CN209532647U - A kind of semi-automatic torque machine structure for spool assembling - Google Patents
A kind of semi-automatic torque machine structure for spool assembling Download PDFInfo
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- CN209532647U CN209532647U CN201822009549.3U CN201822009549U CN209532647U CN 209532647 U CN209532647 U CN 209532647U CN 201822009549 U CN201822009549 U CN 201822009549U CN 209532647 U CN209532647 U CN 209532647U
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Abstract
The utility model provides a kind of semi-automatic torque machine structure for spool assembling, including fuselage, circle rail and box spanner；Tooling described in being bolted connection one group at the top of the fuselage；The aerodynamic wind drape over one's shoulders fixed glides front end face be fastenedly connected with one group described in aerodynamic wind drape over one's shoulders；The bottom that the aerodynamic wind drapes over one's shoulders be equipped with one group described in box spanner；Cylinder described in being fixedly connected with one group at the top of the air cylinder fixed plate；It is fixedly connected at the top of the cylinder push-rod end and the fuselage；The fuselage right upper portion be placed with one group described in control device.Aerodynamic wind is driven to put on lower slider by setting cylinder, and it is draped over one's shoulders by aerodynamic wind and nut is tightened, change the previous mounting means installed manually, reduce generated in manual hand manipulation the problems such as damaging, assembly efficiency is improved, labour is reduced, reduces assembly man-hour, assembling cost is reduced, is increased economic efficiency.
Description
Technical field
The utility model belongs to make-up machinery technical field, more specifically, in particular to it is a kind of for spool assembling
Semi-automatic torque machine structure.
Background technique
The shrink assembly of valve core nut is the important link of spool assembly in the assembly of spool, existing spool assembly one
As be that spool is put into main body, place into spool fixture nut, the torque spanner of adjustable torsion covers in fixture nut,
Spool fixture nut is being tightened manually.
Based on above-mentioned, the inventors discovered that, existing assembling mode manually operates, and production efficiency is very low, in people
It is easy to damage in work operating process, often will appear in rundown process and lead to the problem of sleave since nut turns out of plumb
And cause waste product, while if to tighten torque value unstable for spool fixture nut when operating not in place, when it is high when it is low, lead to nut
When pine when it is tight, cause yields not high, waste of time, economic benefit is poor.
Then, in view of this, for existing structure and missing study improvement, provide it is a kind of for spool assemble
Semi-automatic torque machine structure, to achieve the purpose that with more more practical value.
Utility model content
In order to solve the above-mentioned technical problem, the utility model provides a kind of semi-automatic torsion machine knot for spool assembling
Structure is manually operated with solving existing assembling mode, and production efficiency is very low, is easy to touch during manual operation
Wound often will appear in rundown process and lead to the problem of sleave since nut turns out of plumb and cause waste product, while if
It is unstable to tighten torque value for spool fixture nut when operating not in place, when it is high when it is low, it is tight when pine when leading to nut, cause yields
It is not high, waste of time, economic benefit poor.
Purpose and effect of the utility model for the semi-automatic torque machine structure of spool assembling, by technology hand in detail below
Section is reached:
A kind of semi-automatic torque machine structure for spool assembling, including fuselage, circle rail, tooling, control device, aerodynamic wind
Drape over one's shoulders that fixed glides, sliding block, aerodynamic wind drape over one's shoulders stationary fixture, aerodynamic wind drapes over one's shoulders, air cylinder fixed plate, axis hole, locking slot, cylinder and sleeve barrel spanner
Hand；Tooling described in being bolted connection one group at the top of the fuselage；It is slidably connected on the fuselage described in one group
Aerodynamic wind drapes over one's shoulders air cylinder fixed plate described in fixed glides and one group；The aerodynamic wind drapes over one's shoulders between fixed glides and the air cylinder fixed plate
To be fixedly connected；The aerodynamic wind drape over one's shoulders fixed glides front end face be fastenedly connected with one group described in aerodynamic wind drape over one's shoulders；The aerodynamic wind drapes over one's shoulders
Bottom be equipped with one group described in box spanner；Cylinder described in being fixedly connected with one group at the top of the air cylinder fixed plate；It is described
It is fixedly connected at the top of cylinder push-rod end and the fuselage；The fuselage right upper portion be placed with one group described in control device.
Further, the rear end face of the fuselage be provided with two groups described in circle rail, after the aerodynamic wind drapes over one's shoulders fixed glides
End face be threadably secured be connected with two groups described in sliding block, the sliding block is slidably connected with the round rail.
Further, the front end face that the aerodynamic wind drapes over one's shoulders fixed glides be provided with one group described in aerodynamic wind drape over one's shoulders stationary fixture,
What the aerodynamic wind draped over one's shoulders stationary fixture is internally provided with semi-circular groove.
Further, be provided with one group at left and right sides of the air cylinder fixed plate described in axis hole, the air cylinder fixed plate
It is slidably matched by the axis hole and the round rail.
Further, offer one group on axis hole described in every group described in locking slot, and by bolt by the locking slot
It tenses, the air cylinder fixed plate is adjusted by bolt and the cooperation of the round rail is elastic.
Further, the aerodynamic wind drapes over one's shoulders to be driven by air pressure and driving box spanner rotation, while can be according to difference
Product different torque values is set.
Compared with prior art, the utility model has the following beneficial effects:
It drives aerodynamic wind to put on lower slider by setting cylinder, and is draped over one's shoulders by aerodynamic wind and nut is tightened, change
The previous mounting means installed manually, reduce generated in manual hand manipulation the problems such as damaging, improve assembly efficiency,
Labour is reduced, assembly man-hour is reduced, assembling cost is reduced, increases economic efficiency；It is oriented to by the circle rail for being arranged vertical,
It prevents from nut occur in assembly turning out of plumb and leads to the problem of sleave and cause waste product, raising yields；By will be pneumatic
Wind, which drapes over one's shoulders, to be set as the aerodynamic wind of adjustable torque value and drapes over one's shoulders, control nut check torque value that can be stable in assembly, torsion
Value control is stablized, and the problem that misoperation causes torsion too large or too small is avoided, and improves yields, reduces rejection rate,
It increases economic efficiency.
Detailed description of the invention
Fig. 1 is the axis side structure schematic diagram of the utility model.
Fig. 2 is the air cylinder fixed plate axis side structure schematic diagram of the utility model.
Fig. 3 is the air cylinder fixed plate schematic cross-sectional view of the utility model.
Fig. 4 is that the aerodynamic wind of the utility model drapes over one's shoulders fixed glides axis side structure schematic diagram.
In figure, the corresponding relationship of component names and accompanying drawing number are as follows:
1- fuselage, 101- circle rail, 2- tooling, 3- control device, 4- aerodynamic wind drape over one's shoulders fixed glides, 401- sliding block, 402- gas
Dynamic wind drapes over one's shoulders stationary fixture, and 5- aerodynamic wind drapes over one's shoulders, 6- air cylinder fixed plate, 601- axis hole, 602- locking slot, 7- cylinder, 8- box spanner.
Specific embodiment
The embodiments of the present invention is described in further detail with reference to the accompanying drawings and examples.Following embodiment
For illustrating the utility model, but cannot be used to limit the scope of the utility model.
In the description of the present invention, unless otherwise indicated, the meaning of " plurality " is two or more；Term
The orientation of the instructions such as "upper", "lower", "left", "right", "inner", "outside", " front end ", " rear end ", " head ", " tail portion " or position are closed
System is to be based on the orientation or positional relationship shown in the drawings, and is merely for convenience of describing the present invention and simplifying the description, rather than
The device or element of indication or suggestion meaning must have a particular orientation, be constructed and operated in a specific orientation, therefore cannot
It is construed as a limitation of the present invention.In addition, term " first ", " second ", " third " etc. are used for description purposes only, and cannot
It is interpreted as indication or suggestion relative importance.
In the description of the present invention, it should be noted that unless otherwise clearly defined and limited, term " phase
Even ", " connection " shall be understood in a broad sense, for example, it may be being fixedly connected, may be a detachable connection, or be integrally connected；It can
To be mechanical connection, it is also possible to be electrically connected；It can be directly connected, it can also be indirectly connected through an intermediary.For this
For the those of ordinary skill in field, the concrete meaning of above-mentioned term in the present invention can be understood with concrete condition.
Embodiment:
As shown in attached drawing 1 to attached drawing 4:
The utility model provides a kind of semi-automatic torque machine structure for spool assembling, including fuselage 1, circle rail 101, work
Fill 2, control device 3, that aerodynamic wind drapes over one's shoulders fixed glides 4, sliding block 401, aerodynamic wind drape over one's shoulders stationary fixture 402, aerodynamic wind drapes over one's shoulders 5, cylinder is solid
Fixed board 6, axis hole 601, locking slot 602, cylinder 7 and box spanner 8；The top of the fuselage 1 has been bolted connection one
The group tooling 2；Aerodynamic wind described in slidably connecting one group on the fuselage 1 drapes over one's shoulders cylinder described in fixed glides 4 and one group and fixes
Plate 6；It is to be fixedly connected between fixed glides 4 and the air cylinder fixed plate 6 that the aerodynamic wind, which drapes over one's shoulders,；The aerodynamic wind drapes over one's shoulders fixed glides
4 front end faces be fastenedly connected with one group described in aerodynamic wind drape over one's shoulders 5；The bottom that the aerodynamic wind drapes over one's shoulders 5 be equipped with one group described in box spanner
8；The top of the air cylinder fixed plate 6 be fixedly connected with one group described in cylinder 7；The top of 7 push rod end of cylinder and the fuselage 1
Portion is fixedly connected；1 right upper portion of fuselage be placed with one group described in control device 3.
Wherein, the rear end face of the fuselage 1 be provided with two groups described in circle rail 101, after the aerodynamic wind drapes over one's shoulders fixed glides 4
End face be threadably secured be connected with two groups described in sliding block 401, the sliding block 401 is slidably connected with the round rail 101, makes pneumatic
Wind drapes over one's shoulders fixed glides 4 and can smoothly slide on the fuselage 1, at the same prevent assembly when occur nut turn out of plumb generate
The problem of sleave and cause waste product.
Wherein, the front end face that the aerodynamic wind drapes over one's shoulders fixed glides 4 be provided with one group described in aerodynamic wind drape over one's shoulders stationary fixture 402,
The aerodynamic wind drapes over one's shoulders the semi-circular groove that is internally provided with of stationary fixture 402, and the periphery that aerodynamic wind drapes over one's shoulders 5 is matched with semi-circular groove to be merged
It is fastened by bolts aerodynamic wind is draped over one's shoulders 5 to drape over one's shoulders fixed glides 4 in the aerodynamic wind and be fastenedly connected.
Wherein, the left and right sides of the air cylinder fixed plate 6 be provided with one group described in axis hole 601, the air cylinder fixed plate 6
It is slidably matched by the axis hole 601 and the round rail 101, guarantees that the air cylinder fixed plate 6 smooth can be slided.
Wherein, offer one group on axis hole 601 described in every group described in locking slot 602, and by bolt by the locking
Slot 602 tenses, and adjusts the air cylinder fixed plate 6 by bolt and the cooperation of the round rail 101 is elastic.
Wherein, the aerodynamic wind drapes over one's shoulders 5 and drives the rotation of box spanner 8 to drive by air pressure, while can be according to different
Different torque values is arranged in product, and torque value control is stablized during turning.
The specifically used mode and effect of the present embodiment:
By tooling 2 that product is fixed on the fuselage 1, adjustment aerodynamic wind drapes over one's shoulders 5 torque value to the value of needs, by spool spiral shell
Mother is placed in box spanner 8, starts 7 pusher cylinder fixed plate 6 of cylinder and aerodynamic wind drapes over one's shoulders fixed glides 4 and slides down, start
Aerodynamic wind drapes over one's shoulders 5, and aerodynamic wind drapes over one's shoulders 5 rotations and box spanner 8 is driven to rotate, and valve core nut is tightened, when the torsion of valve core nut reaches
Setting value, aerodynamic wind drape over one's shoulders 5 and are unable to drive the rotation of box spanner 8, stop the gas source that aerodynamic wind drapes over one's shoulders 5, and aerodynamic wind is draped over one's shoulders in the contraction of cylinder 7
5 lift, and complete assembly working.
The embodiments of the present invention are given for the purpose of illustration and description, and are not exhaustively or to incite somebody to action
The utility model is limited to disclosed form.Many modifications and variations are aobvious and easy for the ordinary skill in the art
See.Embodiment was chosen and described in order to better illustrate the principle and practical application of the utility model, and makes this field
Those of ordinary skill it will be appreciated that the utility model to designing various embodiments suitable for specific applications with various modifications.
Claims (6)
1. a kind of semi-automatic torque machine structure for spool assembling, it is characterised in that: this is used for the semi-automatic torsion of spool assembling
Power machine structure includes that fuselage (1), circle rail (101), tooling (2), control device (3), aerodynamic wind drape over one's shoulders fixed glides (4), sliding block
(401), aerodynamic wind drape over one's shoulders stationary fixture (402), aerodynamic wind drape over one's shoulders (5), air cylinder fixed plate (6), axis hole (601), locking slot (602),
Cylinder (7) and box spanner (8)；Tooling (2) described in being bolted connection one group at the top of the fuselage (1)；It is described
Aerodynamic wind described in slidably connecting one group on fuselage (1) drapes over one's shoulders air cylinder fixed plate (6) described in fixed glides (4) and one group；The gas
It is to be fixedly connected between fixed glides (4) and the air cylinder fixed plate (6) that dynamic wind, which drapes over one's shoulders,；Before the aerodynamic wind drapes over one's shoulders fixed glides (4)
End face be fastenedly connected with one group described in aerodynamic wind drape over one's shoulders (5)；The bottom that the aerodynamic wind drapes over one's shoulders (5) be equipped with one group described in box spanner
(8)；Cylinder (7) described in being fixedly connected with one group at the top of the air cylinder fixed plate (6)；Cylinder (7) push rod end with it is described
Fuselage is fixedly connected at the top of (1)；Fuselage (1) right upper portion be placed with one group described in control device (3).
2. the semi-automatic torque machine structure for spool assembling as described in claim 1, it is characterised in that: the fuselage (1)
Rear end face justifies rail (101) described in being provided with two groups, and the rear end face that the aerodynamic wind drapes over one's shoulders fixed glides (4) is threadably secured connection
Sliding block described in having two groups (401), the sliding block (401) are slidably connected with the round rail (101).
3. the semi-automatic torque machine structure for spool assembling as described in claim 1, it is characterised in that: the aerodynamic wind drapes over one's shoulders solid
Determine slide plate (4) front end face be provided with one group described in aerodynamic wind drape over one's shoulders stationary fixture (402), the aerodynamic wind drapes over one's shoulders stationary fixture
(402) be internally provided with semi-circular groove.
4. the semi-automatic torque machine structure for spool assembling as described in claim 1, it is characterised in that: the air cylinder fixed plate
(6) axis hole described in being provided with one group at left and right sides of (601), the air cylinder fixed plate (6) pass through the axis hole (601) and institute
Round rail (101) is stated to be slidably matched.
5. the semi-automatic torque machine structure for spool assembling as described in claim 1, it is characterised in that: axis hole described in every group
(601) locking slot (602) described in offering one group on, and tensed the locking slot (602) by bolt, pass through bolt tune
It saves the air cylinder fixed plate (6) and the cooperation of the round rail (101) is elastic.
6. the semi-automatic torque machine structure for spool assembling as described in claim 1, it is characterised in that: the aerodynamic wind drapes over one's shoulders
(5) box spanner (8) rotation is driven to drive by air pressure, while different torque values can be set according to different products.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201822009549.3U CN209532647U (en) | 2018-12-03 | 2018-12-03 | A kind of semi-automatic torque machine structure for spool assembling |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201822009549.3U CN209532647U (en) | 2018-12-03 | 2018-12-03 | A kind of semi-automatic torque machine structure for spool assembling |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209532647U true CN209532647U (en) | 2019-10-25 |
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ID=68263183
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201822009549.3U Active CN209532647U (en) | 2018-12-03 | 2018-12-03 | A kind of semi-automatic torque machine structure for spool assembling |
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| CN (1) | CN209532647U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114290038A (en) * | 2021-12-27 | 2022-04-08 | 武汉航空仪表有限责任公司 | Technological equipment applied to assembly of pressure core of pressure sensor sensitive assembly |
-
2018
- 2018-12-03 CN CN201822009549.3U patent/CN209532647U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114290038A (en) * | 2021-12-27 | 2022-04-08 | 武汉航空仪表有限责任公司 | Technological equipment applied to assembly of pressure core of pressure sensor sensitive assembly |
| CN114290038B (en) * | 2021-12-27 | 2024-04-09 | 武汉航空仪表有限责任公司 | Technological equipment applied to pressure core assembly of pressure sensor sensitive component |
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