CN208772750U - A kind of laser cutting device of aviation components - Google Patents
A kind of laser cutting device of aviation components Download PDFInfo
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- CN208772750U CN208772750U CN201821468091.1U CN201821468091U CN208772750U CN 208772750 U CN208772750 U CN 208772750U CN 201821468091 U CN201821468091 U CN 201821468091U CN 208772750 U CN208772750 U CN 208772750U
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- laser cutting
- fixedly connected
- shell
- bracket
- processing plate
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Abstract
The utility model discloses a kind of laser cutting devices of aviation components, its structure includes bracket, process plate, laser cutting machine main body and protection cylindrical cap, processing plate is fixedly connected at the top of the bracket, the bottom of the bracket is fixedly connected with damping base, the left side of the processing plate is equipped with support rod, sliding support is fixedly connected at the top of the support rod, the bottom of the sliding support is equipped with slideway, the right side of the support rod is equipped with electric pushrod, the right side of the electric pushrod is equipped with laser cutting machine main body, the bottom of the laser cutting machine main body is equipped with shell, the bottom of the shell is equipped with laser cutting head, the two sides of the shell are equipped with bayonet connection, the outside of the laser cutting head is equipped with protection cylindrical cap.A kind of laser cutting device of aviation components, is cased with protection cylindrical cap by the outside in laser cutting head, can prevent that sparks flying off in all directions, and is more favorable for checking for staff, and practicability is stronger.
Description
Technical field
The utility model relates to a kind of aviation parts machining technical field, specially a kind of laser of aviation components is cut
Cut device.
Background technique
In recent years, China's Civil Aviation Industry enters fast-developing period, and research and production level is obviously improved, key technology
Tackling key problem makes important progress, and in this context, the manufacture processing of aviation components reaches a new high therewith, establishes substantially independent
Industrial system, make remarkable achievements, and be one biggish for high-intensitive aviation components cutting processing
Problem, now most of laser cutting of aviation components on the market is all straight without safeguard procedures during cutting processing
It connects and laser cutting is exposed to outside, will appear the phenomenon that sparks flying off in all directions with cutting, the spark of splashing not only has
Some potential safety problems, and dazzling brightness is unfavorable for checking for staff, it is more inconvenient.
Therefore, in order to solve these problems, it is proposed that a kind of laser cutting device of aviation components.
Utility model content
The purpose of this utility model is to provide a kind of laser cutting devices of aviation components, to solve above-mentioned background skill
The problem of being proposed in art.
To achieve the above object, the utility model provides the following technical solutions: a kind of laser cutting dress of aviation components
It sets, structure includes bracket, processing plate, laser cutting machine main body and protection cylindrical cap, is fixedly connected at the top of the bracket
Plate is processed, the bottom of the bracket is fixedly connected with damping base, and the left side of the processing plate is equipped with support rod, the support rod
Top is fixedly connected with sliding support, and the bottom of the sliding support is equipped with slideway, and the right side of the support rod is equipped with electric pushrod,
The right side of the electric pushrod is equipped with laser cutting machine main body, and the bottom of the laser cutting machine main body is equipped with shell, the shell
The bottom of body is equipped with laser cutting head, and the two sides of the shell are equipped with bayonet connection, and the outside of the laser cutting head is equipped with
Cylindrical cap is protected, the inside of the protection cylindrical cap is fixedly connected with bayonet connection, and the surface of the processing plate is evenly distributed solid
The outside of fixed pole, the fixed link is equipped with pressing plate.
As a kind of preferred embodiment of the utility model, the top of the bracket connects processing by welding
Plate, the bottom of the bracket connect damping base by welding, and the left side top of the processing plate is fixedly connected with support
Bar.
As a kind of preferred embodiment of the utility model, sliding support, the cunning are welded in the top of the support rod
The bottom of dynamic bracket is fixedly connected with slideway, and the left side of the electric pushrod is equipped with connection pedestal, and the left side of the connection pedestal is solid
Surely driving motor is connected.
As a kind of preferred embodiment of the utility model, sliding is fixedly connected at the top of the laser cutting machine main body
Module, the sliding block are flexibly connected slideway, and the left side of the laser cutting machine main body is equipped with screw nipple, the laser
The bottom of cutter body is fixedly connected with expansion and cotraction regulator, and the bottom of the expansion and cotraction regulator is equipped with shell, and the two of the shell
Side is fixedly connected with bayonet connection.
As a kind of preferred embodiment of the utility model, the surface of the processing plate is fixedly connected with fixed link, described
The outside of fixed link is cased with pressing plate, and the top of the pressing plate is equipped with threaded pressure ring.
Compared with prior art, the beneficial effects of the utility model are as follows:
A kind of laser cutting device of aviation components, is cased with protection cylindrical cap by the outside in laser cutting head,
The spark of splashing can be covered when being cut by laser and stop to get off, prevent that sparks flying off in all directions, and be more favorable for work
Make checking for personnel, will not be with dazzling feeling, security protection performance is stronger, and overall structure is simple, and practicability is stronger.
Detailed description of the invention
Upon reading the detailed description of non-limiting embodiments with reference to the following drawings, other spies of the utility model
Sign, objects and advantages will become more apparent upon:
Fig. 1 is a kind of overall structure diagram of the laser cutting device of aviation components of the utility model.
Fig. 2 is that a kind of laser cutting machine main structure of laser cutting device of aviation components of the utility model is illustrated
Figure.
Fig. 3 is a kind of protection cylindrical cap structural schematic diagram of the laser cutting device of aviation components of the utility model.
In figure: bracket -1, damping base -2, processing plate -3, support rod -4, driving motor -5, electric pushrod -6, connection bottom
Seat -7, sliding support -8, slideway -9, laser cutting machine main body -10, sliding block -11, screw nipple -12, telescopic adjustment
Device -13, shell -14, laser cutting head -15, bayonet connection -16, protection cylindrical cap -17, fixed link -18, pressing plate -19, spiral shell
Line pressure ring -20.
Specific embodiment
To be easy to understand the technical means, creative features, achievement of purpose, and effectiveness of the utility model, below
In conjunction with specific embodiment, the utility model is further described.
Fig. 1-3 is please referred to, the utility model provides a kind of technical solution: a kind of laser cutting device of aviation components,
Its structure includes bracket 1, processing plate 3, laser cutting machine main body 10 and protection cylindrical cap 17, and the top of the bracket 1 is fixed
Connection processing plate 3, the bottom of the bracket 1 are fixedly connected with damping base 2, and the left side of the processing plate 3 is equipped with support rod 4, institute
The top for stating support rod 4 is fixedly connected with sliding support 8, and the bottom of the sliding support 8 is equipped with slideway 9, the right side of the support rod 4
Side is equipped with electric pushrod 6, and the right side of the electric pushrod 6 is equipped with laser cutting machine main body 10, the laser cutting machine main body 10
Bottom be equipped with shell 14, the bottom of the shell 14 is equipped with laser cutting head 15, and the two sides of the shell 14 are equipped with buckle and connect
Fitting 16, the outside of the laser cutting head 15 are equipped with protection cylindrical cap 17, and the inside of the protection cylindrical cap 17 is fixedly connected
Bayonet connection 16, the surface of the processing plate 3 are evenly distributed fixed link 18, and the outside of the fixed link 18 is equipped with pressing plate 19.
Referring to Fig. 1, the top of the bracket 1 connects processing plate 3 by welding, the bottom of the bracket 1 is logical
The mode for crossing welding connects damping base 2, and the left side top of the processing plate 3 is fixedly connected with support rod 4, passes through the damping being equipped with
Pedestal 2 can reduce shaking force during laser cutting, more practical.
Referring to Fig. 1, sliding support 8 is welded at the top of the support rod 4, the bottom of the sliding support 8 is fixedly connected
Slideway 9, the left side of the electric pushrod 6 are equipped with connection pedestal 7, and the left side of the connection pedestal 7 is fixedly connected with driving motor 5,
By the electric pushrod 6 being equipped with, it can easily connect laser cutting machine main body 10 and carry out straight reciprocating motion, structure is simple.
Referring to Fig. 2, the top of the laser cutting machine main body 10 is fixedly connected with sliding block 11, the sliding block 11
It is flexibly connected slideway 9, the left side of the laser cutting machine main body 10 is equipped with screw nipple 12, the laser cutting machine main body 10
Bottom be fixedly connected with expansion and cotraction regulator 13, the bottom of the expansion and cotraction regulator 13 is equipped with shell 14, the two sides of the shell 14
It is fixedly connected with bayonet connection 16, it, can be when being cut by laser by splashing by the protection cylindrical cap 17 being equipped with
Spark covers and stops to get off, and prevents that sparks flying off in all directions, and security protection performance is stronger.
Referring to Fig. 1, the surface of the processing plate 3 is fixedly connected with fixed link 18, the outside of the fixed link 18 is cased with pressure
The top of plate 19, the pressing plate 19 is equipped with threaded pressure ring 20, by being equipped with pressing plate 19, can carry out at reinforcing to aviation plate
Reason.
A kind of laser cutting device of aviation components described in the utility model, working principle are to put aviation components
On processing plate, while the aviation plate of bulk is pressed using pressing plate, and rotation threaded pressure ring is reinforced, and then passes through drive
Dynamic motor provides power, connection pedestal connection electric pushrod operation, while the slideway of sliding support bottom being cooperated to be slided, real
Existing straight reciprocating motion, then the laser cutting head of laser cutting machine main body connection housing bottom emits laser beam, to processing
Aviation components on plate carry out cutting processing, while the protection cylindrical cap that hull outside is cased with can will splash in cutting process
Spark stop, and the bayonet connection that is equipped with facilitates and is mounted and dismounted on shell and protection cylindrical cap.
Bracket 1, damping base 2, processing plate 3, support rod 4, driving motor 5, the electric pushrod 6, connection of the utility model
Pedestal 7, sliding support 8, slideway 9, laser cutting machine main body 10, sliding block 11, screw nipple 12, expansion and cotraction regulator 13,
Shell 14, laser cutting head 15, bayonet connection 16, protection cylindrical cap 17, fixed link 18, pressing plate 19, threaded pressure ring 20, component
It is universal standard part or component as known to those skilled in the art, structure and principle are all that this technology personnel can pass through skill
Art handbook learns or knows by routine experiment method the utility model solves the problems, such as it is existing aviation components on the market
Most of laser cutting, without safeguard procedures, is all that laser cutting is directly exposed to outside during cutting processing, with
Cutting carry out will appear the phenomenon that sparks flying off in all directions, the spark of splashing not only has some potential safety problems, and dazzling brightness
Be unfavorable for checking for staff, it is more inconvenient the problems such as, the utility model is combined with each other by above-mentioned component, by swashing
The outside of light cutting head is cased with protection cylindrical cap, under the spark of splashing being covered and be stopped when being cut by laser
Come, prevent that sparks flying off in all directions, and is more favorable for checking for staff, will not be with dazzling feeling, security protection performance is stronger, whole
Body structure is simple, and practicability is stronger.
The basic principles and main features of the present invention and the advantages of the present invention have been shown and described above, for
For those skilled in the art, it is clear that the present invention is not limited to the details of the above exemplary embodiments, and without departing substantially from this
In the case where the spirit or essential attributes of utility model, the utility model can be realized in other specific forms.Therefore, no matter
From the point of view of which point, the present embodiments are to be considered as illustrative and not restrictive, and the scope of the utility model is by institute
Attached claim rather than above description limit, it is intended that will fall within the meaning and scope of the equivalent elements of the claims
All changes are embraced therein.It should not treat any reference in the claims as limiting related right
It is required that.
In addition, it should be understood that although this specification is described in terms of embodiments, but not each embodiment is only wrapped
Containing an independent technical solution, this description of the specification is merely for the sake of clarity, and those skilled in the art should
It considers the specification as a whole, the technical solutions in the various embodiments may also be suitably combined, forms those skilled in the art
The other embodiments being understood that.
Claims (5)
1. a kind of laser cutting device of aviation components, structure includes bracket (1), processing plate (3), laser cutting machine main body
(10) and cylindrical cap (17) are protected, it is characterised in that: processing plate (3), the bracket are fixedly connected at the top of the bracket (1)
(1) bottom is fixedly connected damping base (2), and the left side of processing plate (3) is equipped with support rod (4), the support rod (4)
Top is fixedly connected sliding support (8), and the bottom of the sliding support (8) is equipped with slideway (9), the right side of the support rod (4)
Equipped with electric pushrod (6), the right side of the electric pushrod (6) is equipped with laser cutting machine main body (10), the laser cutting owner
The bottom of body (10) is equipped with shell (14), and the bottom of the shell (14) is equipped with laser cutting head (15), the shell (14)
Two sides are equipped with bayonet connection (16), and the outside of the laser cutting head (15) is equipped with protection cylindrical cap (17), the anti-guard circle
The inside of barrel cover (17) is fixedly connected bayonet connection (16), and the surface of processing plate (3) is evenly distributed fixed link (18), institute
The outside for stating fixed link (18) is equipped with pressing plate (19).
2. a kind of laser cutting device of aviation components according to claim 1, it is characterised in that: the bracket (1)
Top connect by welding processing plate (3), the bottom of the bracket (1) connects damping base by welding
(2), the left side top of processing plate (3) is fixedly connected with support rod (4).
3. a kind of laser cutting device of aviation components according to claim 1, it is characterised in that: the support rod
(4) sliding support (8) are welded at top, and the bottom of the sliding support (8) is fixedly connected slideway (9), the electric pushrod (6)
Left side be equipped with connection pedestal (7), be fixedly connected with driving motor (5) on the left of the connection pedestal (7).
4. a kind of laser cutting device of aviation components according to claim 1, it is characterised in that: the laser cutting
It is fixedly connected at the top of owner's body (10) sliding block (11), the sliding block (11) is flexibly connected slideway (9), the laser
The left side of cutter body (10) is equipped with screw nipple (12), and the bottom of the laser cutting machine main body (10), which is fixedly connected, stretches
The bottom of contracting adjuster (13), the expansion and cotraction regulator (13) is equipped with shell (14), and the two sides of the shell (14) are fixedly connected
Bayonet connection (16).
5. a kind of laser cutting device of aviation components according to claim 1, it is characterised in that: the processing plate
(3) surface is fixedly connected fixed link (18), and the outside of the fixed link (18) is cased with pressing plate (19), the pressing plate (19) it is upper
Side is equipped with threaded pressure ring (20).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821468091.1U CN208772750U (en) | 2018-09-07 | 2018-09-07 | A kind of laser cutting device of aviation components |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821468091.1U CN208772750U (en) | 2018-09-07 | 2018-09-07 | A kind of laser cutting device of aviation components |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208772750U true CN208772750U (en) | 2019-04-23 |
Family
ID=66160346
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821468091.1U Active CN208772750U (en) | 2018-09-07 | 2018-09-07 | A kind of laser cutting device of aviation components |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208772750U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110153570A (en) * | 2019-06-14 | 2019-08-23 | 郭五连 | A kind of metal plate laser cutting machine |
-
2018
- 2018-09-07 CN CN201821468091.1U patent/CN208772750U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110153570A (en) * | 2019-06-14 | 2019-08-23 | 郭五连 | A kind of metal plate laser cutting machine |
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