CN104227359A - Manufacturing method of centrifugal vapor compressor diffuser - Google Patents

Manufacturing method of centrifugal vapor compressor diffuser Download PDF

Info

Publication number
CN104227359A
CN104227359A CN201410470380.5A CN201410470380A CN104227359A CN 104227359 A CN104227359 A CN 104227359A CN 201410470380 A CN201410470380 A CN 201410470380A CN 104227359 A CN104227359 A CN 104227359A
Authority
CN
China
Prior art keywords
face
diffuser
endoporus
cylindrical
small
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.)
Granted
Application number
CN201410470380.5A
Other languages
Chinese (zh)
Other versions
CN104227359B (en
Inventor
段昌文
柯益
徐海燕
罗兵
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.)
Chongqing Jiangjin Shipbuilding Industry Co Ltd
Original Assignee
Chongqing Jiangjin Shipbuilding Industry 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 Chongqing Jiangjin Shipbuilding Industry Co Ltd filed Critical Chongqing Jiangjin Shipbuilding Industry Co Ltd
Priority to CN201410470380.5A priority Critical patent/CN104227359B/en
Publication of CN104227359A publication Critical patent/CN104227359A/en
Application granted granted Critical
Publication of CN104227359B publication Critical patent/CN104227359B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23PMETAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P15/00Making 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)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

The invention provides a manufacturing method of a centrifugal vapor compressor diffuser. The method comprises the following steps: performing heat treatment on a blank; roughly turning the end surface, excircle, inner bore and second step end surface of a large end of a diffuser; roughly turning the end surface, excircle, inner bore and first step end surface of a small end of the diffuser; drilling and milling a locating hole in the edge of the end surface of the large end, mounting a milling tool, locating by virtue of the locating hole, and roughly milling a blade on the small end; performing half finish turning on the end surface, excircle, inner bore and first step end surface of the small end of the diffuser; performing half finish turning on the end surface, excircle, inner bore and second step end surface of the large end of the diffuser; mounting a milling tool, locating by virtue of the locating hole, performing fine milling on the blade, and delivering the product into a coordinate measuring machine for inspection after fine milling is finished; if the product is qualified, marking center lines for drilling on the end surfaces of the large and small ends and the first step end surface; aligning the center liens; drilling and threading; finely turning the end surface and inner bore of the large end of the diffuser; performing draw filing on the bottom of a blade passage; performing penetrant inspection on the blade.

Description

The manufacture method of centrifugal vapor compressor diffuser
Technical field
The present invention relates to centrifugal vapor compressor field, particularly relate to a kind of manufacture method of centrifugal vapor compressor diffuser.
Background technology
Centrifugal vapor compressor is the energy re-using the indirect steam that it self produces, thus reduces a power-saving technology of energy demand to external world.Centrifugal vapor compressor is heat recovery system improves steam pressure by compression key equipment to the live steam produced.Its operation principle is: compression impellor rotates on the axle of compressor, and the gas entering compression impellor by with rotation, then enters in diffuser, by pressure that the speed-shifting of gas is required in diffuser.In recent years, along with economize energy is more and more paid attention to, centrifugal vapor compressor is more widely used.
Centrifugal vapor compressor is made up of rotor and stator two parts.Rotor is made up of parts such as impeller, main shaft, balancing frame, thrust discs, and stator is made up of parts such as diffuser, bend, return channel, spiral cases.The function of diffuser is mainly converted into pressure energy effectively from the impeller air-flow with larger kinetic energy out.So the quality of diffuser workmanship directly affects the height of the pressure energy of conversion.
Existing diffuser manufacture method due to blade place milling surplus a lot, after disposable milling blade, diffuser distortion is comparatively large, and the vane type line profile tolerance after machining is poor; Face deformation causes the perpendicularity between diffuser end face and locating hole poor simultaneously; In addition, existing diffuser manufacture method owing to processing whole connecting hole before half finish turning and finish turning end face, when subsequent turning end face because be interrupted cut, each amount of feeding and bite are all less, working (machining) efficiency is slow, and the vibrations of tool wear and lathe are comparatively large, affect the precision of lathe.
Summary of the invention
For in prior art, the vane type line profile tolerance of diffuser is poor, the technical problem of the perpendicularity difference between end face and locating hole; Further, for first processing reface end face after connecting hole in prior art, interrupted cut causes that efficiency is low, tool wear is large and affect the technical problem of lathe precision, the invention provides a kind of manufacture method of centrifugal vapor compressor diffuser, by rough milling blade passage, remove large surplus, then half finish-milling, last finish-milling blade passage again, reduce the deflection of diffuser after milling blade, avoid the impact on subsequent handling, improve the vane type line profile tolerance of diffuser and the perpendicularity between end face and locating hole; In addition, before half finish turning and finish turning end face, only machined end face two locating holes, improve working (machining) efficiency when half finish turning and finish turning end face, reduce the wearing and tearing to cutter.
To achieve these goals, technical scheme of the present invention is:
A manufacture method for centrifugal vapor compressor diffuser, comprises the following steps:
A. blank heat treatment;
B. the end face of the large end of rough turn diffuser, cylindrical, endoporus and second step end face;
C. the end face of rough turn diffuser small end, cylindrical, endoporus and first step end face;
D. in the end face edge of large end, bore milling locating hole, milling tool is installed, and is located by locating hole, rough mill the blade on small end;
E. the end face of half finish turning diffuser small end, cylindrical, endoporus and first step end face;
F. the end face of the large end of half finish turning diffuser, cylindrical, endoporus and second step end face;
G. milling tool is installed, and is located by locating hole, finish-milling blade, after finish-milling completes, send three-dimensional to check;
H. after the assay was approved, stroke boring center line on the end face and first step end face of large end and small end;
I. centering center line, drilling and tapping;
J. the end face of the large end of finish turning diffuser and endoporus;
K. file is repaiied bottom blade passage;
L. penetrating inspection is carried out to blade.
Further, in step b, four paws folder small end cylindrical, centering, the end face of the large end of rough turn diffuser, cylindrical, endoporus and second step end face.
Further, in step c, four paws folder holds cylindrical greatly, and by putting down end face greatly, centering is the large end endoporus of car, the end face of rough turn diffuser small end, cylindrical, endoporus and first step end face.
Further, in step e, soft three-jaw folder holds cylindrical greatly, and by putting down end face greatly, centering is the large end endoporus of car, the end face of half finish turning diffuser small end, cylindrical, endoporus and first step end face.
Further, in step f, soft three-jaw folder small end cylindrical, by flat first step end face, the large end endoporus of centering, jerk value is less than or equal to 0.015mm, the end face of the large end of half finish turning diffuser, cylindrical, endoporus and second step end face.
Further, in step I, large end end face is downward, and centering center line is pressed figure holes drilled through, small end end face is bored stepped hole on the first step end face of large end; Turn-over, centering center line, large end end face bores tapping female bore by figure.
Further, in step j, soft three-jaw folder small end cylindrical, by flat first step end face, centering is the large end endoporus of car, and jerk value is less than or equal to 0.015mm, the large end end face of finish turning diffuser.
Advantageous Effects of the present invention is:
1, blade milling be divided into rough mill, finish-milling processing, large surplus is removed when rough milling, and then finish-milling blade, solve the technical problem that in prior art, disposable milling surplus causes more greatly diffuser to be out of shape, reduce the impact of the deflection after blade milling on subsequent handling, improve the molded line profile tolerance of diffuser vane and the perpendicularity between end face and locating hole;
2, owing to only machined end face edge two locating holes before half finish turning diffuser end face, be continuous cutting when half finish turning end face, each amount of feeding and bite are comparatively large, improve working (machining) efficiency, reduce the wearing and tearing to cutter and the damage to lathe;
3, by the large end end face of finish turning diffuser, the local deformation near because of the large end end face aperture that causes of holing is eliminated.
Accompanying drawing explanation
Fig. 1 is the rough turn large end process drawing of step b;
Fig. 2 is the rough turn small end process drawing of step c;
Fig. 3 is the rough turn small end process drawing of step e;
Fig. 4 is the rough turn large end process drawing of step f;
Fig. 5 is step I small end boring local process accompanying drawing;
Fig. 6 is step I large end boring local process accompanying drawing;
Fig. 7 is the large end process drawing of step j finish turning;
Reference numeral
The large end of 1-; 2-small end; 3-blade; 4-through hole; 5-stepped hole; 6-screwed hole; 7-first step end face;
The large end end face of 8-; 9-second step end face; 10-reinforcement place endoporus; 11-reinforcement bottom surface
Detailed description of the invention
Below in conjunction with accompanying drawing, the specific embodiment of the present invention is described in further details.
As shown in figs. 1-7, the manufacture method of centrifugal vapor compressor diffuser of the present invention, comprises the following steps:
A. blank heat treatment;
B. the end face of the large end 1 of rough turn diffuser, cylindrical, endoporus and second step end face 9;
C. the end face of rough turn diffuser small end 2, cylindrical, endoporus and first step end face 7;
D. in the end face edge of large end 1, bore milling locating hole, milling tool is installed, and is located by locating hole, rough mill the blade 3 on small end 2;
E. the end face of half finish turning diffuser small end 2, cylindrical, endoporus and first step end face 7;
F. the end face of the large end 1 of half finish turning diffuser, cylindrical, endoporus and second step end face 9;
G. milling tool is installed, and is located by locating hole, finish-milling blade 3, after finish-milling completes, send three-dimensional to check;
H. after the assay was approved, the end face holding greatly 1 and small end 2 and first step end face 7 draw boring center line;
I. centering center line, drilling and tapping;
J. the large end end face of finish turning diffuser and endoporus;
K. file is repaiied bottom blade 3 runner;
L. penetrating inspection is carried out to blade 3.
As shown in Figure 1, in step b, four paws folder small end 2 cylindrical, centering large end reinforcement place endoporus 10, with reinforcement bottom surface 11 for original bench mark, the second step end face 9 of the large end 1 of rough turn diffuser, the end face of rough turn large end 1, cylindrical and endoporus.
As shown in Figure 2, in step c, the large end of four paws folder 1 cylindrical, hold end face 8 greatly by flat, centering is the large end endoporus of car, the end face of rough turn diffuser small end 2, cylindrical, endoporus and first step end face 7.
As shown in Figure 3, in step e, the large end of soft three-jaw folder 1 cylindrical, hold end face 8 greatly by flat, centering is the large end endoporus of car, the end face of half finish turning diffuser small end 2, cylindrical, endoporus and first step end face 7.
As shown in Figure 4, in step f, soft three-jaw folder small end 2 cylindrical, by flat first step end face 7, the large end endoporus of centering, jerk value is less than or equal to 0.015mm, with first step end face 7 for original bench mark, end face, cylindrical, the endoporus of the large end 1 of second step end face 9, the half finish turning diffuser of the large end 1 of half finish turning diffuser.
As shown in Figure 5 and Figure 6, in step I, large end end face is downward, and centering center line is pressed figure holes drilled through 4, the end face of small end 2 is bored stepped hole 5 on the first step end face 7 of large end; Turn-over, centering center line, large end end face 8 bores tapping female bore 6 by figure.
As shown in Figure 7, in step j, soft three-jaw folder small end 2 cylindrical, by flat first step end face 7, centering is the large end endoporus of car, and jerk value is less than or equal to 0.015mm, the large end end face 8 of finish turning diffuser.
What finally illustrate is, above embodiment is only in order to illustrate technical scheme of the present invention and unrestricted, although with reference to preferred embodiment to invention has been detailed description, those of ordinary skill in the art is to be understood that, can modify to technical scheme of the present invention or equivalent replacement, and not departing from aim and the scope of technical solution of the present invention, it all should be encompassed in the middle of right of the present invention.

Claims (7)

1. a manufacture method for centrifugal vapor compressor diffuser, is characterized in that, comprises the following steps:
A. blank heat treatment;
B. the end face of the large end of rough turn diffuser (1), cylindrical, endoporus and second step end face (9);
C. the end face of rough turn diffuser small end (2), cylindrical, endoporus and first step end face (7);
D. in the end face edge of large end (1), bore milling locating hole, milling tool is installed, and is located by locating hole, rough mill the blade (3) on small end (2);
E. the end face of half finish turning diffuser small end (2), cylindrical, endoporus and first step end face (7);
F. the end face of the large end of half finish turning diffuser (1), cylindrical, endoporus and second step end face (9);
G. milling tool is installed, and is located by locating hole, finish-milling blade (3), after finish-milling completes, send three-dimensional to check;
H. after the assay was approved, the end face of (1) and small end (2) and the upper stroke boring center line of first step end face (7) is held large;
I. centering center line, drilling and tapping;
J. the end face of the large end of finish turning diffuser (1) and endoporus;
K. file is repaiied bottom blade (3) runner;
L. penetrating inspection is carried out to blade (3).
2. the manufacture method of centrifugal vapor compressor diffuser according to claim 1, it is characterized in that: in step b, four paws folder small end (1) cylindrical, centering, the end face of the large end (1) of rough turn diffuser, cylindrical, endoporus and second step end face (9).
3. the manufacture method of centrifugal vapor compressor diffuser according to claim 1, it is characterized in that: in step c, the large end of four paws folder (1) cylindrical, by flat end face (8) greatly, centering is the large end endoporus of car, the end face of rough turn diffuser small end (2), cylindrical, endoporus and first step end face (7).
4. the manufacture method of centrifugal vapor compressor diffuser according to claim 1, it is characterized in that: in step e, the large end of soft three-jaw folder (1) cylindrical, by flat end face (8) greatly, centering is the large end endoporus of car, the end face of half finish turning diffuser small end (2), cylindrical, endoporus and first step end face (7).
5. the manufacture method of centrifugal vapor compressor diffuser according to claim 1, it is characterized in that: in step f, soft three-jaw folder small end (2) cylindrical, by flat first step end face (7), centering car small end endoporus jerk value is less than or equal to 0.015mm,, the end face of the large end (1) of half finish turning diffuser, cylindrical, endoporus and second step end face (9).
6. the manufacture method of centrifugal vapor compressor diffuser according to claim 1, it is characterized in that: in step I, large end end face (8) is downward, centering center line, above press figure holes drilled through (4) at the first step end face (7) of large end, small end (2) end face bores stepped hole (5); Turn-over, centering center line, bores tapping female bore (6) by figure end face (8) is greatly upper.
7. the manufacture method of centrifugal vapor compressor diffuser according to claim 1, it is characterized in that: in step j, soft three-jaw folder small end (2) cylindrical, by flat first step end face (7), centering is the large end endoporus of car, jerk value is less than or equal to 0.015mm, the large end end face (8) of finish turning diffuser.
CN201410470380.5A 2014-09-15 2014-09-15 The manufacture method of centrifugal vapor compressor diffuser Active CN104227359B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201410470380.5A CN104227359B (en) 2014-09-15 2014-09-15 The manufacture method of centrifugal vapor compressor diffuser

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201410470380.5A CN104227359B (en) 2014-09-15 2014-09-15 The manufacture method of centrifugal vapor compressor diffuser

Publications (2)

Publication Number Publication Date
CN104227359A true CN104227359A (en) 2014-12-24
CN104227359B CN104227359B (en) 2016-09-07

Family

ID=52216732

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201410470380.5A Active CN104227359B (en) 2014-09-15 2014-09-15 The manufacture method of centrifugal vapor compressor diffuser

Country Status (1)

Country Link
CN (1) CN104227359B (en)

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107234404A (en) * 2017-07-31 2017-10-10 重庆江增船舶重工有限公司 A kind of manufacture method of vapour compression machine diffuser
CN107398746A (en) * 2017-09-22 2017-11-28 重庆江增船舶重工有限公司 A kind of cutting tool and processing method of nozzle outer shroud
CN107790974A (en) * 2017-11-13 2018-03-13 重庆江增船舶重工有限公司 A kind of processing method of vapour compression machine diffuser
CN108994545A (en) * 2018-09-06 2018-12-14 重庆江增船舶重工有限公司 A kind of processing method and its turning measuring tool of TC bearings shell
CN109128718A (en) * 2018-10-24 2019-01-04 重庆江增船舶重工有限公司 A kind of manufacturing method of mechanical vapor compressor combination diffuser
CN111673396A (en) * 2020-07-09 2020-09-18 湖南南方通用航空发动机有限公司 Machining method for large-diameter thin-wall diffuser of aero-engine
CN112355571A (en) * 2020-09-22 2021-02-12 苏州润凯机械有限公司 Processing method of corrosion-resistant diffuser
CN112372242A (en) * 2020-10-30 2021-02-19 重庆江增船舶重工有限公司 Processing method of variable throat diffuser of supercharger

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20050039334A1 (en) * 2003-08-22 2005-02-24 Steve Roby Method for the manufacture of a vaned diffuser
US20110142609A1 (en) * 2009-12-14 2011-06-16 Honeywell International Inc. Centrifugal compressor with pipe diffuser
CN103008996A (en) * 2012-12-16 2013-04-03 齐齐哈尔市金车工业公司 Front cover machining process
CN103244462A (en) * 2012-02-14 2013-08-14 珠海格力电器股份有限公司 Tandem vane diffuser and method of making same
CN103244461A (en) * 2012-02-14 2013-08-14 珠海格力电器股份有限公司 Low solidity blade diffuser and manufacturing method thereof

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20050039334A1 (en) * 2003-08-22 2005-02-24 Steve Roby Method for the manufacture of a vaned diffuser
US20110142609A1 (en) * 2009-12-14 2011-06-16 Honeywell International Inc. Centrifugal compressor with pipe diffuser
CN103244462A (en) * 2012-02-14 2013-08-14 珠海格力电器股份有限公司 Tandem vane diffuser and method of making same
CN103244461A (en) * 2012-02-14 2013-08-14 珠海格力电器股份有限公司 Low solidity blade diffuser and manufacturing method thereof
CN103008996A (en) * 2012-12-16 2013-04-03 齐齐哈尔市金车工业公司 Front cover machining process

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107234404A (en) * 2017-07-31 2017-10-10 重庆江增船舶重工有限公司 A kind of manufacture method of vapour compression machine diffuser
CN107398746A (en) * 2017-09-22 2017-11-28 重庆江增船舶重工有限公司 A kind of cutting tool and processing method of nozzle outer shroud
CN107790974A (en) * 2017-11-13 2018-03-13 重庆江增船舶重工有限公司 A kind of processing method of vapour compression machine diffuser
CN108994545A (en) * 2018-09-06 2018-12-14 重庆江增船舶重工有限公司 A kind of processing method and its turning measuring tool of TC bearings shell
CN108994545B (en) * 2018-09-06 2020-06-23 重庆江增船舶重工有限公司 Turning measuring tool of supercharger bearing shell
CN109128718A (en) * 2018-10-24 2019-01-04 重庆江增船舶重工有限公司 A kind of manufacturing method of mechanical vapor compressor combination diffuser
CN111673396A (en) * 2020-07-09 2020-09-18 湖南南方通用航空发动机有限公司 Machining method for large-diameter thin-wall diffuser of aero-engine
CN112355571A (en) * 2020-09-22 2021-02-12 苏州润凯机械有限公司 Processing method of corrosion-resistant diffuser
CN112372242A (en) * 2020-10-30 2021-02-19 重庆江增船舶重工有限公司 Processing method of variable throat diffuser of supercharger

Also Published As

Publication number Publication date
CN104227359B (en) 2016-09-07

Similar Documents

Publication Publication Date Title
CN104227359A (en) Manufacturing method of centrifugal vapor compressor diffuser
CN104295608B (en) Ring processing method in oscillating bearing
CN105252233B (en) A kind of aero-engine high temperature alloy counterweight blade machining process
CN105643205B (en) Large-size machine shell processing technology
CN107790974A (en) A kind of processing method of vapour compression machine diffuser
CN202114292U (en) Blade drilling device of steam engine
CN105307400A (en) Processing method of square slot of printed wiring board
CN109128718B (en) Manufacturing method of mechanical type steam compressor combined diffuser
CN203171033U (en) Multi-stage composite chamfering forming drill
CN104741881B (en) Production method of blade of compressor impeller
CN205414423U (en) Numerically controlled lathe
CN104014989B (en) A kind of semicircle orifice processing method
CN104209713A (en) Manufacturing method of blind-hole compressor impeller
CN204470633U (en) A kind of numerically-controlled slide toolbox
CN205362793U (en) Processing interior cold ladder of rail rail body hole is altogether bored
CN107654369A (en) A kind of processing method and its special fixture of graphite vanes pump rotor
CN104259758A (en) Bearing block machining method beneficial to boring precision
CN105436832A (en) Machining process of compressor cylinder
CN206425567U (en) A kind of process tool of big depth-to-width ratio groove
CN205599990U (en) Integrative boring of high accuracy multiplex step
CN205020906U (en) Upper and lower chamfer sword
CN203992643U (en) A kind of reamer of deep hole processing
CN102922340A (en) Machining fixture
CN107378383B (en) The processing method of gear-box
CN204504299U (en) A kind of drill bit for valve opening reaming

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C14 Grant of patent or utility model
GR01 Patent grant