barrel a, and cooling effect is preferable.
It should be noted that then radiating piece 20 is inhaled since radiating piece 20 and cooling tube 30 are all set in accommodating chamber
While the heat and atmosphere for receiving gun barrel a carry out heat exchange, some heat can be carried out with the coolant liquid in cooling tube 30
Heat exchange, i.e. cooling tube 30 can directly absorb heat from gun barrel a or absorb heat from gun barrel a indirectly by radiating piece 20.
In order to match with the shape of gun barrel a, in the present embodiment, the shape of setting shell 10 is with a central axis
Semi-circular, semiorbicular shell 10 has half-via, and shell 10 is socketed on outside gun barrel a by half-via.It is understood that
Shell 10 can also be the annular with a central axis, and annular shell 10 has through-hole, and shell 10 is socketed on by through-hole
Outside gun barrel a.
In some other embodiment, the shape and the shape phase of the heating position for the weapon to be cooled down of shell 10 are set
Matching.
In the present embodiment, the first half-shell 11 and the second half-shell 12 of shell 10 including split settings, first half-shell 11 and
The connection of second half-shell 12 is defined to form above-mentioned accommodating chamber.Specifically, first half-shell 11 is arranged close to gun barrel a, and the second half-shell 12 is remote
It is arranged from gun barrel a, first half-shell 11 includes the first semi-circular plate 111, limit plate 113 and end plate 112, and two end plates 112 are distinguished
Positioned at both ends of first semi-circular plate 111 in the axial direction of gun barrel a, two limit plates 113 are located at the first semi-circular plate 111
Along the same both ends radially of gun barrel a, the second half-shell 12 includes the second semi-circular plate, the second semi-circular plate of the second half-shell 12
The connection of one end that both ends in the axial direction of gun barrel a are not connect with the first semi-circular plate 111 with two end plates 112 respectively, the second half
Second semi-circular plate of shell 12 along the same both ends radially of gun barrel a respectively with two limit plates 113 not with the first semi-circular plate
One end connection of 111 connections, such shell 10 form the semicircular with closed accommodating chamber.It is understood that
In other embodiments, as the setting form of shell 10 is different, the accommodating chamber of shell 10 may be the accommodating chamber of non-close.
And when shell 10 is annular, shell 10 be may be set to be including first half-shell 11 and the second half-shell 12, at this time
First half-shell 11 includes first annular plate and end plate 112, and two end plates 112 are located at first annular plate along the axial direction of gun barrel a
On both ends, the second half-shell 12 include the second annular slab, both ends of second annular slab in gun barrel a axial direction respectively with two end plates
The 112 one end connections not connect with first annular plate.
In one embodiment, enter the accommodating chamber of shell 10 for the ease of the heat conduction of gun barrel a, and facilitate access for
The heat of the accommodating chamber of shell 10 is conducted out of shell 10, and the first heat transfer hole 1111 and the second heat transfer are offered on shell 10
Hole 121, the first heat transfer hole 1111 are connected to the second heat transfer hole 121 with accommodating chamber, and the first hole 1111 of conducting heat is opened in the first half
Shell 11, the second heat transfer hole 121 are opened in the second half-shell 12.Specifically, the quantity in the first heat transfer hole 1111 is multiple, Duo Ge
One heat transfer hole 1111, which is spaced apart, to be set in first half-shell 11, and the quantity in the second heat transfer hole 121 is multiple, multiple second heat transfers hole
121 are spaced apart in first half-shell 11.
In one embodiment, in order to fix weapon cooling device 100 and gun barrel a, weapon cooling device 100 is also wrapped
Fastener 40 is included, weapon cooling device 100 will be fixedly connected by fastening with gun barrel a.
Specifically, fastener 40 is fastening screw, and fastening screw is arranged in first half-shell 11 from the second half-shell 12 and abuts
In gun barrel a shell 10 to be fixedly connected with gun barrel a, fastener 40 selects fastening screw to be relatively convenient for weapon cooling device 100
It is fixed on gun barrel a and is disassembled from gun barrel a.
In one embodiment, radiating piece 20 is arranged compared with cooling tube 30 far from gun, is so convenient for radiating piece 20 from gun barrel
The heat that a absorbs is exchanged heat by the second heat transfer hole 121 with atmosphere.It is understood that being dissipated in some other embodiment
Warmware 20 can also be arranged compared with cooling tube 30 close to gun, and radiating piece 20 can also pass through the second heat transfer hole 121 and atmosphere at this time
Heat exchange is carried out, only effect is relatively poor.
Specifically, radiating piece 20 includes multiple heat-dissipating pipes and multiple fins, and multiple heat-dissipating pipes are flat with above-mentioned central axis
Row and between each other interval setting, each fin is socketed on outside multiple heat-dissipating pipes, and multiple fins are along above-mentioned central axis side
It is arranged to interval, so convenient for the heat absorption faster of radiating piece 20 and heat dissipation.
More specifically, in order to further guarantee heat dissipation effect, radiating piece 20 be semicircular, with above-mentioned semicircular
The shape of shell 10 matches, at this time multiple heat-dissipating pipes being provided at circumferentially spaced along shell 10.Correspondingly, when the shape of shell 10
When for annular, the shape of radiating piece 20 is also configured as annular.
In one embodiment, accommodating chamber has opposite first end and second end, cooling tube 30 along above-mentioned central axis
It is repeatedly bent from first end end to second end with U-shaped shape, to form multiple intervals being provided at circumferentially spaced along shell 10
Row, also as cooling tube 30 includes more U-tubes interconnected, opposite per the opening direction between adjacent two single u-shaped pipe.
Guarantee that each section of accommodating chamber has cooling tube 30, so to guarantee cooling effect.
When shell 10 is semi-circular, the monnolithic case of cooling tube 30 also mutually should be semi-circular；It is cold when shell is annular
But the monnolithic case of pipe 30 also mutually should be annular.It is understood that the shape of cooling tube 30 is not in some other embodiment
Circumscribed.
In one embodiment, circulating for the ease of the coolant liquid in cooling tube 30, setting cooling tube 30 include
Inlet and liquid outlet, coolant liquid enter in cooling tube 30 from inlet, and flow out after carrying out heat exchange from liquid outlet.
Specifically, cooling tube 30 has the liquid feeding end 31 and outlet end 32 for stretching out shell 10, feed liquor along the axial direction of gun barrel a
Mouth is opened in liquid feeding end 31 and outlet end 32 with liquid outlet respectively.
Refering to Fig. 4 and Fig. 5, in one embodiment, for the ease of leading to coolant liquid, weapon cooling device into coolant liquid
100 further include liquid storage mechanism 50, and the coolant liquid saved in liquid storage mechanism 50 enters cooling tube 30 from the inlet of cooling tube 30
It is interior, and liquid storage mechanism 50 is flowed to from the liquid outlet of cooling tube 30 after carrying out heat exchange, then it is located at cold in liquid storage mechanism 50
But liquid again goes into cooling tube 30, circuits sequentially.
With continued reference to Fig. 4, specifically, above-mentioned liquid storage mechanism 50 is liquid reserve tank, and liquid reserve tank passes through input duct 60 and cooling
The liquid feeding end 31 of pipe 30 connects, and liquid reserve tank is connect by liquid outlet pipe 70 with the outlet end 32 of cooling tube 30.For the ease of cold
But the flowing of liquid can also install liquid pump in input duct 60 and liquid outlet pipe 70.And for the ease of installation, input duct
60 are connect with the inlet tube of cooling tube 30 with outlet tube by quick coupling 80 respectively with liquid outlet pipe 70.
With continued reference to Fig. 5, in another embodiment, above-mentioned liquid storage mechanism 50 is soldier's air-conditioning, and soldier's air-conditioning leads to respectively
Input duct 60 is crossed to connect with liquid outlet pipe 70 with the liquid feeding end 31 of cooling tube 30 with outlet end 32.
Specifically, input duct 60 includes the first branch pipe and the second branch pipe, the liquid feeding end 31 of the first branch pipe and cooling tube 30
Connection, liquid outlet pipe 70 include third branch pipe and the 4th branch pipe, and third branch pipe is connected to the outlet end 32 of cooling tube 30, and second
Branch pipe is connected to the 4th branch pipe and the coolant liquid that circulates is for body temperature lowering.
More specifically, the bifurcation of input duct 60 is provided with triple valve, the bifurcation of liquid outlet pipe 70 is also equipped with three
Port valve is provided with check valve 90 on the first branch pipe, the second branch pipe and third branch pipe, so that coolant liquid is in the first branch pipe, first
One-way flow in branch pipe and third branch pipe.
Weapon cooling device 100 provided in an embodiment of the present invention, has the advantages that
The heat of gun barrel a by first heat transfer hole 1111 enter accommodating chamber, radiating piece 20 absorb above-mentioned heat and with cooling
Pipe 30 carries out heat exchange, and when coolant liquid flows through cooling tube 30, by the heat absorption of cooling tube 30 and cooling tube 30 is discharged, to realize
To the water cooling of gun barrel a, and radiating piece 20 carries out heat exchange by the second heat transfer hole 121 and atmosphere, to realize to gun barrel a's
Air cooling, so realizes cold " double cold " mode of air cooling liquid feeding, and cooling effect is preferable.
Each technical characteristic of embodiment described above can be combined arbitrarily, for simplicity of description, not to above-mentioned reality
It applies all possible combination of each technical characteristic in example to be all described, as long as however, the combination of these technical characteristics is not deposited
In contradiction, all should be considered as described in this specification.
The embodiments described above only express several embodiments of the present invention, and the description thereof is more specific and detailed, but simultaneously
It cannot therefore be construed as limiting the scope of the patent.It should be pointed out that coming for those of ordinary skill in the art
It says, without departing from the inventive concept of the premise, various modifications and improvements can be made, these belong to protection of the invention
Range.Therefore, the scope of protection of the patent of the invention shall be subject to the appended claims.
Claims (11)
1. a kind of weapon cooling device (100), is installed on outside the heating position of the weapon, which is characterized in that including shell
(10), radiating piece (20) and cooling tube (30), the shell (10) have accommodating chamber, the radiating piece (20) and the cooling tube
(30) it is all set in the accommodating chamber, the radiating piece (20) is in communication with the outside, for absorbing the heating position of the weapon
The heat of conduction simultaneously carries out heat exchange with atmosphere, and the cooling tube (30) is configured to radiating piece (20) and is disposed adjacent, and described cold
But circulation has the coolant liquid that heat exchange is carried out with the heating position of the weapon in pipe (30).
2. weapon cooling device (100) according to claim 1, which is characterized in that the shell (10) has a center
Axis, the radiating piece (20) include multiple heat-dissipating pipes and multiple fins, and the multiple heat-dissipating pipe is flat with the central axis
Row and between each other interval setting, each fin is socketed on outside the multiple heat-dissipating pipe, and the multiple fin is along institute
State the setting of central axis interval.
3. weapon cooling device (100) according to claim 2, which is characterized in that the accommodating chamber is along the central axis
Line has opposite first end and second end, and the cooling tube (30) is turned back from the first end to the second end with U-shaped
Shape is repeatedly bent, to form multiple spaced rows.
4. weapon cooling device (100) according to claim 3, which is characterized in that the shell (10) be semi-circular or
Shape of the shape of annular, the radiating piece (20) and the cooling tube (30) with the shell (10) matches.
5. weapon cooling device (100) according to claim 1, which is characterized in that the both ends of the cooling tube (30) point
There is not be used for the inlet of feed liquor and the liquid outlet for going out liquid.
6. weapon cooling device (100) according to claim 5, which is characterized in that the weapon cooling device (100) is also
Including liquid storage mechanism (50), the inlet and the liquid outlet are connected to the liquid storage mechanism (50).
7. weapon cooling device (100) according to claim 6, which is characterized in that the liquid storage mechanism (50) includes storage
One of liquid case or soldier's air-conditioning.
8. weapon cooling device (100) according to claim 1, which is characterized in that the radiating piece (20) is more described cold
But pipe (30) is arranged far from the heating position of the weapon.
9. weapon cooling device (100) according to claim 1, which is characterized in that the shell (10) sets including fission
The first half-shell (11) and the second half-shell (12) set, the first half-shell (11) connect to define to be formed with second half-shell (12)
The accommodating chamber.
10. weapon cooling device (100) according to claim 1, which is characterized in that offer on the shell (10)
One heat transfer hole (1111) and second heat transfer hole (121), it is described first heat transfer hole (1111) and it is described second heat transfer hole (121) with
The accommodating chamber connection, first heat transfer hole (1111) are opened in the heating position of the shell (10) close described weapon
One end, second heat transfer hole (121) are opened in one end of the heating position of the shell (10) far from the weapon.
11. -10 described in any item weapon cooling devices (100) according to claim 1, which is characterized in that the weapon is cooling
Device (100) further includes fastener (40), and the fastener (40) is for being arranged in the shell (10) so that the weapon is cold
But device (100) is fixedly connected with the weapon.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810978895.4A CN109084616A (en) | 2018-08-27 | 2018-08-27 | weapon cooling device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810978895.4A CN109084616A (en) | 2018-08-27 | 2018-08-27 | weapon cooling device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN109084616A true CN109084616A (en) | 2018-12-25 |
Family
ID=64794756
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810978895.4A Pending CN109084616A (en) | 2018-08-27 | 2018-08-27 | weapon cooling device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN109084616A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109682253A (en) * | 2019-01-18 | 2019-04-26 | 广州国曜科技有限公司 | A kind of magnetic artillery orbit launching mouth cooling device |
| CN111280159A (en) * | 2020-04-15 | 2020-06-16 | 杨应松 | Bird repellent device utilizing mixed explosion sound of two gases |
Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6945154B1 (en) * | 2004-01-15 | 2005-09-20 | Luth Randy E | Finned carbine handguard assembly |
| CN101056522A (en) * | 2006-04-14 | 2007-10-17 | 鸿富锦精密工业（深圳）有限公司 | Radiator and liquid-cooled heat radiator applying the same |
| US7464496B1 (en) * | 2006-05-26 | 2008-12-16 | Davies Robert B | Heat exchanger barrel nut |
| US8408285B2 (en) * | 2009-11-19 | 2013-04-02 | Fu Zhun Precision Industry (Shen Zhen) Co., Ltd. | Heat dissipation apparatus |
| CN204634236U (en) * | 2015-01-13 | 2015-09-09 | 李振彬 | A kind of liquid-cooling heat radiation row |
| CN205119931U (en) * | 2015-11-16 | 2016-03-30 | 成都奇航系统集成有限公司 | Ripples that possesses two heat radiation structure hits big gun barrel |
| CN205563436U (en) * | 2016-04-01 | 2016-09-07 | 陈佳露 | Heat dissipation device |
| CN205610422U (en) * | 2016-03-04 | 2016-09-28 | 莱芜钢铁集团有限公司 | Heat dissipation mechanism of motor and motor |
| CN208847022U (en) * | 2018-08-27 | 2019-05-10 | 珠海格力电器股份有限公司 | Weapon cooling device |
-
2018
- 2018-08-27 CN CN201810978895.4A patent/CN109084616A/en active Pending
Patent Citations (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6945154B1 (en) * | 2004-01-15 | 2005-09-20 | Luth Randy E | Finned carbine handguard assembly |
| CN101056522A (en) * | 2006-04-14 | 2007-10-17 | 鸿富锦精密工业（深圳）有限公司 | Radiator and liquid-cooled heat radiator applying the same |
| CN101056522B (en) * | 2006-04-14 | 2010-08-04 | 鸿富锦精密工业（深圳）有限公司 | Liquid-cooled radiator and liquid-cooled heat radiator applying the same |
| US7464496B1 (en) * | 2006-05-26 | 2008-12-16 | Davies Robert B | Heat exchanger barrel nut |
| US8408285B2 (en) * | 2009-11-19 | 2013-04-02 | Fu Zhun Precision Industry (Shen Zhen) Co., Ltd. | Heat dissipation apparatus |
| CN204634236U (en) * | 2015-01-13 | 2015-09-09 | 李振彬 | A kind of liquid-cooling heat radiation row |
| CN205119931U (en) * | 2015-11-16 | 2016-03-30 | 成都奇航系统集成有限公司 | Ripples that possesses two heat radiation structure hits big gun barrel |
| CN205610422U (en) * | 2016-03-04 | 2016-09-28 | 莱芜钢铁集团有限公司 | Heat dissipation mechanism of motor and motor |
| CN205563436U (en) * | 2016-04-01 | 2016-09-07 | 陈佳露 | Heat dissipation device |
| CN208847022U (en) * | 2018-08-27 | 2019-05-10 | 珠海格力电器股份有限公司 | Weapon cooling device |
Non-Patent Citations (1)
| Title |
|---|
| 刘长生: "风力灭火机", vol. 1, 中国林业出版社, pages: 117 - 118 * |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109682253A (en) * | 2019-01-18 | 2019-04-26 | 广州国曜科技有限公司 | A kind of magnetic artillery orbit launching mouth cooling device |
| CN111280159A (en) * | 2020-04-15 | 2020-06-16 | 杨应松 | Bird repellent device utilizing mixed explosion sound of two gases |
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Application publication date: 20181225 |