CN101740144B - Magnetic steel heat-insulating shield and manufacturing method thereof - Google Patents
Magnetic steel heat-insulating shield and manufacturing method thereof Download PDFInfo
- Publication number
- CN101740144B CN101740144B CN2009102419131A CN200910241913A CN101740144B CN 101740144 B CN101740144 B CN 101740144B CN 2009102419131 A CN2009102419131 A CN 2009102419131A CN 200910241913 A CN200910241913 A CN 200910241913A CN 101740144 B CN101740144 B CN 101740144B
- Authority
- CN
- China
- Prior art keywords
- heat
- insulating
- magnetic steel
- layer
- insulating shield
- 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
Links
Images
Landscapes
- Shielding Devices Or Components To Electric Or Magnetic Fields (AREA)
Abstract
The invention relates to a magnetic steel heat-insulating shield and a manufacturing method thereof, belonging to the technical field of magnetic steel protection. The shield comprises an upper shield (1) and a mounting bottom plate (2), wherein the mounting bottom plate (2) is provided with two mounting holes (3), and the upper shield (1) comprises three heat-insulating layers including an aviatic heat-insulating dope layer (4), a glass reinforced plastic heat-insulating layer (5) and an asbestos heat-insulating layer (6). In the manufacturing method, a mold for the magnetic steel heat-insulating shield is manufactured according to the volume and the contour of magnetic steel, asbestos casing is packed at the outer layer of the mold, and resin, talcum powder and spun yarn which are mixed by the ratio of 3:2:1 are evenly coated to the surface of the asbestos for 3-5mm, and are naturally dried or died by an oven; and finally, the aviatic heat-insulating dope is evenly coated at the outermost layer for 1-2 mm. The invention has the advantage that the working temperature of the magnetic steel is controlled to be below 65 DEG C, and completely reaches the working temperature required by the magnetic steel, thereby the microwave radio-frequency recognition technology can be used in an iron cased following system of a steel company.
Description
Technical field
The invention belongs to magnet steel guard technology field, particularly relate to a kind of magnetic steel heat-insulating shield and manufacture method thereof, be not subjected to the heat-insulating shield of extraneous thermal effect when making communication products work.
Background technology
Adopt the microwave radio recognition technology, realize that the application of logistics management on railway supplyline is ripe, but in iron and steel enterprise,, make this The Application of Technology be restricted because communication products are subjected to iron bag Temperature Influence.Reason is that the communication products (magnet steel and antenna) of iron packet tracing need to be installed on track and the sleeper respectively, because the surface temperature of ladle reaches more than 130 degrees centigrade, cause the magnet steel that is installed on track and the sleeper and antenna (70 degrees centigrade of the working temperature upper limits) at the iron bag through out-of-date because of being subjected to Temperature Influence cisco unity malfunction even damage.
Summary of the invention
The object of the present invention is to provide a kind of magnetic steel heat-insulating shield and manufacture method thereof, solved the working environment problem of magnet steel, make magnet steel under its protection, not be subjected to Temperature Influence and work that can normal reliable.And then the reliable application of realization microwave radio recognition technology in iron packet tracing system of iron and steel enterprise.
Originally give out a contract for a project and draw together cover (or antenna heat-insulating shield), installation base plate, base plate is processed with 2 rectangle mounting holes, and the adjusting when conveniently magnet steel being installed is with fixing.
The cover of going up of the present invention is made up of three thermofins, comprises aviation insulating moulding coating layer, frp layer, asbestos layer.
Of the present invention to go up the cover innermost layer be asbestos, because it is soft relatively, its processing in the innermost layer, in heat insulation, bumped the mill of magnet steel and played buffer action through out-of-date vibrations and middle layer housing to magnet steel the iron hired car.
Upward cover of the present invention middle layer is a fiberglass, and the one-tenth of fiberglass is grouped into has selected resin+talcum powder+weak point yarn cutting, makes it when finishing heat-blocking action, also plays effect fire-retardant and increase heat-insulating shield intensity.
Upward cover outermost layer of the present invention is the aviation insulating moulding coating: be used for further strengthening effect of heat insulation, the heat reflectivity of this material heat is 0.85, and the continuous firing temperature is-51 ℃-206 ℃.
The manufacture method of heat-insulating shield of the present invention is: the mould for preparing magnetic steel heat-insulating shield by magnet steel volume and profile, asbestos cover on the outer pad of mould, resin, talcum powder, three kinds of materials of short yarn cutting are mixed in (3: 2: 1) ratio, evenly be applied to asbestos surface 3-5mm, nature or baking box oven dry are evenly coated aviation insulating moulding coating 1-2mm at outermost layer at last.
Effect of the present invention: after using heat-insulating shield of the present invention that the magnet steel that is installed in the track inboard is carried out heat insulation protection, the working temperature of magnet steel is controlled in below 65 degrees centigrade, reached the desired working temperature of magnet steel fully, made the microwave radio recognition technology in iron packet tracing system of iron and steel enterprise, obtain to use.
Description of drawings
Fig. 1 is a structural representation of the present invention.Wherein, cover 1 on, base plate 2 is installed, installs on the base plate and be processed with mounting hole 3, aviation insulating moulding coating layer 4, fiberglass thermofin 5, insulating layer of asbestos 6.In addition, as the magnet steel 7 that also has magnetic steel heat-insulating shield to protect and annex bushing 8 thereof, the communications cable 9.
Fig. 2 is the magnetic steel heat-insulating shield synoptic diagram.Wherein, cover 1 on, base plate 2, mounting hole 3, aviation insulating moulding coating layer 4, fiberglass thermofin 5, insulating layer of asbestos 6 are installed.
Fig. 3 is the magnet steel synoptic diagram.Wherein, magnet steel 7, annex bushing 8, the communications cable 9.
Fig. 4 is an antenna heat-insulating shield structural representation among the embodiment 2 of heat-insulating shield.Wherein, antenna heat-insulating shield 10 is processed into the shape that has internal buckle edge, can be sleeved on easily outside the antenna during use, and the antenna 11, the antenna fixing holder 12 that also have the antenna heat-insulating shield to be protected in addition, antenna fixing holder has fixed orifice 13.
Fig. 5 is an antenna heat-insulating shield synoptic diagram in the variation of heat-insulating shield.
Embodiment
Fig. 1~6 are the specific embodiment of the present invention
As shown in Figure 1.Magnetic steel heat-insulating shield is made up of last cover and installation base plate, is processed with 2 rectangle mounting holes on the base plate, and the adjusting when conveniently magnet steel being installed is with fixing.Heat-insulating shield is made up of aviation insulating moulding coating layer, fiberglass thermofin, three thermofins of insulating layer of asbestos.
Embodiment 1: press magnet steel volume and the profile skilled worker mould with magnetic steel heat-insulating shield, asbestos cover on the outer pad of grinding tool, resin, talcum powder, three kinds of materials of short yarn cutting are mixed (3: 2: 1) by a certain percentage evenly be applied to asbestos surface 3-5mm, nature or baking box oven dry are evenly coated aviation insulating moulding coating 1-2mm at outermost layer at last.During use, with magnetic steel heat-insulating shield with the magnet steel suit, be installed on the rail inboard of appointment in the iron packet tracing system with set bolt and the fixing magnetic steel heat-insulating shield that will be set with magnet steel with annex, the communications cable that the high pressure pillar will be arranged passes under the rail with communication facilities in the case of rail limit and is connected.
Embodiment 2: as the variation of embodiment magnetic steel heat-insulating shield, the mould of heat-insulating shield can be pressed communication products antenna volume and profile processing in the iron packet tracing system, produce the antenna magnetic steel heat-insulating shield, during use the antenna heat-insulating shield is packed into the other end of pusher to antenna from an end of antenna, antenna is all covered, with bolt by antenna fixed mount and fixingly antenna is fixed on the sleeper with annex, set bolt plays the effect of fixed antenna and antenna heat-insulating shield thereof simultaneously.
Claims (5)
1. magnetic steel heat-insulating shield, it is characterized in that, comprise cover (1), base plate (2) is installed, base plate (2) is installed is processed with 2 mounting holes (3), last cover (1) is made up of three thermofins, and thermofin is respectively aviation insulating moulding coating layer (4), fiberglass thermofin (5), insulating layer of asbestos (6);
Described aviation insulating moulding coating heat reflectivity is 0.85, and the continuous firing temperature is-51 ℃-206 ℃.
2. magnetic steel heat-insulating shield according to claim 1 is characterized in that, last cover (1) innermost layer is an insulating layer of asbestos, and the middle layer is the fiberglass thermofin, and outermost layer is an aviation insulating moulding coating layer.
3. magnetic steel heat-insulating shield according to claim 1 and 2 is characterized in that, described fiberglass thermofin composition is resin+talcum powder+weak point yarn cutting, makes it when finishing heat-blocking action, also plays effect fire-retardant and increase heat-insulating shield intensity.
4. magnetic steel heat-insulating shield according to claim 1 is characterized in that, mounting hole (3) is a rectangle.
5. method for preparing the described magnetic steel heat-insulating shield of claim 1, it is characterized in that, the mould for preparing magnetic steel heat-insulating shield by magnet steel volume and profile, asbestos cover on the outer pad of mould, resin, talcum powder, three kinds of materials of short yarn cutting are mixed in 3: 2: 1 ratios, evenly be applied to asbestos surface 3-5mm, nature or baking box oven dry are evenly coated aviation insulating moulding coating 1-2mm at outermost layer at last.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN2009102419131A CN101740144B (en) | 2009-12-16 | 2009-12-16 | Magnetic steel heat-insulating shield and manufacturing method thereof |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN2009102419131A CN101740144B (en) | 2009-12-16 | 2009-12-16 | Magnetic steel heat-insulating shield and manufacturing method thereof |
Publications (2)
Publication Number | Publication Date |
---|---|
CN101740144A CN101740144A (en) | 2010-06-16 |
CN101740144B true CN101740144B (en) | 2011-11-09 |
Family
ID=42463461
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN2009102419131A Expired - Fee Related CN101740144B (en) | 2009-12-16 | 2009-12-16 | Magnetic steel heat-insulating shield and manufacturing method thereof |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN101740144B (en) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN107677853A (en) * | 2017-10-25 | 2018-02-09 | 佟元江 | Locomotive signal testing loop wire support |
-
2009
- 2009-12-16 CN CN2009102419131A patent/CN101740144B/en not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
CN101740144A (en) | 2010-06-16 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN103287568B (en) | A kind of high-speed aircraft anti-heat insulation structural of large area interlayer and forming method thereof | |
CN103264509B (en) | Preparation method of antenna housing of resin matrix composite material | |
CN103715502A (en) | High-wave transmission hollow-structure radome | |
CN103936390B (en) | The preparation method of phosphate composite material antenna house cover body | |
CN203747037U (en) | High wave permeability hollow structure antenna housing | |
CN109624369A (en) | A kind of preparation method of coldblade | |
CN102001212A (en) | Glass fiber reinforced plastic processing technology | |
CN101740144B (en) | Magnetic steel heat-insulating shield and manufacturing method thereof | |
CN102694257A (en) | Beautified radome and preparation method thereof | |
CN107994338A (en) | Mars exploration landing rover integral antenna protective cover and preparation method thereof | |
KR20190109611A (en) | Fabrication method of ceramic core based on 3d printing | |
CN106365667A (en) | Preparation method of low-density integrated heat preservation felt for high-temperature furnace | |
CN101494107A (en) | Method for producing sandstorm resistance insulator core pin with umbrella for railway | |
CN102649302A (en) | Forming process for covering carbon fiber on outer surface of structural part | |
CN104690982B (en) | A kind of composite stator blade of engine and preparation method thereof | |
CN103448183A (en) | Molding method for surface layer with composite coating | |
CN102371650A (en) | Preparation method for high-strength composite cable holder | |
CN105694453A (en) | O-phthalodinitrile composite material cable cover and preparation method of o-phthalodinitrile composite material cable cover | |
CN109455924B (en) | Fiber-reinforced ceramic-based wave-transmitting material with frequency selective structure and preparation method thereof | |
CN103318103B (en) | The production method of automobile top-cap trim board | |
CN104628239A (en) | Method for preparing vacuum insulated panel (VIP) core material by using dry process | |
CN117326820B (en) | 3D printing manufacturing method of special-shaped heat insulation piece based on aerogel powder | |
CN106751481B (en) | A kind of glass reinforced plastic and glass reinforced plastic dovetail as made from it | |
CN108908961A (en) | Glass fiber composite structure absorbing material and preparation method | |
AU2015373310B2 (en) | Method for measuring inside a batt of mineral or plant fibres |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
C06 | Publication | ||
PB01 | Publication | ||
C10 | Entry into substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
CF01 | Termination of patent right due to non-payment of annual fee | ||
CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20111109 Termination date: 20201216 |