CN110265748B - Hydrogen-nickel storage battery for space - Google Patents
Hydrogen-nickel storage battery for space Download PDFInfo
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- CN110265748B CN110265748B CN201910549756.4A CN201910549756A CN110265748B CN 110265748 B CN110265748 B CN 110265748B CN 201910549756 A CN201910549756 A CN 201910549756A CN 110265748 B CN110265748 B CN 110265748B
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
- H01M10/00—Secondary cells; Manufacture thereof
- H01M10/24—Alkaline accumulators
- H01M10/28—Construction or manufacture
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
- H01M10/00—Secondary cells; Manufacture thereof
- H01M10/24—Alkaline accumulators
- H01M10/30—Nickel accumulators
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
- H01M10/00—Secondary cells; Manufacture thereof
- H01M10/60—Heating or cooling; Temperature control
- H01M10/61—Types of temperature control
- H01M10/613—Cooling or keeping cold
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
- H01M10/00—Secondary cells; Manufacture thereof
- H01M10/60—Heating or cooling; Temperature control
- H01M10/62—Heating or cooling; Temperature control specially adapted for specific applications
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
- H01M10/00—Secondary cells; Manufacture thereof
- H01M10/60—Heating or cooling; Temperature control
- H01M10/65—Means for temperature control structurally associated with the cells
- H01M10/653—Means for temperature control structurally associated with the cells characterised by electrically insulating or thermally conductive materials
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
- H01M10/00—Secondary cells; Manufacture thereof
- H01M10/60—Heating or cooling; Temperature control
- H01M10/65—Means for temperature control structurally associated with the cells
- H01M10/655—Solid structures for heat exchange or heat conduction
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
- H01M2220/00—Batteries for particular applications
- H01M2220/20—Batteries in motive systems, e.g. vehicle, ship, plane
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- 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
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- 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
- Y02P—CLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
- Y02P70/00—Climate change mitigation technologies in the production process for final industrial or consumer products
- Y02P70/50—Manufacturing or production processes characterised by the final manufactured product
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- Manufacturing & Machinery (AREA)
- Chemical & Material Sciences (AREA)
- Chemical Kinetics & Catalysis (AREA)
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- General Chemical & Material Sciences (AREA)
- Secondary Cells (AREA)
- Battery Mounting, Suspending (AREA)
Abstract
A hydrogen-nickel storage battery for space comprises a hydrogen-nickel storage battery monomer, a heat dissipation sleeve and heat-conducting silica gel; the hydrogen-nickel storage battery monomer is installed in the heat dissipation sleeve, and a gap between the hydrogen-nickel storage battery monomer and the heat dissipation sleeve is filled with heat conduction silica gel. The invention also discloses an assembling method of the hydrogen-nickel storage battery for the space, which can realize the uniformity of filling no gap and bonding of the sizing material, enhance the bonding strength of the structure, improve the heat transfer efficiency, improve the performance, the service life and the stability of the hydrogen-nickel storage battery, simplify the procedure and improve the efficiency.
Description
Technical Field
The invention relates to a hydrogen-nickel storage battery for a space, belonging to the technical field of space batteries.
Background
The hydrogen-nickel storage battery monomer for the space is a cylinder with two hemispherical ends, when the storage battery pack is assembled, the hydrogen-nickel storage battery monomer is combined with the conical heat dissipation sleeve, then the heat dissipation sleeve is fixed on the bottom plate through a fastener, the combination of the hydrogen-nickel storage battery monomer and the conical heat dissipation sleeve adopts a cementing method, namely a certain gap is designed between a shell of the hydrogen-nickel storage battery and the heat dissipation sleeve so as to be filled with heat-conducting silica gel, and the battery monomer is supported and fixed by utilizing the good bonding performance of the heat-conducting silica gel. The silica gel is required to meet the requirement of mechanical and thermal properties, and meanwhile, a silica gel bonding area must have an enough area, because the bonding strength is related to the shearing strength of the silica gel, and is also directly related to the size of the bonding area of the silica gel, if the bonding area of the silica gel is not enough, a storage battery monomer is separated from a heat dissipation sleeve under the mechanical environment conditions of impact, vibration and the like in the process of launching, attitude adjustment or orbital transfer of a spacecraft, and the storage battery pack fails.
Moreover, the heat-conducting silica gel filled between the storage battery monomer and the heat dissipation sleeve also plays a role in transferring the heat of the storage battery. On a spacecraft with a vacuum environment, the most important heat transfer routes are as follows: the heat generated in the storage battery monomer is conducted out from the storage battery shell to the bottom plate through the heat conducting silica gel, the heat conducting silica gel and the heat radiating sleeve, and then the heat is conducted out from the bottom plate through the spacecraft cabin plate. If the heat conduction silica gel between the storage battery monomer and the heat dissipation sleeve is not uniformly or insufficiently filled, the area which is not coated is in a vacuum heat insulation state or a gas state (the heat conductivity coefficient of air is about 0.0251W/m.K), the heat conduction of the part is blocked, the temperature of different parts of the storage battery monomer is uneven, the performance of the storage battery monomer is reduced, meanwhile, the silicon rubber shortage between the storage battery monomer and the heat dissipation sleeve is equivalent to the reduction of the heat transfer area of the storage battery monomer, the heat flow density is increased, the aggravation of unsmooth heat transfer is caused, the heat transfer effect is poor, the temperature among the storage battery monomers is uneven, the performance and the reliability of the battery pack are reduced.
The existing heat-conducting silica gel filling process adopts a method of manually coating natural flow gel, namely, a layer of glue material is manually coated on the surface of a straight cylinder section of a storage battery shell by a scraper, and then the glue material is inserted into a heat dissipation sleeve to be cured.
During manual coating, the thickness of the sizing material on the shell is not uniform, and during the process of inserting the heat dissipation sleeve, because the silicon rubber has viscosity and is difficult to flow under the condition that the gap is very small, most of the silicon rubber is blocked outside the gap, so that the sizing material in the gap is not completely filled, even less than 50%. Therefore, the manual coating process has poor filling effect, low production efficiency and is not suitable for the requirement of batch production.
Disclosure of Invention
The technical problem to be solved by the invention is as follows: the defects of the prior art are overcome, the space hydrogen-nickel storage battery is provided, the uniformity of filling no gap and bonding of sizing materials can be realized, the structural bonding strength is enhanced, the heat transfer efficiency is improved, the performance, the service life and the stability of the hydrogen-nickel storage battery are improved, the procedure is simplified, and the efficiency is improved.
The purpose of the invention is realized by the following technical scheme:
a hydrogen-nickel storage battery for space comprises a hydrogen-nickel storage battery monomer, a heat dissipation sleeve and heat-conducting silica gel;
the hydrogen-nickel storage battery monomer is arranged in the heat dissipation sleeve, and a gap between the hydrogen-nickel storage battery monomer and the heat dissipation sleeve is filled with heat-conducting silica gel;
the heat-conducting silica gel comprises the following components in percentage by mass:
42 to 45 percent of carborundum, 42 to 45 percent of vulcanized silicone rubber 107A, 12 to 15 percent of ethyl orthosilicate and 0.1 to 0.3 percent of dibutyltin dilaurate.
The middle part of the single body of the hydrogen-nickel storage battery is a cylinder, and two ends of the single body of the hydrogen-nickel storage battery are hemispheroids; the heat dissipation sleeve is a hollow cone.
The middle part of the single hydrogen-nickel storage battery is provided with a positioning strip, the positioning strip is used for keeping the single hydrogen-nickel storage battery and the uniform gap between the heat dissipation sleeves, and the positioning strip is parallel to the axis of the single hydrogen-nickel storage battery.
The thickness of the positioning strip of the nickel-hydrogen storage battery for the space is 0.25 mm-1.0 mm.
The heat dissipation sleeve is made of magnesium-lithium alloy or O-state hard aluminum alloy materials.
The assembling method of the hydrogen-nickel storage battery for the space comprises the following steps:
(1) pouring the heat-conducting silica gel into a pit of an external gel storage device; sleeving the heat dissipation sleeve on an external glue storage device, and sealing the external glue storage device and the heat dissipation sleeve by using an external sealing ring;
(2) the single hydrogen-nickel storage battery is arranged in the hollow cavity of the heat dissipation sleeve until the single hydrogen-nickel storage battery contacts an external glue storage device;
(3) and keeping the single hydrogen-nickel storage battery in contact with an external glue storage device, and curing for 12-24 h.
And (3) after the hydrogen-nickel storage battery is used in the space, the external glue storage device and the external sealing ring are removed.
The space hydrogen-nickel storage battery adopts an assembly method of the space hydrogen-nickel storage battery, and the sizing material filling material of the gap between the hydrogen-nickel storage battery monomer and the heat dissipation sleeve is more than or equal to 90 percent.
The heat-conducting silica gel comprises the following components in percentage by mass:
42 to 45 percent of carborundum, 107A42 to 45 percent of vulcanized silicone rubber, 12 to 15 percent of ethyl orthosilicate and 0.1 to 0.3 percent of dibutyltin dilaurate.
A preparation method of heat-conducting silica gel comprises the following steps:
(1) weighing the following components in percentage by mass:
42 to 45 percent of carborundum, 107A42 to 45 percent of vulcanized silicone rubber, 12 to 15 percent of ethyl orthosilicate and 0.1 to 0.3 percent of dibutyltin dilaurate;
(2) weighing ethyl orthosilicate by weight which is 8-10 times of that of dibutyltin dilaurate, adding the weighed ethyl orthosilicate into the dibutyltin dilaurate, and uniformly mixing to form a catalyst;
(3) adding carborundum into vulcanized silicone rubber 107A, and uniformly mixing to form a first mixture;
(4) adding the rest tetraethoxysilane into the first mixture, and uniformly mixing to form a second mixture;
(5) adding the catalyst into the second mixture, and stirring uniformly to prepare the heat-conducting silica gel.
Compared with the prior art, the invention has the following beneficial effects:
(1) by adopting the invention, the filling rate of the sizing material is greatly improved and reaches more than 90 percent of the theoretical filling rate of the sizing material;
(2) the invention can realize the uniformity of filling no gap and bonding of the sizing material, enhance the bonding strength of the structure, improve the heat transfer efficiency, improve the performance, the service life and the stability of the nickel-hydrogen storage battery, simplify the procedure and improve the efficiency.
Drawings
FIG. 1 is an assembly view of a nickel-hydrogen storage battery for space use according to the present invention.
Detailed Description
In order to make the objects, technical solutions and advantages of the present invention more apparent, embodiments of the present invention will be described in detail with reference to the accompanying drawings.
The heat-conducting silica gel comprises the following components in percentage by mass:
42 to 45 percent of carborundum, 42 to 45 percent of vulcanized silicone rubber 107A, 12 to 15 percent of ethyl orthosilicate and 0.1 to 0.3 percent of dibutyltin dilaurate.
Preferably, the heat-conducting silica gel comprises the following components in percentage by mass:
comprises 43 percent of carborundum, 43 percent of vulcanized silicone rubber 107A, 13.8 percent of ethyl orthosilicate and 0.2 percent of dibutyltin dilaurate.
A preparation method of heat-conducting silica gel comprises the following steps:
(1) weighing the following components in percentage by mass:
43% of carborundum, 107A 43% of vulcanized silicone rubber, 13.8% of ethyl orthosilicate and 0.2% of dibutyltin dilaurate;
(2) adding ethyl orthosilicate into dibutyltin dilaurate, wherein the mass of the added ethyl orthosilicate is 9 times that of the dibutyltin dilaurate, and then manually shaking up to form a catalyst;
(3) adding carborundum into vulcanized silicone rubber 107A and uniformly mixing to form a first mixture;
(4) adding the rest of the ethyl orthosilicate into the first mixture, and uniformly mixing to form a second mixture;
(5) and adding the catalyst formed in the first step into the second mixture, and uniformly stirring by using a glass rod to form the heat-conducting silica gel.
A method for combining a hydrogen-nickel storage battery and a heat dissipation sleeve comprises the following steps:
uniformly adhering six positioning strips 2 to a straight cylinder section of a hydrogen-nickel storage battery monomer 1 along the circumferential direction according to six equal division points, wherein the positioning strips 2 are axially parallel to the straight cylinder section of the hydrogen-nickel storage battery monomer 1, the thickness of the positioning strips 2 is determined according to the size of a gap between a shell of the hydrogen-nickel storage battery monomer 1 and a heat dissipation sleeve, the part adhered with the positioning strips 2 is tightly contacted with the inner wall of the heat dissipation sleeve 3, and the thickness of the positioning strips 2 is generally between 0.25mm and 1.0 mm. The clearance between the shell of the hydrogen-nickel storage battery monomer 1 and the heat dissipation sleeve 3 is determined according to the mechanical requirements of the spacecraft and the mass of the hydrogen-nickel storage battery monomer.
Step two, according to the figure 1, firstly, the O-shaped sealing ring 6 is sleeved into a groove of the glue storage device 5, then the heat dissipation sleeve 3 is sleeved on the glue storage device 5 and is fastened with the glue storage device 5, the outer diameter of the O-shaped sealing ring 6 is the same as the inner diameter of the heat dissipation sleeve 3, the inner diameter of the O-shaped sealing ring 6 is slightly smaller than the outer diameter of the groove of the glue storage device 5, and the heat dissipation sleeve 3, the glue storage device 5 and the O-shaped sealing ring form a sealing concave cavity. The appearance of the glue storage device 5 is a cylinder, the outer diameter of the cylinder is 0.1-0.5 mm smaller than the inner diameter of the heat dissipation sleeve shell 3, the upper end of the glue storage device 5 is a hemispherical pit, the spherical radius of the pit of the glue storage device 5 is 0.1-1.0 mm larger than the spherical radius of the lower end of the hydrogen-nickel storage battery monomer 1, and the pit of the glue storage device 5 is used for containing heat-conducting silica gel. The heat dissipation sleeve 3 is made of magnesium-lithium alloy or O-state hard aluminum alloy material, the heat dissipation sleeve 3 is in the shape of a cone with a thin upper part and a thick lower part, and the upper wall is thick h1Lower wall thickness h2,h1The thickness H2 is determined according to the heating power W of the single body of the hydrogen-nickel storage battery, the outer diameter D of the single body of the hydrogen-nickel storage battery, the height H of the heating body (pole stack) in the single body of the hydrogen-nickel storage battery, the distance L from the heat transmission of the heating body (pole stack) to the bottom of the heat dissipation sleeve, the heat conductivity lambda of the heat dissipation sleeve and the like, and the thickness H of the middle-upper wall in the embodiment10.8 mm-1.5 mm, lower wall thickness h2Is 1.5 mm-2.5 mm.
And step three, preparing the heat-conducting silica gel according to the preparation method of the heat-conducting silica gel.
And step four, pouring the prepared heat-conducting silica gel 4 into a gel storage device 5.
And fifthly, the single hydrogen-nickel storage battery 1 is placed into the heat dissipation sleeve 3, the single hydrogen-nickel storage battery 1 is pressed downwards at a certain speed through a tool to be in contact with the pit part of the glue storage device 5, and the heat conduction silica gel 4 in the pit of the glue storage device 5 is extruded by the single hydrogen-nickel storage battery 1 and automatically flows to the gap between the shell of the hydrogen-nickel storage battery and the heat dissipation sleeve 3 until the whole gap is filled.
And sixthly, after the whole gap is filled with the heat-conducting silica gel 4, continuously maintaining constant pressure at the upper end of the single body 1 of the nickel-hydrogen storage battery, and standing for 12-24 hours at normal temperature until the heat-conducting silica gel is solidified. And finally, the glue storage device and the sealing ring are detached.
Example (b):
step 1, pasting a positioning strip
And uniformly sticking six positioning strips 2 to the straight cylinder section of the single hydrogen-nickel storage battery 1 along the circumferential direction according to six equal division points, wherein the positioning strips 2 are axially parallel to the straight cylinder section of the single hydrogen-nickel storage battery 1, and the thickness of the positioning strips 2 is 0.45 mm.
Step 2, assembling
According to the figure 1, the O-shaped sealing ring 6 is sleeved into the groove of the glue storage device 5, and then the heat dissipation sleeve 3 is sleeved on the glue storage device 5 and fastened with the glue storage device 5. The outer diameter of the cylinder of the glue storage device 5 is 0.1mm smaller than the inner diameter of the heat dissipation sleeve shell 3, the upper end of the glue storage device 5 is a hemispherical pit, and the spherical radius of the pit of the glue storage device 5 is 0.5mm larger than that of the lower end of the hydrogen-nickel storage battery monomer 1.
Carborundum, room temperature vulcanized silicone rubber 107A, ethyl orthosilicate, dibutyltin dilaurate and the like are mixed according to a certain sequence and proportion and are stirred uniformly.
And pouring the prepared heat-conducting silica gel 4 into the gel storage device 5, and pouring the heat-conducting silica gel to the position of two thirds of the height of the pit of the gel storage device 5.
The hydrogen-nickel storage battery monomer 1 is arranged in the heat dissipation sleeve 2, the hydrogen-nickel storage battery monomer 1 is pressed downwards at a certain speed through the tool to be in contact with the pit part of the glue storage device 5, and the heat conduction silica gel 4 in the pit of the glue storage device 5 is extruded by the hydrogen-nickel storage battery monomer 1 and automatically flows to the gap between the hydrogen-nickel storage battery shell and the heat dissipation sleeve 3 until the whole gap is filled.
Step 6, curing at normal temperature (25 ℃)
And (3) maintaining constant pressure at the upper end of the single hydrogen-nickel storage battery 1, standing for 16 hours at normal temperature, and curing the heat-conducting silica gel. And finally, the glue storage device and the sealing ring are detached.
The mechanism of the present assembly method is described below
According to the principles of fluid mechanics, pressure is applied to one end of a fluid, and the fluid flows toward the other end. Namely, the heat-conducting silica gel 4 automatically flows to the gap between the hydrogen-nickel storage battery monomer 1 and the heat dissipation sleeve 3 by applying a certain pressure on the sizing material until the whole gap is filled.
Those skilled in the art will appreciate that those matters not described in detail in the present specification are well known in the art.
Claims (6)
1. A hydrogen-nickel storage battery for space is characterized by comprising a hydrogen-nickel storage battery monomer, a heat dissipation sleeve and heat-conducting silica gel;
the hydrogen-nickel storage battery monomer is arranged in the heat dissipation sleeve, and a gap between the hydrogen-nickel storage battery monomer and the heat dissipation sleeve is filled with heat-conducting silica gel;
the heat-conducting silica gel comprises the following components in percentage by mass:
42 to 45 percent of carborundum, 42 to 45 percent of vulcanized silicone rubber 107A, 12 to 15 percent of ethyl orthosilicate and 0.1 to 0.3 percent of dibutyltin dilaurate;
the heat dissipation sleeve is a hollow cone;
the heat dissipation sleeve is made of magnesium-lithium alloy or O-state hard aluminum alloy material;
the middle part of the single hydrogen-nickel storage battery is provided with a positioning strip, the positioning strip is used for keeping the single hydrogen-nickel storage battery and the uniform gap between the heat dissipation sleeves, and the positioning strip is parallel to the axis of the single hydrogen-nickel storage battery.
2. The hydrogen-nickel storage battery for the space according to claim 1, characterized in that the middle part of the hydrogen-nickel storage battery monomer is a cylinder, and two ends are hemispheroids; the heat dissipation sleeve is a cone with a thin upper part and a thick lower part, and the upper wall thickness is h1Lower wall thickness of h2Upper wall thickness h10.8 mm-1.5 mm, lower wall thickness h2Is 1.5 mm-2.5 mm.
3. A spatial ni-h battery according to claim 1, characterized in that the thickness of the tie bars is 0.25mm to 1.0 mm.
4. The space hydrogen-nickel storage battery according to claim 1, characterized in that the assembling method of the space hydrogen-nickel storage battery is as follows:
(1) pouring the heat-conducting silica gel into a pit of an external gel storage device; sleeving the heat dissipation sleeve on an external glue storage device, and sealing the external glue storage device and the heat dissipation sleeve by using an external sealing ring;
(2) the single hydrogen-nickel storage battery is arranged in the hollow cavity of the heat dissipation sleeve until the single hydrogen-nickel storage battery contacts an external glue storage device;
(3) and keeping the single hydrogen-nickel storage battery in contact with an external glue storage device, and curing for 12-24 h.
5. A nickel-hydrogen storage battery for spaces according to claim 4, characterized in that after (3), the external glue reservoir and the external sealing ring are removed.
6. The hydrogen-nickel storage battery for the space is characterized in that the sizing filling material of the gap between the hydrogen-nickel storage battery monomer and the heat dissipation sleeve is greater than or equal to 90 percent by adopting the assembling method of the hydrogen-nickel storage battery for the space.
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CN105219092A (en) * | 2015-10-29 | 2016-01-06 | 惠州市粤泰翔科技有限公司 | A kind of high filling flexible heat-conducting silicon rubber and preparation method thereof |
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