CN107999355A - A kind of thermal-curable system - Google Patents
A kind of thermal-curable system Download PDFInfo
- Publication number
- CN107999355A CN107999355A CN201810021173.XA CN201810021173A CN107999355A CN 107999355 A CN107999355 A CN 107999355A CN 201810021173 A CN201810021173 A CN 201810021173A CN 107999355 A CN107999355 A CN 107999355A
- Authority
- CN
- China
- Prior art keywords
- heater box
- cover
- fuselage
- fuselage cover
- curing room
- 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.)
- Withdrawn
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B05—SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
- B05D—PROCESSES FOR APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
- B05D3/00—Pretreatment of surfaces to which liquids or other fluent materials are to be applied; After-treatment of applied coatings, e.g. intermediate treating of an applied coating preparatory to subsequent applications of liquids or other fluent materials
- B05D3/02—Pretreatment of surfaces to which liquids or other fluent materials are to be applied; After-treatment of applied coatings, e.g. intermediate treating of an applied coating preparatory to subsequent applications of liquids or other fluent materials by baking
- B05D3/0209—Multistage baking
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B05—SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
- B05D—PROCESSES FOR APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
- B05D3/00—Pretreatment of surfaces to which liquids or other fluent materials are to be applied; After-treatment of applied coatings, e.g. intermediate treating of an applied coating preparatory to subsequent applications of liquids or other fluent materials
- B05D3/02—Pretreatment of surfaces to which liquids or other fluent materials are to be applied; After-treatment of applied coatings, e.g. intermediate treating of an applied coating preparatory to subsequent applications of liquids or other fluent materials by baking
- B05D3/0218—Pretreatment, e.g. heating the substrate
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B05—SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
- B05D—PROCESSES FOR APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
- B05D3/00—Pretreatment of surfaces to which liquids or other fluent materials are to be applied; After-treatment of applied coatings, e.g. intermediate treating of an applied coating preparatory to subsequent applications of liquids or other fluent materials
- B05D3/02—Pretreatment of surfaces to which liquids or other fluent materials are to be applied; After-treatment of applied coatings, e.g. intermediate treating of an applied coating preparatory to subsequent applications of liquids or other fluent materials by baking
- B05D3/0254—After-treatment
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B05—SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
- B05D—PROCESSES FOR APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
- B05D3/00—Pretreatment of surfaces to which liquids or other fluent materials are to be applied; After-treatment of applied coatings, e.g. intermediate treating of an applied coating preparatory to subsequent applications of liquids or other fluent materials
- B05D3/04—Pretreatment of surfaces to which liquids or other fluent materials are to be applied; After-treatment of applied coatings, e.g. intermediate treating of an applied coating preparatory to subsequent applications of liquids or other fluent materials by exposure to gases
- B05D3/0406—Pretreatment of surfaces to which liquids or other fluent materials are to be applied; After-treatment of applied coatings, e.g. intermediate treating of an applied coating preparatory to subsequent applications of liquids or other fluent materials by exposure to gases the gas being air
- B05D3/0426—Cooling with air
Landscapes
- Heating, Cooling, Or Curing Plastics Or The Like In General (AREA)
Abstract
The invention discloses a kind of thermal-curable system,Including fuselage cover and fixed pedestal,The inside both sides of the fuselage cover are symmetrically arranged with preheating chamber,Curing room is provided between two preheating chambers,The insertion of the both sides of the preheating chamber and curing room is provided with electric heater,The quantity of curing room inside electric heater is twice of electric heater quantity inside preheating chamber,One end of the fuselage cover is provided with import,And the other end of fuselage cover is provided with outlet,The present invention is respectively arranged with the first sealing cover and the second sealing cover in the entrance of fuselage cover and exit,The inlet and outlet at fuselage cover both ends can be sealed,Prevent the heat losses inside preheating chamber and curing room when solid,And first sealing cover and the second sealing cover can be slided respectively by telescopic rod and fixed link,It is convenient to be adjusted according to the position of the first heater box and the second heater box,It is easy to use.
Description
Technical field
The invention belongs to thermal-curable system technical field, and in particular to a kind of thermal-curable system.
Background technology
Thermal-curable system be widely used in the precuring of OC, photoresist, Protection glue, silver paste, ink etc. in CTP industries,
The curing of LENS ink and the curing of OGS ink, the structure of thermal-curable system currently on the market are similar to baking oven.
Now with thermal-curable system in use there are some defects, such as thermal-curable system is airtight to some
Property more demanding product when being fixed, it is most of can not achieve it is continuous it is reciprocal cure, although small part equipment being capable of the company of realization
It is continuous to cure, but since the leakproofness of device is poor, the qualification rate of product is relatively low.
The content of the invention
It is an object of the invention to provide a kind of thermal-curable system, is disguised with solving thermosetting proposed in the above background technology
Put when the more demanding product of some air-tightness is fixed, it is most of to can not achieve continuous curing, although small part equipment
It can realize continuous reciprocal curing, but due to the problem of leakproofness of device is poor, and product qualification rate is relatively low.
To achieve the above object, the present invention provides following technical solution：A kind of thermal-curable system, including fuselage cover and solid
Determine pedestal, the inside both sides of the fuselage cover are symmetrically arranged with preheating chamber, curing room are provided between two preheating chambers,
The both sides of the preheating chamber and curing room are embedded to be provided with electric heater, and the quantity of curing room inside electric heater is pre-
Twice of electric heater quantity inside hot cell, one end of the fuselage cover is provided with import, and the other end of fuselage cover is set
It is equipped with outlet.
Preferably, the preheating chamber on the fuselage cover at entrance location is internally provided with the second heater box, described
Curing room is internally provided with the first heater box, and first heater box in the second heater box by hinge with being rotatably connected to
Chamber door, and thermal insulation board is provided between the first heater box and the second heater box, away from the first heater box in second heater box
One end be fixedly connected with head rod, one end of the head rod is connected with telescopic rod, the outside of the telescopic rod
The first sealing cover is slidably connected, the telescopic rod is installed on the inside of hydraulic cylinder.
Preferably, the side at the top of the fixed pedestal close to hydraulic cylinder is provided with fixed case, the inside of the fixed case
Hydraulic oil container is installed, one end of the hydraulic oil container is provided with hydraulic pump, and the hydraulic pump passes through hydraulic oil pipe and hydraulic cylinder
Connection, the hydraulic cylinder are bolted to connection with fixed case.
Preferably, the side away from the second heater box is provided with the second connecting rod in first heater box, and described second
One end of connecting rod is connected with fixed link, and the fixed link is retractable structure, and the slide outside of fixed link is connected with second
Sealing cover, one end away from the second connecting rod is connected with sliding block in the fixed link, and the bottom symmetrical of the sliding block offers cunning
Groove, and sliding block is slidably connected by slide and fixed pedestal, the slide is symmetrically mounted on fixed pedestal close to the one of outlet
Side, is provided with limited block on the fixed pedestal with the symmetrical one end of fixed case.
Preferably, air compressor machine is installed, one end of the air compressor machine is communicated with connecting tube, institute at the top of the fuselage cover
State connecting tube to connect with curing room through fuselage cover, side is provided with AT89S52 controllers outside the fuselage cover, described
Exhaust pipe is installed close to the side of AT89S52 controllers on fuselage cover, the exhaust pipe is connected with curing room.
Preferably, first sealing cover and fuselage cover are rectangular parallelepiped structure, the size of first sealing cover with
The size of fuselage cover upper inlet is identical, and the outside of the first sealing cover is provided with sealing ring.
Compared with prior art, the present invention have the advantages that：
(1) present invention is internally provided with two preheating chambers and a curing room in fuselage cover, and preheating chamber can be to needing
The defects of wanting cured product to be preheated, can preventing excessive temperature differentials from bringing such as bubble, wrinkle to product surface, improves production
The qualification rate of product, curing room are arranged between two preheating chambers, and preheating chamber is internally provided with the second heater box wherein,
The first heater box, and the position of the first heater box and the second heater box inside preheating chamber and curing room are internally provided with curing room
Putting to switch over, and when being put into the cured product of needs from the entrance of fuselage cover, the second heater box is made at this time
For preheating cabinet, it is arranged on inside preheating chamber, product is preheated, is entered after the completion of preheating inside curing room and product is carried out
Cure, after the completion of curing, enter back into inside another preheating chamber, carry out Slow cooling, until cooling completion, from the second heating
Article is taken out inside case, be again put into the first heater box as preheating cabinet needs cured product at this time, is introduced into preheating chamber
Inside is preheated, and after the completion of preheating, is entered back into inside curing room and is fixed, after the completion of curing, enters opposite side
Cooled down inside preheating chamber, taken out after the completion of cooling, you can complete continuous cyclic process.
(2) present invention is respectively arranged with the first sealing cover and the second sealing cover in the entrance of fuselage cover and exit,
The inlet and outlet at fuselage cover both ends can be sealed, prevent the heat stream inside preheating chamber and curing room when solid
Lose, and the first sealing cover and the second sealing cover can be slided by telescopic rod and fixed link respectively, it is convenient to add according to first
The position of hot tank and the second heater box is adjusted, easy to use.
(3) hydraulic cylinder that is moved through of the first heater box of the invention and the second heater box drives telescopic rod to stretch to carry out
Move back and forth, it is not necessary to it is manually mobile, it is more convenient to use, and there is provided sliding block to be slidably connected with the slide on fixed pedestal,
The first heater box and the second heater box can be made more to stablize in movement.
Brief description of the drawings
Fig. 1 is the structure diagram of the present invention；
Fig. 2 is the top view of the present invention；
Fig. 3 is the side view of the present invention；
Fig. 4 is the circuit block diagram of the present invention；
In figure：1- hydraulic oil pipes, 2- hydraulic oil containers, 3- hydraulic pumps, 4- hydraulic cylinders, 5- telescopic rods, 6- fixed cases, 7- first
Connecting rod, the first sealing covers of 8-, 9- fuselage covers, 10- thermal insulation boards, 11- connecting tubes, 12- air compressor machines, 13- preheating chambers, 14-
Two sealing covers, 15- limited blocks, 16- slides, 17- sliding blocks, 18- fixed pedestals, 19- fixed links, the second connecting rods of 20-, 21- electricity
Heater, 22- curing rooms, the first heater boxes of 23-, the second heater boxes of 24-, 25- imports, 26- outlets, 27- exhaust pipes, 28-
AT89S52 controllers.
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, belongs to the scope of protection of the invention.
- 4 are please referred to Fig.1, the present invention provides a kind of technical solution：A kind of thermal-curable system, including fuselage cover 9 and fixation
Pedestal 18, the inside both sides of fuselage cover 9 are symmetrically arranged with preheating chamber 13, can for being preheated to the cured product of needs
The defects of to prevent excessive temperature differentials from bringing such as bubble, wrinkle to product surface, improve the qualification rate of product, two preheating chambers 13
Between be provided with curing room 22, for curing to the product after preheating, the both sides of preheating chamber 13 and curing room 22 are embedded
Electric heater 21 is installed, the quantity of 22 inside electric heater 21 of curing room is the two of 13 inside electric heater of preheating chamber, 21 quantity
Times, one end of fuselage cover 9 is provided with import 25, and the other end of fuselage cover 9 is provided with outlet 26.
Further, the preheating chamber 13 on fuselage cover 9 at 25 position of import is internally provided with the second heater box 24,
Curing room 22 is internally provided with the first heater box 23, is rotated and connected by hinge in the first heater box 23 and the second heater box 24
Chamber door is connected to, easy to take and be put into product, and thermal insulation board 10 is provided between the first heater box 23 and the second heater box 24, is prevented
Only heat flows between the first heater box 23 and the second heater box 24, one end away from the first heater box 23 in the second heater box 24
Head rod 7 is fixedly connected with, one end of head rod 7 is connected with telescopic rod 5, and the slide outside of telescopic rod 5 is connected with
First sealing cover 8, can seal up import 25 carrying out curing room, prevent the heat stream inside preheating chamber and curing room when solid
Lose, telescopic rod 5 is installed on the inside of hydraulic cylinder 4.
Preferably, the top of fixed pedestal 18 is provided with fixed case 6, the inside installation of fixed case 6 close to the side of hydraulic cylinder 4
There is hydraulic oil container 2, one end of hydraulic oil container 2 is provided with hydraulic pump 3, and hydraulic pump 3 uses KCB-55 type hydraulic pumps, and hydraulic pump 3 is logical
Cross hydraulic oil pipe 1 to connect with hydraulic cylinder 4, hydraulic cylinder 4 is bolted to connection with fixed case 6.
What deserves to be explained is the side away from the second heater box 24 is provided with the second connecting rod 20 in the first heater box 23,
One end of second connecting rod 20 is connected with fixed link 19, and fixed link 19 is retractable structure, and the slide outside of fixed link 19 connects
The second sealing cover 14 is connected to, one end away from the second connecting rod 20 is connected with sliding block 17, the bottom pair of sliding block 17 in fixed link 19
Title offers sliding slot, and sliding block 17 is slidably connected by slide 16 and fixed pedestal 18, and sliding block 17 is by sliding slot on slide 16
Sliding, the stability of the slip of sliding block 17 can be improved, slide 16 is symmetrically mounted on fixed pedestal 18 close to the side of outlet 26,
Limited block 15 is installed with 6 symmetrical one end of fixed case on fixed pedestal 18, the position that can be slided to sliding block 17 is defined.
In addition, the top of fuselage cover 9 is provided with air compressor machine 12, and one end of air compressor machine 12 is communicated with connecting tube 11,
Connecting tube 11 is connected through fuselage cover 9 with curing room 22, and 9 outside side of fuselage cover is provided with AT89S52 controllers 28, machine
Exhaust pipe 27 is installed close to the side of AT89S52 controllers 28 on body shell 9, exhaust pipe 27 is connected with curing room 22.
The first sealing cover 8 and the second sealing cover 14 is slided to seal the import 25 of fuselage cover 9 and outlet 26 respectively,
Specifically, the first sealing cover 8 and fuselage cover 9 are rectangular parallelepiped structure, outside the size and fuselage of the first sealing cover 8
The size of 9 upper inlet 25 of shell is identical, and the outside of the first sealing cover 8 is provided with sealing ring.
The operation principle and process for using of the present invention：After the thermal-curable system installs, first pass through first at import 25
Chamber door in 23 and second heater box 24 of heater box opens the first heater box 23 and the second heater box 24, to 23 He of the first heater box
Being added inside second heater box 24 needs cured product, then hydraulic pump 3 is worked by AT89S52 controllers 28, hydraulic pressure
Hydraulic oil in hydraulic oil container 2 is pressed into inside hydraulic cylinder 4 by the work of pump 3 by hydraulic oil pipe 1, and hydraulic cylinder 4 promotes telescopic rod 5 by the
Two heater boxes 24 are pushed into inside fuselage cover 9 by import 25, and the second heater box 24 moves to side and drives the first heater box 23
Mobile, the first heater box 23 movement band movable slider 17 slides on slide 16, when the first heater box 23 is completely into outside fuselage
Behind 9 inside of shell, start electric heater 21, the first heater box 23 is internally heated, first pass through preheating chamber 13 and heated to first
23 internal product of case is heated, and after the completion of heating, then by AT89S52 controllers 28 hydraulic pump 3 is worked, 3 work of hydraulic pump
Work continues forward to promote the second heater box 24, until the second heater box 24 is completely into inside fuselage cover 9, at this time first
Heater box 23 is pushed into inside curing room 22, and 23 internal product of the first heater box is cured, in the second heater box 24
Portion is preheated, and after the completion of 23 internal product of the first heater box cures, is further continued for promoting forward, makes the production of the inside of the first heater box 23
Product are moved to inside another preheating chamber 13 and are precooled, and the second heater box 24, which is entered inside curing room 22, at this time is consolidated
It is fixed, after the completion of 23 internal product of the first heater box precools, it will continue forward to promote 23 internal product of the first heater box, until
Promote outside fuselage cover 9, the good product of 24 inside solidification of the second heater box enters another and carries out in preheating chamber 13 at this time
Portion is precooled, and after the completion of cooling, is taken out 23 internal product of the first heater box, is then further continued for promoting forward, second is added
24 internal product of hot tank is cooled down, until the first heater box 23 and the second heater box 24 are all pushed to the outside of outlet 26, the
After the completion of the cooling of two heater boxes, 24 internal product, product is taken out, then respectively to inside the first heater box 23 and the second heater box 24
Adding needs cured product, is cured again by outlet 26, and solidification process is identical with solidification process at import 25, not superfluous
State, reciprocation cycle curing can be carried out by this Thermocuring equipment, effectively increase cured efficiency.
Although an embodiment of the present invention has been shown and described, for the ordinary skill in the art, can be with
Understanding without departing from the principles and spirit of the present invention can carry out these embodiments a variety of changes, modification, replace
And modification, the scope of the present invention is defined by the appended.
Claims (6)
1. a kind of thermal-curable system, including fuselage cover (9) and fixed pedestal (18), it is characterised in that：The fuselage cover (9)
Inside both sides be symmetrically arranged with preheating chamber (13), be provided with curing room (22) between two preheating chambers (13), it is described pre-
The both sides insertion of hot cell (13) and curing room (22) is provided with electric heater (21), the internal electric heater of the curing room (22)
(21) quantity is twice of internal electric heater (21) quantity of preheating chamber (13), and one end of the fuselage cover (9) is provided with
Import (25), and the other end of fuselage cover (9) is provided with outlet (26).
A kind of 2. thermal-curable system according to claim 1, it is characterised in that：Close to import on the fuselage cover (9)
(25) preheating chamber at position (13) is internally provided with the second heater box (24), and the curing room (22) is internally provided with first
Heater box (23), is rotatably connected to chamber door in first heater box (23) and the second heater box (24) by hinge, and the
Thermal insulation board (10) is provided between one heater box (23) and the second heater box (24), away from first on second heater box (24)
One end of heater box (23) is fixedly connected with head rod (7), and one end of the head rod (7) is connected with telescopic rod
(5), the slide outside of the telescopic rod (5) is connected with the first sealing cover (8), and the telescopic rod (5) is installed on hydraulic cylinder (4)
It is internal.
A kind of 3. thermal-curable system according to claim 1, it is characterised in that：Close to liquid at the top of the fixed pedestal (18)
The side of cylinder pressure (4) is provided with fixed case (6), and the inside of the fixed case (6) is provided with hydraulic oil container (2), the hydraulic oil
One end of case (2) is provided with hydraulic pump (3), and the hydraulic pump (3) is connected by hydraulic oil pipe (1) with hydraulic cylinder (4), the liquid
Cylinder pressure (4) is bolted to connection with fixed case (6).
A kind of 4. thermal-curable system according to claim 2, it is characterised in that：Away from the on first heater box (23)
The side of two heater boxes (24) is provided with the second connecting rod (20), and one end of second connecting rod (20) is connected with fixed link
(19), the fixed link (19) is retractable structure, and the slide outside of fixed link (19) is connected with the second sealing cover (14), institute
State one end away from the second connecting rod (20) in fixed link (19) and be connected with sliding block (17), the bottom symmetrical of the sliding block (17) is opened
Equipped with sliding slot, and sliding block (17) is slidably connected by slide (16) and fixed pedestal (18), and the slide (16) is symmetrically mounted on
Installed on fixed pedestal (18) on the side of outlet (26), the fixed pedestal (18) with the symmetrical one end of fixed case (6)
There is limited block (15).
A kind of 5. thermal-curable system according to claim 1, it is characterised in that：The top installation of the fuselage cover (9)
There is air compressor machine (12), one end of the air compressor machine (12) is communicated with connecting tube (11), and the connecting tube (11) runs through fuselage cover
(9) connected with curing room (22), the exterior side of the fuselage cover (9) is provided with AT89S52 controllers (28), outside the fuselage
Exhaust pipe (27), the exhaust pipe (27) and curing room (22) are installed close to the side of AT89S52 controllers (28) on shell (9)
Connection.
A kind of 6. thermal-curable system according to claim 1, it is characterised in that：Outside first sealing cover (8) and fuselage
Shell (9) is rectangular parallelepiped structure, and the size of first sealing cover (8) is identical with the size of fuselage cover (9) upper inlet (25),
And first the outside of sealing cover (8) be provided with sealing ring.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810021173.XA CN107999355A (en) | 2018-01-10 | 2018-01-10 | A kind of thermal-curable system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810021173.XA CN107999355A (en) | 2018-01-10 | 2018-01-10 | A kind of thermal-curable system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107999355A true CN107999355A (en) | 2018-05-08 |
Family
ID=62049952
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810021173.XA Withdrawn CN107999355A (en) | 2018-01-10 | 2018-01-10 | A kind of thermal-curable system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107999355A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109459874A (en) * | 2018-11-14 | 2019-03-12 | 蚌埠高华电子股份有限公司 | A kind of ito glass sylphon frame glue curing mechanism device |
| CN113894023A (en) * | 2021-10-15 | 2022-01-07 | 山东润马光能科技有限公司 | Sealant accelerated curing device for solar cell module |
-
2018
- 2018-01-10 CN CN201810021173.XA patent/CN107999355A/en not_active Withdrawn
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109459874A (en) * | 2018-11-14 | 2019-03-12 | 蚌埠高华电子股份有限公司 | A kind of ito glass sylphon frame glue curing mechanism device |
| CN109459874B (en) * | 2018-11-14 | 2021-09-17 | 蚌埠高华电子股份有限公司 | ITO glass empty box frame glue curing mechanism device |
| CN113894023A (en) * | 2021-10-15 | 2022-01-07 | 山东润马光能科技有限公司 | Sealant accelerated curing device for solar cell module |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN106476304B (en) | Fast curing prepreg answers material product moulding pressing device and method | |
| CN107999355A (en) | A kind of thermal-curable system | |
| CN209368114U (en) | A kind of glass heat bender | |
| CN201220483Y (en) | High temperature vacuum press | |
| CN101532793A (en) | Sealing equipment of boiling and exhaust of semi-automatic heat pipe | |
| CN107342390A (en) | Pole plate drying unit is used in a kind of lithium battery manufacture | |
| CN207825461U (en) | A kind of membrane pressure device for phone housing production | |
| CN203863900U (en) | Extreme cold and extreme hot shaping machine | |
| CN109624247A (en) | A kind of Clamping Device of Injection Moulding Machine | |
| CN209334716U (en) | A kind of powder metallurgy sintered device of clean type | |
| CN210362092U (en) | Quick forming die of preimpregnation material product | |
| CN209133953U (en) | GIS device SF6Gas leaks quick lash-up recovering device | |
| CN208514846U (en) | A kind of TPU secondary frothing forming mechanism | |
| CN208416866U (en) | A kind of afterheat recovery unit of air compressor | |
| CN208517267U (en) | A kind of glass heat bender | |
| CN107575743B (en) | A kind of efficient air temperature heat exchange type compressed natural gas pressure-relief device and decompression method | |
| CN206083619U (en) | Car stopper shaping mold processing | |
| CN208930715U (en) | A kind of quickening speed of production and energy-saving and environment-friendly six pipes pipe-expanding machine | |
| CN208091137U (en) | A kind of hot air circulation energy-saving baking box prepared based on medicine intermediate | |
| CN207861429U (en) | Apply the transmission mechanism on non-spherical glass lens moulding press | |
| CN207481080U (en) | A kind of injection machine mould fixing device | |
| CN205864236U (en) | Portable air water cooling arrangements for speed regulation | |
| CN217752702U (en) | Vacuum cooling shaping table for processing sealing strips | |
| CN208946744U (en) | A kind of bag with square bottom process equipment of removable adjusting | |
| CN203672175U (en) | Horizontal condenser |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WW01 | Invention patent application withdrawn after publication | ||
| WW01 | Invention patent application withdrawn after publication |
Application publication date: 20180508 |