CN208651840U - A kind of stainless steel for aviation steel pipe with heat sinking function - Google Patents
A kind of stainless steel for aviation steel pipe with heat sinking function Download PDFInfo
- Publication number
- CN208651840U CN208651840U CN201821396742.0U CN201821396742U CN208651840U CN 208651840 U CN208651840 U CN 208651840U CN 201821396742 U CN201821396742 U CN 201821396742U CN 208651840 U CN208651840 U CN 208651840U
- Authority
- CN
- China
- Prior art keywords
- steel pipe
- stainless
- heat dissipation
- steel
- inner chamber
- 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.)
- Active
Links
Abstract
The utility model discloses a kind of stainless steel for aviation steel pipe with heat sinking function, including stainless-steel pipe ontology and heat dissipation tank, stainless-steel pipe body interior is equipped with second inner chamber, second inner chamber one end is equipped with first inner chamber, first inner chamber inner wall is equipped with internal screw thread, the utility model is by being respectively arranged with external screw thread and internal screw thread to steel pipe both ends, direction can be replaced according to mounting means, convenient for preferably connecting equipment, and stainless steel steel pipe body itself has water pipe ditch, heat dissipation pipe can be penetrated in water pipe ditch, cold water is connected with inside heat dissipation pipe, it is quickly reduced convenient for steel duct temperature, improve heat dissipation effect, and heat dissipation tank is installed on stainless-steel pipe ontology, thermal effect is considerably increased by placing ice cube, on the one hand ice melting water can continue to cool down steel pipe, on the other hand it can be discharged out It is utilized again by other equipment, accomplishes energy conservation and environmental protection.
Description
Technical field
The utility model relates to a kind of stainless-steel pipe, in particular to a kind of stainless steel for aviation steel with heat sinking function
Pipe, belongs to air equipment technical field.
Background technique
Stainless-steel pipe is a kind of hollow strip circular steel, is widely used mainly in petroleum, chemical industry, medical treatment, food, light
The industrial transportation pipe lines such as work, machinery instrument and machine structural parts etc., in addition, when bending, torsional strength are identical, weight compared with
Gently, so being also widely used in manufacture machine components and engineering structure, furniture kitchen tools etc. is also commonly used for, air equipment is used
Stainless-steel pipe needs to have certain function, and the stainless-steel pipe that existing aviation uses does not have good heat sinking function,
For the fuel tank oil pipe used as air equipment and tracheae etc., certain heat can be all generated in use process, and it is traditional
Stainless-steel pipe be far from reaching good heat dissipation effect, even if there is certain heat sinking function, heat dissipation effect is very poor, and
And connection type is very single.
Utility model content
The utility model provides a kind of stainless steel for aviation steel pipe with heat sinking function, and the utility model passes through to steel pipe
Both ends are respectively arranged with external screw thread and internal screw thread, can replace direction according to mounting means, convenient for preferably connecting equipment, without
Steel steel pipe body itself of becoming rusty has water pipe ditch, heat dissipation pipe can be penetrated in water pipe ditch, cold water is connected with inside heat dissipation pipe, just
It is quickly reduced in steel duct temperature, heat dissipation effect is improved, and heat dissipation tank is installed on stainless-steel pipe ontology, by putting
It sets ice cube and considerably increases thermal effect, on the one hand ice melting water can continue to cool down steel pipe, on the other hand may be used
It is utilized again by other equipment with being discharged, accomplishes energy conservation and environmental protection.
In order to solve the above-mentioned technical problem, the utility model provides the following technical solution:
A kind of stainless steel for aviation steel pipe with heat sinking function of the utility model, including stainless-steel pipe ontology and heat dissipation
Case, the stainless-steel pipe body interior are equipped with second inner chamber, and described second inner chamber one end is equipped with first inner chamber, in described first
Cavity wall is fixedly connected with connection equipped with internal screw thread, the second inner chamber other end and positioned at stainless-steel pipe outer body
Pipe, the connection pipe surface are equipped with external screw thread, and the stainless-steel pipe ontology upper and lower surface is equipped with multiple water pipe ditchs, stainless steel
Steel pipe body upper and lower surface is equipped with the heat dissipation pipe being arranged between multiple water pipe ditchs, described this body surface of stainless-steel pipe
Face is fixed with multiple heat dissipation tanks, and heat dissipation tank upper end internal slide is connected with slip lid, below the slip lid and is located at heat dissipation
The inside of case is equipped with upper radiating groove and lower radiating groove, is fixedly connected with a pair of of partition between the upper radiating groove and lower radiating groove,
Multiple ice cubes are equipped with inside the upper radiating groove, the heat dissipation tank lowermost end is threaded with valve, and the valve is located at lower dissipate
One end inside heat channel is fixedly connected with block, and the valve surface is equipped with threaded line.
As a kind of optimal technical scheme of the utility model, the first inner chamber and second inner chamber intersection are equipped with first
Sealing ring, the connecting tube are cased with the second sealing ring close to the end surface of stainless-steel pipe ontology.
As a kind of optimal technical scheme of the utility model, the heat dissipation tank, which is internally located at slip lid, is equipped with sliding slot, and
The sliding slot is communicated with upper radiating groove.
As a kind of optimal technical scheme of the utility model, the diaphragm internal is equipped with multiple through-holes.
As a kind of optimal technical scheme of the utility model, the end surface that the valve is located in lower radiating groove is cased with
Third sealing ring.
The utility model beneficial effect achieved is: the utility model provides a kind of aviation with heat sinking function with not
Become rusty steel steel pipe, and internal structure design is reasonable, can be according to peace by being respectively arranged with external screw thread and internal screw thread to steel pipe both ends
Dress mode replaces direction, and convenient for preferably connecting equipment, and stainless steel steel pipe body itself has water pipe ditch, can be by water of radiation
Pipe penetrates in water pipe ditch, and cold water is connected with inside heat dissipation pipe, quickly reduces convenient for steel duct temperature, improves heat dissipation effect, and
And heat dissipation tank is installed on stainless-steel pipe ontology, thermal effect, ice melting water are considerably increased by placing ice cube
On the one hand it can continue to cool down steel pipe, on the other hand can be discharged and be utilized again by other equipment, accomplish to save
It can environmental protection.
Detailed description of the invention
Attached drawing is used to provide a further understanding of the present invention, and constitutes part of specification, practical with this
Novel embodiment is used to explain the utility model together, does not constitute limitations of the present invention.In the accompanying drawings:
Fig. 1 is the positive structure schematic of the utility model；
Fig. 2 is the heat dissipation tank schematic diagram of internal structure of the utility model.
In figure: 1, stainless-steel pipe ontology；2, first inner chamber；3, internal screw thread；4, the first sealing ring；5, second inner chamber；6,
Heat dissipation pipe；7, water pipe ditch；8, heat dissipation tank；9, slip lid；10, valve；11, the second sealing ring；12, connecting tube；13, external screw thread；
14, sliding slot；15, ice cube；16, upper radiating groove；17, through-hole；18, partition；19, lower radiating groove；20, block；21, third seals
Circle；22, threaded line.
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.
Embodiment: as shown in Figs. 1-2, a kind of stainless steel for aviation steel pipe with heat sinking function of the utility model, including
Stainless-steel pipe ontology 1 and heat dissipation tank 8, are equipped with second inner chamber 5 inside stainless-steel pipe ontology 1, and 5 one end of second inner chamber is equipped with the
One inner cavity 2,2 inner wall of first inner chamber are equipped with internal screw thread 3,5 other end of second inner chamber and solid on the outside of stainless-steel pipe ontology 1
Surely it is connected with connecting tube 12,12 surface of connecting tube is equipped with external screw thread 13, and 1 upper and lower surface of stainless-steel pipe ontology is equipped with multiple water
Tube seat 7,1 upper and lower surface of stainless-steel pipe ontology is equipped with the heat dissipation pipe 6 being arranged between multiple water pipe ditchs 7, stainless
1 surface of steel steel pipe body is fixed with multiple heat dissipation tanks 8, and 8 upper end internal slide of heat dissipation tank is connected with slip lid 9,9 lower section of slip lid and
It is equipped with upper radiating groove 16 and lower radiating groove 19 positioned at the inside of heat dissipation tank 8, it is fixed between upper radiating groove 16 and lower radiating groove 19 to connect
It is connected to a pair of of partition 18, is equipped with multiple ice cubes 15 inside upper radiating groove 16,8 lowermost end of heat dissipation tank is threaded with valve 10, valve
One end that door 10 is located inside lower radiating groove 19 is fixedly connected with block 20, and 10 surface of valve is equipped with threaded line 22.
First inner chamber 2 and 5 intersection of second inner chamber are equipped with the first sealing ring 4, and connecting tube 12 is close to stainless-steel pipe ontology 1
End surface be cased with the second sealing ring 11, convenient for preferably connection stainless-steel pipe ontology 1, avoid revealing, inside heat dissipation tank 8
Sliding slot 14 is equipped at slip lid 9, and sliding slot 14 is communicated with upper radiating groove 16, and ice cube 15 is avoided to fall, and is equipped with inside partition 18
Multiple through-holes 17, convenient for being utilized again in the lower radiating groove 19 of ice water inflow of thawing, valve 10 is located in lower radiating groove 19
End surface is cased with third sealing ring 21, and ice water after tightening valve 10 is avoided to still flow out.
Specifically, when the utility model is used, entire stainless-steel pipe ontology 1 is pacified by internal screw thread 3 and external screw thread 13
On air equipment, heat dissipation pipe 6 is penetrated in water pipe ditch 7, then the certain cold water of circulation in heat dissipation pipe 6 is opened and slided
Lid 9 up puts into a certain amount of ice cube 15 in radiating groove 16, at the same time, valve 10 is tight condition, uses certain time
Afterwards, ice cube 15 melts, and ice water can finally be led to by that can continue to be utilized to cool down in the lower radiating groove 19 of the inflow of through-hole 17
Crossing release valve 10 will have the water liquid of certain temperature to flow out from heat dissipation tank 8, is then further continued for repeating the above process and
Realize that stainless-steel pipe ontology 1 cools down.
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 (5)
1. a kind of stainless steel for aviation steel pipe with heat sinking function, including stainless-steel pipe ontology (1) and heat dissipation tank (8),
It is characterized in that, be equipped with second inner chamber (5) inside the stainless-steel pipe ontology (1), described second inner chamber (5) one end is equipped with first
Inner cavity (2), first inner chamber (2) inner wall is equipped with internal screw thread (3), second inner chamber (5) other end and positioned at stainless steel
It is fixedly connected with connecting tube (12) on the outside of steel pipe body (1), connecting tube (12) surface is equipped with external screw thread (13), described stainless
Steel steel pipe body (1) upper and lower surface is equipped with multiple water pipe ditchs (7), and stainless-steel pipe ontology (1) upper and lower surface is equipped with
A piece heat dissipation pipe (6) being arranged between multiple water pipe ditchs (7), stainless-steel pipe ontology (1) surface are fixed with more
A heat dissipation tank (8), heat dissipation tank (8) upper end internal slide are connected with slip lid (9), below the slip lid (9) and are located at heat dissipation
The inside of case (8) is equipped with upper radiating groove (16) and lower radiating groove (19), between the upper radiating groove (16) and lower radiating groove (19)
It is fixedly connected with a pair of of partition (18), is equipped with multiple ice cubes (15) inside the upper radiating groove (16), heat dissipation tank (8) the most bottom
End is threaded with valve (10), and the valve (10) is located at the internal one end of lower radiating groove (19) and is fixedly connected with block
(20), valve (10) surface is equipped with threaded line (22).
2. a kind of stainless steel for aviation steel pipe with heat sinking function according to claim 1, which is characterized in that described
One inner cavity (2) and second inner chamber (5) intersection are equipped with the first sealing ring (4), and the connecting tube (12) is close to stainless-steel pipe sheet
The end surface of body (1) is cased with the second sealing ring (11).
3. a kind of stainless steel for aviation steel pipe with heat sinking function according to claim 1, which is characterized in that described to dissipate
Hot tank (8) is internally located at slip lid (9) and is equipped with sliding slot (14), and the sliding slot (14) is communicated with upper radiating groove (16).
4. a kind of stainless steel for aviation steel pipe with heat sinking function according to claim 1, which is characterized in that it is described every
Multiple through-holes (17) are equipped with inside plate (18).
5. a kind of stainless steel for aviation steel pipe with heat sinking function according to claim 1, which is characterized in that the valve
The end surface that door (10) is located in lower radiating groove (19) is cased with third sealing ring (21).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821396742.0U CN208651840U (en) | 2018-08-29 | 2018-08-29 | A kind of stainless steel for aviation steel pipe with heat sinking function |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821396742.0U CN208651840U (en) | 2018-08-29 | 2018-08-29 | A kind of stainless steel for aviation steel pipe with heat sinking function |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208651840U true CN208651840U (en) | 2019-03-26 |
Family
ID=65791906
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821396742.0U Active CN208651840U (en) | 2018-08-29 | 2018-08-29 | A kind of stainless steel for aviation steel pipe with heat sinking function |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208651840U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111996569A (en) * | 2020-07-31 | 2020-11-27 | 常州费曼生物科技有限公司 | Reaction tank heat dissipation method in preparation process of anodized aluminum porous infusion filter membrane |
-
2018
- 2018-08-29 CN CN201821396742.0U patent/CN208651840U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111996569A (en) * | 2020-07-31 | 2020-11-27 | 常州费曼生物科技有限公司 | Reaction tank heat dissipation method in preparation process of anodized aluminum porous infusion filter membrane |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN208651840U (en) | A kind of stainless steel for aviation steel pipe with heat sinking function | |
| CN206308444U (en) | A kind of single crystal growing furnace and its water-cooled component | |
| CN111946929A (en) | Environmental protection equipment pipeline heating device | |
| CN204176251U (en) | A kind of novel combined type multilayer valve body lagging casing | |
| CN205079044U (en) | Heat preservation liquified gas storage tank of crashproof | |
| CN204594279U (en) | A kind of specific hot heat exchange insulating case | |
| CN203772491U (en) | Pressure test tool for heat exchanger | |
| CN204164525U (en) | The snakelike cooling by water pipe of high-efficiency water-saving | |
| CN209500823U (en) | A kind of distillation still Heat preservation structure | |
| CN209085053U (en) | A kind of Split type air source heat pump unit of anti-freeze type | |
| CN208268436U (en) | A kind of top-pulling type low temperature adjusting angle valve | |
| CN206771668U (en) | A kind of water tank for being used to freeze unit | |
| CN203163582U (en) | Improved tube type heat exchanger tube box | |
| CN219111548U (en) | Heating insulation structure of coating stirring kettle | |
| CN203869340U (en) | Compact-type solar water heater | |
| CN216409852U (en) | Low-temperature heat recycling device for preparing olefin from methanol | |
| CN104061695B (en) | One is superthermal leads the two inner bag solar engineering double-row heat collector of U-tube | |
| CN210123253U (en) | High-efficient pot-type heat exchanger | |
| CN210830981U (en) | Energy-saving device for oil field gathering and transportation pipeline | |
| CN204188031U (en) | A kind of cisten mechanism of heat-exchanging water tank | |
| CN219827854U (en) | Radiator temperature control valve regulating valve | |
| CN204100629U (en) | The bearing water tank of built-in heavy caliber band fin heat exchange pipe | |
| CN206929492U (en) | A kind of high temperature resistant is not easy the PPR pipe of deformation | |
| CN208457371U (en) | A kind of insulating tube | |
| CN209681379U (en) | A kind of quick assembled multifunctional crosses tin furnace smelting tool |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |