CN208817068U - A kind of aviation aluminum profile of advanced composite material (ACM) - Google Patents
A kind of aviation aluminum profile of advanced composite material (ACM) Download PDFInfo
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- CN208817068U CN208817068U CN201821138571.1U CN201821138571U CN208817068U CN 208817068 U CN208817068 U CN 208817068U CN 201821138571 U CN201821138571 U CN 201821138571U CN 208817068 U CN208817068 U CN 208817068U
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- aluminium sheet
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- block
- bullet
- link
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Abstract
The utility model discloses a kind of aviation aluminum profiles of advanced composite material (ACM), including bindiny mechanism and damping, the bindiny mechanism includes aluminium sheet, one side surface of aluminium sheet offers the card slot of integral structure, the card slot both ends are connected with limited block, and the limited block side is internally connected with link block b relative to aluminium sheet relative to spring b, the limited block top is fixed with inside aluminium sheet, the aluminium sheet is connected with bullet block away from the side of card slot, and bullet block surface offers limiting slot；By being connected with bullet block and card slot in aluminium sheet two sides, aluminium sheet is installed convenient for staff, is dismantled, and it avoids because junction loosening leads to occur gap between aluminium sheet, the labor intensity of staff is effectively reduced, and improves the working efficiency of staff, by being fixed with damper inside aluminium sheet, and vibration damper plate is connected in aluminium sheet two sides, it avoids aluminium sheet after by external force, because itself generates vibration, connector is caused to loosen, fall off.
Description
Technical field
The utility model belongs to aluminum profile technical field, and in particular to a kind of aviation aluminum profile of advanced composite material (ACM).
Background technique
Titanium-plating technology for aluminium section material belongs to coating technique, it is to increase preplating and plating on the basis of conventional technology for plating titanium
Processing step, aluminum profile technique are that the plating piece after activation is placed in the aqueous solution of salt and hydrochloric acid to be chemically treated, and are electroplated
The plating solution composition of technique includes nickel sulfate, nickel chloride, boric acid, lauryl sodium sulfate, saccharin, brightener.This technique has letter
The advantages that single, practical, effect is good, than plating under Ticoated aluminium shaped material its film hardness HV ≈ 1500, equal conditions made from this technique
Wear-resisting 150 times of 22K gold, it can be processed into gold, the colour of various forms, bright a variety of serial aluminium profile products such as black.
However the aviation of existing advanced composite material (ACM) with aluminum profile during use there are still some shortcomings,
The aviation of existing advanced composite material (ACM) with aluminum profile when in use:
1. the aviation aluminum profile of existing advanced composite material (ACM) is during installation, not convenient for staff in aluminium
The device spliced between profile not only causes a degree of work difficulty to staff, reduces staff's
Working efficiency, and be not easy to increase the connection between aluminum profile, so that aluminum profile is after a period of use, and because connection loosens, aluminium
Occurs crack between profile.
2. the aviation of existing advanced composite material (ACM) with aluminum profile during use, may be by external influence
Cause itself to generate vibration in the case where power, so that junction loosens, reduces the service life of aluminum profile.
Utility model content
The purpose of this utility model is to provide a kind of aviation aluminum profiles of advanced composite material (ACM), to solve above-mentioned background
The aviation aluminum profile of existing advanced composite material (ACM) is proposed in technology during installation, not convenient for staff in aluminium
The device spliced between profile not only causes a degree of work difficulty to staff, reduces staff's
Working efficiency, and be not easy to increase the connection between aluminum profile, so that aluminum profile is after a period of use, and because connection loosens, aluminium
Occur crack between profile, the aviation of existing advanced composite material (ACM) with aluminum profile during use, may by
Cause itself to generate vibration in the case where external forces, so that junction loosens, reduces the service life of aluminum profile
The problem of.
To achieve the above object, the utility model provides the following technical solutions: a kind of aviation aluminium of advanced composite material (ACM)
Profile, including bindiny mechanism and damping, the bindiny mechanism include aluminium sheet, and one side surface of aluminium sheet offers integral type
The card slot of structure, the card slot both ends are connected with limited block, the limited block side relative to being fixed with spring b inside aluminium sheet,
It is internally connected with link block b relative to aluminium sheet at the top of the limited block, the aluminium sheet is connected with bullet block, institute away from the side of card slot
It states bullet block surface and offers limiting slot, bullet block side is internally connected with spring a relative to aluminium sheet, and the bullet block top is opposite
It is fixed with link block a inside aluminium sheet, and offers bullet block slot inside the aluminium sheet, the bullet block groove top portion is relative to aluminium sheet table
Face offers aluminium sheet loose slot, and the aluminium sheet top and bottom is connected with vibration damper plate, and the damping plate surface offers loose slot a
With loose slot b, and the loose slot a and loose slot b are internally connected with link block a and link block b.
Preferably, the damping includes aluminium sheet, offers damping tank inside the aluminium sheet, in the damping tank
Portion is fixed with damper, and the damping plate surface offers link slot compatible with damper.
Preferably, aluminium sheet is run through in the link block a and the one end link block b, and at the top of the link block a and link block b with
Same level height is at the top of loose slot a, loose slot b.
Preferably, the bullet block can spring a compress in the state of taken in inside bullet block slot completely, and the limited block with
Limiting slot is adapted, and the bullet block is adapted with card slot.
Preferably, the link slot is corresponding with damping slot locations, and the link slot, damping tank are in damping
The quadrangle of plate, aluminium sheet, and position corresponds to each other.
Compared with prior art, the utility model has the beneficial effects that
1. installing, dismantling to aluminium sheet convenient for staff, and keep away by being connected with bullet block and card slot in aluminium sheet two sides
Exempt to lead to occur gap between aluminium sheet because junction loosens, has effectively reduced the labor intensity of staff, and improve
The working efficiency of staff.
2. be connected with vibration damper plate by being fixed with damper inside aluminium sheet, and in aluminium sheet two sides, avoid aluminium sheet by
To after external force, because itself generates vibration, causes connector to loosen, fall off, effectively extend the service life of aluminium sheet, have
Effect is that user reduces use cost.
Detailed description of the invention
Fig. 1 is the structural schematic diagram of the utility model；
Fig. 2 is the cross-sectional view of the utility model aluminium sheet；
Fig. 3 is the plan view of the utility model aluminium sheet；
Fig. 4 is the cross-sectional view of the utility model damping tank；
In figure: 1, vibration damper plate；2, loose slot a；3, link block a；4, bullet block；5, link block b；6, loose slot b；7, aluminium sheet；
8, limited block；9, card slot；10, spring a；11, aluminium sheet loose slot；12, limiting slot；13, bullet block slot；14, spring b；15, it connects
Slot；16, damping tank.
Specific embodiment
The following will be combined with the drawings in the embodiments of the present invention, carries out the technical scheme in the embodiment of the utility model
Clearly and completely describe, it is clear that the described embodiments are only a part of the embodiments of the utility model, rather than whole
Embodiment.Based on the embodiments of the present invention, those of ordinary skill in the art are without making creative work
Every other embodiment obtained, fall within the protection scope of the utility model.
Embodiment one
Fig. 1-Fig. 4 is please referred to, the utility model provides a kind of technical solution: a kind of aviation aluminium profiles of advanced composite material (ACM)
Material, including bindiny mechanism and damping, bindiny mechanism include aluminium sheet 7, and 7 one side surface of aluminium sheet offers the card of integral structure
There is limited block 8 at slot 9,9 both ends of card slot by being fixed, and there is bullet in 8 side of limited block by being fixed relative to inside aluminium sheet 7
Spring b14,8 top of limited block are welded with bullet block away from the side of card slot 9 relative to link block b5, aluminium sheet 7 is pasted with inside aluminium sheet 7
4,4 surface of bullet block offers limiting slot 12, and there is spring a10 in 4 side of bullet block relative to 7 interior welds of aluminium sheet, and 4 top of bullet block is opposite
There is link block a3 by being fixed inside aluminium sheet 7, and offer bullet block slot 13 inside aluminium sheet 7,13 top of bullet block slot is opposite
Aluminium sheet loose slot 11 is offered in 7 surface of aluminium sheet, 7 top and bottom of aluminium sheet is connected with vibration damper plate 1, vibration damper plate 1 by damper
Surface offers loose slot a2 and loose slot b6, and loose slot a2 and loose slot b6 are internally connected with link block a3 and link block
b5。
For the ease of 7 damping of aluminium sheet, in the present embodiment, it is preferred that damping includes aluminium sheet 7, is offered inside aluminium sheet 7
Damper has been bolted inside damping tank 16 in damping tank 16, and 1 surface of vibration damper plate is offered to be adapted with damper
Link slot 15.
It is displaced for the ease of generating bullet block 4 and limited block 8 by link block a3 and link block b5, it is excellent in the present embodiment
Choosing, aluminium sheet 7, and the top link block a3 and link block b5 and loose slot a2, activity are run through in link block a3 and the one end link block b5
Same level height is at the top of slot b6.
For the ease of being connected with each other two blocks of aluminium sheets 7, in the present embodiment, it is preferred that bullet block 4 can be compressed in spring a10
It is taken in completely under state inside bullet block slot 13, and limited block 8 is adapted with limiting slot 12, bullet block 4 is adapted with card slot 9.
In order to increase the damping property of aluminium sheet 7, in the present embodiment, it is preferred that link slot 15 is opposite with 16 position of damping tank
It answers, and link slot 15, damping tank 16 are in the quadrangle of vibration damper plate 1, aluminium sheet 7, and position corresponds to each other.
Embodiment two
Fig. 1-Fig. 4 is please referred to, the utility model provides a kind of technical solution: a kind of aviation aluminium profiles of advanced composite material (ACM)
Material, including bindiny mechanism and damping, bindiny mechanism include aluminium sheet 7, and 7 one side surface of aluminium sheet offers the card of integral structure
Slot 9,9 both ends of card slot have been bolted limited block 8, and 8 side of limited block is relative to being bolted bullet inside aluminium sheet 7
There is link block b5 at spring b14,8 top of limited block relative to 7 interior welds of aluminium sheet, and aluminium sheet 7 is connected away from the side of card slot 9 by bolt
It is connected to bullet block 4,4 surface of bullet block offers limiting slot 12, and 4 side of bullet block is relative to being bolted spring inside aluminium sheet 7
A10, there is link block a3 at 4 top of bullet block relative to 7 interior welds of aluminium sheet, and bullet block slot 13 is offered inside aluminium sheet 7, bullet block slot 13
Top offers aluminium sheet loose slot 11 relative to 7 surface of aluminium sheet, and 7 top and bottom of aluminium sheet is connected with vibration damper plate 1 by damper,
1 surface of vibration damper plate offers loose slot a2 and loose slot b6, and loose slot a2 and loose slot b6 be internally connected with link block a3 with
Link block b5.
For the ease of 7 damping of aluminium sheet, in the present embodiment, it is preferred that damping includes aluminium sheet 7, is offered inside aluminium sheet 7
Damping tank 16,16 interior welds of damping tank have damper, and 1 surface of vibration damper plate offers link slot compatible with damper
15。
It is displaced for the ease of generating bullet block 4 and limited block 8 by link block a3 and link block b5, it is excellent in the present embodiment
Choosing, aluminium sheet 7, and the top link block a3 and link block b5 and loose slot a2, activity are run through in link block a3 and the one end link block b5
Same level height is at the top of slot b6.
For the ease of being connected with each other two blocks of aluminium sheets 7, in the present embodiment, it is preferred that bullet block 4 can be compressed in spring a10
It is taken in completely under state inside bullet block slot 13, and limited block 8 is adapted with limiting slot 12, bullet block 4 is adapted with card slot 9.
In order to increase the damping property of aluminium sheet 7, in the present embodiment, it is preferred that link slot 15 is opposite with 16 position of damping tank
It answers, and link slot 15, damping tank 16 are in the quadrangle of vibration damper plate 1, aluminium sheet 7, and position corresponds to each other.
The working principle and process for using of the utility model: by being respectively equipped with card slot 9 and bullet block 4 in 7 two sides of aluminium sheet, benefit
It is attached with card slot 9 between two blocks of aluminium sheets 7 with the engaging of bullet block 4, and by being connected with limited block 8 in card slot 9, in bullet
4 surface of block offers limiting slot 12, using being fixed between limiting slot 12 and limited block 8, convenient for carrying out two blocks of aluminium sheets 7
It is fixed, it is connected with vibration damper plate 1 in 7 two sides of aluminium sheet by being fixed with damper inside aluminium sheet 7, and by damper, is utilized
After damper stress, inhibit the effect of telescopic spring, avoid aluminium sheet 7 after stress, generates vibration.
By pulling link block b5 to two sides, so that limited block 8 is taken in inside aluminium sheet 7, then by pushing link block a3
So that bullet block 4 stretches out aluminium sheet 7 and makes spring a10 flexible, then by the bullet block 4 on 7 surface of aluminium sheet and another 7 surface of aluminium sheet
Card slot 9 is engaged, and by pushing away link block b5 to centre, so that limited block 8 is fixed with limiting slot 12, to press down
Spring a10 processed is shunk, and when aluminium sheet 7 is by external force power, absorber active force, and is inhibited contained spring retractility, is kept away
Exempt from aluminium sheet 7 and generates vibration, it, can be by pulling link block b5 to two sides, so that limiting slot 12 when needing to remove aluminium sheet 7
It is detached from limited block 8, under the action of spring a10, bullet block 4 is withdrawn inside another aluminium sheet 7.
While there has been shown and described that the embodiments of the present invention, for the ordinary skill in the art,
It is understood that these embodiments can be carried out with a variety of variations in the case where not departing from the principles of the present invention and spirit, repaired
Change, replacement and variant, the scope of the utility model is defined by the appended claims and the equivalents thereof.
Claims (5)
1. a kind of aviation aluminum profile of advanced composite material (ACM), including bindiny mechanism and damping, it is characterised in that: the company
Connection mechanism includes aluminium sheet (7), and (7) one side surface of aluminium sheet offers the card slot (9) of integral structure, the card slot (9) two
End is connected with limited block (8), and limited block (8) side is fixed with spring b(14 relative to aluminium sheet (7) inside), the limit
Link block b(5 is internally connected with relative to aluminium sheet (7) at the top of block (8)), the aluminium sheet (7) is connected with away from the side of card slot (9)
Bullet block (4), bullet block (4) surface offer limiting slot (12), and bullet block (4) side is connected relative to inside aluminium sheet (7)
Have spring a(10), bullet block (4) top is fixed with link block a(3 relative to aluminium sheet (7) inside), and in the aluminium sheet (7)
Portion offers bullet block slot (13), and bullet block slot (13) top offers aluminium sheet loose slot (11), institute relative to aluminium sheet (7) surface
State aluminium sheet (7) top and bottom to be connected with vibration damper plate (1), vibration damper plate (1) surface offers loose slot a(2) and loose slot b
(6), and the loose slot a(2) with loose slot b(6) be internally connected with link block a(3) and with link block b(5).
2. a kind of aviation aluminum profile of advanced composite material (ACM) according to claim 1, it is characterised in that: the damping machine
Structure includes aluminium sheet (7), is offered damping tank (16) inside the aluminium sheet (7), is fixed with and subtracts inside the damping tank (16)
Device is shaken, vibration damper plate (1) surface offers link slot (15) compatible with damper.
3. a kind of aviation aluminum profile of advanced composite material (ACM) according to claim 1, it is characterised in that: the link block
A(3) with link block b(5) one end run through aluminium sheet (7), and the link block a(3) with link block b(5) top with loose slot a(2),
Loose slot b(6) top be in same level height.
4. a kind of aviation aluminum profile of advanced composite material (ACM) according to claim 1, it is characterised in that: the bullet block
(4) can be in spring a(10) compression in the state of to take in bullet block slot (13) completely internal, and the limited block (8) and limiting slot
(12) it is adapted, the bullet block (4) is adapted with card slot (9).
5. a kind of aviation aluminum profile of advanced composite material (ACM) according to claim 2, it is characterised in that: the link slot
(15) corresponding with damping tank (16) position, and the link slot (15), damping tank (16) are in vibration damper plate (1), aluminium sheet
(7) quadrangle, and position corresponds to each other.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821138571.1U CN208817068U (en) | 2018-07-18 | 2018-07-18 | A kind of aviation aluminum profile of advanced composite material (ACM) |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821138571.1U CN208817068U (en) | 2018-07-18 | 2018-07-18 | A kind of aviation aluminum profile of advanced composite material (ACM) |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208817068U true CN208817068U (en) | 2019-05-03 |
Family
ID=66271086
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821138571.1U Expired - Fee Related CN208817068U (en) | 2018-07-18 | 2018-07-18 | A kind of aviation aluminum profile of advanced composite material (ACM) |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208817068U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112344196A (en) * | 2020-10-13 | 2021-02-09 | 安徽省金兰金盈铝业有限公司 | Crossbeam aluminium alloy layer board |
| CN113250313A (en) * | 2021-05-28 | 2021-08-13 | 四川齐飞新材料科技有限公司 | Aluminum profile installation mosaic structure for building |
-
2018
- 2018-07-18 CN CN201821138571.1U patent/CN208817068U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112344196A (en) * | 2020-10-13 | 2021-02-09 | 安徽省金兰金盈铝业有限公司 | Crossbeam aluminium alloy layer board |
| CN113250313A (en) * | 2021-05-28 | 2021-08-13 | 四川齐飞新材料科技有限公司 | Aluminum profile installation mosaic structure for building |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20190503 Termination date: 20200718 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |