CN201266626Y - Mounting structure of aeroplane accumulator set - Google Patents
Mounting structure of aeroplane accumulator set Download PDFInfo
- Publication number
- CN201266626Y CN201266626Y CNU2008201489867U CN200820148986U CN201266626Y CN 201266626 Y CN201266626 Y CN 201266626Y CN U2008201489867 U CNU2008201489867 U CN U2008201489867U CN 200820148986 U CN200820148986 U CN 200820148986U CN 201266626 Y CN201266626 Y CN 201266626Y
- Authority
- CN
- China
- Prior art keywords
- base
- roller
- nut
- battery group
- battery
- 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
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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
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- Battery Mounting, Suspending (AREA)
Abstract
The utility model discloses an installing structure for an airplane storage battery group and relates to a mechanism for fixing the battery group. The technical proposal of the utility model is as follows: the installing structure for the airplane storage battery group comprises a base and a slide way, the base is fixed on a bottom plate of a battery bin by screws, rollers are arranged in grooves on the upper surfaces of the front side and back side of the base, roller shafts are arranged in the holes at the two sides of the grooves, the rollers are higher than the surface of the base, a locating block is connected with the right end of the base by screws and provided with a groove with steps which is corresponding to an inclined plane of a fastening board on a battery shell, the lower end of a swing bolt is articulated with the left end of the base, the upper part of the swing bolt has a nut, and the lower part has a sleeve which is provided with a thread via hole and a taper hole, the opposite end surfaces of the nut and the sleeve are provided with engaged end teeth, and the battery shell at the left side of the battery group is provided with a fastening hook which is corresponding to the taper hole in the sleeve on the swing bolt. The base outside the front roller and the back roller is provided with a vertical guide board. The installing structure is used for the airplane storage battery group.
Description
Technical field:
The utility model relates to a kind of self-contained battery group mechanism, particularly a kind of installing mechanism of aircraft batteries.
Background technology:
All need be equipped with batteries on the civilian or military aircraft.Battery pack at first is contained on the pallet, be fixed to be integral on the guide rail that is placed in the battery compartment with bolt and pressing plate and advance in the battery compartment, with pin that battery pack is fixing in the horizontal direction, for the collision that prevents that battery pack and battery compartment top from producing because of vibration, be placed on rubber blanket on the end face of battery pack, rubber blanket is connected on the battery bulkhead with rope, when battery pack is detected, when maintenance or replacing, need extract the location pin, after taking out battery pack and pallet, unscrew nut battery pack is taken off from pallet, could change or overhaul battery pack, dismounting is time-consuming, and battery pack is fixing not tight at above-below direction, has potential safety hazard.
Summary of the invention:
The purpose of this utility model is a kind of installing mechanism of installing and removing convenient and fixed aircraft batteries of design.The technical solution of the utility model is, the mounting structure of aircraft batteries, comprise base and slideway, it is characterized in that: base through screws is fixed on the base plate of battery compartment, before roller is located at base, in the groove in the upper surface of back both sides, roller shaft places in the hole of groove both sides, roller is higher than the surface of base, locating piece is connected with the right-hand member of base by screw, the inclined-plane that is provided with the tightening plate on groove with the level and the battery case in the locating piece is relative, the lower end and the base left end that wave bolt are hinged; nut is arranged at the top of rocking arm bolt, and cover is arranged at the bottom, and screw thread via hole and taper hole are arranged in the cover; be provided with intermeshing end tooth on the opposing end faces of nut and cover, and the taper hole of the cover on the battery case in battery pack left side is provided with the tightening hook and waves bolt matches.Be provided with vertical guide plate on the base outside forward and backward roller.The utility model has the mounting or dismounting convenience compared with the prior art and fixation can vibrative advantage.
Description of drawings:
Fig. 1 is the front view of the installing mechanism of the utility model aircraft batteries, and Fig. 2 is the vertical view of Fig. 1.
Embodiment:
In conjunction with above accompanying drawing the utility model is described in detail, base 1 is provided with the screw thread via hole, base is fixed on the base plate of battery compartment with screw, roller 5 places before and after the base in the groove on the both side surface, exceed the surface of base plate above the roller, roller shaft is through in the hole of base groove both sides, before and after base, be provided with horizontal limiting plate 7 outside the groove of both sides, on the right-hand member caster bed face of base, be provided with backing plate successively, locating piece 2, backing plate and locating piece are provided with the screw thread via hole, screw 3 places above-mentioned screw thread via hole and screwed hole on the base to match, above-mentioned locating piece and cushion block and base are solidly fixed, on the end face of the left end head of above-mentioned base, be provided with overhanging convex body, the termination and the above-mentioned convex body that wave bolt 11 are hinged, nut 9 matches with the screw thread that waves bolt, on the bolt cylinder below the nut 9, be with 10, on the opposing end faces of above-mentioned nut and cover, be provided with the tooth that is meshed, there are a taper hole or post hole in body inside, and the bottom of the battery container in battery pack left side is provided with an overhanging hook 8.
Mounting and dismounting method of the present utility model is, at first base is fixed by bolts on the base plate in aircraft battery storehouse, and original slideway is removed, the battery pack 6 that assembles is placed on is advanced in the battery compartment to the right on the roller of base left end, when the overhanging tightening plate 4 in battery pack right side enters in the groove of locating piece 2 at the ramp of tightening plate with till the step of locating piece contacts, with the nut on the bolt 11 be threaded to the upper end after, put and move and when body inner cone hole wall being contacted bolt rotation to the right with the inclined-plane of tightening hook, the rotation nut makes cover and tightening hook compress and lock to moving down.When needs detect battery pack or during maintain and replace, to wave bolt after the disengagement of tightening hook, can haul out battery compartment to battery pack from the roller of base, thereby install and remove convenient and swift, simultaneously, because tightening plate on the battery-pack exterior casing and tightening hook are with locating piece and wave bolt battery pack and base and battery compartment base plate are solidly fixed, thereby fixation can not produce and vibrates the dangerous phenomenon of generation.
Claims (2)
1, the mounting structure of aircraft batteries, comprise base and slideway, it is characterized in that: base through screws is fixed on the base plate of battery compartment, before roller is located at base, in the groove in the upper surface of back both sides, roller shaft places in the hole of groove both sides, roller is higher than the surface of base, locating piece is connected with the right-hand member of base by screw, the inclined-plane that is provided with the tightening plate on groove with the level and the battery case in the locating piece is relative, the lower end and the base left end that wave bolt are hinged; nut is arranged at the top of rocking arm bolt; cover is arranged at the bottom; screw thread via hole and taper hole are arranged in the cover, are provided with intermeshing end tooth on the opposing end faces of nut and cover, and the taper hole of the cover on the battery case in battery pack left side is provided with the tightening hook and waves bolt matches.
2, the mounting structure of aircraft batteries as claimed in claim 1 is characterized in that: be provided with vertical guide plate on the base outside forward and backward roller.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNU2008201489867U CN201266626Y (en) | 2008-08-29 | 2008-08-29 | Mounting structure of aeroplane accumulator set |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNU2008201489867U CN201266626Y (en) | 2008-08-29 | 2008-08-29 | Mounting structure of aeroplane accumulator set |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN201266626Y true CN201266626Y (en) | 2009-07-01 |
Family
ID=40833001
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CNU2008201489867U Expired - Fee Related CN201266626Y (en) | 2008-08-29 | 2008-08-29 | Mounting structure of aeroplane accumulator set |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN201266626Y (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105702897A (en) * | 2016-04-13 | 2016-06-22 | 江苏峰谷源储能技术研究院有限公司 | Stable type 6.4V and 100Ah energy storage battery module |
| CN105742537A (en) * | 2016-04-13 | 2016-07-06 | 江苏峰谷源储能技术研究院有限公司 | Shock-resistant 6.4V and 100Ah energy storage battery module |
| CN105938886A (en) * | 2016-04-13 | 2016-09-14 | 江苏峰谷源储能技术研究院有限公司 | Easy-to-assemble 6.4V and 100Ah energy storage battery module |
| CN105938885A (en) * | 2016-04-13 | 2016-09-14 | 江苏峰谷源储能技术研究院有限公司 | 6.4V and 100Ah energy storage battery module |
-
2008
- 2008-08-29 CN CNU2008201489867U patent/CN201266626Y/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105702897A (en) * | 2016-04-13 | 2016-06-22 | 江苏峰谷源储能技术研究院有限公司 | Stable type 6.4V and 100Ah energy storage battery module |
| CN105742537A (en) * | 2016-04-13 | 2016-07-06 | 江苏峰谷源储能技术研究院有限公司 | Shock-resistant 6.4V and 100Ah energy storage battery module |
| CN105938886A (en) * | 2016-04-13 | 2016-09-14 | 江苏峰谷源储能技术研究院有限公司 | Easy-to-assemble 6.4V and 100Ah energy storage battery module |
| CN105938885A (en) * | 2016-04-13 | 2016-09-14 | 江苏峰谷源储能技术研究院有限公司 | 6.4V and 100Ah energy storage battery module |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C17 | Cessation of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20090701 Termination date: 20090929 |