CN105234640B - A kind of processing method of locking plate - Google Patents
A kind of processing method of locking plate Download PDFInfo
- Publication number
- CN105234640B CN105234640B CN201510779560.6A CN201510779560A CN105234640B CN 105234640 B CN105234640 B CN 105234640B CN 201510779560 A CN201510779560 A CN 201510779560A CN 105234640 B CN105234640 B CN 105234640B
- Authority
- CN
- China
- Prior art keywords
- locking plate
- size
- fan
- processing method
- blank material
- 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
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
- B23P15/00—Making specific metal objects by operations not covered by a single other subclass or a group in this subclass
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Laser Beam Processing (AREA)
Abstract
The invention discloses a kind of processing method of locking plate, comprise the following steps：Step 1: steel plate is processed into fan-shaped blank material；Step 2: the center section of fan-shaped blank material is suppressed into groove by size requirement；Step 3: compressing fan-shaped blank material redundance is carried out into laser ablation, inside and outside circular arc respectively stays certain surplus；Step 4: the workpiece after excision is heat-treated；Step 5: the reserved surplus of the Workpiece internal-external circle arc after heat treatment is cut off, the size of product requirement is reached；Step 6: short transverse is repaiied into file to the size of product requirement；Complete the processing of locking plate.The present invention can improve locking plate passing rate of processing and dimensional stability, there is larger improvement compared with traditional sheet metal component processing method, and processing method has in place of certain use for reference, and meets the processing demand of locking plate.
Description
Technical field
The present invention relates to mach technical field, and in particular to a kind of processing method of locking plate.
Background technology
Locking plate is the vital part of turbogenerator, and most of rotor is all to be connected to one by blade and center rotating part
Rise, its vital part connected is exactly locking plate, locking plate there are many kinds, such as Fig. 1 is exactly one of which locking efficiency very high locking plate,
N number of blade can be locked simultaneously, be the newest development trend for engine locking plate, but this locking plate requirement on machining accuracy is very
Height, difficulty of processing is big.
The locking plate uses Conventional processing methods institute produced problem：
1st, locking plate material selection high temperature alloy metal plate material, due to the performance of high-temperature alloy material in itself, shaping difficulty than larger,
Resilience is big after shaping, is difficult to ensure design requirement.
2nd, locking plate is cambered surface molding part, is difficult to ensure that height dimension is consistent in short transverse.
3rd, the required precision of locking plate appearance and size is high, is much skillful in conventional sheet metal component appearance and size precision, size is difficult to ensure that,
Conventional method passing rate of processing bottom.
The content of the invention
In view of this, the invention provides a kind of processing method of locking plate, it is possible to increase locking plate passing rate of processing and size
Stability, there is larger improvement compared with traditional sheet metal component processing method, and processing method has in place of certain use for reference, and meets locking plate
Processing demand.
Realize that technical scheme is as follows：
A kind of processing method of locking plate, comprises the following steps：
Step 1: steel plate is processed into fan-shaped blank material；
Step 2: the center section of fan-shaped blank material is suppressed into groove by size requirement；
Step 3: compressing fan-shaped blank material redundance is carried out into laser ablation, inside and outside circular arc respectively stays certain remaining
Amount；
Step 4: the workpiece after excision is heat-treated；
Step 5: the reserved surplus of the Workpiece internal-external circle arc after heat treatment is cut off, the size of product requirement is reached；
Step 6: short transverse is repaiied into file to the size of product requirement, the processing of locking plate is completed.
Beneficial effect：
Processing method of the present invention, reserves certain allowance so that can after heat treatment before heat treatment
Qualified locking plate is processed further out according to the size requirement of locking plate, the present invention improves locking plate passing rate of processing and dimensionally stable
Property, there is larger improvement compared with traditional sheet metal component processing method.
Brief description of the drawings
Fig. 1 is the structural representation of locking plate of the present invention.
Fig. 2 is Fig. 1 A-A diagrammatic cross-sections.
Fig. 3 is the schematic diagram of the fan-shaped hair dispensing of the present invention.
Fig. 4 is the compressing fan-shaped blank material schematic diagram of the present invention.
Fig. 5 is the Workpiece structure schematic diagram after first time laser ablation of the invention.
Fig. 6 is the Workpiece structure schematic diagram after second of laser ablation of the invention.
Fig. 7 repaiies the Workpiece structure schematic diagram after file for the present invention.
Embodiment
The present invention will now be described in detail with reference to the accompanying drawings and examples.
The invention provides a kind of processing method of locking plate, comprise the following steps：
Step 1: it is the fan-shaped blank material that δ central angles are 90 ° that steel plate, which is processed into thickness,；As shown in Figure 3.
Step 2: the center section of fan-shaped blank material is suppressed into groove by size requirement；As shown in Figure 1, Figure 2 and Figure 4,
When compacting tool set is designed, profile angle carries out the processing and fabricating of compacting tool set according to the upper limit of tolerance：This is in order to full
Sufficient workpiece has the surplus for repairing file in the later stage；
Step 3: compressing fan-shaped blank material redundance is carried out into laser ablation, inside and outside circular arc respectively stays certain remaining
Amount；As shown in figure 5, be the workpiece of first time laser ablation, H is the semidiameter of the inside and outside circular arc after first time laser ablation.Should
The excision of step is that it is for energy after being heat-treated to leave certain surplus in order that obtaining workpiece can be put into the frock of heat treatment
The radius of the inside and outside circular arc of workpiece is further finished, surplus is left for finishing, in heat treatment, frock energy used
Ensure that the thermal deformation of workpiece is as small as possible, but workpiece still can have trickle change in size in frock, so needing reserved
Allowance, it is ensured that after heat treatment, moreover it is possible to further finished to workpiece, reaches product size requirement；
Step 4: the workpiece after cutting is heat-treated；The purpose of heat treatment：Distortional stress is eliminated, product is improved
Energy；
Step 5: the reserved surplus of the Workpiece internal-external circle arc after heat treatment is carried out into laser ablation, product requirement is reached
Size；As shown in fig. 6, being the workpiece after second of laser ablation.G ± 0.05 is the chi of the semidiameter of final inside and outside circular arc
It is very little.
Step 6: short transverse is repaiied into file to the size of product requirement；As shown in fig. 7, to repair the workpiece after file.F±
0.05 and E ± 0.05 be the final short transverse of workpiece size.
Thus complete the processing of locking plate.
Then, the detection of workpiece is carried out：1st, whether the locking plate surface that fluoroscopic examination is processed has crackle；2nd, locking plate is detected
Whether appearance and size is qualified；
In summary, presently preferred embodiments of the present invention is these are only, is not intended to limit the scope of the present invention.
Within the spirit and principles of the invention, any modification, equivalent substitution and improvements made etc., should be included in the present invention's
Within protection domain.
Claims (1)
1. a kind of processing method of locking plate, it is characterised in that comprise the following steps：
Step 1: steel plate is processed into fan-shaped blank material；
Step 2: the center section of fan-shaped blank material is suppressed into groove by size requirement；
Step 3: compressing fan-shaped blank material redundance is carried out into laser ablation, inside and outside circular arc respectively stays certain surplus；
Step 4: the workpiece after excision is heat-treated；
Step 5: the reserved surplus of the Workpiece internal-external circle arc after heat treatment is cut off, the size of product requirement is reached；
Step 6: short transverse is repaiied into file to the size of product requirement；
Complete the processing of locking plate.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510779560.6A CN105234640B (en) | 2015-11-13 | 2015-11-13 | A kind of processing method of locking plate |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510779560.6A CN105234640B (en) | 2015-11-13 | 2015-11-13 | A kind of processing method of locking plate |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN105234640A CN105234640A (en) | 2016-01-13 |
| CN105234640B true CN105234640B (en) | 2017-10-13 |
Family
ID=55032590
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510779560.6A Active CN105234640B (en) | 2015-11-13 | 2015-11-13 | A kind of processing method of locking plate |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN105234640B (en) |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107738068A (en) * | 2017-09-25 | 2018-02-27 | 中国航发沈阳发动机研究所 | Special-shaped locking plate small lot processing method |
| CN112727967A (en) * | 2020-12-30 | 2021-04-30 | 潍坊埃锐制动系统有限公司 | Method for processing automobile brake pad |
Family Cites Families (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101943205B (en) * | 2010-08-30 | 2012-05-09 | 贵州航天新力铸锻有限责任公司 | Manufacturing method for ultrathin tegular locking plate of nuclear reactor pressure vessel main bolt |
| CN102441762A (en) * | 2010-10-04 | 2012-05-09 | 温永林 | Orange peeler locking plate manufacturing process |
| US8974188B2 (en) * | 2012-03-06 | 2015-03-10 | Hamilton Sundstrand Corporation | Blade clip |
| CN104148499B (en) * | 2014-07-25 | 2016-06-08 | 上海海业机电设备有限公司 | A kind of processing technology of gas turbine locking plate |
-
2015
- 2015-11-13 CN CN201510779560.6A patent/CN105234640B/en active Active
Also Published As
| Publication number | Publication date |
|---|---|
| CN105234640A (en) | 2016-01-13 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| Shi et al. | Electric hot incremental forming of low carbon steel sheet: accuracy improvement | |
| CN101774045A (en) | Turbine disk fir-shaped mortise broaching tool | |
| CN105252233B (en) | A kind of aero-engine high temperature alloy counterweight blade machining process | |
| CN103252687B (en) | A kind of race finishing broach profile of tooth numerical control grinding technique | |
| CN101418811B (en) | Hollow fan blade for aircraft engine | |
| CN101774048A (en) | Bevel gear machining method | |
| CN102947596A (en) | Method for producing a metal reinforcement for a turbomachine blade | |
| CN105234640B (en) | A kind of processing method of locking plate | |
| CN106270515B (en) | 3D printing, heat treatment and finishing integral processing method | |
| CN107120273A (en) | The molded line and processing technology of a kind of Roots's mechanical supercharger Twisted impeller | |
| CN103042090B (en) | Turbine runner blade compression-moulding methods | |
| CN103056627B (en) | Forming method of high-precision closed blisk | |
| Lin et al. | Additive manufacturing with secondary processing of curve-face gears | |
| RU2403119C2 (en) | Method to produce gas turbine engine vanes | |
| CN103631197B (en) | Skew ruled surface blade-side cutter spindle vector program method | |
| Shih | Mathematical model for face-hobbed straight bevel gears | |
| CN110497261A (en) | A method of solid end mill appearance is obtained based on pixel method and cuts slot end face section shape | |
| CN104439468A (en) | Milling cutter suitable for layered milling forming process of integral leaf disk structural profile | |
| CN103530452A (en) | Calculation method of flattened hollow blade near-net forming blank | |
| CN105479120A (en) | Machining technology of hitting surface of golf club head | |
| CN107350569A (en) | Pre-grinding hob and its processing method | |
| CN105312483B (en) | Method for forging beryllium bronze blade of engine | |
| CN103722116A (en) | Device and method for forming gear through rotary swaging in radial direction | |
| CN106424966A (en) | Grinding technology and device for wheel groove finishing broach with equal cutting angles | |
| CN103286536B (en) | Adopt the method for cold heading technique processing cross recess formpiston |
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 |