CN105690299B - One kind vapour deposition shallow layer solidification frock - Google Patents
One kind vapour deposition shallow layer solidification frock Download PDFInfo
- Publication number
- CN105690299B CN105690299B CN201610224063.4A CN201610224063A CN105690299B CN 105690299 B CN105690299 B CN 105690299B CN 201610224063 A CN201610224063 A CN 201610224063A CN 105690299 B CN105690299 B CN 105690299B
- Authority
- CN
- China
- Prior art keywords
- side plate
- seat board
- ribs
- loading blocks
- spacing
- 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.)
- Active
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B25—HAND TOOLS; PORTABLE POWER-DRIVEN TOOLS; MANIPULATORS
- B25B—TOOLS OR BENCH DEVICES NOT OTHERWISE PROVIDED FOR, FOR FASTENING, CONNECTING, DISENGAGING OR HOLDING
- B25B11/00—Work holders not covered by any preceding group in the subclass, e.g. magnetic work holders, vacuum work holders
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
- G01N19/00—Investigating materials by mechanical methods
- G01N19/04—Measuring adhesive force between materials, e.g. of sealing tape, of coating
Landscapes
- Physics & Mathematics (AREA)
- Health & Medical Sciences (AREA)
- Life Sciences & Earth Sciences (AREA)
- Chemical & Material Sciences (AREA)
- Analytical Chemistry (AREA)
- Biochemistry (AREA)
- General Health & Medical Sciences (AREA)
- General Physics & Mathematics (AREA)
- Immunology (AREA)
- Pathology (AREA)
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Sampling And Sample Adjustment (AREA)
- Physical Vapour Deposition (AREA)
Abstract
The invention provides a kind of vapour deposition shallow layer solidification frock, including seat board, side plate and loading blocks；The side plate is fixed on the both sides of the seat board；The seat board center is provided with the ribs parallel with side plate, the ribs and is evenly equipped with some grooves；The loading blocks are in ladder shaft-like, and relatively described ribs are symmetrical and uniform along the bearing of trend of the ribs in pairs；The groove that the small end of the loading blocks is located at the ribs is interior and spacing by groove this described, and the big end of the loading blocks is located on any upper surface of the seat board of ribs both sides and positioned by the upper surface；Some screw holes matched with trip bolt are also evenly equipped with the side plate, the end of the trip bolt penetrates between side plate from the screw hole and contacted with the big end outer surface centre bore of the loading blocks, the trip bolt can by the centre bore to loading blocks apply axial load.The invention can be reliably controlled axial pre tightening force, accurate positioning, efficiency high.
Description
Technical field
The invention belongs to coating binding force detection device technical field, more particularly to a kind of PVD (sink by physical vapor
Product) and CVD (chemical vapor deposition) shallow layer solidify frock.
Background technology
Coating prepared by PVD (physical vapour deposition (PVD)) and CVD (chemical vapor deposition) coating has bond strength high, tough
The good, wearability of property is good, and the features such as high and good heat endurance of chemical stability is good is high-end component of machine surfacecti proteon
The coating of future is most applied in coating material.Such as CrN, TiN, TiCN, WCN coating are widely used in cutter, measuring tool, mould
Has contour terminal tool part field.
But coating prepared by PVD (physical vapour deposition (PVD)) and CVD (chemical vapor deposition) is very thin, majority is 2~20 μm, is given
Clamping during the adhesion detection of coating brings very big difficulty.The preparation of existing coating test is difficult to obtain reliable dress
Press from both sides pretightning force.
The content of the invention
The invention, can to solve the problems of the prior art there is provided one kind vapour deposition shallow layer solidification frock
It is good with simple and easy to operate, highly versatile, accurate positioning, efficiency high and security reliably to be controlled axial pre tightening force
The features such as.
A kind of vapour deposition shallow layer solidification frock that the invention is provided, including seat board, side plate and loading blocks；It is described
Side plate is fixed on the both sides of the seat board；The seat board center is provided with the ribs parallel with side plate, the ribs
It is furnished with some grooves；The loading blocks are in ladder shaft-like, and relatively described ribs are symmetrical in pairs and along the extension of the ribs
Direction is uniform；The small end of the loading blocks is located in the groove of the ribs and, the loading blocks spacing by groove this described
Big end be located at ribs both sides seat board any upper surface on and positioned by the upper surface；It is also uniform on the side plate
Have some screw holes matched with trip bolt, the end of the trip bolt penetrated from the screw hole between side plate and with institute
The big end outer surface centre bore contact of loading blocks is stated, the trip bolt can be applied by the centre bore to loading blocks axially to be carried
Lotus.
Wherein, the side plate outer surface is in alternate concaveconvex structure, and the female parts of the side plate are evenly equipped with can be with consolidating
Determine the fixing hole of screw mates, the correspondence position of the seat board bottom also is provided with the base plate hole that can be matched with fixing screws, institute
Side plate is stated to be fixedly connected with the bottom of the seat board by the fixing screws for being distributed in female parts.It is preferred that, the fixing screws
From hexagon socket cap head screw.
Wherein, the trip bolt is distributed in the concave portion of side plate.
Wherein, the trip bolt is sequentially provided with head, threaded portion, guide rod portion and end；Head is preferably turret head
Portion；End is in the angle of horn shape, preferably 60 °.
Wherein, the groove of the ribs of the seat board is preferably in inverted trapezoidal groove.
Wherein, at least one pair of spacing hole is symmetrically arranged with also relative to seat board oblique angle on the side plate, the spacing hole is supplied
Spacer pin by and go deep into inside seat board realizing between seat board and side plate further consolidate it is spacing.The preferred status of spacing hole
In the female parts of the side plate, it more preferably can directly replace fixing screws relevant position required on side plate and set.
Wherein, it is additionally provided with the seat board and the limit channels of stop screw is communicated and can accommodated with groove, it is described spacing
Passage coordinates with the stop screw screw thread.
Further, the stop screw is sequentially provided with spacing head, thread segment and spacing end；The thread segment is excellent
Selection of land uses fine thread；The end face of the spacing end is plane.
Wherein, the centre bore of the loading blocks is preferably the hole made according to GB/T4459.5-B2/5.Further, it is described
The end Ying Qing angles processing of the small end of loading blocks.
The invention is simple in construction, easy to operate, versatility is good, and clamping position is stable and position is accurate, and can lead to
Cross fine setting and eliminate workpiece machining error, reduce offset deviation, the blessing that can be applied to 2~20 μm of shallow layers is fixed.
Brief description of the drawings
Fig. 1 is a kind of overall structure diagram of embodiment of the invention；
Fig. 2 is structural representations of the Fig. 1 in overlook direction；
Fig. 3 is the sectional view in A-A directions in Fig. 2；
Fig. 4 is the structural representation of Fig. 1 latus inframediums；
Fig. 5 is the sectional view in B-B directions in Fig. 4；
Fig. 6 is the structural representation of seat board in Fig. 1；
Fig. 7 is structural representations of the Fig. 6 in left view direction；
Fig. 8 is structural representations of the Fig. 6 in overlook direction；
Fig. 9 is the structural representation of trip bolt in Fig. 1；
Figure 10 is structural representations of the Fig. 9 in left view direction；
Figure 11 is the structural representation of loading blocks in Fig. 1；
Figure 12 is structural representations of the Figure 11 in overlook direction；
Figure 13 is the structural representation of stop screw in Fig. 1；
Figure 14 is structural representations of the Figure 13 in left view direction.
Wherein, 1- seat boards；11- ribs；111- grooves；12- base plate holes；13- limit channels；2- side plates；21- screws
Hole；22- fixing holes；3- loading blocks；4- trip bolts；41- heads；42- threaded portions；43- guide rods portion；44- ends；5- fixes spiral shell
Nail；6- spacer pins；7- stop screws；The spacing heads of 71-；72- thread segments；The spacing ends of 73-.
Embodiment
The invention is further described below by with reference to accompanying drawing.
A kind of embodiment of the invention structure as Figure 1-3, including seat board 1, side plate 2 and loading blocks 3；The side
Plate 2 is fixed on the both sides of the seat board 1；The center of seat board 1 is provided with the ribs 11 parallel with side plate 2, the ribs
Some grooves 111 are evenly equipped with 11；The loading blocks 3 are in ladder shaft-like, and relatively described ribs 11 are symmetrical in pairs and along described
The bearing of trend of ribs 11 is uniform；The small end of the loading blocks 3 is located in the groove 111 of the ribs 11 and by this described
Groove 111 is spacing, and the big end of the loading blocks 3 is located on any upper surface of the seat board 1 of the both sides of ribs 11 and by the upper table
Face contact positioning；Some screw holes 21 matched with trip bolt 4, the end of the trip bolt 4 are also evenly equipped with the side plate 2
Portion penetrates between side plate 2 from the screw hole 21 and contacted with the big end outer surface centre bore of the loading blocks 3, the fastening spiral shell
Nail 4 can by the centre bore to loading blocks 3 apply axial load.
Wherein, the side plate 2 is as illustrated in figures 4-5.The outer surface of side plate 2 is in alternate concaveconvex structure, the side plate 2
Female parts are evenly equipped with the fixing hole 22 that can be matched with fixing screws 5, and the correspondence position of the bottom of seat board 1 also is provided with can
The base plate hole 12 matched with fixing screws 5, the side plate 2 is by being distributed in the fixing screws 5 of female parts and the bottom of the seat board 1
Portion is fixedly connected, and the attachment structure helps to realize the steadiness of the two connection.It is preferred that, the fixing screws 5 are from interior six
Angle fillister head screw.
Wherein, the trip bolt 4 is distributed in the concave portion of side plate 2, contributes to increase trip bolt 4 and the phase of side plate 2
The length of mutual contact portion, is more beneficial for improving positioning precision.
Wherein, the trip bolt 4 is as shown in figs. 9-10.The trip bolt 4 be sequentially provided with head 41, threaded portion 42,
Guide rod portion 43 and end 44；Head 41 is preferably hexagon-head；Threaded portion 42 be used for in the screw hole 21 of the side plate 2
Screw thread is mutually engaged and positioned；Guide rod portion 43 and the gap of screw hole 21 of the side plate 2, which coordinate, is easy to stretching for the trip bolt 4
Enter；End 44 is in the angle of horn shape, preferably 60 °, is easy to accurately contact with the big end outer surface centre bore of loading blocks 3.
Wherein, the groove 111 of the ribs 11 of the seat board 1 is in preferably inverted trapezoidal groove, and positioning precision is higher, be easy to
Trip bolt 4 coordinates the positioning action reached to loading blocks 3.
Wherein, at least one pair of spacing hole, the spacing hole are symmetrically arranged with also relative to the oblique angle of seat board 1 on the side plate 2
For spacer pin 6 by and go deep into realizing inside seat board 1 between seat board 1 and side plate 2 further consolidate it is spacing.The spacing hole is excellent
Selection of land is located at the female parts of the side plate 2, the relevant position of fixing screws 5 needed for more preferably can directly replacing on side plate 2
And set.
Wherein, the seat board 1 is as shown in figs 6-8.It is additionally provided with the seat board 1 and limit is communicated and can accommodated with groove 111
The limit channels 13 of position screw 7, the limit channels 13 coordinate with the screw thread of stop screw 7, and the stop screw 7 can lead to
Minor adjustment of the lift action realization to the small end position of loading blocks 3 of screw thread cooperation is crossed, so as to eliminate part manufacturing tolerance
Caused loading position skew.
Further, the stop screw 7 is as illustrated in figs. 13-14.It is sequentially provided with spacing head 71, thread segment 72 and limit
Position end 73；It is easy to the twisting in position adjustment in the spacing head 71；The thread segment 72 be used to it is described spacing logical
The screw thread in road 13 coordinates, and preferably by fine thread, is easy to the control of small lifting travel；The end face of the spacing end 73
For plane, it is easy to contact with the small end outer surface of loading blocks 3.
Wherein, the loading blocks 3 are as depicted in figs. 11-12.The centre bore of the loading blocks 3 is preferably according to GB/
The hole that T4459.5-B2/5 makes.Further, the end Ying Qing angles processing of the small end of the loading blocks 3.
The invention is in use, only need scumbling to be detected being placed between symmetrically arranged loading blocks 3, and make
Symmetrical loading blocks 3 clamp shallow layer to be detected under the tiny pretightning force effect in axial direction that both sides trip bolt 4 applies,
When needing to be finely adjusted to eliminate deviation the position of loading blocks 3, slight adjustment stop screw 7.
The preferred embodiment of the invention is the foregoing is only, creation is not intended to limit the invention, it is all at this
Within the spirit and principle of innovation and creation, any modification, equivalent substitution and improvements made etc. should be included in the invention
Protection domain within.
Claims (6)
1. one kind vapour deposition shallow layer solidification frock, including seat board, side plate and loading blocks；The side plate is fixed on the seat board
Both sides；The seat board center is provided with the ribs parallel with side plate, the ribs and is evenly equipped with some grooves；It is described to add
It is in ladder shaft-like to carry block, and relatively described ribs are symmetrical and uniform along the bearing of trend of the ribs in pairs；The loading blocks
Small end be located in the groove of the ribs and spacing by groove this described, the big ends of the loading blocks is located at ribs both sides
Seat board any upper surface on and positioned by the upper surface；Also it is evenly equipped with and some is matched with trip bolt on the side plate
Screw hole, the end of the trip bolt penetrated from the screw hole between side plate and with the big end outer surface of the loading blocks
Centre bore contact, the trip bolt can by the centre bore to loading blocks apply axial load；
The groove of the ribs of the seat board is in inverted trapezoidal groove；It is additionally provided with the seat board and communicates and can accommodate spacing with groove
The limit channels of screw, the limit channels coordinate with the stop screw screw thread；The stop screw is sequentially provided with spacing head
Portion, thread segment and spacing end；The thread segment uses fine thread；The end face of the spacing end is plane.
2. a kind of vapour deposition shallow layer solidification frock according to claim 1, it is characterised in that the side plate outer surface
In alternate concaveconvex structure, the female parts of the side plate are evenly equipped with the fixing hole that can be matched with fixing screws, the seat board
The correspondence position of bottom also is provided with the base plate hole that can be matched with fixing screws, and the side plate is by being distributed in the fixations of female parts
Screw is fixedly connected with the bottom of the seat board.
3. a kind of vapour deposition shallow layer solidification frock according to claim 2, it is characterised in that the trip bolt is equal
It is distributed in the concave portion of side plate.
4. a kind of vapour deposition shallow layer solidification frock according to claim 1, it is characterised in that the trip bolt according to
It is secondary to be provided with head, threaded portion, guide rod portion and end；Head is preferably hexagon-head；End is in horn shape.
5. a kind of vapour deposition shallow layer solidification frock according to claim 1, it is characterised in that phase is gone back on the side plate
Be symmetrically arranged with least one pair of spacing hole for seat board oblique angle, the spacing hole for spacer pin by and go deep into realization inside seat board
Further consolidated between seat board and side plate spacing.
6. a kind of vapour deposition shallow layer solidification frock according to claim 1, it is characterised in that in the loading blocks
Heart hole is preferably the hole made according to GB/T4459.5-B2/5；The end Zuo Qing angles processing of the small end of the loading blocks.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610224063.4A CN105690299B (en) | 2016-04-08 | 2016-04-08 | One kind vapour deposition shallow layer solidification frock |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610224063.4A CN105690299B (en) | 2016-04-08 | 2016-04-08 | One kind vapour deposition shallow layer solidification frock |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN105690299A CN105690299A (en) | 2016-06-22 |
| CN105690299B true CN105690299B (en) | 2017-08-25 |
Family
ID=56219813
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610224063.4A Active CN105690299B (en) | 2016-04-08 | 2016-04-08 | One kind vapour deposition shallow layer solidification frock |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN105690299B (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107900930A (en) * | 2017-10-12 | 2018-04-13 | 重庆长安工业(集团)有限责任公司 | A kind of multi-functional embedding solidification equipment |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE4100215A1 (en) * | 1991-01-07 | 1992-07-09 | Reichsbahn Ingenieurbuero Fuer | Symmetrical work automatic clamping and centring mechanism - comprises pairs of spring-loaded bell crank levers |
| CN201355343Y (en) * | 2008-12-24 | 2009-12-02 | 中国航空工业第一集团公司北京航空制造工程研究所 | Tensile specimen for testing bonding strength of coating |
| CN202479786U (en) * | 2012-02-26 | 2012-10-10 | 玉溪台正智能机械有限公司 | Micro-adjustment structure of junction surface of machine tool |
| CN103921229A (en) * | 2014-04-25 | 2014-07-16 | 成都西图科技有限公司 | Sheet clamp |
| CN204195219U (en) * | 2014-09-30 | 2015-03-11 | 中国科学院西安光学精密机械研究所 | A kind of slit assembly adjustment frock |
Family Cites Families (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US10167571B2 (en) * | 2013-03-15 | 2019-01-01 | Veeco Instruments Inc. | Wafer carrier having provisions for improving heating uniformity in chemical vapor deposition systems |
-
2016
- 2016-04-08 CN CN201610224063.4A patent/CN105690299B/en active Active
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE4100215A1 (en) * | 1991-01-07 | 1992-07-09 | Reichsbahn Ingenieurbuero Fuer | Symmetrical work automatic clamping and centring mechanism - comprises pairs of spring-loaded bell crank levers |
| CN201355343Y (en) * | 2008-12-24 | 2009-12-02 | 中国航空工业第一集团公司北京航空制造工程研究所 | Tensile specimen for testing bonding strength of coating |
| CN202479786U (en) * | 2012-02-26 | 2012-10-10 | 玉溪台正智能机械有限公司 | Micro-adjustment structure of junction surface of machine tool |
| CN103921229A (en) * | 2014-04-25 | 2014-07-16 | 成都西图科技有限公司 | Sheet clamp |
| CN204195219U (en) * | 2014-09-30 | 2015-03-11 | 中国科学院西安光学精密机械研究所 | A kind of slit assembly adjustment frock |
Also Published As
| Publication number | Publication date |
|---|---|
| CN105690299A (en) | 2016-06-22 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN213916243U (en) | Work fixture | |
| CN202571920U (en) | Dual-face drilling clamp | |
| CN103801952A (en) | Positioning fixture for hole machining | |
| US2771821A (en) | Angular work table | |
| CN105690299B (en) | One kind vapour deposition shallow layer solidification frock | |
| CN101434041A (en) | Clamping fixture for transverse alignment of multiple-boss workpiece, and transverse alignment and position method thereof | |
| CN105034115A (en) | Irregular-shaped timber pressing device | |
| US20160332235A1 (en) | Workpiece clamping device with face driver | |
| TW201008696A (en) | Modular slide rail and slide base structure | |
| CN218017212U (en) | End face internal clamping tool | |
| CN203738411U (en) | Fixture for precision boring of bores in big ends of connecting rods | |
| CN111390644B (en) | Clamp capable of rotating and adjusting eccentricity on indexing chuck | |
| CN113319334B (en) | High-precision end face characteristic reverse milling process method | |
| CN213998637U (en) | Self-centering tool for circular workpiece | |
| CN211991587U (en) | Landing leg dish welding set | |
| CN203649938U (en) | Fastening and clamping device | |
| CN204094407U (en) | A kind of deflection welding device | |
| CN205074788U (en) | Square support centre gripping frock | |
| CN204748096U (en) | Locking mechanism helicoid processingequipment | |
| CN211804924U (en) | Positioning and clamping mechanism | |
| CN210121687U (en) | Turning tool height-adjusting device based on slope principle | |
| CN207119995U (en) | Rotary table and lathe | |
| CN214392502U (en) | Clamping and positioning device for milling plane or square groove of pin hole of caterpillar track link | |
| CN208304443U (en) | A kind of bull-dozer semiaxis outer circle groove milling mould | |
| CN206169353U (en) | Flexible clamp suitable for servo mechanism gyration type part production |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| EE01 | Entry into force of recordation of patent licensing contract | ||
| EE01 | Entry into force of recordation of patent licensing contract |
Application publication date: 20160622 Assignee: Dongguan Yibao Metal Technology Co.,Ltd. Assignor: AEROSPACE PRECISION PRODUCTS Corp. Contract record no.: X2022120000001 Denomination of invention: A curing tooling for vapor deposition thin coating Granted publication date: 20170825 License type: Common License Record date: 20220223 |