CN106525625B - Hardness frock is beaten to compressor blade forging - Google Patents
Hardness frock is beaten to compressor blade forging Download PDFInfo
- Publication number
- CN106525625B CN106525625B CN201611228838.1A CN201611228838A CN106525625B CN 106525625 B CN106525625 B CN 106525625B CN 201611228838 A CN201611228838 A CN 201611228838A CN 106525625 B CN106525625 B CN 106525625B
- Authority
- CN
- China
- Prior art keywords
- blade
- base
- forging
- fixed
- bottom plate
- 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
- 238000005242 forging Methods 0.000 title claims abstract description 27
- 230000004308 accommodation Effects 0.000 claims 3
- 238000004519 manufacturing process Methods 0.000 abstract description 6
- 238000000034 method Methods 0.000 description 3
- 238000003860 storage Methods 0.000 description 3
- 238000010438 heat treatment Methods 0.000 description 1
- 238000003825 pressing Methods 0.000 description 1
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
- G01N3/00—Investigating strength properties of solid materials by application of mechanical stress
- G01N3/40—Investigating hardness or rebound hardness
- G01N3/42—Investigating hardness or rebound hardness by performing impressions under a steady load by indentors, e.g. sphere, pyramid
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
- G01N3/00—Investigating strength properties of solid materials by application of mechanical stress
- G01N3/40—Investigating hardness or rebound hardness
Abstract
The invention discloses a hardening tool for a compressor blade forging, which comprises a bottom plate and a base movably fixed on the bottom plate, wherein the base is provided with a containing groove for containing a blade root of a blade, one side of the containing groove is provided with a blade root cushion block, the other side of the containing groove is provided with a positioning part, one side of the blade root is arranged close to the blade root cushion block, the other side of the blade root is fixed in the containing groove through the positioning part, and a blade top supporting component for supporting a blade top of the blade is movably fixed on one side of the base on the bottom plate. The hardness forging tool for the compressor blade forging can well fix the compressor blade forging, and achieves faster and safer production; and the universality is good, and the blade root cushion blocks with different specifications can be replaced and the spacing between the blade top supporting assembly and the base can be adjusted, so that the production cost is reduced to a certain extent.
Description
Technical Field
The invention belongs to the processing technology of compressor blades, and particularly relates to a hardness forging tool for a compressor blade forging.
Background
The hardening process is generally an indispensable process after heat treatment of the compressor blade forging. In practical production, the hardness is usually achieved by using some cushion blocks randomly by operators themselves to temporarily use the cushion blocks as auxiliary tools, and even by hand. During operation, because the cushion blocks are randomly selected, the fastening acting force is lacked between the cushion blocks and the forgings, and the cushion blocks for different forgings have certain differences in size and quantity due to different sizes, different workers also have certain differences in operation, and during actual hardness, dangerous situations caused by instability can occur, and the efficiency is greatly reduced.
Disclosure of Invention
The invention aims to provide a hardness forging tool for a compressor blade forging, which has the characteristics of good universality, high production efficiency and safe and reliable operation, and aims to solve the problems in the prior art when the compressor blade forging is hardened.
To achieve the purpose, the invention adopts the following technical scheme:
the utility model provides a hardness frock is beaten to compressor blade forging, its includes the bottom plate and movably be fixed in base on the bottom plate, wherein, have the storage tank that is used for placing the blade root on the base, one side of storage tank is provided with the blade root cushion, and the opposite side is provided with the locating part, one side of blade root is leaned on the blade root cushion setting, and the opposite side is fixed in through the locating part in the storage tank, on the bottom plate in one side of base movably be fixed with the top of blade supporting component that is used for supporting the top of blade.
Particularly, a plurality of T-shaped grooves are formed in the bottom plate in parallel, the two ends of the base are provided with fixing grooves with openings, and the base is fixed in the T-shaped grooves through T-shaped bolts.
In particular, the positioning component is a plurality of fastening screws arranged on the side wall of the accommodating groove.
In particular, the blade tip support assembly includes a fixed plate movably secured to the base plate and a "V" shaped seat within which the blade tip is disposed.
Particularly, both ends of the fixing plate are provided with open fixing grooves, and the fixing plate is fixed in the T-shaped grooves through T-shaped bolts.
Compared with the prior art, the hardness forging tool for the compressor blade forging has the following advantages:
1) The method can better fix the compressor blade forging, provide the required stable state of the forging when the forging is hardened, and realize faster and safer production;
2) The universality is good, the blade root cushion blocks with different specifications can be replaced, the spacing between the blade top supporting assembly and the base can be adjusted, and the production cost is reduced to a certain extent.
Drawings
Fig. 1 is a schematic perspective view of a hardening tool for a compressor blade forging according to embodiment 1 of the present invention;
FIG. 2 is a front view of a compressor blade forging hardness tool provided in embodiment 1 of the present invention;
FIG. 3 is a side view of a compressor blade forging hardness tool provided in embodiment 1 of the present invention;
fig. 4 is a top view of a hardening tool for a compressor blade forging provided in embodiment 1 of the present invention.
Detailed Description
The technical scheme of the invention is further described below by the specific embodiments with reference to the accompanying drawings.
Referring to fig. 1 to 4, in this embodiment, a hardness tool for forging a compressor blade includes a base plate 1 and a base plate 2, a plurality of T-shaped grooves 3 are parallel arranged on the base plate 1, two ends of the base plate 2 are provided with open fixing grooves 4, the base plate 2 is fixed in the T-shaped grooves 3 through T-shaped bolts, and the fixing position of the base plate 2 on the base plate 1 can be adjusted through the T-shaped grooves 3.
The base 1 is provided with a containing groove 6 for containing the blade root 5, one side of the containing groove 6 is provided with a blade root cushion block 7, the other side is provided with a plurality of fastening screws 8, one side of the blade root 5 is arranged by being attached to the blade root cushion block 7, and the other side is fastened in the containing groove 6 through the top of the fastening screws 8.
The blade top support assembly for supporting the blade top 9 is movably fixed on one side of the base 2 on the base plate 1, the blade top support assembly comprises a fixing plate 10 and a V-shaped seat 11, both ends of the fixing plate 10 are provided with fixing grooves with openings, the fixing plate 10 is fixed in the T-shaped groove 3 through T-shaped bolts, the fixing position of the fixing plate 10 on the base plate 1 can be adjusted through the T-shaped groove 3, and the blade top 9 is arranged in the V-shaped seat 11 and is supported and limited by the V-shaped seat 11.
When the novel blade root fixing device is used, the blade root cushion block 7 of a corresponding product is arranged on the base 2, meanwhile, the distance between the fixing plate 10 and the base 2 is adjusted according to different sizes of the product, the blade top 9 of the blade is placed in the V-shaped seat 11, the fastening screw 8 is rotated to fix the blade root 5 on the base 2, and finally, the hardness is achieved by pressing down the hardness tester pressure head 12.
The above embodiments merely illustrate the basic principles and features of the present invention, and the present invention is not limited to the above examples, but can be variously changed and modified without departing from the spirit and scope of the present invention, which is within the scope of the present invention as claimed. The scope of the invention is defined by the appended claims and equivalents thereof.
Claims (2)
1. The utility model provides a hardness frock is beaten to compressor blade forging, its includes the bottom plate and is fixed in the base on the bottom plate movably, its characterized in that has the accommodation groove that is used for placing the blade root on the base, one side of accommodation groove is provided with the blade root cushion, and the opposite side is provided with the locating part, one side of blade root is leaned on the blade root cushion setting, and the opposite side is fixed in the accommodation groove through the locating part, be fixed with the top of blade supporting component that is used for supporting the top of blade on one side of base on the bottom plate movably;
a plurality of T-shaped grooves are formed in the bottom plate in parallel, two ends of the base are provided with open fixing grooves, and the base is fixed in the T-shaped grooves through T-shaped bolts;
the blade top supporting component comprises a fixing plate and a V-shaped seat, the fixing plate is movably fixed on the bottom plate, and the blade top is arranged in the V-shaped seat;
the positioning component is a plurality of fastening screws arranged on the side wall of the accommodating groove.
2. The compressor blade forging hardness tool as recited in claim 1, wherein both ends of the fixing plate are provided with open fixing grooves, and the fixing plate is fixed in the T-shaped grooves through T-shaped bolts.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611228838.1A CN106525625B (en) | 2016-12-27 | 2016-12-27 | Hardness frock is beaten to compressor blade forging |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611228838.1A CN106525625B (en) | 2016-12-27 | 2016-12-27 | Hardness frock is beaten to compressor blade forging |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN106525625A CN106525625A (en) | 2017-03-22 |
| CN106525625B true CN106525625B (en) | 2023-10-24 |
Family
ID=58337776
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201611228838.1A Active CN106525625B (en) | 2016-12-27 | 2016-12-27 | Hardness frock is beaten to compressor blade forging |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106525625B (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107270827A (en) * | 2017-06-12 | 2017-10-20 | 上海理工大学 | The qualified detection device of rotating blade assembly based on ZigBee communication |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103659378A (en) * | 2013-12-13 | 2014-03-26 | 无锡透平叶片有限公司 | Universal clamp device for vane overall length machining |
| CN104191274A (en) * | 2014-08-07 | 2014-12-10 | 南京赛达机械制造有限公司 | Tool for double-center-hole machining device for steam turbine blade |
| CN105414853A (en) * | 2015-12-31 | 2016-03-23 | 无锡透平叶片有限公司 | Blade root positioning structure for laser cladding of steam turbine blades |
| CN206362653U (en) * | 2016-12-27 | 2017-07-28 | 无锡透平叶片有限公司 | A kind of compressor blade forging beats hardness frock |
-
2016
- 2016-12-27 CN CN201611228838.1A patent/CN106525625B/en active Active
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103659378A (en) * | 2013-12-13 | 2014-03-26 | 无锡透平叶片有限公司 | Universal clamp device for vane overall length machining |
| CN104191274A (en) * | 2014-08-07 | 2014-12-10 | 南京赛达机械制造有限公司 | Tool for double-center-hole machining device for steam turbine blade |
| CN105414853A (en) * | 2015-12-31 | 2016-03-23 | 无锡透平叶片有限公司 | Blade root positioning structure for laser cladding of steam turbine blades |
| CN206362653U (en) * | 2016-12-27 | 2017-07-28 | 无锡透平叶片有限公司 | A kind of compressor blade forging beats hardness frock |
Also Published As
| Publication number | Publication date |
|---|---|
| CN106525625A (en) | 2017-03-22 |
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