CN220470963U - Aviation stainless steel pipe with heat dissipation function - Google Patents
Aviation stainless steel pipe with heat dissipation function Download PDFInfo
- Publication number
- CN220470963U CN220470963U CN202321906759.7U CN202321906759U CN220470963U CN 220470963 U CN220470963 U CN 220470963U CN 202321906759 U CN202321906759 U CN 202321906759U CN 220470963 U CN220470963 U CN 220470963U
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- China
- Prior art keywords
- pipe
- heat dissipation
- stainless steel
- steel pipe
- dissipation function
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- 229910001220 stainless steel Inorganic materials 0.000 title claims abstract description 31
- 239000010935 stainless steel Substances 0.000 title claims abstract description 31
- 230000017525 heat dissipation Effects 0.000 title claims abstract description 30
- 239000007788 liquid Substances 0.000 claims abstract description 23
- 238000005260 corrosion Methods 0.000 claims abstract description 21
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims abstract description 18
- 238000005192 partition Methods 0.000 claims abstract description 16
- 238000002347 injection Methods 0.000 claims abstract description 14
- 239000007924 injection Substances 0.000 claims abstract description 14
- 239000003973 paint Substances 0.000 claims abstract description 12
- 238000001816 cooling Methods 0.000 claims abstract description 8
- 238000003466 welding Methods 0.000 claims description 8
- 239000007787 solid Substances 0.000 claims description 3
- 230000007797 corrosion Effects 0.000 abstract description 12
- 241000886569 Cyprogenia stegaria Species 0.000 abstract description 4
- 230000035939 shock Effects 0.000 abstract description 4
- 239000000126 substance Substances 0.000 abstract description 4
- 239000006096 absorbing agent Substances 0.000 abstract description 3
- 238000000889 atomisation Methods 0.000 abstract description 2
- 230000009467 reduction Effects 0.000 description 4
- 238000004880 explosion Methods 0.000 description 3
- 239000000463 material Substances 0.000 description 3
- 229910000831 Steel Inorganic materials 0.000 description 2
- 238000010521 absorption reaction Methods 0.000 description 2
- 238000005336 cracking Methods 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 238000009826 distribution Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 230000005855 radiation Effects 0.000 description 2
- 239000010959 steel Substances 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 230000007246 mechanism Effects 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 239000000243 solution Substances 0.000 description 1
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- Cooling Or The Like Of Electrical Apparatus (AREA)
Abstract
The utility model relates to the technical field of aviation equipment and discloses an aviation stainless steel pipe with a heat dissipation function, which comprises an outer pipe, a liquid heat dissipation device and a physical radiator, wherein a threaded connecting piece is arranged on the rear side of the outer pipe, a fixing piece is arranged in the middle of the outer pipe, the fixing piece comprises a fixing ring and a hanging piece, a main valve is arranged at the upper end of the outer pipe, the main valve comprises a valve base, a rubber gasket, a movable column and a valve handle, an anti-collision spring is arranged at the rear end of the main valve, a water injection pipe is arranged in the outer pipe, an inner pipe is arranged at the lower end of the water injection pipe, the liquid heat dissipation device is arranged in the inner pipe, the liquid heat dissipation device comprises a partition plate, anti-corrosion paint, a liquid cooling pipe and an atomization pipe, a physical radiator is arranged on the right side of the inner pipe, the physical radiator comprises a fan shell and a fan, and a shock absorber is arranged on the rear side of the anti-collision spring, so that corrosion caused by high temperature, high humidity and chemical environment in the aviation field is solved.
Description
Technical Field
The utility model relates to an avionics technical field, concretely relates to aviation stainless steel pipe with heat dissipation function.
Background
An aviation stainless steel pipe with heat dissipation function is a pipeline specially designed for conducting heat and exchanging heat in the aviation field, and is usually made of stainless steel materials, and has good corrosion resistance and high temperature resistance.
Through searching, the patent with the publication of CN208651840U discloses an aviation stainless steel pipe with a heat dissipation function, and the patent is proposed: the novel heat dissipation device comprises a stainless steel pipe body and a heat dissipation box, wherein a second inner cavity is formed in the stainless steel pipe body, a first inner cavity is formed in one end of the second inner cavity, and an inner thread is formed in the inner wall of the first inner cavity. "
However, when implementing the above technical solution, the following problems exist: corrosion, stainless steel itself has better corrosion resistance, but under certain extreme conditions, such as high temperature, high humidity, chemical environment and the like in the aviation field, corrosion can still occur, the corrosion can lead to the reduction of the wall thickness of a pipeline, the reduction of heat dissipation efficiency, even the cracking of the pipeline, uneven heat conduction, and uneven conditions of the stainless steel pipe during heat conduction can occur, which can be caused by factors such as non-uniformity of materials, non-uniformity in the manufacturing process or difference of the internal environment and the external environment of the pipeline, and uneven heat conduction can lead to uneven distribution of heat in the steel pipe, and influence on the heat dissipation effect.
Disclosure of Invention
The utility model provides an aviation stainless steel pipe with a heat dissipation function, which is used for solving the problems that corrosion exists in the prior aviation stainless steel pipe in the background technology, stainless steel has good corrosion resistance, corrosion can still occur under certain extreme conditions such as high temperature, high humidity, chemical environment and the like in the aviation field, the corrosion can lead to the reduction of the wall thickness of a pipeline, the heat dissipation efficiency is reduced, even the pipeline breakage can be caused, the heat conduction is uneven, the stainless steel pipe can generate uneven conditions when conducting heat, the uneven heat conduction can be caused by factors such as the non-uniformity of materials, the non-uniformity in the manufacturing process or the difference of the internal environment and the external environment of the pipeline, and the like, and the uneven heat conduction can lead to the uneven distribution of heat in the steel pipe, so that the heat dissipation effect is influenced.
In order to solve the technical problems, the utility model provides the following technical scheme: the utility model provides an aviation stainless steel pipe with heat dissipation function, includes outer tube, liquid heat abstractor and physical radiator, the outer tube rear side is provided with threaded connection spare, the middle part of outer tube is provided with the mounting, the mounting includes solid fixed ring and pendant, the upper end of outer tube is provided with total valve, total valve includes valve base, rubber gasket, movable column and valve handle, the rear end of total valve is provided with anti-collision spring, the inside of outer tube is provided with the water injection pipe, the lower extreme of water injection pipe is provided with the inner tube, the inside of inner tube is provided with liquid heat abstractor, liquid heat abstractor includes division board, anticorrosive paint, liquid cold tube and atomizing pipe, the right side of inner tube is provided with physical radiator, physical radiator includes fan housing and fan, anti-collision spring's rear side is provided with shock absorber.
Preferably, the outer tube is in threaded connection with the threaded connecting piece, the outer tube is in clamping groove connection with the fixing ring, and the fixing ring is in threaded connection with the hanging piece.
Preferably, the outer tube is welded with the valve base, and the valve base is in threaded connection with the rubber gasket.
Preferably, the rubber gasket is movably connected with the movable column, the movable column is welded with the valve handle, and the outer tube is connected with the anti-collision spring in an embedded mode.
Preferably, the outer pipe is connected with the water injection pipe through a clamping groove, the outer pipe is connected with the inner pipe through welding, and the inner pipe is connected with the partition plate through welding.
Preferably, the surface of the partition plate is attached with anti-corrosion paint, and the partition plate is connected with the liquid cooling pipe in a welding way.
Preferably, the partition plate is in welded connection with the atomizing pipe, and the inner pipe is in welded connection with the fan shell.
Preferably, the fan shell is movably connected with the fan, and the outer tube is welded with the shockproof damper.
Compared with the related art, the aviation stainless steel pipe with the heat dissipation function provided by the utility model has the following structure
The beneficial effects are that:
the utility model provides an aviation stainless steel pipe with a heat dissipation function, which comprises the following components: by arranging the partition plate, the anti-corrosion paint, the liquid cooling pipe, the atomizing pipe, the fan shell and the fan, the utility model can realize that the anti-corrosion performance of the stainless steel is improved by arranging the anti-corrosion paint, solve the problems that the corrosion possibly causes the reduction of the wall thickness of a pipeline, reduces the heat radiation efficiency and causes the cracking of the pipeline under certain extreme conditions such as high temperature, high humidity, chemical environment and the like in the aviation field, and solve the uneven condition of the stainless steel pipe when heat is conducted by arranging the liquid heat radiation device.
Drawings
The utility model will be described in further detail with reference to the drawings and the detailed description.
FIG. 1 is a schematic diagram of the front structure of the present utility model;
FIG. 2 is a schematic diagram of the internal mechanism of the present utility model;
FIG. 3 is a schematic view of the internal cutaway structure of the present utility model;
fig. 4 is a schematic view of the back structure of the present utility model.
Reference numerals in the drawings: 1. an outer tube; 2. a threaded connection; 3. a fixing member; 301. a fixing ring; 302. a hanging piece; 4. a main valve; 401. a valve base; 402. a rubber gasket; 403. a movable column; 404. a valve handle; 5. an anti-collision spring; 6. a water injection pipe; 7. an inner tube; 8. a liquid heat sink; 801. a partition plate; 802. anticorrosive paint; 803. a liquid-cooled tube; 804. an atomizing tube; 9. a physical heat sink; 901. a fan housing; 902. a fan; 10. vibration-proof damper.
Detailed Description
The following description of the embodiments of the present utility model will be made clearly and fully with reference to the accompanying drawings, in which it is evident that the embodiments described are only some, but not all embodiments of the utility model; all other embodiments, which can be made by those skilled in the art based on the embodiments of the utility model without making any inventive effort, are intended to be within the scope of the utility model.
1-4, an aviation stainless steel pipe with heat dissipation function, including outer tube 1, liquid heat abstractor 8 and physical radiator 9, outer tube 1 rear side is provided with threaded connection 2, the middle part of outer tube 1 is provided with mounting 3, mounting 3 includes solid fixed ring 301 and pendant 302, the upper end of outer tube 1 is provided with total valve 4, total valve 4 includes valve base 401, rubber gasket 402, movable column 403 and valve handle 404, the rear end of total valve 4 is provided with anticollision spring 5, the inside of outer tube 1 is provided with water injection pipe 6, the lower extreme of water injection pipe 6 is provided with inner tube 7, the inside of inner tube 7 is provided with liquid heat abstractor 8, liquid heat abstractor 8 includes division board 801, anticorrosive paint 802, liquid cooling pipe 803 and atomizing pipe 804, the right side of inner tube 7 is provided with physical radiator 9, physical radiator 9 includes fan housing 901 and fan 902, the rear side of anticollision spring 5 is provided with shock absorber 10.
When the anti-explosion device is used, the outer tube 1 and the inner tube 7 are assembled, the threaded connecting piece 2 of the stainless steel tube is installed on a device of the stainless steel tube, the problem of welding defects can be well solved through threaded connection, water is injected into the water injection tube 6, the liquid cooling tube 803 is subjected to water injection operation, the atomization tube 804 can also play a role in physical heat absorption and heat dissipation, the anti-corrosion paint 802 solves the problem of corroding a pipeline, the fan 902 performs physical heat dissipation when the pipeline works, the anti-collision spring 5 can cooperate with the anti-collision damper 10 to play a role in anti-collision and shock absorption when in use, the water flow can be adjusted when the water is injected through the main valve 4, the explosion is prevented, and the anti-explosion device can be fixed through the fixing ring 301 in cooperation with the hanging piece 302 when in installation.
Specifically, the outer tube 1 is in threaded connection with the threaded connecting piece 2, the outer tube 1 is in clamping groove connection with the fixing ring 301, the fixing ring 301 is in threaded connection with the hanging piece 302, and the hanging piece 302 can be used for conveniently installing and fixing a pipeline.
Specifically, the outer tube 1 is in welded connection with the valve base 401, the valve base 401 is in threaded connection with the rubber gasket 402, and the rubber gasket 402 can play a role in preventing water leakage.
Specifically, the rubber gasket 402 is movably connected with the movable column 403, the movable column 403 is welded with the valve handle 404, the outer tube 1 is connected with the anti-collision spring 5 in an embedded manner, and the anti-collision spring 5 can reduce damage caused by collision to a pipeline.
Specifically, the outer tube 1 is connected with the water injection tube 6 through a clamping groove, the outer tube 1 is connected with the inner tube 7 through welding, the inner tube 7 is connected with the partition plate 801 through welding, and the partition plate 801 can play a role in separating liquid.
Specifically, the anti-corrosion paint 802 is attached to the surface of the partition plate 801, and the partition plate 801 is welded to the liquid cooling pipe 803, so that the anti-corrosion paint 802 can play a role in preventing corrosion.
Specifically, the partition plate 801 is welded to the atomizing pipe 804, and the inner pipe 7 is welded to the fan casing 901, so that the welded connection is more firm.
The foregoing description of the preferred embodiments of the utility model is not intended to be limiting, but rather is intended to cover all modifications, equivalents, alternatives, and improvements that fall within the spirit and scope of the utility model.
Claims (8)
1. The utility model provides an aviation stainless steel pipe with heat dissipation function, includes outer tube (1), liquid heat abstractor (8) and physical radiator (9), a serial communication port, outer tube (1) rear side is provided with threaded connection spare (2), the middle part of outer tube (1) is provided with mounting (3), mounting (3) are including solid fixed ring (301) and pendant (302), the upper end of outer tube (1) is provided with total valve (4), total valve (4) include valve base (401), rubber gasket (402), movable column (403) and valve handle (404), the rear end of total valve (4) is provided with anticollision spring (5), the inside of outer tube (1) is provided with water injection pipe (6), the lower extreme of water injection pipe (6) is provided with inner tube (7), the inside of inner tube (7) is provided with liquid heat abstractor (8), liquid heat abstractor (8) include division board (801), anticorrosive paint (802), 803) and air cooling pipe (804), the right side of inner tube (7) is provided with radiator (902) physical radiator (9), radiator (902) are provided with fan (902), the rear side of the anti-collision spring (5) is provided with an anti-collision damper (10).
2. The aviation stainless steel pipe with the heat dissipation function according to claim 1, wherein the outer pipe (1) is in threaded connection with the threaded connecting piece (2), the outer pipe (1) is in clamping groove connection with the fixing ring (301), and the fixing ring (301) is in threaded connection with the hanging piece (302).
3. The aviation stainless steel pipe with the heat dissipation function according to claim 1, wherein the outer pipe (1) is welded with the valve base (401), and the valve base (401) is in threaded connection with the rubber gasket (402).
4. An aviation stainless steel pipe with a heat dissipation function according to claim 3, wherein the rubber gasket (402) is movably connected with the movable column (403), the movable column (403) is welded with the valve handle (404), and the outer pipe (1) is connected with the anti-collision spring (5) in an embedded manner.
5. The aviation stainless steel pipe with the heat dissipation function according to claim 1, wherein the outer pipe (1) is connected with the water injection pipe (6) through a clamping groove, the outer pipe (1) is connected with the inner pipe (7) through welding, and the inner pipe (7) is connected with the partition plate (801) through welding.
6. The aviation stainless steel pipe with the heat dissipation function according to claim 1, wherein anti-corrosion paint (802) is attached to the surface of the partition plate (801), and the partition plate (801) is welded with the liquid cooling pipe (803).
7. The aviation stainless steel pipe with the heat dissipation function according to claim 6, wherein the partition plate (801) is welded with the atomizing pipe (804), and the inner pipe (7) is welded with the fan housing (901).
8. The aviation stainless steel pipe with the heat dissipation function according to claim 1, wherein the fan casing (901) is movably connected with the fan (902), and the outer pipe (1) is welded with the shockproof damper (10).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321906759.7U CN220470963U (en) | 2023-07-20 | 2023-07-20 | Aviation stainless steel pipe with heat dissipation function |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321906759.7U CN220470963U (en) | 2023-07-20 | 2023-07-20 | Aviation stainless steel pipe with heat dissipation function |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN220470963U true CN220470963U (en) | 2024-02-09 |
Family
ID=89775158
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202321906759.7U Active CN220470963U (en) | 2023-07-20 | 2023-07-20 | Aviation stainless steel pipe with heat dissipation function |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN220470963U (en) |
-
2023
- 2023-07-20 CN CN202321906759.7U patent/CN220470963U/en active Active
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| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |