CN218123474U - Hydrogen power battery mounting structure for hydrogen unmanned aerial vehicle - Google Patents

Hydrogen power battery mounting structure for hydrogen unmanned aerial vehicle Download PDF

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Publication number
CN218123474U
CN218123474U CN202221768193.1U CN202221768193U CN218123474U CN 218123474 U CN218123474 U CN 218123474U CN 202221768193 U CN202221768193 U CN 202221768193U CN 218123474 U CN218123474 U CN 218123474U
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Prior art keywords
hydrogen
power battery
wall
rectangle
hydrogen power
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CN202221768193.1U
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Chinese (zh)
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徐伟强
高鼎
公昆颖
陈黎
吴国浩
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Hepeng Technology (Zhejiang) Co.,Ltd.
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Zhejiang Xinchuang Hydrogen Wing Technology Co ltd
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    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E60/00Enabling technologies; Technologies with a potential or indirect contribution to GHG emissions mitigation
    • Y02E60/30Hydrogen technology
    • Y02E60/50Fuel cells

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Abstract

The utility model belongs to the technical field of the battery installation, a hydrogen power battery mounting structure for hydrogen unmanned aerial vehicle, the following scheme is proposed at present, including the rectangle protection casing, its characterized in that, the semiconductor refrigeration piece that the equidistance distributes is installed to the outer wall all around to the rectangle protection casing, and the rectangle protection casing inner wall welding all around has the arc elasticity conducting strip that the equidistance distributes, the welding of arc elasticity conducting strip bottom has the rectangle metal conducting strip, and the relative one side outer wall of rectangle metal conducting strip is fixed with hydrogen power battery. The utility model discloses an outside at hydrogen power battery sets up the protection casing to utilize the continuous acceleration gas flow of semiconductor refrigeration piece cooperation heat dissipation fan, thereby cool down the hydrogen power battery who generates heat and handle, and arc elasticity conducting strip and yielding rubber post can support hydrogen power battery, and can carry out certain shock attenuation buffering when appearing rocking and handle, thereby can be high to the protective effect of battery.

Description

Hydrogen power battery mounting structure for hydrogen unmanned aerial vehicle
Technical Field
The utility model relates to a battery installation technical field especially relates to a hydrogen power battery mounting structure for hydrogen unmanned aerial vehicle.
Background
A hydrogen fuel cell is a cell that uses a chemical element, hydrogen, and is manufactured to store energy. The basic principle is the reverse reaction of electrolyzed water, hydrogen and oxygen are supplied to the anode and cathode respectively, and after the hydrogen diffuses out through the anode and reacts with the electrolyte, electrons are released to reach the cathode through an external load.
Because the characteristic of hydrogen power battery, consequently need protect it in hydrogen power battery's installation, and among the current hydrogen power battery mounting structure, often because hydrogen power battery can generate heat to only possess certain heat dissipation function, but because certain vibration can appear in the use, and lack relevant buffering safeguard measure, can cause certain damage to hydrogen power battery.
SUMMERY OF THE UTILITY MODEL
The utility model aims at solving the defects existing in the prior art and providing a hydrogen power battery mounting structure for a hydrogen unmanned aerial vehicle.
In order to achieve the above purpose, the utility model adopts the following technical scheme:
the utility model provides a hydrogen power battery mounting structure for hydrogen unmanned aerial vehicle, includes the rectangle protection casing, its characterized in that, the semiconductor refrigeration piece that the equidistance distributes is installed to rectangle protection casing outer wall all around, and the welding of rectangle protection casing inner wall all around has the arc elasticity conducting strip that the equidistance distributes, the welding of arc elasticity conducting strip bottom has the rectangle metal conducting strip, and the relative one side outer wall of rectangle metal conducting strip is fixed with hydrogen power battery, fixed slot has all been opened to rectangle protection casing both ends outer wall both sides, and the inside joint of fixed slot has the fixing clip pole, the welding of fixing clip pole has the sealed lid of rectangle, and the sealed lid of rectangle is opened there is positioning slot.
Preferably, the rectangular sealing cover is provided with a rectangular mounting groove, and the inner wall of the rectangular mounting groove is provided with a heat dissipation fan.
Preferably, the middle part of the outer wall of one side, opposite to the rectangular sealing cover, is bonded with a rubber non-slip pad, and the outer wall of the rubber non-slip pad is in contact with the two ends of the hydrogen power battery.
Preferably, the semiconductor refrigeration piece and the heat dissipation fan are both connected with a switch through a wire, and the switch is connected with an external power supply.
Preferably, the heat absorption surface of the semiconductor refrigeration piece faces the inner wall of the rectangular protective cover, the heat dissipation surface of the semiconductor refrigeration piece faces the outside, and a metal heat dissipation sheet is bonded outside the heat dissipation surface of the semiconductor refrigeration piece.
Preferably, the damping rubber columns are bonded between the arc-shaped elastic heat conducting sheets on the inner wall of the periphery of the rectangular protective cover at equal intervals, and the gap between each damping rubber column and the hydrogen power battery is 0.3-0.7cm.
The beneficial effects of the utility model are that:
the hydrogen power battery mounting structure of this design sets up the protection casing through the outside at hydrogen power battery to utilize semiconductor refrigeration piece cooperation heat dissipation fan to be continuous to accelerate gas flow, thereby cool down the hydrogen power battery who generates heat and handle, and arc elasticity conducting strip and yielding rubber post can support hydrogen power battery, and can carry out certain shock attenuation buffering when appearing rocking and handle, thereby can be high to the protective effect of battery.
Drawings
Fig. 1 is a front view of an overall split structure of a hydrogen power battery mounting structure for a hydrogen unmanned aerial vehicle according to the present invention;
fig. 2 is a side view of the overall structure of a hydrogen power battery mounting structure for a hydrogen unmanned aerial vehicle according to the present invention;
fig. 3 is a side view of the internal structure of the hydrogen power battery mounting structure for a hydrogen unmanned aerial vehicle according to the present invention.
In the figure: 1 rectangle protection casing, 2 semiconductor refrigeration pieces, 3 arc elasticity conducting strip, 4 rectangle metal conducting strips, 5 hydrogen power battery, 6 shock-absorbing rubber posts, 7 fixed slot, 8 fixing clip poles, 9 sealed lids of rectangle, 10 positioning slot, 11 rectangle mounting grooves, 12 heat dissipation fans, 13 rubber slipmats.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments.
Embodiment 1, refer to fig. 1 to 3, a hydrogen power battery mounting structure for a hydrogen unmanned aerial vehicle includes a rectangular protective cover 1, semiconductor refrigeration fins 2 are mounted on the outer wall of the periphery of the rectangular protective cover 1 and are distributed equidistantly, and arc-shaped elastic heat conduction fins 3 are welded on the inner wall of the periphery of the rectangular protective cover 1 and are distributed equidistantly;
the bottom of the arc-shaped elastic heat conducting strip 3 is welded with a rectangular metal heat conducting strip 4, the outer wall of one side, opposite to the rectangular metal heat conducting strip 4, of the rectangular metal heat conducting strip is fixed with a hydrogen power battery 5, the heat absorbing surface of the semiconductor refrigerating strip 2 faces the inner wall of the rectangular protective cover 1, the heat radiating surface of the semiconductor refrigerating strip 2 faces the outside, and a metal radiating fin is bonded outside the heat radiating surface of the semiconductor refrigerating strip 2;
fixed slot 7 has all been opened to 1 both ends outer wall both sides of rectangle protection casing, and the inside joint of fixed slot 7 has fixing clip pole 8, and semiconductor refrigeration piece 2 all is connected with the switch through the wire with heat dissipation fan 12, and the switch connection has external power source, and rectangle protection casing 1 inner wall all around is located the damping rubber post 6 that bonds between arc elasticity conducting strip 3 and have the equidistance and distribute.
Example 2:
the embodiment is a further optimization process of embodiment 1, and specifically includes:
the protective cover 1 is arranged outside the hydrogen power battery, and the semiconductor refrigerating sheet 2 is matched with the heat dissipation fan 12 to accelerate the gas flow continuously, so that the heat-generating hydrogen power battery is cooled, the arc-shaped elastic heat conducting sheet 3 and the damping rubber column 6 can support the hydrogen power battery, and certain damping buffering treatment can be carried out when the hydrogen power battery shakes, so that the battery can be protected well;
the clearance between the damping rubber column 6 and the hydrogen power battery 5 is 0.3-0.7cm, the rectangular sealing cover 9 is welded on the fixing clamping rod 8, the rectangular sealing cover 9 is provided with the positioning slot 10, the rectangular sealing cover 9 is provided with the rectangular mounting groove 11, the inner wall of the rectangular mounting groove 11 is provided with the heat dissipation fan 12, the middle part of the outer wall of one side, opposite to the rectangular sealing cover 9, of the rectangular sealing cover is bonded with the rubber non-slip mat 13, and the outer wall of the rubber non-slip mat 13 is in mutual contact with the two ends of the hydrogen power battery 5.
The working principle is as follows: when using this hydrogen unmanned aerial vehicle hydrogen power battery mounting structure, at first open the sealed lid 9 of rectangle with 1 both sides of rectangle protection casing, then slide hydrogen power battery 5 and peg graft inside rectangle protection casing 1, thereby arc elasticity conducting strip 3 cooperation rectangle metal conducting strip 4 extrudees hydrogen power battery 5 fixedly, then fix the sealed lid 9 joint of rectangle protection casing at 1 both ends of rectangle protection casing and fix, and the rubber slipmat 13 extrusion of both sides is fixed at hydrogen power battery 5 both ends, and open heat dissipation fan 12 and accelerate gas flow, and utilize semiconductor refrigeration piece 2 to refrigerate, when hydrogen power battery 5 vibrates, inside yielding rubber post 6 and arc elasticity conducting strip 3 can carry out the shock attenuation protection to it.
The above, only be the concrete implementation of the preferred embodiment of the present invention, but the protection scope of the present invention is not limited thereto, and any person skilled in the art is in the technical scope of the present invention, according to the technical solution of the present invention and the utility model, the concept of which is equivalent to replace or change, should be covered within the protection scope of the present invention.

Claims (6)

1. The utility model provides a hydrogen power battery mounting structure for hydrogen unmanned aerial vehicle, includes rectangle protection casing (1), its characterized in that, rectangle protection casing (1) outer wall all around installs semiconductor refrigeration piece (2) that the equidistance distributes, and rectangle protection casing (1) inner wall welding all around has arc elasticity conducting strip (3) that the equidistance distributes, the welding of arc elasticity conducting strip (3) bottom has rectangle metal conducting strip (4), and one side outer wall is fixed with hydrogen power battery (5) relatively in rectangle metal conducting strip (4), fixed slot (7) have all been opened to rectangle protection casing (1) both ends outer wall both sides, and fixed slot (7) inside joint has fixing clip pole (8), fixing clip pole (8) welding has sealed lid (9) of rectangle, and opens on the sealed lid (9) of rectangle and has positioning slot (10).
2. The hydrogen power battery mounting structure for the hydrogen unmanned aerial vehicle as claimed in claim 1, wherein the rectangular sealing cover (9) is provided with a rectangular mounting groove (11), and a heat dissipation fan (12) is mounted on the inner wall of the rectangular mounting groove (11).
3. The mounting structure of the hydrogen power battery for the hydrogen unmanned aerial vehicle according to claim 1, wherein a rubber anti-slip pad (13) is bonded to the middle of the outer wall of the rectangular sealing cover (9) on the opposite side, and the outer wall of the rubber anti-slip pad (13) is in contact with the two ends of the hydrogen power battery (5).
4. The hydrogen power battery mounting structure for the hydrogen unmanned aerial vehicle according to claim 2, characterized in that the semiconductor refrigeration sheet (2) and the heat dissipation fan (12) are connected with a switch through a wire, and the switch is connected with an external power supply.
5. The hydrogen power battery mounting structure for the hydrogen unmanned aerial vehicle as claimed in claim 1, wherein the heat absorbing surface of the semiconductor refrigeration sheet (2) faces the inner wall of the rectangular protective cover (1), the heat dissipating surface of the semiconductor refrigeration sheet (2) faces the outside, and a metal heat sink is bonded outside the heat dissipating surface of the semiconductor refrigeration sheet (2).
6. The hydrogen power battery mounting structure for the hydrogen unmanned aerial vehicle according to claim 1, wherein shock-absorbing rubber columns (6) are bonded between the arc-shaped elastic heat-conducting sheets (3) on the inner wall of the periphery of the rectangular protective cover (1) and are distributed at equal intervals, and a gap between each shock-absorbing rubber column (6) and the hydrogen power battery (5) is 0.3-0.7cm.
CN202221768193.1U 2022-07-11 2022-07-11 Hydrogen power battery mounting structure for hydrogen unmanned aerial vehicle Active CN218123474U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202221768193.1U CN218123474U (en) 2022-07-11 2022-07-11 Hydrogen power battery mounting structure for hydrogen unmanned aerial vehicle

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202221768193.1U CN218123474U (en) 2022-07-11 2022-07-11 Hydrogen power battery mounting structure for hydrogen unmanned aerial vehicle

Publications (1)

Publication Number Publication Date
CN218123474U true CN218123474U (en) 2022-12-23

Family

ID=84517640

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202221768193.1U Active CN218123474U (en) 2022-07-11 2022-07-11 Hydrogen power battery mounting structure for hydrogen unmanned aerial vehicle

Country Status (1)

Country Link
CN (1) CN218123474U (en)

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CP01 Change in the name or title of a patent holder

Address after: 312500 Floor 1, Building 2, No. 48, Zhenqian Road, Chengtan Street, Xinchang County, Shaoxing City, Zhejiang Province

Patentee after: Hepeng Technology (Zhejiang) Co.,Ltd.

Address before: 312500 Floor 1, Building 2, No. 48, Zhenqian Road, Chengtan Street, Xinchang County, Shaoxing City, Zhejiang Province

Patentee before: Zhejiang Xinchuang hydrogen Wing Technology Co.,Ltd.

CP01 Change in the name or title of a patent holder