CN204257731U - Electric airplane traction vehicle battery box - Google Patents

Electric airplane traction vehicle battery box Download PDF

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Publication number
CN204257731U
CN204257731U CN201420844525.9U CN201420844525U CN204257731U CN 204257731 U CN204257731 U CN 204257731U CN 201420844525 U CN201420844525 U CN 201420844525U CN 204257731 U CN204257731 U CN 204257731U
Authority
CN
China
Prior art keywords
plate
right baffle
backboard
front apron
casing
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
Application number
CN201420844525.9U
Other languages
Chinese (zh)
Inventor
夏鹏
徐强
姜仁淑
高慧君
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Weihai Guangtai Airport Equipment Co Ltd
Original Assignee
Weihai Guangtai Airport Equipment Co Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Weihai Guangtai Airport Equipment Co Ltd filed Critical Weihai Guangtai Airport Equipment Co Ltd
Priority to CN201420844525.9U priority Critical patent/CN204257731U/en
Application granted granted Critical
Publication of CN204257731U publication Critical patent/CN204257731U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • 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
    • Y02E60/10Energy storage using batteries

Landscapes

  • Battery Mounting, Suspending (AREA)

Abstract

The utility model relates to aircraft floor facility technology field, specifically a kind of electric airplane traction vehicle battery box, be provided with casing, described casing is by base plate, front apron, backboard, right baffle-plate is formed by fixedly connecting with right baffle plate is mutually vertical, it is characterized in that described base plate is provided with leaking hole, described front apron, backboard, right baffle-plate and right baffle plate are respectively equipped with louvre, be beneficial to prevent cell heat from not distributing not go out cause temperature too high and affect battery life, simultaneously, also mitigate hoisting weight, described right baffle-plate and right baffle plate upper end center are respectively equipped with hoisting board, described hoisting board is vertical with right baffle-plate to be respectively fixedly connected with, described hoisting board is provided with lifting eye, be beneficial to lift by crane battery case in narrow space, described front apron or backboard upper end are provided with away line groove, be beneficial to orderly wiring, the utility model is owing to adopting said structure, there is compact conformation, easy to operate, good heat dissipation effect, change the advantages such as quick.

Description

Electric airplane traction vehicle battery box
Technical field
The utility model relates to aircraft floor facility technology field, specifically a kind of electric airplane traction vehicle battery box.
Background technology
As everyone knows; air pollution is day by day serious in recent years; haze weather occurs often, and its main cause is exactly Global Auto increasing number, and emission increases; in order to protection of the environment improves human life quality; the emission request of people to automobile is more and more higher, also strengthen research and development capabilities to the electric motor car of zero discharge, and aircraft tractor discharge capacity is large simultaneously; serious to air pollution, research and development electrically propelled traction vehicle becomes highly significant.
During the work of electric airplane tractor, power consumption is larger; the installation method of a large amount of storage batterys and fast changeable storage battery is needed to ensure the normal work of electric airplane tractor; electric airplane tractor directly operates various aircraft simultaneously; in order to protect aircraft and facilitate driver to observe rear situation; so the height of civil aviaton to aircraft tractor has strict restriction; this just needs us to find a kind of effective scheme; both can a large amount of storage battery of installation neatly compactly onboard, again can these storage batterys of quick-replaceable.
Summary of the invention
The purpose of this utility model solves above-mentioned the deficiencies in the prior art, provides a kind of compact conformation, easy to operate, good heat dissipation effect, changes the vehicle battery box of electric airplane traction efficiently.
The utility model solves the technical scheme that its technical problem adopts:
A kind of electric airplane traction vehicle battery box, be provided with casing, described casing is the front apron by base plate and base plate upper periphery, backboard, right baffle-plate is formed by fixedly connecting with right baffle plate is mutually vertical, it is characterized in that described base plate is provided with leaking hole, described front apron, backboard, right baffle-plate and right baffle plate are respectively equipped with louvre, be beneficial to prevent cell heat from not distributing not go out cause temperature too high and affect battery life, simultaneously, also mitigate hoisting weight, described right baffle-plate and right baffle plate upper end center are respectively equipped with hoisting board, described hoisting board is vertical with right baffle-plate to be respectively fixedly connected with, described hoisting board is provided with lifting eye, be beneficial to lift by crane battery case in narrow space, described front apron or backboard upper end are provided with away line groove, be beneficial to orderly wiring.
The utility model can be provided with longitudinally-moving dividing plate and horizontal active clapboard in casing, described longitudinally-moving dividing plate and the mutual grafting of horizontal active clapboard, be beneficial to space cells, and, be convenient to neat putting, prevent between battery bonded to each other, and described longitudinally-moving dividing plate and horizontal active clapboard are laid with thermal vias respectively, the heat effectively solved between battery distributes.
The utility model, owing to adopting said structure, has the advantages such as compact conformation, easy to operate, good heat dissipation effect, replacing are quick.
Accompanying drawing explanation
Fig. 1 is front view of the present utility model.
Fig. 2 is the vertical view of Fig. 1.
Fig. 3 is stereogram of the present utility model.
Fig. 4 is the schematic diagram after the utility model fills storage battery.
Reference numeral: base plate 1, front apron 2, backboard 3, right baffle-plate 4, right baffle plate 5, leaking hole 6, louvre 7, hoisting board 8, walk line groove 9.
Embodiment:
Below in conjunction with accompanying drawing, the utility model is further illustrated:
As shown in drawings, a kind of electric airplane traction vehicle battery box, be provided with casing, described casing is the front apron 2 by base plate 1 and base plate upper periphery, backboard 3, right baffle-plate 4 is formed by fixedly connecting with right baffle plate 5 is mutually vertical, it is characterized in that described base plate 1 is provided with leaking hole 6, described front apron 2, backboard 3, right baffle-plate 4 and right baffle plate 5 are respectively equipped with louvre 7, be beneficial to prevent cell heat from not distributing not go out cause temperature too high and affect battery life, simultaneously, also mitigate hoisting weight, described right baffle-plate 4 and right baffle plate 5 upper end center are respectively equipped with hoisting board 8, described hoisting board 8 is fixedly connected with right baffle-plate 4 is vertical respectively, described hoisting board 8 is provided with lifting eye, be beneficial to lift by crane battery case in narrow space, described front apron or backboard upper end are provided with away line groove 9, be beneficial to orderly wiring.
The utility model can be provided with longitudinally-moving dividing plate 10 and horizontal active clapboard 11 in casing, described longitudinally-moving dividing plate 10 and horizontal active clapboard 11 grafting mutually, be beneficial to space cells, and, be convenient to neat putting, prevent between battery bonded to each other, and described longitudinally-moving dividing plate 10 and horizontal active clapboard 11 are laid with thermal vias respectively, the heat effectively solved between battery distributes.
Storage battery can neatly be put in battery case as can be seen from Figure 3, but battery is not stick together closely, but between battery, placed longitudinally-moving dividing plate and horizontal active clapboard, can effectively prevent cell heat from not distributing not go out by the louvre 7 of casing surrounding like this and the temperature caused is too high, louvre also mitigates the weight of battery case simultaneously, battery is neatly arranged and is beneficial to wiring, FCL battery can be regarded a bulk of battery as thus also simplify the wiring of car load, battery case can mounted on top, cabling is not affected after stacking, reserve in the side of casing and walked line groove 9, conveniently in narrow space, battery case is lifted by crane, hoisting board 8 is specially placed on the top of casing, hoisting board 8 is welded on outside casing, and two reinforcements have been added in inner side, be enough to meet requirement of strength.Battery case profile is simple and easy to manufacture as can be seen from Figure 2, and convenient carrying.Between battery case, interchangeability is strong, because each battery case only has two lines to be connected with the external world, so fast changeable does not have the battery case of electricity, thus ensures that electric airplane tractor can continuous operation.
The utility model, owing to adopting said structure, has the advantages such as compact conformation, easy to operate, good heat dissipation effect, replacing are quick.

Claims (2)

1. an electric airplane traction vehicle battery box, be provided with casing, described casing is formed by fixedly connecting by base plate, front apron, backboard, right baffle-plate and right baffle plate are mutually vertical, it is characterized in that described base plate is provided with leaking hole, described front apron, backboard, right baffle-plate and right baffle plate are respectively equipped with louvre, described right baffle-plate and right baffle plate upper end center are respectively equipped with hoisting board, described hoisting board is vertical with right baffle-plate to be respectively fixedly connected with, described hoisting board is provided with lifting eye, and described front apron or backboard upper end are provided with away line groove.
2. a kind of electric airplane traction vehicle battery box according to claim 1, it is characterized in that in described casing, being provided with longitudinally-moving dividing plate and horizontal active clapboard, described longitudinally-moving dividing plate and the mutual grafting of horizontal active clapboard, and described longitudinally-moving dividing plate and horizontal active clapboard are laid with thermal vias respectively.
CN201420844525.9U 2014-12-29 2014-12-29 Electric airplane traction vehicle battery box Expired - Fee Related CN204257731U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201420844525.9U CN204257731U (en) 2014-12-29 2014-12-29 Electric airplane traction vehicle battery box

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201420844525.9U CN204257731U (en) 2014-12-29 2014-12-29 Electric airplane traction vehicle battery box

Publications (1)

Publication Number Publication Date
CN204257731U true CN204257731U (en) 2015-04-08

Family

ID=52962004

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201420844525.9U Expired - Fee Related CN204257731U (en) 2014-12-29 2014-12-29 Electric airplane traction vehicle battery box

Country Status (1)

Country Link
CN (1) CN204257731U (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105161648A (en) * 2015-09-25 2015-12-16 江苏峰谷源储能技术研究院有限公司 Portable battery box
CN105826501A (en) * 2016-05-16 2016-08-03 福建易动力电子科技有限公司 Battery box with hidden-type lifting tools
CN106654111A (en) * 2017-03-15 2017-05-10 安徽江淮汽车集团股份有限公司 Storage battery fixing mechanism and storage battery module assembly

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105161648A (en) * 2015-09-25 2015-12-16 江苏峰谷源储能技术研究院有限公司 Portable battery box
CN105826501A (en) * 2016-05-16 2016-08-03 福建易动力电子科技有限公司 Battery box with hidden-type lifting tools
CN105826501B (en) * 2016-05-16 2018-07-20 福建易动力电子科技股份有限公司 A kind of Battery case with concealed suspender
CN106654111A (en) * 2017-03-15 2017-05-10 安徽江淮汽车集团股份有限公司 Storage battery fixing mechanism and storage battery module assembly
CN106654111B (en) * 2017-03-15 2020-05-05 安徽江淮汽车集团股份有限公司 Storage battery fixing mechanism and storage battery module assembly

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Legal Events

Date Code Title Description
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: 20150408

Termination date: 20211229