CN205156710U - Interior foreign minister's wing needle recuperator heat exchange tube - Google Patents

Interior foreign minister's wing needle recuperator heat exchange tube Download PDF

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Publication number
CN205156710U
CN205156710U CN201520956630.6U CN201520956630U CN205156710U CN 205156710 U CN205156710 U CN 205156710U CN 201520956630 U CN201520956630 U CN 201520956630U CN 205156710 U CN205156710 U CN 205156710U
Authority
CN
China
Prior art keywords
foreign minister
wing needle
needle recuperator
recuperator heat
heat exchanger
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.)
Expired - Fee Related
Application number
CN201520956630.6U
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Chinese (zh)
Inventor
李军凯
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
DALIAN MELAD TECHNOLOGY Co Ltd
Original Assignee
DALIAN MELAD TECHNOLOGY Co Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by DALIAN MELAD TECHNOLOGY Co Ltd filed Critical DALIAN MELAD TECHNOLOGY Co Ltd
Priority to CN201520956630.6U priority Critical patent/CN205156710U/en
Application granted granted Critical
Publication of CN205156710U publication Critical patent/CN205156710U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The utility model provides an interior foreign minister's wing needle recuperator heat exchange tube, include: a plurality of fins (2) of body (1) and body outer wall, its characterized in that, body (1) inner wall be along radially setting up a plurality of inner fins (3), the cross -section of inner fin (3) is the cylindricality. The utility model discloses an interior foreign minister's wing needle recuperator heat exchange tube greatly increased internal and external surface heat transfer area increases intraductal fluidic reynolds number and turbulence scale, is showing and is improving heat exchange coefficient.

Description

Interior foreign minister's wing needle recuperator heat exchanger tube
Technical field
The utility model relates to technical field of heat exchangers, particularly relates to a kind of interior foreign minister's wing needle recuperator heat exchanger tube.
Background technology
In prior art, application number 201120168646.2, utility model title " a kind of fin heat exchange pipe ", provides the heat exchanger tube that a kind of inboard wall of tube body sets up rack structure, increases the heat exchange area of traditional smooth inboard wall of tube body to a certain extent; But, physical arrangement in pipe is also increased for the rack structure under material same levels pressure piping of the same race and pressure reduction conditions, makes heat exchanging medium flow quantitative change few, very little for the contribution margin increasing the coefficient of heat transfer; Therefore, how to increase the coefficient of heat transfer, increasing the turbulivity of inner surface heat exchange area and increase tube fluid, is problem demanding prompt solution.
Utility model content
The utility model mainly solves and ensures how heat transferring medium in body increases the technical problem of the heat exchange area of inboard wall of tube body under the condition of certain flow, pressure and allowable pressure drop, propose a kind of in foreign minister's wing needle recuperator heat exchanger tube.
In order to achieve the above object, interior foreign minister's wing needle recuperator heat exchanger tube that the utility model provides, comprising: some fins 2 of body 1 and tube wall, is characterized in that, body 1 inwall is disposed radially some inner fins 3, and the cross section of described inner fin 3 is cylindricality.
Preferably, the height of described inner fin 3 and the ratio of body 1 internal diameter are: 1:2 to 30.
Preferably, the height of described inner fin 3 and the ratio of body 1 internal diameter are: 1:4 or 8.
Preferably, the height of described inner fin 3 is consistent.
Preferably, adjacent inner fins 3 is staggered in height.
Preferably, the aspect ratio of adjacent inner fins 3 is: 1:0.1 to 5.
Preferably, the aspect ratio of adjacent inner fins 3 is: 1:2.
Preferably, the root of adjacent inner fins 3 connects with arcuate structure.
Preferably, connector 4 is set at interval of on the fin 2 of 22.5 degree, 30 degree, 45 degree or 90 degree.
Preferably, described connector 4 is spherical or Polygonal column shape.
Beneficial effect: interior foreign minister's wing needle recuperator heat exchanger tube of the present utility model increases surfaces externally and internally heat exchange area greatly, increases Reynolds number and the turbulivity of tube fluid, significantly improves the coefficient of heat transfer 10 to 30%.
Accompanying drawing explanation
Fig. 1 for the utility model embodiment 1 provide in foreign minister's wing needle recuperator heat exchange tube structure figure.
Fig. 2 for the utility model embodiment 1 provide in the tubular body structure chart of foreign minister's wing needle recuperator heat exchanger tube.
Fig. 3 for the utility model embodiment 1 provide in the connector structure chart of foreign minister's wing needle recuperator heat exchanger tube.
Fig. 4 for the utility model embodiment 2 provide in foreign minister's wing needle recuperator heat exchange tube structure figure.
Fig. 5 for the utility model embodiment 2 provide in the tubular body structure chart of foreign minister's wing needle recuperator heat exchanger tube.
Fig. 6 for the utility model embodiment 2 provide in the connector structure chart of foreign minister's wing needle recuperator heat exchanger tube.
Detailed description of the invention
Embodiment 1: foreign minister's wing needle recuperator heat exchanger tube in a kind of, comprise: 16 (2 to 20 integer sheet) sheet fin 2 of body 1 and tube wall, body 1 inwall is disposed radially 16 (2 to 20 integer sheet) inner fin 3, and the cross section of described inner fin 3 is cylindricality; The height of described inner fin 3 and the ratio of body 1 internal diameter are: 1:4 or 8.The height of described inner fin 3 is consistent, and the root of adjacent inner fins 3 connects with arcuate structure; Fin 2 at interval of 90 degree (45 degree, 30 degree or 22.5 degree) arranges spherical connector 4.Extruded by aluminum section extruder.
Embodiment 2: one seed wing needle recuperator, comprise: 16 (2 to 20 integer sheet) sheet fin 2 of body 1 and tube wall, body 1 inwall is disposed radially 16 (2 to 20 integer sheet) inner fin 3, and the cross section of described inner fin 3 is cylindricality; Adjacent inner fins 3 is staggered in height; The aspect ratio of adjacent inner fins 3 is: 1:2, and the height of described inner fin 3 and the ratio of body 1 internal diameter are: 1:4 or 8, maximum increase intraductal heat exchange area and Reynolds number.Fin 2 at interval of 90 degree (45 degree, 30 degree or 22.5 degree) arranges Polygonal column shape connector 4.Extruded by aluminum section extruder.

Claims (10)

1. foreign minister's wing needle recuperator heat exchanger tube in a kind, comprise: some fins (2) of body (1) and tube wall, it is characterized in that, body (1) inwall is disposed radially some inner fins (3), and the cross section of described inner fin (3) is cylindricality.
2. interior foreign minister's wing needle recuperator heat exchanger tube according to claim 1, is characterized in that, the height of described inner fin (3) and the ratio of body (1) internal diameter are: 1:2 to 30.
3. interior foreign minister's wing needle recuperator heat exchanger tube according to claim 2, is characterized in that, the height of described inner fin (3) and the ratio of body (1) internal diameter are: 1:4 or 8.
4. in any one according to claims 1 to 3, foreign minister's wing needle recuperator heat exchanger tube, is characterized in that, the height of described inner fin (3) is consistent.
5. in any one according to claims 1 to 3, foreign minister's wing needle recuperator heat exchanger tube, is characterized in that, adjacent inner fins (3) is staggered in height.
6. interior foreign minister's wing needle recuperator heat exchanger tube according to claim 5, it is characterized in that, the aspect ratio of adjacent inner fins (3) is: 1:0.1 to 5.
7. interior foreign minister's wing needle recuperator heat exchanger tube according to claim 6, it is characterized in that, the aspect ratio of adjacent inner fins (3) is: 1:2.
8. in any one according to claims 1 to 3, foreign minister's wing needle recuperator heat exchanger tube, is characterized in that, the root of adjacent inner fins (3) connects with arcuate structure.
9. in any one according to claims 1 to 3, foreign minister's wing needle recuperator heat exchanger tube, is characterized in that, arranges connector (4) at interval of on the fin (2) of 22.5 degree, 30 degree, 45 degree or 90 degree.
10. interior foreign minister's wing needle recuperator heat exchanger tube according to claim 9, it is characterized in that, described connector (4) is spherical or Polygonal column shape.
CN201520956630.6U 2015-11-26 2015-11-26 Interior foreign minister's wing needle recuperator heat exchange tube Expired - Fee Related CN205156710U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201520956630.6U CN205156710U (en) 2015-11-26 2015-11-26 Interior foreign minister's wing needle recuperator heat exchange tube

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201520956630.6U CN205156710U (en) 2015-11-26 2015-11-26 Interior foreign minister's wing needle recuperator heat exchange tube

Publications (1)

Publication Number Publication Date
CN205156710U true CN205156710U (en) 2016-04-13

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Family Applications (1)

Application Number Title Priority Date Filing Date
CN201520956630.6U Expired - Fee Related CN205156710U (en) 2015-11-26 2015-11-26 Interior foreign minister's wing needle recuperator heat exchange tube

Country Status (1)

Country Link
CN (1) CN205156710U (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105277033A (en) * 2015-11-26 2016-01-27 大连美莱达科技有限公司 Inner and outer long finned heat exchange pipe of heat exchanger
CN110260704A (en) * 2019-05-24 2019-09-20 浙江中达特钢股份有限公司 A kind of New-type boiler heat exchanger seamless pipe

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105277033A (en) * 2015-11-26 2016-01-27 大连美莱达科技有限公司 Inner and outer long finned heat exchange pipe of heat exchanger
CN110260704A (en) * 2019-05-24 2019-09-20 浙江中达特钢股份有限公司 A kind of New-type boiler heat exchanger seamless pipe

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GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20160413