CN205752324U - A kind of fixed mechanism of aircraft battery - Google Patents
A kind of fixed mechanism of aircraft battery Download PDFInfo
- Publication number
- CN205752324U CN205752324U CN201620612643.6U CN201620612643U CN205752324U CN 205752324 U CN205752324 U CN 205752324U CN 201620612643 U CN201620612643 U CN 201620612643U CN 205752324 U CN205752324 U CN 205752324U
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- China
- Prior art keywords
- lid
- locking member
- groove
- box body
- fixed mechanism
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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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- Battery Mounting, Suspending (AREA)
Abstract
The utility model discloses the fixed mechanism of a kind of aircraft battery, including box body, lid and retaining mechanism, described box body includes the cavity volume with opening, described lid is arranged on the opening of box body, lid includes the first lid and the second lid, described first lid is fixedly installed on box body, first lid is provided with draw-in groove near the end face of the second lid, described retaining mechanism includes sliding part and locking member, described locking member stretches in described draw-in groove, described sliding part is slidably disposed on the second lid, one end of sliding part through the second lid and is connected with described locking member, sliding of sliding part drives locking member to slide along the direction of the first lid to the second lid.The fixed mechanism of a kind of aircraft battery that this utility model provides, not only versatility is good, and avoids using the fixtures such as screw so that easy accessibility, the most also has the technique effect of simple in construction.
Description
Technical field
This utility model relates to aircraft field, particularly relates to the fixed mechanism of a kind of aircraft battery.
Background technology
Carry-on battery, as the important devices of aircraft, for providing the flying power of aircraft.Aircraft exists
Flight course easily produces vibration, in order to prevent battery because rocking or mobile, and and connection between equipment to be powered produce
Loosen, cause aircraft to occur abnormal, battery need to be fixed on board the aircraft.
The Chinese invention patent of Application No. 201510998771.9 discloses a kind of battery and aircraft, described battery bag
Include battery core, battery container, at least one unblock button and at least one first power connector；Described battery core is positioned at described battery
In housing, at least one each unblock button unlocked in button described is arranged on described battery container, described unblock button
Including button, resilient panel, button erecting bed and the first tight lock part, described button erecting bed is provided with installing hole, described button bag
Include press section and axle is installed；Described resilient panel is fixed on described battery container, and described button erecting bed is fixed on described electricity
On the housing of pond, and described resilient panel is between described battery container and described button erecting bed；One end of described installation axle
Being fixed on described press section, the other end contacts through described installing hole with described resilient panel, and described first tight lock part is positioned at
Around described resilient panel；Described aircraft is provided with battery settling groove, is provided with and described battery in described battery settling groove
In the second tight lock part corresponding to the first tight lock part of each unblock button, the first tight lock part and the second tight lock part coordinate, by institute
State battery lock in battery settling groove.In above-mentioned patent, the unblock button for self-contained battery need to be arranged on battery, for one
As battery will be unable to be fixed in battery settling groove, the versatility of above-mentioned fixed form is poor, is unfavorable for using on a large scale；With
Time, the structure of this unblock button is more complicated, can increase manufacturing cost.
Additionally, in the prior art, fix also by the mode being screwed battery cover on battery settling groove
Battery, during fetching battery, needs to unscrew screw, is taken out by battery again, then re-use screw by battery after being taken off by battery cover
Lid is fixed on battery settling groove.The installation and removal process of this kind of mode battery cover is cumbersome, and under screw dismounting after easily
Lose, without standby screw, will be unable to self-contained battery lid, make troubles to use.
Utility model content
Technical problem to be solved in the utility model is: provide the aircraft battery of a kind of simple in construction and easy accessibility
Fixed mechanism.
In order to solve above-mentioned technical problem, the technical solution adopted in the utility model is:
The fixed mechanism of a kind of aircraft battery, including box body, lid and retaining mechanism, described box body includes having opening
Cavity volume, described lid is arranged on the opening of box body, and lid includes that the first lid and the second lid, described first lid are fixed
Being arranged on box body, the first lid is provided with draw-in groove near the end face of the second lid, and described retaining mechanism includes sliding part and lock
Tight part, described locking member stretches in described draw-in groove, and described sliding part is slidably disposed on the second lid, one end of sliding part
Being connected through the second lid and with described locking member, sliding of sliding part drives locking member along the side of the first lid to the second lid
To slip.
Further, described retaining mechanism also includes that elastic component, one end of described elastic component are arranged on described second lid
On, the other end of elastic component is arranged on described locking member.
Further, also include that banking stop, described elastic component are arranged between the second lid and banking stop and prop up described
Banking stop.
Further, the material of described banking stop is rustless steel.
Further, the surface of the bottom of described draw-in groove is inclined plane, and described locking member stretches into the end of one end of draw-in groove
Surface be inclined plane.
Further, described locking member is provided with stage portion near one end of described draw-in groove, and described stage portion stretches into described card
In groove.
Further, described locking member is provided with locating slot, and described sliding part is connected with locking member by described locating slot.
Further, also include that shell fragment, described shell fragment are arranged on described box body and prop up described lid.
Further, described second lid is hinged on described box body away from one end of described first lid.
Further, the marginal position of described cavity volume is provided with groove.
The beneficial effects of the utility model are: be arranged in the cavity volume on box body by battery, and arrange lid on box body
Body, can be stably placed at battery in the closing space of box body and lid composition, without arranging unblock button on battery, logical
Good by property, the installation being adaptable to multiple battery is fixed；First lid is provided with draw-in groove, and sliding part is slidably arranged, sliding part
Driving locking member to slide during slip, the slip of locking member makes locking member stretch into or away from draw-in groove, thus realizes the lock of the second lid
Tight or open；Avoid using the accessories such as screw to be fixed, not only easy accessibility, and simple in construction.
Accompanying drawing explanation
Fig. 1 is the decomposing schematic representation of the fixed mechanism of the aircraft battery of this utility model embodiment；
Fig. 2 is the combination schematic diagram of the fixed mechanism of the aircraft battery of this utility model embodiment；
Fig. 3 is the second lid profile at A in Fig. 2 when being in locking state；
Fig. 4 is the second lid profile at A in Fig. 2 when being in opening.
Label declaration:
1, box body；11, cavity volume；111, groove；2, lid；21, the first lid；211, draw-in groove；22, the second lid；31, sliding
Moving part；32, locking member；321, locating dowel；322, stage portion；323, locating slot；33, elastic component；4, banking stop；5, shell fragment；6、
Rotating shaft；7, battery.
Detailed description of the invention
By describing technology contents of the present utility model, structural feature in detail, being realized purpose and effect, below in conjunction with enforcement
Mode also coordinates accompanying drawing to be explained in detail.
The design of this utility model most critical is: arrange retaining mechanism, can avoid using the fixtures such as screw to carry out solid
Fixed, it is not only simple in structure, and easy accessibility.
Referring to Fig. 1 to Fig. 4, the fixed mechanism of a kind of aircraft battery, including box body 1, lid 2 and retaining mechanism, institute
Stating box body 1 and include having the cavity volume 11 of opening, described lid 2 is arranged on the opening of box body 1, and lid 2 includes the first lid 21
With the second lid 22, described first lid 21 is fixedly installed on box body 1, and the first lid 21 is near the end face of the second lid 22
Being provided with draw-in groove 211, described retaining mechanism includes that sliding part 31 and locking member 32, described locking member 32 stretch in described draw-in groove 211,
Described sliding part 31 is slidably disposed on the second lid 22, one end of sliding part 31 through the second lid 22 and with described lock
Tight part 32 connects, and sliding of sliding part 31 drives locking member 32 to slide along the direction of the first lid 21 to the second lid 22.
Knowable to foregoing description, the beneficial effects of the utility model are: be arranged in the cavity volume on box body by battery, and
Box body arranges lid, battery can be stably placed at box body and lid composition closing space in, on battery without
Arranging unblock button, versatility is good, and the installation being adaptable to multiple battery is fixed；First lid is provided with draw-in groove, and sliding part can
Sliding and arrange, drive locking member to slide when sliding part slides, the slip of locking member makes locking member stretch into or away from draw-in groove, thus real
The locking of existing second lid or unlatching；Avoid using the accessories such as screw to be fixed, not only easy accessibility, and simple in construction.
Further, described retaining mechanism also includes that elastic component 33, one end of described elastic component 33 are arranged on described second
On lid 22, the other end of elastic component 33 is arranged on described locking member 32.
Seen from the above description, elastic component can be spring, and when the second lid is closed, locking member is stretched under the effect of elastic component
Entering in draw-in groove, realize the first lid and the connection of the second lid by locking member, when opening the second lid, elastic component is in compression
State, locking member stretches out draw-in groove.
Further, also include that banking stop 4, described elastic component 33 are arranged between described second lid 22 and banking stop 4
And prop up described banking stop 4.
Seen from the above description, banking stop is set, can prevent elastic component such as spring from arching upward when being in compressive state, with spacing
Sheet pushes down elastic component can play the position-limiting action to elastic component, and can prevent elastic component from blocking when stretching, and makes elastic component flexible more
Smooth and easy.
Further, the material of described banking stop 4 is rustless steel.
Seen from the above description, the material of banking stop is rustless steel, and stainless surface is more smooth, can be to elastic component such as bullet
The long-term flexible of spring plays a wear-resisting effect, makes telescopic spring more smooth and easy, and the exception that will not block or produce " click click " is loud
Sound.
Further, the surface of the bottom of described draw-in groove 211 is inclined plane, and described locking member 32 stretches into the one of draw-in groove 211
The surface of the end of end is inclined plane.
Seen from the above description, the bottom of draw-in groove is inclined plane, and the end of locking member is that the bottom with draw-in groove matches
Inclined plane, makes locking piece be easy to when sliding snap in, and has certain guide effect.
Further, described locking member 32 is provided with stage portion 322, described stage portion 322 near one end of described draw-in groove 211
Stretch in described draw-in groove 211.
Seen from the above description, locking member arranges stage portion, can the sliding stroke of locking member be carried out spacing.
Further, described locking member 32 is provided with locating slot 323, described sliding part 31 by described locating slot 323 with
Locking member 32 connects.
Seen from the above description, locking member arranging locating slot, sliding part can be with the locating slot close-fitting on locking member or adopt
It is attached by mode for dispensing glue.
Further, also include that shell fragment 5, described shell fragment 5 are arranged on described box body 1 and prop up described lid 2.
Seen from the above description, when the second lid is opened, shell fragment is in the state of flicking, and when battery cover closes, shell fragment is in
Compressive state, when promoting sliding part to make locking member stretch out draw-in groove, the second lid is pushed open certain angle by shell fragment, conveniently will with hands
Battery cover pulls open.
Further, described second lid 22 is hinged on described box body 1 away from one end of described first lid 21.
Seen from the above description, the second lid is hinged on box body, and when the second lid is opened, the second lid is without departing from box
Body itself, which prevent when box body is opened the possibility coming off, losing.
Further, the marginal position of described cavity volume 11 is provided with groove 111.
Seen from the above description, the marginal position of cavity volume is provided with groove, can conveniently put into cavity volume battery pick and place behaviour
Make, and the hand-held groove facilitating battery taking and placing can be set on battery.
Refer to Fig. 1 to Fig. 4, embodiment one of the present utility model is:
The fixed mechanism of a kind of aircraft battery, including box body 1, lid 2, retaining mechanism, banking stop 4 and shell fragment 5, box body
1 includes the cavity volume 11 with opening, and cavity volume 11 is for placing battery 7, and the marginal position of cavity volume 11 is provided with groove 111, lid 2
Being arranged on the opening of box body 1, lid 2 includes the first lid 21 and the second lid 22, and the first lid 21 is fixedly installed on box body 1
On, the second lid 22 can open and close to be arranged on box body 1, and the second lid 22 is cut with scissors by rotating shaft 6 away from one end of the first lid 21
It is connected on box body 1.
First lid 21 is provided with draw-in groove 211 near the end face of the second lid 22, and retaining mechanism includes sliding part 31, locking
Part 32 and elastic component 33, sliding part 31 is arranged on second lid 22 side away from box body 1, and locking member 32 is arranged on the second lid
The opposite side of 22, sliding part 31 is slidably disposed on the second lid 22, and one end of sliding part 31 is through the second lid 22 also
Being connected with locking member 32, sliding of sliding part 31 drives locking member 32 to slide along the direction of the first lid 21 to the second lid 22,
When locking member 32 slides, in draw-in groove 211 is stretched in one end of locking member 32 or away from draw-in groove 211.Set on the other end of locking member 32
Having locating dowel 321, one end of elastic component 33 to be arranged on the second lid 22, the other end of elastic component 33 is set in locating dowel 321
On.Banking stop 4 is arranged on the second lid 22 in the one side of box body 1, and elastic component 33 is arranged at the second lid 22 and banking stop 4
Between and prop up banking stop 4.The material of banking stop 4 is rustless steel.
The surface of the bottom of draw-in groove 211 is inclined plane, locking member 32 stretch into the surface of the end of one end of draw-in groove 211 for
The inclined plane that the bottom of draw-in groove 211 matches.Locking member 32 is additionally provided with stage portion 322 and locating slot 323, and stage portion 322 stretches into
In draw-in groove 211.One end that sliding part 31 is connected with locking member 32 is arranged in locating slot 323, and sliding part 31 and locking member 32 can
It is attached by close-fitting or mode for dispensing glue.Shell fragment 5 is arranged on box body 1 and props up lid 2.
In sum, the fixed mechanism of a kind of aircraft battery that this utility model provides, not only versatility is good, and keeps away
Exempt to use the fixtures such as screw so that easy accessibility, the most also there is the technique effect of simple in construction.
The foregoing is only embodiment of the present utility model, not thereby limit the scope of the claims of the present utility model, every
Utilize the equivalents that this utility model description and accompanying drawing content are made, or be directly or indirectly used in relevant technology neck
Territory, is the most in like manner included in scope of patent protection of the present utility model.
Claims (10)
1. the fixed mechanism of an aircraft battery, it is characterised in that include box body, lid and retaining mechanism, described box body bag
Including the cavity volume with opening, described lid is arranged on the opening of box body, and lid includes the first lid and the second lid, and described
One lid is fixedly installed on box body, and the first lid is provided with draw-in groove near the end face of the second lid, and described retaining mechanism includes
Sliding part and locking member, described locking member stretches in described draw-in groove, and described sliding part is slidably disposed on the second lid, sliding
One end of moving part is through the second lid being connected with described locking member, and the slip of sliding part drives locking member along the first lid to the
Slide in the direction of two lids.
The fixed mechanism of aircraft battery the most according to claim 1, it is characterised in that described retaining mechanism also includes bullet
Property part, one end of described elastic component is arranged on described second lid, and the other end of elastic component is arranged on described locking member.
The fixed mechanism of aircraft battery the most according to claim 2, it is characterised in that also include banking stop, described bullet
Property part is arranged between the second lid and banking stop and props up described banking stop.
The fixed mechanism of aircraft battery the most according to claim 3, it is characterised in that the material of described banking stop is not
Rust steel.
The fixed mechanism of aircraft battery the most according to claim 1, it is characterised in that the surface of the bottom of described draw-in groove
For inclined plane, it is inclined plane that described locking member stretches into the surface of the end of one end of draw-in groove.
The fixed mechanism of aircraft battery the most according to claim 1, it is characterised in that described locking member is near described card
One end of groove is provided with stage portion, and described stage portion stretches in described draw-in groove.
The fixed mechanism of aircraft battery the most according to claim 1, it is characterised in that described locking member is provided with location
Groove, described sliding part is connected with locking member by described locating slot.
The fixed mechanism of aircraft battery the most according to claim 1, it is characterised in that also include shell fragment, described shell fragment
It is arranged on described box body and props up described lid.
The fixed mechanism of aircraft battery the most according to claim 1, it is characterised in that described second lid is away from described
One end of first lid is hinged on described box body.
The fixed mechanism of aircraft battery the most according to claim 1, it is characterised in that the marginal position of described cavity volume
It is provided with groove.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620612643.6U CN205752324U (en) | 2016-06-21 | 2016-06-21 | A kind of fixed mechanism of aircraft battery |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620612643.6U CN205752324U (en) | 2016-06-21 | 2016-06-21 | A kind of fixed mechanism of aircraft battery |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205752324U true CN205752324U (en) | 2016-11-30 |
Family
ID=57383555
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620612643.6U Active CN205752324U (en) | 2016-06-21 | 2016-06-21 | A kind of fixed mechanism of aircraft battery |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205752324U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105977421A (en) * | 2016-06-21 | 2016-09-28 | 深圳市高巨创新科技开发有限公司 | Fixing mechanism for aircraft battery |
-
2016
- 2016-06-21 CN CN201620612643.6U patent/CN205752324U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105977421A (en) * | 2016-06-21 | 2016-09-28 | 深圳市高巨创新科技开发有限公司 | Fixing mechanism for aircraft battery |
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| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant |