CN206446030U - A kind of sheet material injection machine airframe structure - Google Patents
A kind of sheet material injection machine airframe structure Download PDFInfo
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- CN206446030U CN206446030U CN201621345748.6U CN201621345748U CN206446030U CN 206446030 U CN206446030 U CN 206446030U CN 201621345748 U CN201621345748 U CN 201621345748U CN 206446030 U CN206446030 U CN 206446030U
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- flanging
- injection machine
- top plate
- straight beam
- sheet material
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Abstract
The utility model discloses a kind of sheet material injection machine airframe structure, it is characterized in that, fuselage is used by upper-part, column, the integrated frame structure that lower component is directly connected to, the upper-part includes upper straight beam, entablature and the top plate on the upper straight beam and the entablature, the injection portion of injection machine is respectively arranged in the both sides of the top plate upper end with matched moulds part, oil drain pan is provided with positioned at top plate one end where the matched moulds part, the lower component includes lower straight beam, crossbeam and the bottom plate under the lower straight beam and the sill, the upper-part, the single part of column and lower component is formed using one piece of steel plate flanging, and the welding of different parts is carried out at flanging, the injection machine fuselage good reliability, material usage is few, fuselage weight is light, compact conformation, appearance looks elegant, respective country energy-saving and emission-reduction policy.
Description
Technical field
The utility model is related to injection machine field, more specifically, it relates to a kind of sheet material injection machine airframe structure.
Background technology
With the continuous development of scientific technology, the function of various mechanical production devices is also stronger and stronger, sheet material can be added
Work is into the shape become increasingly complex, and the sheet metal thickness of clod wash is also increasingly thicker.Injection machine is the abbreviation of plastic-injection moulding machine, machine
Body structure is an important component in injection machine.Current airframe structure is more single and complexity, is by section bar mostly
The chaotic complexity of comparison is formed by combining with sheet material.And there is problems with：1) profile structure is expanded with heat and contract with cold by being welded
Stress is easily produced, solder joint crator is difficult polishing, time-consuming waste material of taking a lot of work, surface permeability during processing；2) section bar and sheet metal thickness be not
Unanimously welding procedure is caused to complicate；3) injection portion causes the wasting of resources to a certain degree using thick section bar.
Utility model content
For above-mentioned technical problem, the purpose of this utility model is：A kind of good reliability, material usage are provided
Less, fuselage weight is light, compact conformation and the high sheet material injection machine airframe structure of fuselage strength and stiffness.
To achieve the above object, the utility model proposes new technical scheme：A kind of sheet material injection machine airframe structure, including
Upper-part, lower component and some columns being arranged between upper-part and lower part, the upper-part include top plate, the top
Plate includes upper " L " the shape flanging that upper face and both sides be arranged in parallel downwards, is equipped with both sides band water at " L " shape flanging on each
Flat-folded side and the upper straight beam set along its length, the upper straight beam are welded with respect to the flanging of upper face side with upper face, its
Another side edgefold with respect to upper face is overlapped and welded on described upper " L " shape flanging, two upper straight beams be arrangeding in parallel it
Between be additionally provided with some both sides with flanging and the entablature that welds therewith, the lower component includes bottom plate, lower straight beam and sill,
The bottom plate include lower face and under " L " shape flanging, band horizontal flanging in both sides is equipped with per once " L " shape flanging and along length
The lower straight beam that direction is set is spent, the lower straight beam is welded with respect to a side edgefold of lower face with lower face, and the lower straight beam is relative
Another side edgefold of lower face overlap it is described under weld on " L " shape flanging, between two lower straight beams be arrangeding in parallel also
Some both sides are provided with flanging and the sill that welds therewith.
According to above-mentioned technical proposal：The steel plate of each part of fuselage needs to be provided with different flangings, each portion according to load-bearing
Flanging between part is welded to each other into a rigid frame structure, the smooth no-welding-spot in surface between each part after welding, flanging it
Between solder joint and crator area it is small, be more easy to polishing, and be not take up parts surface, the smooth no-welding-spot of top board surface, bottom plate be easy to
Power unit and mailbox linking, it is overall standardized, section bar is saved, cost and fuselage weight are reduced while improving overall flatness
Amount.
It is of the present utility model to be further arranged to：The column is arranged at the both sides of top plate and bottom plate, and interval is set in pairs
Five pairs are equipped with, flanging is provided with per column, is welded per column upper surface with upper " L " the shape flanging, its relatively upper " L "
The other end of shape flanging is welded with bottom plate.
According to above-mentioned technical proposal：Column is used for supporting whole framework, and the load-bearing according to needed for top plate upper face can be spaced many
To setting, each pair is provided with different flangings and is suitable for different load-bearing.
It is of the present utility model to be further arranged to：Matched moulds part and the injection part of injection machine are installed above the top plate
Point, oil drain pan is provided with the top plate of matched moulds part lower end, the oil drain pan is of an inclined plane setting to lower recess and bottom surface,
The sagging one end in its bottom surface, which is provided with, unloads oilhole.
According to above-mentioned technical proposal：Oil drain pan, which is set, conveniently connects oil, and oil is assembled to deep one end, along above along inclined-plane
Unload oilhole collection.
It is of the present utility model to be further arranged to：The relatively described injection portion of the top plate and the docking of the matched moulds part
Place is provided with opening, and the both sides of the opening relative injection part and the matched moulds part are provided with to engage on chute, the chute and set
It is equipped with the active angle bar that can be slidably reciprocated along chute.
According to above-mentioned technical proposal：The setting of active angle bar facilitates operation of the workman to injection machine, charging of such as ascending a height.
It is of the present utility model to be further arranged to：The fuselage side is provided with the steel plate flanging for plug-in electric unit.
According to above-mentioned technical proposal：Steel plate flanging rear-mounted electric unit, can effectively less fuselage height and width,
It is cost-effective.
The utility model is compared to the advantage of prior art：By being welded between the flanging and flanging to each part
A pure sheet material integrative-structure is formed, integral rigidity is high, intensity is big, and then improves the kinematic accuracy of injection (mo(u)lding) machine moving component
And stability, the integrated production of injection machine is improved, at the same it is cost-effective, and relative to the welding of section bar and sheet material, pure sheet material
Welding between stack pile flanging more facilitates, and solder joint crator is more easy to polishing, and more preferably, the setting of oil drain pan is convenient for ability of anti-deformation
Oil-collecting, the setting of active angle bar facilitates operation of the workman to injection machine.
Brief description of the drawings
Fig. 1 is a kind of structural representation of sheet material injection machine airframe structure in the present embodiment；
Fig. 2 is a kind of pillar construction schematic diagram of sheet material injection machine airframe structure in the present embodiment；
Fig. 3 is a kind of straight beam structure schematic diagram of sheet material injection machine airframe structure in the present embodiment；
Fig. 4 is a kind of beam structure schematic diagram of sheet material injection machine airframe structure in the present embodiment；
In figure：1st, top plate；101st, upper face；102nd, upper " L " shape flanging；2nd, bottom plate；201st, lower face；202nd, " L " shape under
Flanging；3rd, upper straight beam；4th, lower straight beam；5th, column；501st, the first column；502nd, the second column；503rd, the 3rd column；504th, the 4th
Column；505th, the 5th column；6th, oil drain pan；601st, oilhole is unloaded；7th, active angle bar；8th, angle bar；9th, entablature；10th, sill.
Embodiment
Below in conjunction with accompanying drawing, embodiment of the present utility model is described in further detail, so that the utility model skill
Art scheme is more readily understood and grasped.
Embodiment
Referring to the drawings shown in 1-4, a kind of sheet material injection machine airframe structure, including upper-part, lower component and be arranged on
Some columns 5 between part and lower component, upper-part includes top plate 1, and it is parallel downwards with both sides that top plate 1 includes upper face 101
Upper " L " the shape flanging 102 set, the top of top plate 1 is provided with matched moulds part and the injection portion of injection machine, matched moulds part lower end
Oil drain pan 6 is provided with top plate 1, the oil drain pan 6 is of an inclined plane setting to lower recess and bottom surface, the sagging one end in its bottom surface is set
It is equipped with and unloads oilhole 601, the joint of the relatively described injection portion of top plate 1 and the matched moulds part is provided with opening, the relative note of opening
The both sides for penetrating part and the matched moulds part are provided with the active angle bar for engaging on chute, chute and being provided with and being slidably reciprocated along chute
7.The horizontal flanging of both sides band and the upper straight beam 3 set along its length, upper straight beam 3 are equipped with " L " shape flanging 102 on each
Flanging with respect to the side of upper face 101 is welded with upper face 101, and it overlaps described with respect to another side edgefold of upper face 101
Welded on upper " L " shape flanging 102, some both sides band flangings are additionally provided between the upper straight beam 3 of two be arranged in parallel and are welded therewith
The entablature 9 connect, lower component includes bottom plate 2, lower straight beam 4 and sill 10, and bottom plate 2 includes " L " shape with of lower face 201 and rolled over
Side 202, the horizontal flanging of both sides band and the lower straight beam 4 set along its length, institute are equipped with per " L " shape flanging 202 once
The side edgefold that lower straight beam 4 is stated with respect to lower face 201 is welded with lower face 201, another side edgefold of its relative lower face 201
Overlap it is described under weld on " L " shape flanging 202, be additionally provided with some both sides between two lower straight beams 4 be arrangeding in parallel
The sill 10 welded with flanging and therewith, column 5 is arranged at the both sides of top plate 1 and bottom plate 2, and is arranged at intervals with five in pairs
It is right, flanging is provided with per column 5, is welded per the upper surface of column 5 with upper " L " the shape flanging 102, its relatively upper " L "
The other end of shape flanging 102 is welded with bottom plate 2, and the angle bar 8 for facilitating workman to trample, above-mentioned each portion are additionally provided with the both sides of bottom plate 2
Steel plate of the part by thickness by 4.5-5.5 millimeters is made, preferably 5 millimeters of steel plate, is additionally provided with fuselage side for plug-in electricity
The steel plate flanging of gas unit.
During assembling, using non-uniform thickness steel plate not of uniform size, top plate 1 and bottom plate 2 use bulk steel plate, the surface of top plate 1
No-welding-spot, rigidity and intensity are high, and surface ne-leakage is respectively mounted injection portion and matched moulds part, bottom in the upper end both sides of top plate 1
The upper ends power original paper of plate 2 and be connected with fuel tank, two side edgefolds of upper straight beam 3 respectively with the upper face 101 of top plate 1 and upper
" L " shape flanging 102 forms cable tray after welding, respectively the first column 501 of the column 5 between top plate 1 and bottom plate 2,
Second column 502, the 3rd column 503, the 4th column 504 and the 5th column 505, per column 5 along the two of top plate 1 and bottom plate 2
Side relative symmetry is set, and the steel plate flanging of fuselage side can be used for suspension electric appliance unit, effectively reduces that fuselage is high-end and width, section
The active angle bar 8 that activity at about material, the upper end open of top plate 1 is set facilitates workman to ascend a height operation, and the overall structure is using pure
Sheet material one, rigidity is high, intensity is big, effectively save material while fuselage strength and stiffness are ensured, while reducing cost
Mitigate fuselage weight, flanging can be arranged to different shape and width according to the difference of load, and customization that can be flexible is various
Specification meets seriation customization to the demand of airframe structure, and then improves the kinematic accuracy of plastic-injection moulding machine moving component
And stability, the integrated production of injection machine is improved, and meet the purpose of national energy-saving emission reduction, relative to the weldering of section bar and sheet material
Connect, pure sheet material stack pile welding more facilitates, and solder joint crator is more easy to polishing, and ability of anti-deformation is more preferably.
Certainly, it is representative instance of the present utility model above, in addition, the utility model can also have other a variety of
The technical scheme of embodiment, all use equivalent substitutions or equivalent transformation formation, all falls within the utility model and is claimed
Within the scope of.
Claims (5)
1. a kind of sheet material injection machine airframe structure, it is characterised in that fuselage includes upper-part, lower component and is arranged on upper-part
Some columns (5) between lower component, the upper-part include top plate (1), the top plate (1) include upper face (101) and
Upper " L " the shape flanging (102) that both sides be arranged in parallel downwards, " L " shape flanging (102) place is equipped with both sides band level folding on each
Side and the upper straight beam (3) set along its length, flanging and upper face of the upper straight beam (3) with respect to upper face (101) side
(101) weld, it overlaps with respect to another side edgefold of upper face (101) and welded on upper " L " the shape flanging (102), parallel
Some both sides are additionally provided between the two upper straight beams (3) set with flanging and the entablature (9) that welds therewith, it is described under
Part include bottom plate (2), lower straight beam (4) and sill (10), the bottom plate (2) including lower face (201) and under " L " shape flanging
(202) the horizontal flanging of both sides band and the lower straight beam set along its length, are being equipped with per " L " shape flanging (202) place once
(4), the lower straight beam (4) is welded with respect to a side edgefold of lower face (201) with lower face (201), and it is with respect to lower face (201)
Another side edgefold overlap it is described under weld on " L " shape flanging (202), between two lower straight beams (4) be arrangeding in parallel
Some both sides are additionally provided with flanging and the sill (10) that welds therewith.
2. a kind of sheet material injection machine airframe structure according to claim 1, it is characterised in that the column (5) is arranged at
The both sides of top plate (1) and bottom plate (2), and be arranged at intervals in pairs, flanging is provided with per column (5), per column (5) upper end
Welded with upper " L " shape flanging (102) welding, the other end of its relatively upper " L " shape flanging (102) with bottom plate (2) in face.
3. a kind of sheet material injection machine airframe structure according to claim 1, it is characterised in that pacify above the top plate (1)
Oil drain pan (6), institute are provided with matched moulds part and injection portion equipped with injection machine, the top plate (1) of matched moulds part lower end
State oil drain pan (6) and be of an inclined plane setting to lower recess and bottom surface, the sagging one end in its bottom surface, which is provided with, unloads oilhole (601).
4. a kind of sheet material injection machine airframe structure according to claim 3, it is characterised in that the top plate (1) is with respect to institute
The joint for stating injection portion and the matched moulds part is provided with opening, the opening relative injection part and the matched moulds part
Both sides are provided with engaging on chute, the chute and are provided with the active angle bar (7) that can be slidably reciprocated along chute.
5. a kind of sheet material injection machine airframe structure according to claim 4, it is characterised in that the fuselage side is provided with use
In the steel plate flanging of plug-in electric unit.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621345748.6U CN206446030U (en) | 2016-12-09 | 2016-12-09 | A kind of sheet material injection machine airframe structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621345748.6U CN206446030U (en) | 2016-12-09 | 2016-12-09 | A kind of sheet material injection machine airframe structure |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206446030U true CN206446030U (en) | 2017-08-29 |
Family
ID=59662954
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621345748.6U Active CN206446030U (en) | 2016-12-09 | 2016-12-09 | A kind of sheet material injection machine airframe structure |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206446030U (en) |
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2016
- 2016-12-09 CN CN201621345748.6U patent/CN206446030U/en active Active
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