CN202871937U - Aviation storage battery heater - Google Patents
Aviation storage battery heater Download PDFInfo
- Publication number
- CN202871937U CN202871937U CN201220542404XU CN201220542404U CN202871937U CN 202871937 U CN202871937 U CN 202871937U CN 201220542404X U CN201220542404X U CN 201220542404XU CN 201220542404 U CN201220542404 U CN 201220542404U CN 202871937 U CN202871937 U CN 202871937U
- Authority
- CN
- China
- Prior art keywords
- heat
- base
- heater
- ing
- coil
- 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 - Lifetime
Links
Images
Classifications
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E60/00—Enabling technologies; Technologies with a potential or indirect contribution to GHG emissions mitigation
- Y02E60/10—Energy storage using batteries
Landscapes
- Secondary Cells (AREA)
Abstract
The utility model discloses an aviation storage battery heater which has lighter weight, higher reliability, longer service life and higher heat transfer efficiency. The heater comprises a base, a heating coil pipe and a heat conduction structure, wherein the heating coil pipe comprises a pipe body and a connection end; the heating coil pipe and the heat conduction structure are in heat transfer connection with the base respectively; the heating coil pipe comprises at least two U-shaped sections; the pipe body of the heating coil pipe is arranged in the base; the heat conduction structure comprises at least one heat conduction plate; the heat conduction plate is vertical to the base; and the thickness of the base is 8-12mm. Through the utility model, the service life of the heater can be prolonged by 30%, the reliability of the heater can be improved by 30%, the whole weight can be reduced by 30%, and the heat transfer efficiency can be improved by 15%, thus the aviation storage battery heater disclosed by the utility model has the characteristics of lighter weight, higher reliability, longer service life and higher heat transfer efficiency.
Description
Technical field
The utility model relates to a kind of heater, relates in particular to a kind of aircraft battery group heater.
Background technology
At this moment the temperature that the aircraft battery group needs to keep each cell batteries in use just needs to use heater that cell batteries is heated in a zone of reasonableness.At present, installation heating tube and batteries combination shell install heating cabinet outward additional between the mode of heating of aircraft battery group employing heating cloth, heat-conducting plate.Above-mentioned 3 kinds of mode average lifes weak point, weight and volume are large, the shortcoming that heat transfer efficiency is low.
The utility model content
The technical problem that the utility model solves provides the aircraft battery group heater that a kind of weight is light, reliability is higher, useful life is long, heat transfer efficiency is higher.
The technical scheme that its technical problem that solves the utility model adopts is: aircraft battery group heater, comprise base, heat(ing) coil and conductive structure, described heat(ing) coil comprises body and link, and described heat(ing) coil is connected with conductive structure to conduct heat with base and is connected.
Further be: described heat(ing) coil comprises at least 2 U-shaped sections.
Further be: the body of described heat(ing) coil is arranged on the inside of base.
Further be: described conductive structure comprises at least 1 heat-conducting plate.
Further be: described heat-conducting plate is vertical with base to be arranged.
Further be: the thickness of described base is 8mm～12mm.
The beneficial effects of the utility model are: the useful life of heater of the present utility model and reliability can improve 30%, and overall weight can reduce by 30%, and heat transference efficiency can improve 15%.Therefore, heater of the present utility model has the advantages that weight is light, reliability is higher, useful life is long, heat transfer efficiency is higher.
Description of drawings
Fig. 1 is the schematic diagram of aircraft battery group heater of the present utility model;
Fig. 2 is the set-up mode schematic diagram of heat-conducting plate;
Fig. 3 is the schematic diagram of heat(ing) coil;
Fig. 4 is the use view of aircraft battery group heater of the present utility model;
Be labeled as among the figure: body 1, link 2, heat(ing) coil 3, base 4, heat-conducting plate 5, cell batteries 6, temperature relay 7.
Embodiment
Below in conjunction with the drawings and specific embodiments the utility model is further specified.
As shown in Figures 1 to 4, aircraft battery group heater comprises base 4, heat(ing) coil 3 and conductive structure, and described heat(ing) coil 3 comprises body 1 and link 2, and described heat(ing) coil 3 is connected with conductive structure to conduct heat with base 4 and is connected.During use, base can be installed in the inside of batteries combination shell, and temperature relay 7 can be installed on the base 4.3 power supplies can make heat(ing) coil produce heat to heat(ing) coil by power supply, heat can pass to cell batteries 6 by conductive structure, and after the internal temperature of batteries combination shell reached predetermined temperature, temperature relay 7 disconnected, disconnect current supply circuit, heat(ing) coil quits work.When temperature was not enough, temperature relay 7 was connected, and current supply circuit is connected, and heat(ing) coil is started working, and then gave cell batteries 6 heating.
For when heat(ing) coil is installed, be conducive to avoid each installing hole on the base, described heat(ing) coil 3 comprises at least 2 U-shaped sections.Owing to when using, base need to be fixed on batteries combination enclosure, therefore need to offer a plurality of installing holes at base, by bolt or screw etc. base is fixed.For fear of heat(ing) coil and the mutual interference of installing hole phase, therefore heat(ing) coil is designed to shape as shown in Figure 3, namely comprise at least 2 U-shaped sections, can effectively avoid installing hole like this.Conveniently base is fixed.In addition, also can strengthen the heating surface (area) (HS of heat(ing) coil.
In order to guarantee to have than the basis of high heat transfer efficiency to protect heat(ing) coil, it is damaged that heat(ing) coil is difficult for, and the body 1 of described heat(ing) coil 3 is arranged on the inside of base 4.When arranging, the body of heat(ing) coil can be arranged on base inside, connect end 2 and expose, be convenient to link to each other with relevant device.When arranging, heat(ing) coil can be arranged on base inside by casting technique.
The execution mode of above-mentioned conductive structure has multiple, such as can be a plurality of heating columns or heat-conducting block etc.Preferred implementation is: described conductive structure comprises at least 1 heat-conducting plate 5.As shown in Figures 1 to 4, the heat-conducting area of heat-conducting plate is large and be convenient to arrange.Above-mentioned heat-conducting plate can tilt with base when arranging, but is not easy to like this shelving of cell batteries 6, in order to overcome above-mentioned deficiency, and when arranging, described heat-conducting plate 5 and base 4 vertical settings.Can be convenient to like this shelve respectively a cell batteries 6 in the both sides of heat-conducting plate 5, and the heat-conducting area that can take full advantage of heat-conducting plate is to cell batteries 6 heating.
In order to improve heat transference efficiency, as shown in Figure 2, the thickness of described base 4 is 8mm～12mm.The thickness of base 4 namely the end face 41 of base apart from the vertical range of bottom surface 42.Arrange like this, can guarantee that base has in the situation of stronger support strength, guarantee to have higher heat transference efficiency.
Claims (6)
1. aircraft battery group heater, it is characterized in that: comprise base (4), heat(ing) coil (3) and conductive structure, described heat(ing) coil (3) comprises body (1) and link (2), and described heat(ing) coil (3) is connected with conductive structure to conduct heat with base (4) and is connected.
2. aircraft battery group heater as claimed in claim 1, it is characterized in that: described heat(ing) coil (3) comprises at least 2 U-shaped sections.
3. aircraft battery group heater as claimed in claim 1, it is characterized in that: the body (1) of described heat(ing) coil (3) is arranged on the inside of base (4).
4. aircraft battery group heater as claimed in claim 1, it is characterized in that: described conductive structure comprises at least 1 heat-conducting plate (5).
5. aircraft battery group heater as claimed in claim 4 is characterized in that: described heat-conducting plate (5) and the vertical setting of base (4).
6. such as the described aircraft battery group of any one in the claim 1 to 5 heater, it is characterized in that: the thickness of described base (4) is 8mm～12mm.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201220542404XU CN202871937U (en) | 2012-10-22 | 2012-10-22 | Aviation storage battery heater |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201220542404XU CN202871937U (en) | 2012-10-22 | 2012-10-22 | Aviation storage battery heater |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN202871937U true CN202871937U (en) | 2013-04-10 |
Family
ID=48038628
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201220542404XU Expired - Lifetime CN202871937U (en) | 2012-10-22 | 2012-10-22 | Aviation storage battery heater |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN202871937U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104362410A (en) * | 2014-11-19 | 2015-02-18 | 奇瑞汽车股份有限公司 | Water-cooling battery module |
-
2012
- 2012-10-22 CN CN201220542404XU patent/CN202871937U/en not_active Expired - Lifetime
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104362410A (en) * | 2014-11-19 | 2015-02-18 | 奇瑞汽车股份有限公司 | Water-cooling battery module |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN102297544A (en) | Semiconductor refrigerating or heating module and production method thereof | |
| CN205141082U (en) | Battery module unit and power battery group | |
| CN203456525U (en) | Energy storage battery device | |
| CN202871937U (en) | Aviation storage battery heater | |
| CN202254474U (en) | Cooling or heating module for semiconductor | |
| CN207116512U (en) | A kind of battery bag of simple installation | |
| CN204966564U (en) | Power assembly | |
| CN208400984U (en) | A kind of novel battery pack arrangement | |
| CN103337992B (en) | Device of solar generating | |
| CN204013395U (en) | Photovoltaic power generation apparatus and heat pump | |
| CN101707268B (en) | Heating device of liquid lead-acid storage battery low-voltage full-bridge series resonance soft-switching circuit | |
| CN204290750U (en) | Energy-saving variable voltage rectifier | |
| CN205264833U (en) | Battery system with preheating device | |
| CN210225341U (en) | Distributed photovoltaic power station energy storage system | |
| CN201536145U (en) | Liquid lead-acid storage battery low-voltage full-bridge serial connection resonant soft switching circuit heating device | |
| CN202940988U (en) | UPS heating structure | |
| CN204943639U (en) | A kind of energy-saving thermal storage formula electric heater | |
| CN201789016U (en) | Battery pack mounting rack | |
| CN207354104U (en) | A kind of double-side assembly mounting bracket | |
| CN101344320A (en) | High-efficiency heat accumulation type electric heater | |
| CN108963129A (en) | A kind of all solid-state thin-film lithium battery with defencive function | |
| CN104638278B (en) | A kind of integrated drive generator for electromechanical servo system | |
| CN106300090A (en) | A kind of energy saving and environment friendly power distribution cabinet | |
| CN101303144A (en) | Thermal storage type oil electric heater | |
| CN212542596U (en) | Lithium battery for communication energy storage |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CX01 | Expiry of patent term | ||
| CX01 | Expiry of patent term |
Granted publication date: 20130410 |