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CN108526565A - The molding device of gas compressor moving blade blade root - Google Patents

The molding device of gas compressor moving blade blade root Download PDF

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Publication number
CN108526565A
CN108526565A CN201810692255.7A CN201810692255A CN108526565A CN 108526565 A CN108526565 A CN 108526565A CN 201810692255 A CN201810692255 A CN 201810692255A CN 108526565 A CN108526565 A CN 108526565A
Authority
CN
China
Prior art keywords
blade
cutter
chip pocket
cutter hub
blade root
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Withdrawn
Application number
CN201810692255.7A
Other languages
Chinese (zh)
Inventor
周乐安
钟成明
钟宇婷
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Deyang Jie Chuang Technology Co Ltd
Original Assignee
Deyang Jie Chuang Technology Co Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Deyang Jie Chuang Technology Co Ltd filed Critical Deyang Jie Chuang Technology Co Ltd
Priority to CN201810692255.7A priority Critical patent/CN108526565A/en
Publication of CN108526565A publication Critical patent/CN108526565A/en
Withdrawn legal-status Critical Current

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23CMILLING
    • B23C5/00Milling-cutters
    • B23C5/02Milling-cutters characterised by the shape of the cutter
    • B23C5/12Cutters specially designed for producing particular profiles

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

The invention discloses the molding devices of gas compressor moving blade blade root, are related to Steam Turbines blade root molding cutter, including cutter hub, and the cutting edge molded line of the cutter hub is consistent with the blade-root molded line of turbine blade;The cutter hub also has multiple cutting tooths, and in circumferential decile or decile is not distributed, and is chip pocket between adjacent cutting tooth, and the chip pocket is helicla flute, and the chip pocket is the helicla flute made according to Fibonacci helix.The cutter hub is made of Powder High-speed Steels.The present invention overcomes existing movable vane blade root molding cutter helixes to lead to the blocking of chip pocket only with medium-sized cylindrical spiral, using Fibonacci helix as helix is exited, transition can be made more smooth, prevents steel cuttings from blocking chip pocket;The increase of cutter grinding number will not change cutter molded line;Have the characteristics that efficiently be molded, it is highly practical.

Description

The molding device of gas compressor moving blade blade root
Technical field
The present invention relates to Steam Turbines blade root molding cutters, and in particular to the molding device of gas compressor moving blade blade root.
Background technology
Steam turbine is the rotary power machinery that the energy of steam is converted to mechanical work, is the main of Steam Power Equipment One of equipment.It is mainly used as prime mover of power generation, can also directly drive various pumps, wind turbine, compressor and propeller for vessels etc.. The steam discharge or intermediate extraction that steam turbine can also be utilized meet production and heat supply needs in life.Steam turbine is that a kind of high temperature is high High-speed rotating machinery is pressed, for power generation turbine, and is high-power output ground motility mechanical, so design It is required that steam turbine has high efficiency, high safety reliability, and adjustability will be got well.Wherein, the operating condition of the blade of steam turbine Complexity is also steamed because it is in overheat respectively in addition to bearing higher static stress and dynamic stress because of high speed rotation and airflow function It works in vapour area, two-phase transition region and moist steam section and bears high temperature, high pressure, corrosion and erosion effect.Therefore the material of blade Material will meet claimed below:Good room temperature and high-temperature mechanical property, good corrosion stability, good damping property and certain The good cold and hot working performance of wearability.The common used material of blade has:
1, straight-chromiun stainless steel 1Cr13 and 2Cr13 belong to martensite heat-resistant steel, they under room temperature and operating temperature in addition to having Outside enough intensity, also there is high corrosion resistance and damping, be most popular turbine materials in the world.
2, enhanced type straight-chromiun stainless steel compensates for the relatively low disadvantage of 1Cr13 type straight-chromiun stainless steel heat resistances, wherein be added molybdenum, Tungsten, vanadium, niobium, boron etc..
3, low-alloy pearlite heat resisting steel, for manufacturing operating temperature in 450 DEG C or less middle-pressure steam turbine movable vane pieces at different levels And stator blade.
4, aluminium alloy and its density of titanium alloy is small, corrosion resistance is high, for manufacturing the long movable vane piece of large steam turbine final stage.
The form of turbine blade root mainly has T-type, bacterial type, forked type and fir-tree type in turbomachinery.And fir-tree type leaf Root has intensity high, the feature that precision is high and connection is reliable.But when the molding tool sharpening fir-tree root of traditional movable vane blade root, Difficulty of processing difficulty for the blade root of other forms such as fork-shaped is much greater, and difficulty is mainly reflected in blade-root molded line essence Degree is high, and cutter making is difficult.To solve, the vibration generated when the cutting of high feed speed is big, finished surface is still with the presence of chatter mark, table Surface roughness is unable to reach the surface quality requirements that blade root surface roughness is Ra0.8, patent document CN101972870A steamers Machine blade root milling cutter is proposed is made helicla flute using the chip pocket of welding milling cutter, and the chip face of welding blade is also a spiral shell Curved surface is revolved, is continuous cutting when cutting, Vibration Condition can be reduced, improve blade root surface quality.
However, during actual use, it often will appear the helicla flute card bits problem of helix, need in blade root is handled Way stops cleaning, to avoid the damage of molding cutter, reduces the efficiency used, basic reason is movable vane blade root forming cutter The extensive setting of the unreasonable type selecting and steel cuttings escape mechanism of the helix of tool, limits the export of steel cuttings jointly.
Invention content
The technical problem to be solved by the present invention is to the unreasonable type selecting of the helix of movable vane blade root molding cutter and steel The extensive setting for considering escape mechanism to be worth doing, limits the export of steel cuttings, and it is an object of the present invention to provide the molding dress of gas compressor moving blade blade root jointly It sets, solves the above problems.
The present invention is achieved through the following technical solutions:
The molding device of gas compressor moving blade blade root, including cutter hub, the cutting edge molded line of the cutter hub and the leaf of turbine blade Root molded line is consistent;The cutter hub also has multiple cutting tooths, and in circumferential decile or decile is not distributed, and is to hold between adjacent cutting tooth Consider slot to be worth doing, the chip pocket is helicla flute, and the chip pocket is the helicla flute made according to Fibonacci helix.Fibonacci spiral shell Spin line, also referred to as golden spiral, are the helical curves drawn according to Fibonacci sequence, and there are many Fibonaccis in nature The pattern of helix is the most perfect classical golden ratio of nature.It is moulded although more difficult compared to cylindrical spiral, On the basis of the numerically-controlled machine tool being becoming better and approaching perfection day by day at present, movable vane blade root molding cutter is made to have been able to manufacture.Overcome existing movable vane Blade root molding cutter helix leads to the blocking of chip pocket only with medium-sized cylindrical spiral, using Fibonacci spiral Line can make transition more smooth as helix is exited, and prevent steel cuttings from blocking chip pocket.
Further, the cutter hub is made of Powder High-speed Steels.Powder High-speed Steels have ASP23, the products such as ELMAX, can To obtain extreme hardness HRC 63~70, and can still keep 60 or more high rigidity HRC and high-wearing feature at 550~600 DEG C Heat-resistance and wear-resistance steel class, main application is to manufacture the cutting element of various lathes, and also part is used for top load mold, and aviation is high Warm bearing and special heat-resistant antifriction parts etc..
Further, the cutter hub and the welded chemical conversion type of blade, welding manner are brazing or silver soldering.When due to welding The high temperature solder materials of use, it is therefore desirable to which, using hard fine weldering, brazing or silver soldering are alternative plan.
Further, the cutting tooth surface has titanium nitride coating.Titanium nitride has fusing point height, hardness big, chemical steady Qualitative good, small with the wetting of metal structural material simultaneously has higher electric conductivity and superconductivity, can be applied to thermal structure material Material and superconductor, and Powder High-speed Steels combination, enable to the increase of cutter grinding number not change cutter molded line.
Compared with prior art, the present invention having the following advantages and advantages:
1, the molding device of gas compressor moving blade blade root of the present invention overcomes existing movable vane blade root molding cutter helix only The blocking for being led to chip pocket using medium-sized cylindrical spiral is used as using Fibonacci helix and exits helix, energy Enough make transition more smooth, prevents steel cuttings from blocking chip pocket;
2, the molding device of gas compressor moving blade blade root of the present invention, the increase of cutter grinding number will not change cutter molded line;
3, the molding device of gas compressor moving blade blade root of the present invention, have the characteristics that efficiently be molded, it is highly practical.
Description of the drawings
Attached drawing described herein is used for providing further understanding the embodiment of the present invention, constitutes one of the application Point, do not constitute the restriction to the embodiment of the present invention.In the accompanying drawings:
Fig. 1 is the structural schematic diagram of an embodiment of the present invention;
Fig. 2 is Fibonacci helix schematic diagram.
Label and corresponding component names in attached drawing:
1- cutter hubs, 2- cutting tooths, 3- chip pockets.
Specific implementation mode
To make the objectives, technical solutions, and advantages of the present invention clearer, with reference to embodiment and attached drawing, to this Invention is described in further detail, and exemplary embodiment of the invention and its explanation are only used for explaining the present invention, do not make For limitation of the invention.
Embodiment 1
As shown in Figs. 1-2, the molding device of gas compressor moving blade blade root of the present invention, including cutter hub 1, the cutting edge of the cutter hub 1 Molded line is consistent with the blade-root molded line of turbine blade;The cutter hub 1 also has multiple cutting tooths 2, in circumferential decile or not decile It is distributed, is chip pocket 3 between adjacent cutting tooth 2, the chip pocket 3 is helicla flute, and the chip pocket 3 is according to Fibonacci spiral shell The helicla flute that spin line makes.Fibonacci helix, also referred to as golden spiral are the helical curves drawn according to Fibonacci sequence Line, there are the patterns of many Fibonacci helixes in nature, are the most perfect classical golden ratios of nature.Although comparing It moulds in cylindrical spiral is more difficult, but on the basis of the numerically-controlled machine tool being becoming better and approaching perfection day by day at present, has made movable vane blade root molding cutter Through that can manufacture.Overcome existing movable vane blade root molding cutter helix causes to hold only with medium-sized cylindrical spiral The blocking for considering slot 3 to be worth doing can make transition more smooth, prevent steel cuttings from blocking using Fibonacci helix as helix is exited Chip pocket 3.
Embodiment 2
The present embodiment is made that restriction further below on the basis of embodiment 1:The cutter hub 1 uses Powder High-speed Steels It is made.Powder High-speed Steels have ASP23, the products such as ELMAX, extreme hardness HRC 63~70 can be obtained, and 550~ 600 DEG C of heat-resistance and wear-resistance steel classes that can still keep 60 or more high rigidity HRC and high-wearing feature, main application are to manufacture various machines The cutting element of bed, also part is for top load mold, aerial high-temperature bearing and special heat-resistant antifriction parts etc..The cutter hub 1 with the welded chemical conversion type of blade, welding manner be brazing or silver soldering.The high temperature solder materials that use when due to welding, It needs using hard fine weldering, brazing or silver soldering are alternative plan.2 surface of the cutting tooth has titanium nitride coating.Nitrogen Change the structural material that titanium is high with fusing point, hardness is big, chemical stability is good, small with the wetting of metal and with higher conduction Property and superconductivity, can be applied to high-temperature structural material and superconductor, and the combination of Powder High-speed Steels, enable to cutter grinding The increase of number will not change cutter molded line.
Above-described specific implementation mode has carried out further the purpose of the present invention, technical solution and advantageous effect It is described in detail, it should be understood that the foregoing is merely the specific implementation mode of the present invention, is not intended to limit the present invention Protection domain, all within the spirits and principles of the present invention, any modification, equivalent substitution, improvement and etc. done should all include Within protection scope of the present invention.

Claims (4)

1. the molding device of gas compressor moving blade blade root, including cutter hub (1), the cutting edge molded line and turbine blade of the cutter hub (1) Blade-root molded line it is consistent;The cutter hub (1) also has multiple cutting tooths (2), and in circumferential decile or decile is not distributed, adjacent cutting It is chip pocket (3) between tooth (2), the chip pocket (3) is helicla flute, which is characterized in that the chip pocket (3) is according to striking wave The helicla flute that contract helix makes.
2. the molding device of gas compressor moving blade blade root according to claim 1, which is characterized in that the cutter hub (1) uses Powder High-speed Steels are made.
3. the molding device of gas compressor moving blade blade root according to claim 1, which is characterized in that the cutter hub (1) and knife The welded chemical conversion type of piece, welding manner are brazing or silver soldering.
4. the molding device of gas compressor moving blade blade root according to claim 1, which is characterized in that cutting tooth (2) table Face has titanium nitride coating.
CN201810692255.7A 2018-06-29 2018-06-29 The molding device of gas compressor moving blade blade root Withdrawn CN108526565A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201810692255.7A CN108526565A (en) 2018-06-29 2018-06-29 The molding device of gas compressor moving blade blade root

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201810692255.7A CN108526565A (en) 2018-06-29 2018-06-29 The molding device of gas compressor moving blade blade root

Publications (1)

Publication Number Publication Date
CN108526565A true CN108526565A (en) 2018-09-14

Family

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Family Applications (1)

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CN201810692255.7A Withdrawn CN108526565A (en) 2018-06-29 2018-06-29 The molding device of gas compressor moving blade blade root

Country Status (1)

Country Link
CN (1) CN108526565A (en)

Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1151261A (en) * 1965-07-07 1969-05-07 Tos Kurim Improvements in or relating to Face-Milling Cutter Heads
CN201300239Y (en) * 2008-06-03 2009-09-02 哈尔滨第一工具制造有限公司 Wheel groove semi-finished milling cutter with wavy cutting edge
CN101972870A (en) * 2010-10-25 2011-02-16 东方电气集团东方汽轮机有限公司 Turbine blade root milling cutter
CN102266975A (en) * 2010-06-02 2011-12-07 日立工具股份有限公司 Firtree-shaped tool and processing method for impeller blade root using the tool
CN205519838U (en) * 2016-03-30 2016-08-31 江阴塞特精密工具有限公司 Steam turbine blade root slot mill
CN106424881A (en) * 2016-10-21 2017-02-22 株洲钻石切削刀具股份有限公司 Milling cutter
CN107350568A (en) * 2017-08-25 2017-11-17 李弘文 Variable helical angle standard module finger-like slotting cutter
US20180079016A1 (en) * 2015-03-31 2018-03-22 Mitsubishi Materials Corporation Formed end mill
CN208483293U (en) * 2018-06-29 2019-02-12 德阳杰创科技有限公司 A kind of movable vane blade root molding cutter

Patent Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1151261A (en) * 1965-07-07 1969-05-07 Tos Kurim Improvements in or relating to Face-Milling Cutter Heads
CN201300239Y (en) * 2008-06-03 2009-09-02 哈尔滨第一工具制造有限公司 Wheel groove semi-finished milling cutter with wavy cutting edge
CN102266975A (en) * 2010-06-02 2011-12-07 日立工具股份有限公司 Firtree-shaped tool and processing method for impeller blade root using the tool
CN101972870A (en) * 2010-10-25 2011-02-16 东方电气集团东方汽轮机有限公司 Turbine blade root milling cutter
US20180079016A1 (en) * 2015-03-31 2018-03-22 Mitsubishi Materials Corporation Formed end mill
CN205519838U (en) * 2016-03-30 2016-08-31 江阴塞特精密工具有限公司 Steam turbine blade root slot mill
CN106424881A (en) * 2016-10-21 2017-02-22 株洲钻石切削刀具股份有限公司 Milling cutter
CN107350568A (en) * 2017-08-25 2017-11-17 李弘文 Variable helical angle standard module finger-like slotting cutter
CN208483293U (en) * 2018-06-29 2019-02-12 德阳杰创科技有限公司 A kind of movable vane blade root molding cutter

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
薛澄岐等: "《工业设计基础 (第2版)》", 30 September 2012, 东南大学出版社 *

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Application publication date: 20180914