CN111106737A - Composite material converter cabinet body and assembling method thereof - Google Patents
Composite material converter cabinet body and assembling method thereof Download PDFInfo
- Publication number
- CN111106737A CN111106737A CN201811177240.3A CN201811177240A CN111106737A CN 111106737 A CN111106737 A CN 111106737A CN 201811177240 A CN201811177240 A CN 201811177240A CN 111106737 A CN111106737 A CN 111106737A
- Authority
- CN
- China
- Prior art keywords
- carbon fiber
- composite material
- cabinet body
- prepreg
- cabinet
- 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.)
- Pending
Links
Images
Classifications
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02M—APPARATUS FOR CONVERSION BETWEEN AC AND AC, BETWEEN AC AND DC, OR BETWEEN DC AND DC, AND FOR USE WITH MAINS OR SIMILAR POWER SUPPLY SYSTEMS; CONVERSION OF DC OR AC INPUT POWER INTO SURGE OUTPUT POWER; CONTROL OR REGULATION THEREOF
- H02M1/00—Details of apparatus for conversion
Landscapes
- Engineering & Computer Science (AREA)
- Power Engineering (AREA)
- Laminated Bodies (AREA)
Abstract
The invention relates to a composite material converter cabinet body and an assembling method thereof, relates to the technical field of railway vehicle converter, and is used for solving the technical problems of large weight and weak structural safety of the converter cabinet body in the prior art. The composite material converter cabinet body comprises a thin plate member, wherein the thin plate member in the converter is provided with a composite material part, namely the thin plate member is made of composite materials, the density of the thin plate member is far lower than that of metal materials such as steel materials, aluminum materials and the like, and the thin plate member has the strength, fatigue resistance and corrosion resistance which are far higher than those of the materials such as the steel materials, the aluminum materials and the like, so that the composite material converter cabinet body is lower than the traditional metal converter cabinet body in weight, and meanwhile, the problems of strength, fatigue, corrosion and the like are solved, and the purposes of improving the light weight level and the structural safety of the.
Description
Technical Field
The invention relates to the technical field of railway vehicle converters, in particular to a composite material converter cabinet body and an assembling method thereof.
Background
The converter product is train power equipment capable of transmitting electric energy, and consists of electric equipment such as a transformer and a module and a converter cabinet body. The converter electrical equipment passes through the lug on the converter cabinet body and passes through the bolt fastening to the train vehicle bottom on, therefore lightweight and the security of converter cabinet body structure have important meaning to train energy consumption and driving safety. The current transformer cabinet is mainly a metal current transformer cabinet, and is generally made of steel (such as carbon steel, stainless steel, etc.) or aluminum (5 series, 6 series, 7 series, etc.). Metal converter cabinets have some inherent disadvantages: for example, in terms of weight, the weight accounts for a large proportion of the whole cabinet, for example, the weight of an aluminum alloy cabinet accounts for 25% -30% of the whole cabinet, and the weight of a carbon steel cabinet can account for 30% -35%; in the aspect of safety, the problems of fatigue, corrosion, high repair difficulty and the like exist in the metal converter cabinet body, and once the cabinet body structure cracks, the safety evaluation difficulty is high.
Disclosure of Invention
The invention provides a composite material converter cabinet body and an assembling method thereof, which are used for solving the technical problems of large weight and poor structural safety of the converter cabinet body in the prior art.
The invention provides a composite material converter cabinet body, which comprises a thin plate component, wherein the thin plate component comprises a filling material and a composite material part covered on the filling material.
In one embodiment, the composite material portion is a carbon fiber laminate or a glass fiber laminate.
In one embodiment, the carbon fiber laminate is formed by laying prepreg carbon fiber cloth or carbon fiber cloth layer by layer.
In one embodiment, the prepreg carbon fiber cloth or the carbon fiber cloth is 4 to 60 layers each.
In one embodiment, the ply angle of the pre-preg carbon fiber cloth is 0 °, ± 30 °, ± 45 °, ± 60 ° or 90 °.
In one embodiment, the ply angle of the carbon fiber cloth is 0 °, ± 30 °, ± 45 °, ± 60 ° or 90 °.
In one embodiment, the prepreg carbon fiber cloth comprises a prepreg unidirectional cloth and a prepreg bidirectional cloth; the carbon fiber cloth comprises non-prepreg unidirectional cloth and non-prepreg bidirectional cloth.
In one embodiment, the filler material is a honeycomb core material, a foam core material, or polyurethane.
In one embodiment, the thin plate members are a cabinet main body, a long partition plate, a short partition plate, an air duct assembly, a bottom cover plate, a cabinet door, an electrical component mounting beam and a lifting lug;
copper meshes are laid in the main box body, the long partition plate and the short partition plate of the cabinet body, and embedded metal mounting seats are arranged in the electrical component mounting beams.
The invention provides an assembling method of a composite material converter cabinet body, which is characterized by comprising the following steps of:
the long partition plate is arranged in the main box body of the cabinet body through bonding;
the short partition plates are respectively arranged on the main box body of the cabinet body, the long partition plate and/or the short partition plate which is arranged in advance through bonding;
the air duct assembly is arranged in the cabinet body main box body in a bonding, bolt connection or riveting mode;
fixedly connecting the electric component mounting beam with the cabinet body main box body, the long partition plate and the short partition plate in one or more of sticking, bolt connection or riveting modes;
the lifting lugs are arranged on the cabinet body main box body in a bolt or riveting mode;
the bottom cover plate and the cabinet door are arranged on the main cabinet body of the cabinet body in a mode of connecting bolts, rivet nuts and/or door locks;
the accessories are arranged on the main box body of the cabinet body in a bolt connection, riveting or sticking mode.
Compared with the prior art, the invention has the advantages that: because the thin plate component in the converter is provided with the composite material part, namely made of the composite material, the density of the thin plate component is far lower than that of metal materials such as steel materials, aluminum materials and the like, and the thin plate component has the characteristics of strength, fatigue resistance and corrosion resistance which are far higher than those of the materials such as the steel materials, the aluminum materials and the like, the weight of the converter cabinet body made of the composite material is lower than that of the traditional metal converter cabinet body, and meanwhile, the problems of strength, fatigue, corrosion and the like are solved, so that the purposes of improving the light weight level and the structural.
Drawings
The invention will be described in more detail hereinafter on the basis of embodiments and with reference to the accompanying drawings.
Fig. 1 is a schematic perspective view of a composite converter cabinet according to an embodiment of the invention;
fig. 2 is an exploded view of the composite material converter cabinet shown in fig. 1;
FIG. 3 is a left side view of a sheet member in an embodiment of the invention;
FIG. 4 is an exploded view of a carbon fiber laminate in one embodiment of the invention;
FIG. 5 is an exploded view of a carbon fiber laminate in another embodiment of the present invention
FIG. 6 is a schematic structural view of a carbon fiber cloth according to an embodiment of the present invention;
fig. 7 is a schematic view of the structure of a prepreg bidirectional fabric or a non-prepreg bidirectional fabric in another embodiment of the invention.
Reference numerals:
100-a sheet member;
101-a composite portion; 102-a filler material;
111-carbon fiber laminate; 112-prepreg carbon fiber cloth; 113-carbon fiber cloth;
1-cabinet body main box body; 2-long partition board; 3-short partition board; 4-an air duct assembly; 5-bottom cover plate; 6-cabinet door; 8-lifting lugs;
7-electrical component mounting beam.
Detailed Description
The invention will be further explained with reference to the drawings.
As shown in fig. 1 and 2, according to an aspect of the present invention, a composite material converter cabinet is provided, comprising a sheet member 100, the sheet member 100 being as shown in fig. 3 and 4, the sheet member 100 comprising a filler material 102 and a composite material portion 101 covering the filler material 102. For example, the composite material portions 101 are provided on the upper and lower surfaces of the filler material 102, respectively, and the filler material 102 can reinforce the strength of the sheet member 100.
It should be noted that the thin plate member 100 of the present invention includes a plate member such as the cabinet main body 1 mentioned below and a beam member such as the electric component mounting beam 7.
Further, the composite material is a glass fiber composite material or a carbon fiber composite material.
Preferably, the density of the carbon fiber composite material is only about 1.8g/cm3Therefore, it has an incomparable advantage in terms of weight reduction. Therefore, the composite material converter cabinet body is a carbon fiber converter cabinet body. Because the converter cabinet body made of the carbon fiber composite material is adopted, under the condition of the same product, the weight of the converter cabinet body can be reduced by more than 25% compared with an aluminum alloy cabinet body, and the weight of the converter cabinet body can be reduced by more than 35% compared with carbon steel and stainless steel cabinet bodies; thereby reach the purpose that promotes cabinet body lightweight level.
Specifically, the composite material portion 101 is a carbon fiber laminate 111 or a glass fiber laminate.
Optionally, the carbon fiber laminate 111 is formed by laying prepreg carbon fiber cloth 112 layer by layer, wherein the number of the prepreg carbon fiber cloth is 4-60 layers.
According to the installation position of the thin plate member 100 and the matching condition with other components, the corresponding stress condition of the thin plate member 100, such as mainly tensile stress or shearing force, can be calculated and obtained. According to different stress conditions of different sheet members 100, the prepreg carbon fiber cloth 112 can be selectively laid in different directions, and different laying angles not only can achieve the purpose of preventing warping, but also can improve the shearing resistance of the sheet members.
The lay-up of the pre-preg carbon fibre cloth 112 may be chosen in a number of ways, for example symmetrical or asymmetrical. Generally, the ply angle of the prepreg carbon fiber cloth 112 is some specific angle, such as 0 °, ± 30 °, ± 45 °, ± 60 ° or 90 °. The laying angle is easy to implement in process and has certain process feasibility.
Preferably, the lay-up angles are different for adjacent prepreg carbon fiber cloth 112.
The following describes a manner of symmetrically laying the prepreg carbon fiber cloth 112.
When the number of the carbon prepreg fibers 112 is a single layer, the carbon prepreg fibers 112 have one intermediate layer, and the lay-up angles of the carbon prepreg fibers 112 above the intermediate layer and the carbon prepreg fibers 112 below the intermediate layer are symmetrical with respect to the intermediate layer. For example, if the number of the prepreg carbon fiber cloth 112 is 7, the 4 th layer is an intermediate layer, and the lay-up angles of the 1 st, 2 nd and 3 th layers are respectively symmetrical with respect to the lay-up angles of the 4 th layer and the 7 th, 6 th and 5 th layers. Assuming that the ply angles of the 1 st, 2 nd and 3 rd plies are 0 °, 30 ° and 60 °, respectively, and the ply angle of the 4 th ply is 90 °, the lay angles of the 5 th, 6 th and 7 th plies are 60 °, 30 ° and 0 °.
In the case where the number of the carbon fiber prepreg sheets 112 is a single layer, it has two intermediate layers, and the lay-up angles of the two intermediate layers may be set to be the same. The lay-up angles of the prepreg carbon fiber cloth 112 above the two intermediate layers and the prepreg carbon fiber cloth 112 below the two intermediate layers are symmetrical with respect to the two intermediate layers. For example, if the number of the prepreg carbon fiber cloth 112 is 8, the 4 th and 5 th layers are intermediate layers, and the lay-up angles of the 1 st, 2 nd and 3 th layers are symmetrical with respect to the lay-up angles of the 4 th and 5 th layers and the 8 th, 7 th and 6 th layers, respectively. Assuming that the ply angles of the 1 st, 2 nd and 3 rd layers are 0 °, 30 ° and 60 °, the ply angle of the 4 th layer is 90 °, and the ply angle of the 5 th layer is 90 °, the lay angles of the 6 th, 7 th and 8 th layers are 60 °, 30 ° and 0 °.
Note that the layer 1 is defined as a layer closest to the filler material 102.
As shown in fig. 5, prepreg carbon fiber cloth layer 111 is formed by stacking 5 layers of prepreg carbon fiber cloth 112, wherein the stacking angles of prepreg carbon fiber cloth 112 are 0 °, 45 °, 90 °, 45 °, and 0 ° from the bottom to the top.
The above-described symmetrical arrangement of the prepreg carbon fiber cloths 112 can prevent the formed carbon fiber laminate 111 from warping and deforming.
For the asymmetric laying of the prepreg carbon fiber cloth 112, different ply angles are adopted for the adjacent prepreg carbon fiber cloth 112. As shown in fig. 4, prepreg carbon fiber cloth layer 111 is formed by stacking 4 layers of prepreg carbon fiber cloth 112, wherein the stacking angles of prepreg carbon fiber cloth 112 are 0 °, 30 °, 60 °, and 90 ° from the bottom to the top, respectively.
It should be noted that the dotted line in fig. 4 and 5 is the main force-receiving direction of the prepreg carbon fiber cloth 112, i.e., the direction of the carbon fiber, and the ply angle is the included angle between the direction of the carbon fiber and the positive direction of the X axis.
In other words, the ply angle of the prepreg carbon fiber cloth 112 in the invention is the included angle between the direction of the carbon fiber in each layer of the prepreg carbon fiber cloth 112 and the positive direction of the X axis.
The rectangular coordinate system of the ply angle is defined as follows: the length direction of the beam member is defined as the X-axis direction, the width direction of the beam member is defined as the Y-axis direction, and the height direction of the beam member is defined as the Z-axis direction.
The prepreg carbon fiber cloth 112 of the present invention is a composite material produced by coating, hot pressing, cooling, coating, and winding a material such as carbon fiber yarn, epoxy resin, and release paper.
Wherein the adopted resin meets the use temperature range of-45 ℃ to 80 ℃; such as an epoxy resin.
Optionally, the carbon fiber laminated plate 111 is formed by laying carbon fiber cloth 113 layer by layer, wherein the number of the carbon fiber cloth 113 is 4-60 layers. In addition, the laying angle of the carbon fiber cloth 113 may be the same as that of the prepreg carbon fiber cloth 112, and will not be described herein.
The difference between the carbon fiber cloth 113 and the prepreg carbon fiber cloth 112 is that the prepreg carbon fiber cloth 112 contains resin, whereas the carbon fiber cloth 113 does not contain resin.
In one embodiment, prepreg carbon fiber cloth 112 is prepreg unidirectional cloth. The prepreg has carbon fibers in only one direction, and since it contains resin itself, the carbon fiber cloth does not scatter. The strength of the whole carbon fiber cloth is concentrated in one direction of the carbon fibers, and the strength of the whole carbon fiber cloth is independent of the gram weight of the whole carbon fiber cloth and only related to the carbon filaments.
In one embodiment, the prepreg carbon fiber cloth 112 is a prepreg bidirectional cloth. The longitudinal and transverse interwoven prepreg bidirectional cloth has a large number of twistless rovings in the longitudinal and transverse directions, and the cloth has two stress directions, and is characterized by multiple interweaving points, firm texture, flat surface, good wear resistance and obviously superior comprehensive stress performance to unidirectional carbon fiber cloth.
Similarly, the carbon fiber cloth 113 includes a non-prepreg unidirectional cloth and a non-prepreg bidirectional cloth, and unlike the prepreg unidirectional cloth, since the non-prepreg unidirectional cloth does not contain resin, there are carbon fibers in one direction, and as shown in fig. 6, there are spun yarns (generally, fine glass fibers) fixed in a direction perpendicular thereto.
The non-prepreg bidirectional cloth is provided with a large number of untwisted rovings in the longitudinal direction and the transverse direction, and the stress directions of the untwisted rovings are the same.
For the prepreg bidirectional cloth and the non-prepreg bidirectional cloth, a traditional weaving plain cloth method is adopted, namely longitudinal carbon fibers and transverse carbon fibers are interwoven in a regular manner from top to bottom. Every other carbon fiber of the longitudinal and transverse carbon fibers is crossed in a cross shape, as shown in fig. 7, the longitudinal carbon fibers are a, b, c and d are arranged above and A, B, C, D is arranged below; the transverse carbon fibers are a, b, c and d above and A, B, C, D below.
Furthermore, the carbon fiber yarns are used for carrying out left-right bidirectional interweaving between the interlayers of the adjacent carbon fiber bidirectional cloth. The interweaving angle of the carbon fiber yarns is 45 degrees, so that the shearing performance can be improved.
The composite material part 101 enables the composite material converter cabinet body to have good effects of rain prevention, dust prevention, temperature insulation, mould prevention, salt fog prevention and damp and heat prevention, and particularly, the composite material converter cabinet body can meet fire risk levels of HL2 and HL3 specified in EN45545-2:2013, is free of electrochemical corrosion and can adapt to the effects of corrosive rain and snow and cleaning agents; and the test requirements of high and low temperature, salt fog and the like specified by IEC 60068-2-1:2007, IEC 60068-2-2:2007, IEC 60068-2-30:2005 and IEC 60068-2-11:1981 are met.
In one embodiment, the filler material 102 is a honeycomb core material. In addition, the filling material 102 may be polyurethane or foam core material to improve the heat insulation effect.
Therefore, the composite material part 101 has high corrosion resistance, strength and designability, and can thoroughly solve the problems of fatigue and corrosion of the converter cabinet body. Meanwhile, the carbon fiber composite material is used as a commonly used repairing material, so that the carbon fiber converter cabinet body has excellent repairability. In addition, since the composite material portion 101 has a multi-layer mesh structure, the overall structural safety is not affected even if cracks occur in the limit, thereby improving the structural safety.
As shown in fig. 2, the plate members are a cabinet main body 1, one or more long partition plates 2, one or more short partition plates 3, an air duct assembly 4, a bottom cover plate 5, one or more cabinet doors 6 and one or more lifting lugs 8, and the beam members are electrical component mounting beams 7; copper nets are laid in the cabinet body main body 1, the long partition plate 2 and the short partition plate 3, the copper nets can improve the conductivity of the cabinet body main body 1, the grounding resistance of the copper nets is not more than 0.1 omega, the copper nets have a certain electromagnetic shielding function, and the copper nets can meet the EMC (Electro Magnetic Compatibility) performance specified by the standard EN 50121-2015.
In addition, an embedded metal mounting seat is arranged in the electrical component mounting beam 7, and the electrical component is conducted with the cabinet body main box body 1 through the metal mounting seat.
The plate component can also be a part with smaller bearing capacity, such as a binding rod, a hook and the like of the cabinet body main box body 1, and the part can be directly pasted on the cabinet body main box body 1.
In one embodiment, each part in the plate member or the beam member is obtained by adopting an integral curing molding method, the manufacturing deformation amount is small, the use of a large number of fasteners is avoided, and the assembly and the maintenance are convenient.
In addition, large cavities such as side door frames, bottom door frames, air inlets and air outlets, internal air ducts and the like are reserved during the molding of each part in the sheet member 100, and small holes are directly formed by machining.
According to a second aspect of the present invention, there is provided an assembling method of a carbon fiber current transformer, comprising the steps of:
firstly, the long clapboard 2 is installed in the cabinet body main box 1 through bonding.
Secondly, the short partition boards 3 are respectively arranged on the cabinet body main box body 1, the long partition board 2 and/or the short partition board 3 which is arranged in advance through bonding.
Thirdly, the air duct assembly 4 is installed in the cabinet body main box 1 in a bonding, bolt connection or riveting mode.
Fourthly, the electric component mounting beam 7 is fixedly connected with the cabinet body main box body 1, the long partition plate 2 and the short partition plate 3 in one or more modes of pasting, bolt connection and/or riveting;
fifthly, the lifting lug 8 is arranged on the cabinet body main box body 1 in a bolt connection, riveting or riveting mode;
sixthly, the bottom cover plate 5 and the cabinet door 6 are arranged on the cabinet body main box body 1 in a mode of connecting bolts, rivet nuts and/or door locks;
and seventhly, accessories are mounted on the main box body of the cabinet body in a bolt or sticking mode. Wherein, the accessories are a binding rod, a hook and a cable clamp.
In the assembly, most parts adopt an integral forming or sticking process, so that the number of fasteners is reduced, and the assembly and the maintenance are convenient.
While the invention has been described with reference to a preferred embodiment, various modifications may be made and equivalents may be substituted for elements thereof without departing from the scope of the invention. In particular, the technical features mentioned in the embodiments can be combined in any way as long as there is no structural conflict. It is intended that the invention not be limited to the particular embodiments disclosed, but that the invention will include all embodiments falling within the scope of the appended claims.
Claims (10)
1. A composite material current transformer cabinet, characterized by comprising a sheet member comprising a filler material and a composite material portion covering the filler material.
2. The composite material current transformer cabinet according to claim 1, characterized in that the composite material portion is a carbon fiber laminate or a glass fiber laminate.
3. The composite material current transformer cabinet according to claim 2, wherein the carbon fiber laminate is formed by laying carbon fiber cloth prepreg or carbon fiber cloth layer by layer.
4. The composite material converter cabinet according to claim 3, characterized in that the prepreg carbon fiber cloth or the carbon fiber cloth is 4-60 layers each.
5. The composite current transformer cabinet according to claim 3 or 4, characterized in that the lay-up angle of the prepreg carbon fiber cloth is 0 °, ± 30 °, ± 45 °, ± 60 ° or 90 °.
6. The composite material current transformer cabinet according to claim 3 or 4, characterized in that the lay angle of the carbon fiber cloth is 0 °, ± 30 °, ± 45 °, ± 60 ° or 90 °.
7. The composite material converter cabinet according to claim 4, wherein the prepreg carbon fiber cloth comprises prepreg unidirectional cloth and prepreg bidirectional cloth; the carbon fiber cloth comprises non-prepreg unidirectional cloth and non-prepreg bidirectional cloth.
8. The composite current transformer cabinet according to any of claims 1 to 4, wherein the filler material is a honeycomb core material, a foam core material or polyurethane.
9. The composite material converter cabinet according to any one of claims 1 to 4, wherein the thin plate members are a cabinet main body, a long partition, a short partition, an air duct assembly, a bottom cover plate, a cabinet door, an electrical component mounting beam and a lifting lug;
copper meshes are laid in the main box body, the long partition plate and the short partition plate of the cabinet body, and embedded metal mounting seats are arranged in the electrical component mounting beams.
10. A method for assembling a composite material converter cabinet body is characterized by comprising the following steps:
the long partition plate is arranged in the main box body of the cabinet body through bonding;
the short partition plates are respectively arranged on the main box body of the cabinet body, the long partition plate and/or the short partition plate which is arranged in advance through bonding;
the air duct assembly is arranged in the cabinet body main box body in a bonding, bolt connection or riveting mode;
fixedly connecting the electric component mounting beam with the cabinet body main box body, the long partition plate and the short partition plate in one or more of sticking, bolt connection or riveting modes;
the lifting lugs are arranged on the cabinet body main box body in a bolt or riveting mode;
the bottom cover plate and the cabinet door are arranged on the main cabinet body of the cabinet body in a mode of connecting bolts, rivet nuts and/or door locks;
the accessories are arranged on the main box body of the cabinet body in a bolt connection, riveting or sticking mode.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811177240.3A CN111106737A (en) | 2018-10-10 | 2018-10-10 | Composite material converter cabinet body and assembling method thereof |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811177240.3A CN111106737A (en) | 2018-10-10 | 2018-10-10 | Composite material converter cabinet body and assembling method thereof |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN111106737A true CN111106737A (en) | 2020-05-05 |
Family
ID=70417520
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201811177240.3A Pending CN111106737A (en) | 2018-10-10 | 2018-10-10 | Composite material converter cabinet body and assembling method thereof |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN111106737A (en) |
Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101289017B (en) * | 2007-04-18 | 2012-09-05 | 上海磁浮交通工程技术研究中心 | Composite material for high-speed train and its manufacturing method |
| CN103496400A (en) * | 2013-09-27 | 2014-01-08 | 奇瑞汽车股份有限公司 | Carbon fiber composite automobile radiator upper cross beam assembly and manufacturing method thereof |
| CN104325756A (en) * | 2013-07-22 | 2015-02-04 | 上海杰事杰新材料(集团)股份有限公司 | Carbon fiber reinforced composite material used for notebook housing and preparation method thereof |
| CN204578346U (en) * | 2015-05-19 | 2015-08-19 | 中国铁道科学研究院 | Be applicable to the casing of EMU AuCT |
| CN205105085U (en) * | 2015-11-05 | 2016-03-23 | 株洲南车时代电气股份有限公司 | Supplementary deflector of diesel locomotive and diesel locomotive |
| CN106300901A (en) * | 2015-05-13 | 2017-01-04 | 中车大连电力牵引研发中心有限公司 | Traction convertor cabinet and light rail vehicle |
| CN206212552U (en) * | 2016-11-28 | 2017-05-31 | 株洲中车时代电气股份有限公司 | A kind of traction convertor for track traffic |
| CN206561391U (en) * | 2016-08-25 | 2017-10-17 | 株洲中车时代电气股份有限公司 | A kind of assembling stand of converter cabinet |
| CN207234652U (en) * | 2017-09-28 | 2018-04-13 | 株洲中车时代电气股份有限公司 | A kind of integrated form traction convertor |
-
2018
- 2018-10-10 CN CN201811177240.3A patent/CN111106737A/en active Pending
Patent Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101289017B (en) * | 2007-04-18 | 2012-09-05 | 上海磁浮交通工程技术研究中心 | Composite material for high-speed train and its manufacturing method |
| CN104325756A (en) * | 2013-07-22 | 2015-02-04 | 上海杰事杰新材料(集团)股份有限公司 | Carbon fiber reinforced composite material used for notebook housing and preparation method thereof |
| CN103496400A (en) * | 2013-09-27 | 2014-01-08 | 奇瑞汽车股份有限公司 | Carbon fiber composite automobile radiator upper cross beam assembly and manufacturing method thereof |
| CN106300901A (en) * | 2015-05-13 | 2017-01-04 | 中车大连电力牵引研发中心有限公司 | Traction convertor cabinet and light rail vehicle |
| CN204578346U (en) * | 2015-05-19 | 2015-08-19 | 中国铁道科学研究院 | Be applicable to the casing of EMU AuCT |
| CN205105085U (en) * | 2015-11-05 | 2016-03-23 | 株洲南车时代电气股份有限公司 | Supplementary deflector of diesel locomotive and diesel locomotive |
| CN206561391U (en) * | 2016-08-25 | 2017-10-17 | 株洲中车时代电气股份有限公司 | A kind of assembling stand of converter cabinet |
| CN206212552U (en) * | 2016-11-28 | 2017-05-31 | 株洲中车时代电气股份有限公司 | A kind of traction convertor for track traffic |
| CN207234652U (en) * | 2017-09-28 | 2018-04-13 | 株洲中车时代电气股份有限公司 | A kind of integrated form traction convertor |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CA2413184C (en) | Energy absorbent laminate | |
| JP4278678B2 (en) | Sandwich panel | |
| CN102686382B (en) | Composite ply stabilizing mechanism and method | |
| US20160361889A1 (en) | Composite sandwich panel with differential resin layers | |
| US20190283361A1 (en) | Composite laminate having a honeycomb core, and method for the manufacture thereof | |
| CN109228547B (en) | Fiber layering structure of reinforced material and pultrusion profile | |
| JP2020001387A (en) | Composite panel and method for forming composite panel | |
| JP4596920B2 (en) | Large composite structure and method for producing large composite structure | |
| EP3863910B1 (en) | Safety cabin for a recreational or camper van with deformation elements, and manufacturing method for such a safety cabin | |
| CN206516679U (en) | A kind of compound material insulation Battery case | |
| CN111106737A (en) | Composite material converter cabinet body and assembling method thereof | |
| JP2013071469A (en) | Railroad vehicle structure, and method for manufacturing the same | |
| CN106476330A (en) | A kind of rail vehicle aramid fiber honeycomb side top board and preparation method thereof | |
| CN204472802U (en) | One is novel adds heat composite floor | |
| CN205255608U (en) | I shape presss from both sides core composite sheet | |
| EP3282067A2 (en) | Flooring assembly with heat dissipation layer | |
| CN101613899A (en) | A kind of orthogonal reinforced integrated hollow sandwich composite | |
| CN111391418A (en) | Three-dimensional sandwich bearing structure, vehicle body and structural member of weaving of high-speed motor car | |
| CN111099026A (en) | Supporting structure of power battery system of electric aircraft | |
| CN213138056U (en) | Light bearing plate for vehicle | |
| CN210174344U (en) | Composite board | |
| JP2008265160A (en) | Frp molding | |
| CN201235826Y (en) | Main friction plate for cam driver of goods train | |
| CN221574762U (en) | Cable bracket and rail vehicle | |
| CN217124780U (en) | Electric heating composite floor and railway vehicle provided with same |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20200505 |