CN108226454A - A kind of Novel rubber material device - Google Patents
A kind of Novel rubber material device Download PDFInfo
- Publication number
- CN108226454A CN108226454A CN201711058813.6A CN201711058813A CN108226454A CN 108226454 A CN108226454 A CN 108226454A CN 201711058813 A CN201711058813 A CN 201711058813A CN 108226454 A CN108226454 A CN 108226454A
- Authority
- CN
- China
- Prior art keywords
- fuselage
- spiral
- outlet
- internally provided
- circular hole
- 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.)
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Classifications
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
- G01N33/00—Investigating or analysing materials by specific methods not covered by groups G01N1/00 - G01N31/00
- G01N33/44—Resins; rubber; leather
- G01N33/445—Rubber
Abstract
The invention discloses a kind of Novel rubber material devices, including fuselage, the bottom of the fuselage is provided with support plate, the bottom of the support plate is fixedly installed pedestal, the fuselage is internally provided with cavity portion, limiting holes are provided on the left of the cavity portion, sealing column is provided on the left of the limiting holes, and the sealing column right side is provided with sealing pad, cavity portion is internally provided with sliding fortune plate, the side of sliding fortune plate is provided with the first sealing circle, and sliding fortune plate right side is fixedly installed horizontal axis, horizontal axis break-through limiting holes, sealing pad, sealing column and fuselage.The configuration of the present invention is simple, it is of low cost, the intensity of leather can be easily measured, service life is long, highly practical.
Description
Technical field
The present invention relates to technical field of rubber material, specially a kind of Novel rubber material device.
Background technology
Rubber refers to the strong flexible polymer material with reversible deformation, has important role in industry, life,
High resilience at room temperature can generate compared with large deformation under the external force effect of very little, remove resilient after external force.Rubber material
And product has stringent quality requirement, needs to measure a series of intensity indexs of material and plasticity index, elastic limit, elongation
Rate, elasticity modulus, proportional limit, area reduction amount, tensile strength, yield point, yield strength and other performance index, current
Rubber mensuration machine is expensive, and inter deterioration rate is high, it is difficult to be accepted extensively by market.
Invention content
The purpose of the present invention is to provide a kind of Novel rubber material device, to solve mentioned above in the background art ask
Topic.
To achieve the above object, the present invention provides following technical solution：
A kind of Novel rubber material device, including fuselage, the bottom of the fuselage is provided with support plate, the bottom of the support plate
Pedestal is fixedly installed, the fuselage is internally provided with cavity portion, limiting holes are provided on the left of the cavity portion, and the limiting holes are left
Side is provided with sealing column, and the sealing column right side is provided with sealing pad, and fortune plate is slided in being internally provided with for the cavity portion, described
The side of sliding fortune plate is provided with the first sealing circle, and the sliding fortune plate right side is fixedly installed horizontal axis, the horizontal axis break-through limitation
Hole, sealing pad, sealing column and fuselage, and the horizontal axis left end is fixedly installed rubber clamp, the fuselage is internally provided with
Break-through limiting holes and the first external outlet circular hole, and the first outlet circular hole is internally provided with the first air valve, the machine
The bottom of body is fixedly installed control device, and the fuselage is internally provided with break-through control device and the second outlet of cavity portion
Circular hole, the fuselage are internally provided with polycondensation portion, the slot hole for being internally provided with break-through polycondensation portion and limiting holes of the fuselage,
The slot hole is internally provided with single air valve, and the polycondensation portion is internally provided with the first cunning fortune block, and described first slides fortune block
Side is provided with the second sealing circle, and the described first middle part switching for sliding fortune block upper surface is connected with quarter butt, the top of the quarter butt
Switching is connected with pressing device, and the bottom patch of described pressing device one end is connected with the top of solid axis, and the bottom of the solid axis is fixed
In the upper surface of fuselage, the other end of the pressing device is fixedly installed spiral line debugging apparatus, the spiral line debugging apparatus
One end be fixedly installed holding handle, the base end face surrounding is fixedly installed stabilizer blade, and each stabilizer blade bottom surface is fixed
The strength fixing sucking disk for enhancing pedestal stability is provided with, trigger device is provided in the fuselage.
Preferably, the spiral line debugging apparatus includes spiral set, spiral line section, the first spiral rasp bar, the second spiral
Rasp bar, debugging limiting holes and limitation bar.
Preferably, the middle part inside spiral set is provided with spiral line section, the spiral line section is respectively with described the
One spiral rasp bar and the second spiral rasp bar agree with the both ends difference of mating connection, the first spiral rasp bar and the second spiral rasp bar
End with holding handle and pressing device is fixed, and the first spiral rasp bar and the second spiral rasp bar are respectively provided in the inside of opposite side
Have a debugging limiting holes, be connected with the limitation bar between the two debugging limiting holes, the first spiral rasp bar with
Second spiral rasp bar spiral line is backwards.
Preferably, the control device includes empty slot portion, empty slot device, aerating blank pipe, aerating circular hole, gas nozzle, second
Sliding fortune block, enters gas circular hole, the first outlet blank pipe, the first outlet circular hole, the second outlet sky at third sealing circle, block resistance valve, vallecular cavity
Pipe, the second outlet circular hole and air valve.
Preferably, the middle part inside the empty slot portion is provided with the empty slot device, one end middle part in the empty slot portion
Aerating blank pipe is provided with, the aerating blank pipe is internally provided with break-through empty slot device and external aerating circular hole, the aerating
Blank pipe is internally provided with gas nozzle, and the empty slot portion is internally provided with vallecular cavity, and the empty slot portion is internally provided with break-through second
Outlet circular hole and vallecular cavity enter gas circular hole, and the side in the empty slot portion is provided with the first outlet blank pipe, and first outlet is empty
Be internally provided with outside break-through and the first outlet circular hole of vallecular cavity of pipe, the side in the empty slot portion are provided with the second outlet sky
Pipe, be internally provided with outside break-through and the second outlet circular hole of empty slot device side of the second outlet blank pipe, described second
Air valve is provided on outlet blank pipe, the empty slot portion is internally provided with described second and slides fortune block, and described second slides the side of fortune block
Third sealing circle is provided with, described second, which slides fortune block top, is provided with block resistance valve.
Preferably, the trigger device includes the trigger and the fixed setting that are fixed in the cavity portion right side wall
Warning lamp in the fuselage right side, the trigger are connect with the warning light circuit.
Compared with prior art, the beneficial effects of the invention are as follows：
The present invention is used as rubber detection device, by the default of air pressure, plays the role of detection, when air pressure is more than
During preset air pressure, the effect of compression will not be further functioned as, so as to simple in equipment, under the premise of low cost, is realized
Specific detection effect, and its use cost is relatively low, the service life is higher, has stronger practicability.
Description of the drawings
Fig. 1 is a kind of complete section structure diagram of Novel rubber material device of the present invention；
Fig. 2 is the structure diagram of spiral line debugging apparatus in a kind of Novel rubber material device of the present invention；
Fig. 3 is the structure diagram of control device in a kind of Novel rubber material device of the present invention；
Fig. 4 is pedestal bottom surface structure schematic diagram in a kind of Novel rubber material device of the present invention.
Specific embodiment
Below in conjunction with the attached drawing in the embodiment of the present invention, the technical solution in the embodiment of the present invention is carried out clear, complete
Site preparation describes, it is clear that described embodiment is only part of the embodiment of the present invention, instead of all the embodiments.It is based on
Embodiment in the present invention, those of ordinary skill in the art are obtained every other without making creative work
Embodiment shall fall within the protection scope of the present invention.
Referring to Fig. 1, a kind of embodiment provided by the invention：A kind of Novel rubber material device, it is described including fuselage 1
The bottom of fuselage 1 is provided with support plate 2, and the bottom of the support plate 2 is fixedly installed pedestal 3, the inside setting of the fuselage 1
There is cavity portion 4,4 left side of cavity portion is provided with limiting holes 5, and 5 left side of limiting holes is provided with sealing column 6, and the sealing column 6
Right side is provided with sealing pad 7, and the cavity portion 4 is internally provided with sliding fortune plate 21, and the side of the sliding fortune plate 21 is provided with the
One sealing circle 22,21 right side of the sliding fortune plate are fixedly installed horizontal axis 12, the 12 break-through limiting holes 5 of horizontal axis, sealing pad 7,
Column 6 and fuselage 1 are sealed, and 12 left end of the horizontal axis is fixedly installed rubber clamp 13, the fuselage 1 is internally provided with break-through
Limiting holes 5 and the first external outlet circular hole 8, and the first outlet circular hole 8 is internally provided with the first air valve 9, the machine
The bottom of body 1 is fixedly installed control device 24, and the fuselage 1 is internally provided with break-through control device 24 and cavity portion 4
Second outlet circular hole 23, the fuselage 1 are internally provided with polycondensation portion 14, and the fuselage 1 is internally provided with break-through polycondensation portion
14 and the slot hole 10 of limiting holes 5, the slot hole 10 be internally provided with single air valve 11, the polycondensation portion 14 is internally provided with
One slides fortune block 15, and the described first side for sliding fortune block 15 is provided with the second sealing circle 150, and described first slides 15 upper surface of fortune block
Middle part is connected with quarter butt 17 by hinge 16, and the top of the quarter butt 17 is connected to pressing device 18, the pressing by hinge 16
The bottom of 18 one end of device is connected to the top of solid axis by hinge 16, and the bottom of the solid axis is fixed on the upper surface of fuselage 1, institute
The other end for stating pressing device 18 is fixedly installed spiral line debugging apparatus 19, and one end of the spiral line debugging apparatus 19, which is fixed, to be set
It is equipped with and holds handle 20, the 3 bottom surface surrounding of pedestal is fixedly installed stabilizer blade 31, and each 31 bottom surface of stabilizer blade is fixedly installed
For enhancing the strength fixing sucking disk 32 of 3 stability of pedestal, trigger device, the trigger device packet are provided in the fuselage 1
It includes the trigger 401 being fixed in 4 right side wall of cavity portion and is fixed at the warning lamp of 1 right side of fuselage
402, the trigger 401 is connect with 402 circuit of warning lamp, encounters the trigger 401 when the sliding fortune plate 21 moves to right
When, the trigger controls the warning lamp 402 to light, and represents that air pressure inside reaches maximum value, operation principle is：Pass through sky
Presetting for atmospheric pressure, plays the role of detection, when air pressure is more than preset air pressure, will not further function as compression
Effect so as to simple in equipment, under the premise of low cost, realizes specific detection effect, and its use cost is relatively low, the service life compared with
Height, specific workflow are：The rubber one end for needing to stretch is fixed on to the inside of a specific fixing device, the other end is fixed
It in the inside of rubber clamp 13, then reciprocating pressing and pulls up and holds handle 20, slided under the action of fortune block 18 and single gas second
Under the action of valve 11, air is constantly compressed to the inside of limiting holes 5, under the action of the powerful air draught constantly compressed,
So that sliding fortune plate 21 is moved to side, at this point, rubber clamp 13 drives rubber to generate mobile trend, which can generate stretching
Effect, so that rubber is stretched, when after hours, the first air valve 9 of opening discharges pressure-air.
Referring to Fig. 2, the spiral line debugging apparatus 19 includes spiral set 191, spiral line section 192, the first spiral rasp bar
193rd, the second spiral rasp bar 194, debugging limiting holes 195 and limitation bar 196；Middle part inside the spiral set 191 is provided with spiral shell
Shape line section 192, the spiral line section 192 are agreed with cooperation with the first spiral rasp bar 193 and the second spiral rasp bar 194 and are connected respectively
It connects, the both ends of the first spiral rasp bar 193 and the second spiral rasp bar 194 are consolidated respectively with holding the end of handle 24 and pressing device 22
Fixed, the first spiral rasp bar 193 and the second spiral rasp bar 194 are both provided with the debugging limiting holes in the inside of opposite side
195, two it is described debugging limiting holes 195 between be connected with it is described limitation bar 196；The first spiral rasp bar 193 and second
194 spiral line of spiral rasp bar is backwards；It can play the role of debugging backwards to spiral line, due to the first spiral rasp bar 193 and the second spiral shell
Backwards, when rotating spiral set, the first spiral rasp bar 193 and the second spiral rasp bar 194 generate opposite fortune to 194 spiral line of shape rasp bar
Dynamic trend so as to play the role of debugging, can increase leverage, reduce the dynamics of force.
Referring to Fig. 3, the control device 24 includes empty slot portion 241, empty slot device 242, aerating blank pipe 243, aerating circle
Hole 244, gas nozzle 245, second slide fortune block 246, third sealing circle 248, block resistance valve 249, vallecular cavity 2410, enter gas circular hole 2411, the
One outlet blank pipe 2412, the first outlet circular hole 2413, the second outlet blank pipe 2414, the second outlet circular hole 2415 and air valve 2416；
Middle part inside the empty slot portion 241 is provided with the empty slot device 242, is provided with and adds in the middle part of the one end in the empty slot portion 241
Gas blank pipe 243, the aerating circular hole 244 for being internally provided with break-through empty slot device 242 and outside of the aerating blank pipe 243 are described
Gas nozzle 245 is provided in aerating blank pipe 243, is provided with vallecular cavity 2410 in the empty slot portion 241, the empty slot portion 241 it is interior
What portion was provided with the second outlet of break-through circular hole 23 and vallecular cavity 2410 enters gas circular hole 2411, and the side in the empty slot portion 241 is provided with
First outlet blank pipe 2412, and the break-through outside and the first of vallecular cavity 2410 that is internally provided with of the first outlet blank pipe 2412 goes out
Gas circular hole 2413, the side in the empty slot portion 241 are provided with the second outlet blank pipe 2414, the second outlet blank pipe 2414 it is interior
Portion is provided with outside break-through and the second outlet circular hole 2415 of 242 side of empty slot device, and the second outlet blank pipe 2414 is in
Air valve 2416 is provided with, described second is provided in the empty slot portion 241 and slides fortune block 246, described second slides the side of fortune block 246
The third sealing circle 248 is provided with, described second, which slides 246 top of fortune block, is provided with block resistance valve 249；It should be noted that using
Before, quantitative air pressure is injected to the inside of empty slot device 242 by air compressor, the air pressure is as preset pressure
Value uses, and preset air pressure is identical with the dynamics that needs detect, when the air pressure of compression is more than in control device 24
Air pressure when, extra air will be caused to discharge, so as to using control device 24 as detect rubber it is whether up to standard
Express.
Specifically used mode：In present invention work, in use, first adjusting spiral line debugging apparatus 19 and control device
24, then the rubber one end for needing to stretch is fixed on to the inside of a specific fixing device, the other end is fixed on rubber clamp
13 inside, then reciprocating to press and pull up holding handle 20, the effect under the action of the second cunning fortune block 18 with list air valve 11
Under, air is constantly compressed to the inside of limiting holes 5, under the action of the powerful air draught constantly compressed so that sliding fortune plate
21 move to side, at this point, rubber clamp 13 drives rubber to generate mobile trend, which can generate stretching action, so as to
So that rubber is stretched, and due to the presence of control device 24, the air pressure being more than when the air pressure of compression in control device 24
During power, extra air will be caused to discharge, so as to, as detecting whether rubber is up to standard expresses, work as work by the use of control device 24
After work, the first air valve 9 is opened, pressure-air is discharged.
It is obvious to a person skilled in the art that the present invention is not limited to the details of above-mentioned exemplary embodiment, Er Qie
In the case of without departing substantially from spirit or essential attributes of the invention, the present invention 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 present invention is by appended power
Profit requirement rather than above description limit, it is intended that all by what is fallen within the meaning and scope of the equivalent requirements of the claims
Variation is included within the present invention.Any reference numeral in claim should not be considered as to the involved claim of limitation.
Claims (6)
1. a kind of Novel rubber material device, including fuselage, it is characterised in that：The bottom of fuselage is provided with support plate, support plate
Bottom be fixedly installed pedestal, fuselage is internally provided with cavity portion, and limiting holes are provided on the left of cavity portion, are set on the left of limiting holes
There is sealing column, and seal column right side and be provided with sealing pad, cavity portion is internally provided with sliding fortune plate, and the side of sliding fortune plate is provided with
First sealing circle, sliding fortune plate right side are fixedly installed horizontal axis, and horizontal axis break-through limiting holes seal pad, sealing column and fuselage, and horizontal
Axis left end is fixedly installed rubber clamp, and fuselage is internally provided with break-through limiting holes and the first external outlet circular hole, and the
One outlet circular hole is internally provided with the first air valve, and the bottom of fuselage is fixedly installed control device, and the inside setting of fuselage
There are break-through control device and the second outlet circular hole of cavity portion, fuselage is internally provided with polycondensation portion, and being internally provided with for fuselage is worn
The poly- portion of deflation and the slot hole of limiting holes, slot hole are internally provided with single air valve, and first cunning that is internally provided in polycondensation portion transports block, the
One side for sliding fortune block is provided with the second sealing circle, and the first middle part switching for sliding fortune block upper surface is connected with quarter butt, the top of quarter butt
Portion's switching is connected with pressing device, and the bottom patch of pressing device one end is connected with the top of solid axis, Gu the bottom of axis is fixed on fuselage
Upper surface, the other end of pressing device is fixedly installed spiral line debugging apparatus, one end fixed setting of spiral line debugging apparatus
There is holding handle, base end face surrounding is fixedly installed stabilizer blade, and each stabilizer blade bottom surface, which is fixedly installed, is useful for enhancing pedestal stabilization
The strength fixing sucking disk of property is provided with trigger device in the fuselage.
2. a kind of Novel rubber material device according to claim 1, it is characterised in that：Spiral line debugging apparatus includes spiral shell
Shape set, spiral line section, the first spiral rasp bar, the second spiral rasp bar, debugging limiting holes and limitation bar.
3. a kind of Novel rubber material device according to claim 2, it is characterised in that：Middle part setting inside spiral set
There is spiral line section, spiral line section agrees with mating connection, the first spiral rasp bar with the first spiral rasp bar and the second spiral rasp bar respectively
It is fixed respectively with holding the end of handle and pressing device with the both ends of the second spiral rasp bar, the first spiral rasp bar and the second spiral rasp bar
Debugging limiting holes are both provided in the inside of opposite side, be connected restricted bar between two debugging limiting holes, the first spiral line
Bar and the second spiral rasp bar spiral line are backwards.
4. a kind of Novel rubber material device according to claim 1, it is characterised in that：Control device include empty slot portion,
Empty slot device, aerating blank pipe, aerating circular hole, gas nozzle, second slide fortune block, third sealing circle, block resistance valve, vallecular cavity, enter gas circular hole, the
One outlet blank pipe, the first outlet circular hole, the second outlet blank pipe, the second outlet circular hole and air valve.
5. a kind of Novel rubber material device according to claim 6, it is characterised in that：Middle part setting inside empty slot portion
Be free slot device, be provided with aerating blank pipe in the middle part of the one end in empty slot portion, aerating blank pipe be internally provided with break-through empty slot device and
External aerating circular hole is provided with gas nozzle on aerating blank pipe, and empty slot portion is internally provided with vallecular cavity, and empty slot portion is internally provided with
Break-through the second outlet circular hole and vallecular cavity enter gas circular hole, and the side in empty slot portion is provided with the first outlet blank pipe, and the first outlet is empty
Being internally provided with outside break-through for pipe is provided with the second outlet blank pipe with the first outlet circular hole of vallecular cavity, the side in empty slot portion, the
The the second outlet circular hole for being internally provided with outside break-through and empty slot device side of two outlet blank pipes is set on the second outlet blank pipe
There is air valve, the second cunning fortune block is provided in empty slot portion, the second side for sliding fortune block is provided with third sealing circle, and second slides fortune block top
Portion is provided with block resistance valve.
6. a kind of Novel rubber material device according to claim 1, it is characterised in that：The trigger device includes fixing
The trigger that is arranged in the cavity portion right side wall and the warning lamp for being fixed at the fuselage right side, the trigger with
The warning light circuit connection.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711058813.6A CN108226454A (en) | 2017-11-01 | 2017-11-01 | A kind of Novel rubber material device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711058813.6A CN108226454A (en) | 2017-11-01 | 2017-11-01 | A kind of Novel rubber material device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108226454A true CN108226454A (en) | 2018-06-29 |
Family
ID=62655731
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201711058813.6A Pending CN108226454A (en) | 2017-11-01 | 2017-11-01 | A kind of Novel rubber material device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108226454A (en) |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2854130Y (en) * | 2005-12-23 | 2007-01-03 | 北京康斯特仪表科技有限公司 | Gas pressure pump |
| CN201487340U (en) * | 2009-07-17 | 2010-05-26 | 陈银宝 | Differential pressure power type liquid level automatic control valve |
| CN106404543A (en) * | 2016-08-31 | 2017-02-15 | 安徽金星预应力工程技术有限公司 | Prestressed carbon fiber plate anchor test device |
| CN106837963A (en) * | 2017-03-28 | 2017-06-13 | 佛山市高明智悦机械工程有限公司 | A kind of anti-rollover fastener |
-
2017
- 2017-11-01 CN CN201711058813.6A patent/CN108226454A/en active Pending
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2854130Y (en) * | 2005-12-23 | 2007-01-03 | 北京康斯特仪表科技有限公司 | Gas pressure pump |
| CN201487340U (en) * | 2009-07-17 | 2010-05-26 | 陈银宝 | Differential pressure power type liquid level automatic control valve |
| CN106404543A (en) * | 2016-08-31 | 2017-02-15 | 安徽金星预应力工程技术有限公司 | Prestressed carbon fiber plate anchor test device |
| CN106837963A (en) * | 2017-03-28 | 2017-06-13 | 佛山市高明智悦机械工程有限公司 | A kind of anti-rollover fastener |
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| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
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Application publication date: 20180629 |