CN208543545U - One kind is semi-automatic to rush aircraft hole machine - Google Patents
One kind is semi-automatic to rush aircraft hole machine Download PDFInfo
- Publication number
- CN208543545U CN208543545U CN201820919264.0U CN201820919264U CN208543545U CN 208543545 U CN208543545 U CN 208543545U CN 201820919264 U CN201820919264 U CN 201820919264U CN 208543545 U CN208543545 U CN 208543545U
- Authority
- CN
- China
- Prior art keywords
- erecting bed
- fixedly arranged
- semi
- rush
- automatic
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
Links
- 238000009434 installation Methods 0.000 claims abstract description 24
- 230000001939 inductive effect Effects 0.000 claims abstract description 15
- 230000001105 regulatory effect Effects 0.000 claims abstract description 15
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 claims description 6
- 229910052802 copper Inorganic materials 0.000 claims description 6
- 239000010949 copper Substances 0.000 claims description 6
- 238000004519 manufacturing process Methods 0.000 description 3
- 238000010586 diagram Methods 0.000 description 2
- 230000006698 induction Effects 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 238000004080 punching Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 238000009423 ventilation Methods 0.000 description 1
Landscapes
- Perforating, Stamping-Out Or Severing By Means Other Than Cutting (AREA)
Abstract
The utility model relates to perforating press technical fields, and in particular to one kind is semi-automatic to rush aircraft hole machine.This is semi-automatic to rush aircraft hole machine, including cabinet, and erecting bed is fixedly arranged on the top of cabinet, and installation riser is fixedly arranged on erecting bed；Mounting plate is fixedly arranged on the top of installation riser, and mounting plate and installation riser form an inversed l-shaped；Lifting cylinder is set to the top of mounting plate; the output end of lifting cylinder is fixedly connected on formed punch through mounting plate; formed punch runs through steadying plate; steadying plate is fixedly arranged in installation riser; guard member is fixedly arranged on one end on steadying plate far from installation riser; protrusive board is fixedly arranged on erecting bed; and it is located at below steadying plate; the two sides of protrusive board are equipped with an inductive pick-up; the inside of cabinet is equipped with control device; the side of cabinet is equipped with air-flow regulating mechanism, and control device is electrically connected air-flow regulating mechanism lifting cylinder and inductive pick-up；The air inlet of air-flow regulating mechanism is circumscribed with air pump, and gas outlet is connected to lifting cylinder.
Description
Technical field
The utility model relates to perforating press technical fields, and in particular to one kind is semi-automatic to rush aircraft hole machine.
Background technique
Due to the market demand, some wrapping papers need to be arranged aircraft hole, facilitate hang-up.And the side in existing production aircraft hole
Method is cut using artificial, time-consuming and laborious, so not only increases the workload of operator, and production efficiency is low.
Utility model content
To solve the above problems, the utility model provides, one kind is semi-automatic to rush aircraft hole machine.
It is a kind of it is semi-automatic rush aircraft hole machine, including cabinet and punch mechanism, punch mechanism include erecting bed, installation riser,
Mounting plate, lifting cylinder, formed punch, steadying plate, guard member and protrusive board, erecting bed are fixedly arranged on the top of cabinet, and installation riser is along peace
The Z axis of dress platform is fixedly arranged on erecting bed, positioned at the rear side of erecting bed；Mounting plate is fixedly arranged on installation riser along the Y-axis of erecting bed
Top, mounting plate and installation riser form an inversed l-shaped；Lifting cylinder is set to the top of mounting plate, lifting along the Z axis of erecting bed
The output end of cylinder is fixedly connected on formed punch through mounting plate, and formed punch runs through steadying plate, and steadying plate is fixedly arranged on along the Y-axis of erecting bed
In installation riser, guard member is fixedly arranged on one end on steadying plate far from installation riser, and protrusive board is fixedly arranged on installation along the Y-axis of erecting bed
On platform, and it is located at below steadying plate, the two sides of protrusive board are equipped with an inductive pick-up, and the inside of cabinet is equipped with control device,
The side of cabinet is equipped with air-flow regulating mechanism, and control device is electrically connected air-flow regulating mechanism lifting cylinder and inductive pick-up；
The air inlet of air-flow regulating mechanism is circumscribed with air pump, and gas outlet is connected to lifting cylinder.
Further scheme as the utility model: the bottom of cabinet is equipped with support leg.
Further scheme as the utility model: formed punch cross section is that aircraft is poroid.
Further scheme as the utility model: protrusive board is equipped with plush copper, and plush copper position is higher than inductive pick-up position, prevents
It is tilted when only product is inserted into.
Further scheme as the utility model: erecting bed is equipped with slot corresponding with punch shape.
Further scheme as the utility model: guard member is made of rubber.
Further scheme as the utility model: inductive pick-up is touch sensor.
The utility model has the beneficial effects that the utility model structure is simple, safe operation is easy to use, effective to reduce
The workload of operator, greatly improves production efficiency and quality.
Detailed description of the invention
Fig. 1 is a kind of semi-automatic positive structure schematic for rushing aircraft hole machine of the utility model.
Fig. 2 is a kind of semi-automatic side structure schematic diagram for rushing aircraft hole machine of the utility model.
Fig. 3 is the utility model punch mechanism positive structure schematic.
Fig. 4 is the utility model punch mechanism side structure schematic diagram.
In figure: 1- cabinet；2- punch mechanism；3- air-flow regulating mechanism；4- support leg；5- inductive pick-up；21- installation
Platform；22- installation riser；23- mounting plate；24- lifting cylinder；25- formed punch；26- steadying plate；27- guard member；28- protrusive board.
Specific embodiment
In order to make the purpose of the utility model, technical solutions and advantages more clearly understood, below in conjunction with attached drawing and implementation
Example, the present invention will be further described in detail.It should be appreciated that specific embodiment described herein is only to explain this
Utility model is not used to limit the utility model.
As shown in Figures 1 to 4, one kind is semi-automatic rushes aircraft hole machine, including cabinet 1 and punch mechanism 2, and punch mechanism 2 wraps
Containing erecting bed 21, installation riser 22, mounting plate 23, lifting cylinder 24, formed punch 25, steadying plate 26, guard member 27 and protrusive board 28, peace
Dress platform 21 is fixedly arranged on the top of cabinet 1, and installation riser 22 is fixedly arranged on erecting bed 21 along the Z axis of erecting bed 21, is located at erecting bed
21 rear side；Mounting plate 23 is fixedly arranged on the top of installation riser 22, mounting plate 23 and 22 shape of installation riser along the Y-axis of erecting bed 21
At an inversed l-shaped；Lifting cylinder 24 is set to the top of mounting plate 23 along the Z axis of erecting bed 21, and the output end of lifting cylinder 24 passes through
It wears mounting plate 23 and is fixedly connected on formed punch 25, formed punch 25 runs through steadying plate 26, and steadying plate 26 is fixedly arranged on peace along the Y-axis of erecting bed 21
It fills on vertical plate 22, guard member 27 is fixedly arranged on one end on steadying plate 26 far from installation riser 22, for preventing hand from going deep into, protrusive board 28
Y-axis along erecting bed 21 is fixedly arranged on erecting bed 21, and is located at 26 lower section of steadying plate, and the two sides of protrusive board 28 are equipped with an induction
Sensor 5.
The inside of cabinet 1 is equipped with control device, and the side of cabinet 1 is equipped with air-flow regulating mechanism 3, and control device is electrically connected
3 lifting cylinder of air-flow regulating mechanism and inductive pick-up 5；The air inlet of air-flow regulating mechanism 3 is circumscribed with air pump, gas outlet connection
In lifting cylinder 24.
Working principle of the utility model is: will need the product (paper) of punching between guard member 27 and erecting bed 21
It is put at preset interval；When product touches the inductive pick-up 5 for being set to the two sides of protrusive board 28 simultaneously, two sides induction sensing
After device 5 senses the signal of object touching, this signal is transferred to control device, control device controls air-flow and adjusts machine
Structure 3 is ventilated, and air-flow regulating mechanism 3 drives lifting cylinder 24 that formed punch 25 is driven to decline, and completes the punching operation of product, after the completion,
3 reverse ventilation of air-flow regulating mechanism, so that lifting cylinder 24 resets.
In the utility model, the bottom of cabinet 1 is equipped with support leg 4.
In the utility model, 25 cross section of formed punch is that aircraft is poroid.
In the utility model, protrusive board 28 is equipped with plush copper, and plush copper position is higher than 5 position of inductive pick-up, product is prevented to be inserted into
When tilt.
In the utility model, erecting bed 21 is equipped with slot corresponding with 25 shape of formed punch.
In the utility model, guard member is made of rubber.
In the utility model, inductive pick-up is touch sensor.
The above is only the preferred embodiment of the utility model only, is not intended to limit the utility model, all at this
Made any modification, equivalent replacement or improvement etc., should be included in the utility model within the spirit and principle of utility model
Protection scope within.
Claims (7)
- Semi-automatic rush aircraft hole machine 1. a kind of, which is characterized in that including cabinet and punch mechanism, punch mechanism include erecting bed, Installation riser, mounting plate, lifting cylinder, formed punch, steadying plate, guard member and protrusive board, erecting bed are fixedly arranged on the top of cabinet, installation Vertical plate is fixedly arranged on erecting bed along the Z axis of erecting bed, positioned at the rear side of erecting bed；Mounting plate is fixedly arranged on peace along the Y-axis of erecting bed The top of vertical plate is filled, mounting plate and installation riser form an inversed l-shaped；Lifting cylinder is set to mounting plate along the Z axis of erecting bed The output end on top, lifting cylinder is fixedly connected on formed punch through mounting plate, and formed punch runs through steadying plate, and steadying plate is along erecting bed Y-axis is fixedly arranged in installation riser, and guard member is fixedly arranged on one end on steadying plate far from installation riser, Y-axis of the protrusive board along erecting bed It is fixedly arranged on erecting bed, and is located at below steadying plate, the two sides of protrusive board are equipped with an inductive pick-up, and the inside of cabinet is equipped with Control device, the side of cabinet are equipped with air-flow regulating mechanism, and control device is electrically connected air-flow regulating mechanism lifting cylinder and sense Inductive sensing device；The air inlet of air-flow regulating mechanism is circumscribed with air pump, and gas outlet is connected to lifting cylinder.
- 2. one kind according to claim 1 is semi-automatic to rush aircraft hole machine, which is characterized in that the bottom of cabinet is equipped with support Foot.
- 3. one kind according to claim 2 is semi-automatic to rush aircraft hole machine, which is characterized in that formed punch cross section is aircraft hole Shape.
- 4. one kind according to claim 1 is semi-automatic to rush aircraft hole machine, which is characterized in that protrusive board is equipped with plush copper, plush copper position It sets and is higher than inductive pick-up position, tilting when product being prevented to be inserted into.
- 5. one kind according to claim 1 is semi-automatic to rush aircraft hole machine, which is characterized in that erecting bed is equipped with and formed punch shape The corresponding slot of shape.
- 6. one kind according to claim 1 is semi-automatic to rush aircraft hole machine, which is characterized in that guard member is made of rubber.
- 7. one kind according to claim 1 is semi-automatic to rush aircraft hole machine, which is characterized in that inductive pick-up is contact biography Sensor.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820919264.0U CN208543545U (en) | 2018-06-13 | 2018-06-13 | One kind is semi-automatic to rush aircraft hole machine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820919264.0U CN208543545U (en) | 2018-06-13 | 2018-06-13 | One kind is semi-automatic to rush aircraft hole machine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208543545U true CN208543545U (en) | 2019-02-26 |
Family
ID=65422620
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820919264.0U Expired - Fee Related CN208543545U (en) | 2018-06-13 | 2018-06-13 | One kind is semi-automatic to rush aircraft hole machine |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208543545U (en) |
-
2018
- 2018-06-13 CN CN201820919264.0U patent/CN208543545U/en not_active Expired - Fee Related
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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: 20190226 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |