CN105014844B - Annular film cooler - Google Patents

Annular film cooler Download PDF

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Publication number
CN105014844B
CN105014844B CN201510375860.8A CN201510375860A CN105014844B CN 105014844 B CN105014844 B CN 105014844B CN 201510375860 A CN201510375860 A CN 201510375860A CN 105014844 B CN105014844 B CN 105014844B
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CN
China
Prior art keywords
fuselage
hanger bracket
film
rotating shaft
temperature inductor
Prior art date
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Application number
CN201510375860.8A
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Chinese (zh)
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CN105014844A (en
Inventor
吕晓刚
吴喜林
王磊
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.)
Wuhu Jituo Rubber Technologies Co Ltd
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Wuhu Jituo Rubber Technologies Co Ltd
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Priority to CN201510375860.8A priority Critical patent/CN105014844B/en
Publication of CN105014844A publication Critical patent/CN105014844A/en
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Publication of CN105014844B publication Critical patent/CN105014844B/en
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Abstract

The present invention provides a kind of annular film cooler, including fuselage, the fuselage interior is provided with hanger bracket, the hanger bracket is in the oval setting of fuselage interior, the hanger bracket both sides are provided with fan, charging aperture is provided with the left of the fuselage, discharging opening is provided with the right side of the fuselage, temperature inductor is provided with the discharging opening, the hanger bracket is provided at both ends with rolling rotating shaft, film is driven to be moved on hanger bracket by rolling rotating shaft, the temperature inductor is electrically connected with rolling rotating shaft, and the work for rolling rotating shaft is controlled by temperature inductor.Pass through the elliptic design of hanger bracket, reduce the floor space of hanger bracket, and due to there is provided fan and temperature inductor, lifting film cooling effectiveness, jet shower nozzle is set, to being blown between hanger bracket, increase the contact area of film and cold air, accelerate film cooling, and length-measuring appliance is set, film length is measured, is easy to record, improves operating efficiency.

Description

Annular film cooler
Technical field
The present invention relates to rubber manufacturing field, more particularly to a kind of annular film cooler for being used to cool down film for rubber.
Background technology
In rubber manufacturing field, chemical reaction can be produced when being manufactured due to rubber, and film for rubber shaping is to pass through Hot briquetting, it is to carry certain temperature that rear film, which is made, in film for rubber, it is therefore desirable to carries out cooling processing to film for rubber. Current film cooler is hung typically by hanger bracket to film, makes its natural cooling, but due to hanger bracket It is typically conplane to set, and floor space is big and length limited, the length that film does not have abundance in cooling are put Put, cooling effectiveness is low.Therefore, solve the problems, such as that film cooler floor space is big and cooling effectiveness is low to be just particularly important .
The content of the invention
It is an object of the invention to provide a kind of annular film cooler for being used to cool down film for rubber, pass through the ellipse of hanger bracket Circular design, reduce the floor space of hanger bracket, and due to there is provided fan and temperature inductor, making film cooling effectiveness Lifting, solves the problems, such as that film cooler floor space is big and cooling effectiveness is low.
The present invention provides a kind of annular film cooler, including fuselage, and the fuselage interior is provided with hanger bracket, described outstanding For hanger in the oval setting of fuselage interior, the hanger bracket both sides are provided with fan, and charging aperture is provided with the left of the fuselage, Discharging opening is provided with the right side of the fuselage, temperature inductor is provided with the discharging opening, the hanger bracket is provided at both ends with rolling Turn axle, film is driven to be moved on hanger bracket by rolling rotating shaft, the temperature inductor electrically connects with rolling rotating shaft, passes through Temperature inductor control rolls the work of rotating shaft.
Further improvement is that:The body upper is provided with jet shower nozzle, and the fuselage upper end is open, passes through spray Gas blowout head carries out jet cooling to fuselage interior.
Further improvement is that:Length-measuring appliance is provided with the charging aperture, by length-measuring appliance to entering The film of fuselage interior carries out linear measure longimetry.
Further improvement is that:Staircase is provided with the fuselage left end face, operator is by staircase up on fuselage Observed in portion.
Beneficial effects of the present invention:By the elliptic design of hanger bracket, reduce the floor space of hanger bracket, and by In there is provided fan and temperature inductor, film cooling effectiveness is lifted, jet shower nozzle is set, to being blown between hanger bracket Gas, increase the contact area of film and cold air, accelerate film cooling, and length-measuring appliance is set, film length is entered Row measurement, is easy to record, and improves operating efficiency.
Brief description of the drawings
Fig. 1 is the structural representation of the present invention.
Fig. 2 is the fuselage top view of the present invention.
Wherein:1- fuselages, 2- hanger brackets, 3- fans, 4- charging apertures, 5- discharging openings, 6- temperature inductors, 7-, which is rolled, to be turned Axle, 8- jet shower nozzles, 9- length-measuring appliances, 10- staircases.
Embodiment
In order to deepen the understanding of the present invention, below in conjunction with embodiment, the invention will be further described, the embodiment It is only used for explaining the present invention, is not intended to limit the scope of the present invention..
As shown in Figure 1, 2, the present embodiment provides a kind of annular film cooler, including fuselage 1, is set inside the fuselage 1 Hanger bracket 2 is equipped with, the hanger bracket 2 oval setting inside fuselage 1, the both sides of hanger bracket 2 are provided with fan 3, institute State the left side of fuselage 1 and be provided with charging aperture 4, the right side of fuselage 1 is provided with discharging opening 5, temperature sense is provided with the discharging opening 5 Device 6 is answered, the hanger bracket 2, which is provided at both ends with, rolls rotating shaft 7, drives film to be moved on hanger bracket 2 by rolling rotating shaft 7, institute State temperature inductor 6 and electrically connected with rolling rotating shaft 7, the work for rolling rotating shaft 7 is controlled by temperature inductor 6.On the fuselage 1 Side is provided with jet shower nozzle 8, and the upper end of fuselage 1 is open, and jet cooling is carried out to the inside of fuselage 1 by jet shower nozzle 8. Length-measuring appliance 9 is provided with the charging aperture 4, is grown by length-measuring appliance 9 to entering the film inside fuselage 1 Degree measurement.Staircase 10 is provided with the left end face of fuselage 1, operator is observed by the up to top of fuselage 1 of staircase 10. By the elliptic design of hanger bracket 2, reduce the floor space of hanger bracket 2, and because there is provided fan 3 and temperature sense Device 6, film cooling effectiveness is lifted, jet shower nozzle 8 is set, to being blown between hanger bracket 2, increase film and cold air Contact area, accelerate film cooling, and length-measuring appliance 9 is set, film length is measured, is easy to record, improve Operating efficiency.

Claims (2)

1. a kind of annular film cooler, including fuselage(1), the fuselage(1)It is internally provided with hanger bracket(2), its feature exists In:The hanger bracket(2)In fuselage(1)Internal oval setting, the hanger bracket(2)Both sides are provided with fan(3), it is described Fuselage(1)Left side is provided with charging aperture(4), the fuselage(1)Right side is provided with discharging opening(5), the discharging opening(5)Upper setting There is temperature inductor(6), the hanger bracket(2)It is provided at both ends with rolling rotating shaft(7), by rolling rotating shaft(7)Film is driven to exist Hanger bracket(2)Upper movement, the temperature inductor(6)With rolling rotating shaft(7)Electrically connect, pass through temperature inductor(6)Control rolling Turn axle(7)Work, the fuselage(1)Top is provided with jet shower nozzle(8), the fuselage(1)Upper end is open, is passed through Jet shower nozzle(8)To fuselage(1)Inside carries out jet cooling, the charging aperture(4)On be provided with length-measuring appliance(9), lead to Cross length-measuring appliance(9)To into fuselage(1)Internal film carries out linear measure longimetry.
2. annular film cooler as claimed in claim 1, it is characterised in that:The fuselage(1)It is provided with left end face Staircase(10), operator passes through staircase(10)Up to fuselage(1)Observed on top.
CN201510375860.8A 2015-06-27 2015-06-27 Annular film cooler Active CN105014844B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201510375860.8A CN105014844B (en) 2015-06-27 2015-06-27 Annular film cooler

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201510375860.8A CN105014844B (en) 2015-06-27 2015-06-27 Annular film cooler

Publications (2)

Publication Number Publication Date
CN105014844A CN105014844A (en) 2015-11-04
CN105014844B true CN105014844B (en) 2017-12-01

Family

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Family Applications (1)

Application Number Title Priority Date Filing Date
CN201510375860.8A Active CN105014844B (en) 2015-06-27 2015-06-27 Annular film cooler

Country Status (1)

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CN (1) CN105014844B (en)

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN2298121Y (en) * 1997-07-21 1998-11-25 天津市橡塑机械联合有限公司 Film cooling machine
CN201002323Y (en) * 2006-08-17 2008-01-09 徐银虎 Stepping pushing mechanism in film cooling device
CN103802010A (en) * 2012-11-08 2014-05-21 史树元 Efficient energy-saving grinding machine
CN203805203U (en) * 2014-04-17 2014-09-03 中国化学工业桂林工程有限公司 Rapid temperature decreasing system of hot rubber sheet

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE20103680U1 (en) * 2001-02-26 2001-05-23 Berstorff Gmbh Cooling system for cooling rubber sheets

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN2298121Y (en) * 1997-07-21 1998-11-25 天津市橡塑机械联合有限公司 Film cooling machine
CN201002323Y (en) * 2006-08-17 2008-01-09 徐银虎 Stepping pushing mechanism in film cooling device
CN103802010A (en) * 2012-11-08 2014-05-21 史树元 Efficient energy-saving grinding machine
CN203805203U (en) * 2014-04-17 2014-09-03 中国化学工业桂林工程有限公司 Rapid temperature decreasing system of hot rubber sheet

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C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant
PE01 Entry into force of the registration of the contract for pledge of patent right

Denomination of invention: Annular rubber-sheet cooling machine

Effective date of registration: 20190710

Granted publication date: 20171201

Pledgee: Wuhu Yangzi rural commercial bank Limited by Share Ltd.

Pledgor: WUHU JITUO RUBBER TECHNOLOGIES Co.,Ltd.

Registration number: 2019340000383

PE01 Entry into force of the registration of the contract for pledge of patent right
PC01 Cancellation of the registration of the contract for pledge of patent right

Date of cancellation: 20230620

Granted publication date: 20171201

Pledgee: Wuhu Yangzi rural commercial bank Limited by Share Ltd.

Pledgor: WUHU JITUO RUBBER TECHNOLOGIES Co.,Ltd.

Registration number: 2019340000383

PC01 Cancellation of the registration of the contract for pledge of patent right