CN205996581U - Engine compressor disk anti-deformation machining tool fixture - Google Patents
Engine compressor disk anti-deformation machining tool fixture Download PDFInfo
- Publication number
- CN205996581U CN205996581U CN201620643454.5U CN201620643454U CN205996581U CN 205996581 U CN205996581 U CN 205996581U CN 201620643454 U CN201620643454 U CN 201620643454U CN 205996581 U CN205996581 U CN 205996581U
- Authority
- CN
- China
- Prior art keywords
- plate
- disc
- compressor
- pressing plate
- processing
- 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
Landscapes
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
This utility model provides a kind of engine compressor disk anti-deformation machining tool fixture.The fastener hole of stationary positioned plate (1) is formed with the bottom disc of base (5), described location-plate center is formed with cylinder boss, one centre bore is supported on the lower section of coxostermum anchor ring under compressor disc (7) more than the resilient support packing ring (6) of described cylinder boss, one is fixed on above-mentioned cylinder boss with shape pressing plate (8) in shape identical in engine compressor disk, one profile pressing plate (2) basically identical with compressor disc profile is passed through the bolt of distribution and central pressing bolt (4) on circumference and compressor disc positioning is fixed on location-plate, between resilient support packing ring and interior shape pressing plate and profile pressing plate.The frock manufacturing according to this utility model, anti-deformation in the titanium alloy compressor disc course of processing can be realized on a sleeve clamp, manufacturing procedure can be reduced simultaneously, so that processing technique, processing content is concentrated, reduce by 50% parts fixation number of times, improve 50% passing rate of processing.
Description
Technical field
This utility model relates generally to the frock clamp of the titanium alloy compressor disc course of processing.
Background technology
The parts such as electromotor mid-game, axle, drum barrel, axle journal are all core rotatable parts and the key components of electromotor, high temperature,
Work under high pressure, high-revolving adverse circumstances.This kind of part material adopts high temperature alloy, powder metallurgy superalloy, titanium alloy mostly
Deng difficult-to-machine material manufacture, dimension precision requirement is high, and technical conditions are strict, and surface quality of workpieces, surface integrity are had high demands,
The height of its crudy directly influences service life and the security reliability of electromotor.Dish axle integrative-structure part is to pass
The compressor disc of system and the important bearing member that becomes one of axle journal, material is titanium alloy, and big end is wheeling disk structure, has wheel
Edge, disc, wheel hub, core hole, wheel rim carry the dovetail slot installing blade, have precision bolt connecting hole at disc.Part
Journal end outer mold surface is threaded, the architectural feature such as tooth of combing, external splines, radial direction inclined hole.Another spy of dish axle integrative-structure part
Point is that axle journal cone wall defines semiclosed deep-small hole structure with wheel disc disc, and processing technology is poor.
After compressor, drum barrel part is to be combined by flywheel friction welding welding by 5 compressor discs, with Pyatyi ring
Shape dovetail slot, disc interior lumen type space of planes is narrow and small, and inner chamber root bottom part radial depth is big, it is poor to open wide property, difficulty of processing is big, outward
Moulding surface structure is complicated, and dimensional accuracy is high, and technical conditions require sternly, and rear drum barrel material is titanium alloy, hardness HB >=388N/mm2.Pass
The processing mode of system, parts size precision relies on the upper tool offset value of operator to control, big by artificial influence factor, dimensional tolerance from
Divergence is big.Generally all carry the tongue-and-groove installing blade on disk drum class part wheel rim, vertical tree-like tongue-and-groove and dovetail can be divided into by shape
Shape tongue-and-groove, is divided into axial tongue-and-groove and annular tongue-and-groove by tongue-and-groove direction again, and axial tongue-and-groove generally adopts wire pulling method, annular dovetail
Groove adopts numerical control workshop.More, the tenon of annular dovetail slot structure is applied on engine compressor disk and drum barrel component
Channel opening is little, inner chamber width, and typically in 0.01 mm, other surfaces profile tolerance is typically 0.025 for tongue-and-groove work surface profile
Mm about, the required precision of manufacture is high, and main processing difficulties are：
（1）Tongue-and-groove work surface node size, position accuracy and true edge diameter dimension tolerance are strict, especially
Tongue-and-groove profile tolerance will ensure on holotype face, and equipment cutter is had high demands, and titanium alloy material machinability is poor, processing hardening phenomenon is tight
Weight, the machining accuracy of impact part and surface quality level.
（2）Tenon groove structure is that chamber is big, mouth is little, and unlimited property is poor, makes that the big neck of tongue-and-groove tool head is little, and cervical region intensity is relatively
Weak, and allowance is larger, chip removal is difficult, easily phenomenon of forging a knife in the course of processing.
Compressor disc by friction welding (FW) or electron beam weldering formed drum barrel molectron after, deep chamber bottom-type face between plate convergence plates at different levels
Processing is always difficult point and bottleneck in processing, and particularly inner chamber radial depth size H is narrow more than the closing of core bore dia φ A
In length, the processing of lumen type face is even more the key in the processing of drum barrel molectron.Because between plate wheel hubs at different levels, spacing C is little, during Tool in Cutting
Blind regarding state under processing it is impossible to observe monitoring cutting situation, processing risk big.Conventional process and cutter cannot complete
The processing of such deep chamber closure profile, can only be processed from longer, thinner thickness the cutter that overhangs, cause cutter poor rigidity,
Intensity is relatively low, easily occurs allowing knife and cuts covibration, aggravate tool wear, after processing, piece surface easily occurs in the course of processing
Chatter mark, difficulty of processing is big.And in the machining of the whole turbine disk, workload is maximum, difficulty highest is that wheel disc chase mortise adds
Work.Variously-shaped complicated circumferential tongue-and-groove commonly uses milling machine milling and broaching machine is broached and to be processed.Because dovetail type tenon groove structure is not advised
Then, complex-shaped, and surface roughness requirements are in more than Ra0.8, according to Milling Process it is necessary to by rough milling, half essence
Milling, finish-milling three road technique, are possible to the surface roughness making tongue-and-groove reach requirement, and high labor intensive, and efficiency is low, processing
Precision is difficult to ensure that, seldom employs in batch production, so adopting wire pulling method more.The broaching of broaching feature is a kind of
In high precision, efficient can final molding machining process, for processing variously-shaped inner and outer surfaces, and have
Helicla flute of rotary motion etc..It is particularly suitable for the part producing in batch and in a large number that machining accuracy is high, surface quality requirements are high.Existing
It is widely used in the processing of the parts such as aero-engine disk at different levels, blade tenon, the turbine disk, compressor disc, installing plate, but
Special cutter, measurer and other accessory must be equipped with.
The unfixing ripe processing method of processing to titanium alloy compressor disc for the prior art.Conventional processing method work
Sequence is many, and frock is many, and the lathe being used is many, and the product size deformation processing is big, and qualification rate is low, takes time and effort；This
Not only production efficiency is low for traditional method, and the product size processing, shape and positional precision, because of relatedness too
By force it is difficult to control；Quality is unstable, is also easy to produce waste product.Engine compressor disk as shown in Figure 1, this compressor disc is large-scale disk
Class thin-walled parts external diameter 527 mm, thinnest part 4 mm, and required precision is very high, is very easy to deformation, traditional manufacturing procedure relates to
And more than 50, need to change 5-10 platform lathe, processing time consuming, qualification rate is only 50%, with the development of Aeronautics and Astronautics industry, right
Product quality requires more and more higher, and this processing method far can not meet the demand of product quality and production efficiency.
Utility model content
This utility model is directed to the problem that above-mentioned prior art exists, and provides a kind of steady quality reliable, qualification rate is high, energy
Enough reduce clamping times, the clamping mechanism of deformation in the titanium alloy compressor disc course of processing can be prevented.
Above-mentioned purpose of the present utility model can be reached by following measures, and a kind of engine compressor disk anti-deformation adds
Work frock clamp, including：The base 5 of fixing compressor disc 7 it is characterised in that：It is fixing fixed to be formed with the bottom disc of base 5
The fastener hole of position plate 1, described location-plate 1 center is formed with cylinder boss, and a centre bore props up more than the elasticity of described cylinder boss
Stake pad circle 6 is supported on the lower section of 7 times coxostermum anchor rings of compressor disc, one with shape in shape identical in engine compressor disk 7
Pressing plate 8 is fixed on above-mentioned cylinder boss, and a profile pressing plate 2 basically identical with compressor disc 7 profile passes through to divide on circumference
Compressor disc 7 positioning is fixed on location-plate 1, resilient support packing ring 6 and interior shape by the bolt of cloth and central pressing bolt 4, packing ring 3
Between pressing plate 8 and profile pressing plate 2, wherein, the endoporus of compressor disc 7 is nested on the cylinder boss of location-plate 1.
This utility model has the advantages that.
Steady quality is reliable, and qualification rate is high, can reduce clamping times, and this utility model adopts one and compressor disc 7
The basically identical profile pressing plate 2 of profile, by the bolt of distribution and central pressing bolt 4, packing ring 3 on circumference by compressor disc 7
Positioning is fixed between location-plate 1, resilient support packing ring 6 and interior shape pressing plate 8 and profile pressing plate 2, the elasticity being made by rubber
Backup washer 6, can effectively prevent the deformation of compressor disc web in process, by disposable clamping, decrease existing
There is the parts fixation of technology 50%.Flexibly support the web position of compressor disc by flexibly supporting packing ring, compression compressor disc
End face, prevents the deformation of the compressor disc course of processing, meets compressor disc to size, shape, position degree requirement, thus improve
The qualification rate of the titanium alloy compressor disc course of processing, the passing rate of processing improving in the titanium alloy compressor disc course of processing almost may be used
To obtain 100%.Fundamentally solve traditional processing method production efficiency low, relatedness is too by force it is difficult to control；Quality
Unstable, it is also easy to produce the problem of waste product.
Due to, during using this utility model, only interior shape pressing plate 8 and profile pressing plate 2 need to be changed, you can realize outside compressor disc
The processing on same a machine tool of shape and interior shape, and then solve traditional processing operation and be related to more than 50, need to change 5-10 platform
Lathe, the defect of processing time consuming.
According to the clamping tooling of this utility model design, manufacture, titanium alloy compressor disc can be realized on a sleeve clamp and add
Anti-deformation during work, can reduce manufacturing procedure simultaneously, so that processing technique, processing content is concentrated, and reduce by 50% part dress
Folder number of times, improves 50% part passing rate of processing.
This utility model adopts the hollow structure base 5 that cast iron makes, and on the one hand mitigates weight, on the other hand can improve
Whole device stability in process.
Brief description
The section view of compressor disc processed by Fig. 1 this utility model engine compressor disk anti-deformation machining tool fixture clamping
Figure.
Fig. 2 is the sectional view after Fig. 1 removes profile pressing plate
Fig. 3 is Fig. 1 base structure schematic diagram
Fig. 4 is the organigram of Fig. 1 location-plate.
Fig. 5 is the organigram of Fig. 1 profile pressing plate.
Fig. 6 is the organigram of shape pressing plate in Fig. 1.
Fig. 7 is the organigram of Fig. 1 resilient support
The front view of Fig. 8 engine compressor disk.
Fig. 9 is the top view of Fig. 8 compressor disc tongue-and-groove.
In figure：1 location-plate, 2 profile pressing plates, 3 packing rings, 4 hold-down bolts, 5 bases, 6 resilient support, 7 compressor discs, in 8
Shape pressing plate.
Specific embodiment
Refering to Fig. 1-Fig. 7.In embodiment described below, engine compressor disk anti-deformation machining tool fixture is main
By the base 5 of stationary engine compressor disc, location-plate 1, profile pressing plate 2, packing ring 3, hold-down bolt 4, resilient support packing ring 6
Form with interior shape pressing plate 8.Wherein, the fastener hole being fixedly connected location-plate 1, described positioning are formed with the bottom disc of base 5
Plate 1 center is formed with cylinder boss, and a centre bore is supported on compressor disc 7 more than the resilient support packing ring 6 of described cylinder boss
The lower section of lower coxostermum anchor ring, one is fixed on above-mentioned cylinder boss with shape pressing plate 8 in shape identical in engine compressor disk 7
On, profile pressing plate 2 basically identical with compressor disc 7 profile pass through the bolt of distribution and central pressing bolt 4 on circumference,
Compressor disc 7 positioning is fixed between location-plate 1, resilient support packing ring 6 and interior shape pressing plate 8 and profile pressing plate 2 packing ring 3, its
In, the endoporus of compressor disc 7 is nested in location-plate（1）Cylinder boss on.Base 5 shown in Fig. 3 is using in cast iron making
Hollow structure, transverse plane on its cylindrical shell being formed with to be connected connect the fastener hole that is circumferentially distributed of location-plate 1 and in
The heart positions fastener hole, is formed with lightening core on the excircle of its cylindrical shell.
During clamping engine compressor disk, base 5 is fixed on lathe, reuses hold-down bolt 4 by location-plate 1 and bottom
Seat 5 connection, then resilient support packing ring 6 is fixed on location-plate, puts compressor disc 7, tighten hold-down bolt 4 and profile pressure
Plate 2, thus realize positioning on device for the engine compressor disk part and clamping（As shown in Figure 1）, start the processing of profile.
Profile portion unclamps hold-down bolt 4 after machining, and takes off profile pressing plate 2, is replaced with interior shape pressing plate 8, then tightens compression spiral shell
Bolt 4, thus realize positioning on device for the engine compressor disk part and clamping（As shown in Figure 2）, start shape in it plus
Work.After processing a face, compressor disc is overturn, then according to above-mentioned steps carry out clamping and processing.
Claims (2)
1. a kind of engine compressor disk anti-deformation machining tool fixture, including：Fixing compressor disc（7）Base（5）, it is special
Levy and be：In base（5）Bottom disc on be formed with stationary positioned plate（1）Fastener hole, described location-plate（1）Center is formed with circle
Post boss, a centre bore is more than the resilient support packing ring of described cylinder boss（6）It is supported on compressor disc（7）Lower coxostermum ring
The lower section in face, one and engine compressor disk（7）Shape pressing plate in interior shape identical（8）It is fixed on above-mentioned cylinder boss, one
Individual and compressor disc（7）The basically identical profile pressing plate of profile（2）By the bolt of distribution and central pressing bolt on circumference（4）
By compressor disc（7）Positioning is fixed on location-plate（1）, resilient support packing ring（6）With interior shape pressing plate（8）With profile pressing plate（2）It
Between, wherein, compressor disc（7）Endoporus be nested in location-plate（1）Cylinder boss on.
2. engine compressor disk anti-deformation machining tool fixture as claimed in claim 1 it is characterised in that：Base（5）It is
The hollow structure being made using cast iron, on the upper transverse plane of its cylindrical shell, is formed with the connection location-plate that is connected（1）Press
The fastener hole of circle distribution and centralized positioning fastener hole, are formed with lightening core on the excircle of its cylindrical shell.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620643454.5U CN205996581U (en) | 2016-06-23 | 2016-06-23 | Engine compressor disk anti-deformation machining tool fixture |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620643454.5U CN205996581U (en) | 2016-06-23 | 2016-06-23 | Engine compressor disk anti-deformation machining tool fixture |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205996581U true CN205996581U (en) | 2017-03-08 |
Family
ID=58205581
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620643454.5U Active CN205996581U (en) | 2016-06-23 | 2016-06-23 | Engine compressor disk anti-deformation machining tool fixture |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205996581U (en) |
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107378572A (en) * | 2017-08-01 | 2017-11-24 | 江阴市惠尔信机械有限公司 | For processing the frock of aerogenerator stator disk |
| CN110732691A (en) * | 2019-11-18 | 2020-01-31 | 中国航发贵州黎阳航空动力有限公司 | Method for machining vibration-proof cutter for thin-wall large-disc parts |
| CN111113093A (en) * | 2019-12-27 | 2020-05-08 | 中国航发湖南南方宇航工业有限公司 | Integral impeller clamp |
| CN111660118A (en) * | 2020-06-12 | 2020-09-15 | 中航力源液压股份有限公司 | Multipurpose milling clamp |
| CN112476002A (en) * | 2020-10-30 | 2021-03-12 | 江西昌河航空工业有限公司 | Workpiece positioning device for inner cavity of spherical cambered surface |
| CN112894406A (en) * | 2021-01-25 | 2021-06-04 | 中国航发贵州黎阳航空动力有限公司 | Tool for machining thin-wall support ring of aero-engine |
| CN113798878A (en) * | 2020-06-15 | 2021-12-17 | 中国航发商用航空发动机有限责任公司 | Broaching clamp for machining mortise of aero-engine disc |
| CN114850911A (en) * | 2022-05-26 | 2022-08-05 | 中国人民解放军第五七一九工厂 | Compacting structure of aeroengine powder high-temperature alloy dual-performance turbine disc |
| CN114918705A (en) * | 2022-06-17 | 2022-08-19 | 中国航发贵州黎阳航空动力有限公司 | Hydraulic floatable repeated positioning and clamping method and device for finish machining of thin-wall disc parts |
| CN114918626A (en) * | 2022-06-17 | 2022-08-19 | 中国航发贵州黎阳航空动力有限公司 | Thread lifting repeated positioning and clamping method and device for finish machining of thin-wall disc type parts |
-
2016
- 2016-06-23 CN CN201620643454.5U patent/CN205996581U/en active Active
Cited By (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107378572A (en) * | 2017-08-01 | 2017-11-24 | 江阴市惠尔信机械有限公司 | For processing the frock of aerogenerator stator disk |
| CN107378572B (en) * | 2017-08-01 | 2023-09-26 | 江阴市惠尔信精密装备股份有限公司 | Tool for machining stator plate of wind driven generator |
| CN110732691A (en) * | 2019-11-18 | 2020-01-31 | 中国航发贵州黎阳航空动力有限公司 | Method for machining vibration-proof cutter for thin-wall large-disc parts |
| CN111113093A (en) * | 2019-12-27 | 2020-05-08 | 中国航发湖南南方宇航工业有限公司 | Integral impeller clamp |
| CN111660118A (en) * | 2020-06-12 | 2020-09-15 | 中航力源液压股份有限公司 | Multipurpose milling clamp |
| CN113798878A (en) * | 2020-06-15 | 2021-12-17 | 中国航发商用航空发动机有限责任公司 | Broaching clamp for machining mortise of aero-engine disc |
| CN112476002A (en) * | 2020-10-30 | 2021-03-12 | 江西昌河航空工业有限公司 | Workpiece positioning device for inner cavity of spherical cambered surface |
| CN112894406A (en) * | 2021-01-25 | 2021-06-04 | 中国航发贵州黎阳航空动力有限公司 | Tool for machining thin-wall support ring of aero-engine |
| CN114850911A (en) * | 2022-05-26 | 2022-08-05 | 中国人民解放军第五七一九工厂 | Compacting structure of aeroengine powder high-temperature alloy dual-performance turbine disc |
| CN114918705A (en) * | 2022-06-17 | 2022-08-19 | 中国航发贵州黎阳航空动力有限公司 | Hydraulic floatable repeated positioning and clamping method and device for finish machining of thin-wall disc parts |
| CN114918626A (en) * | 2022-06-17 | 2022-08-19 | 中国航发贵州黎阳航空动力有限公司 | Thread lifting repeated positioning and clamping method and device for finish machining of thin-wall disc type parts |
| CN114918626B (en) * | 2022-06-17 | 2023-09-22 | 中国航发贵州黎阳航空动力有限公司 | Lifting repeated positioning clamping method and device for finish machining threads of thin-wall disc parts |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN205996581U (en) | Engine compressor disk anti-deformation machining tool fixture | |
| US20210039194A1 (en) | Method of manufacturing a component of a rotary machine and component manufactured using said method | |
| EP1792680B1 (en) | Method for machining components of turbine engines | |
| RU2743542C2 (en) | A method of manufacturing or repairing a part of a rotary machine, as well as a part manufactured or repaired using such a method | |
| CN110666188A (en) | Machining process and manufacturing process of hub | |
| CN111203603B (en) | Interchange clamping device for turbine disc | |
| EP3366884B1 (en) | Method for manufacturing blisk | |
| CN109176058A (en) | A kind of gas turbine circumferential slot profile shaft streaming compressor blade and blade tooling and processing method | |
| CN102152071B (en) | Processing technique of Roots blower impeller component | |
| CN107097044B (en) | Machining process and tool device for large nuclear main pump shielding motor balance ring | |
| CN213164191U (en) | Steel body piston processing location frock | |
| US20230250831A1 (en) | Methods and systems for manufacturing an impeller wheel assembly | |
| CN209598697U (en) | A kind of gas turbine circumferential slot profile shaft streaming compressor blade and blade tooling | |
| CN101196154A (en) | Technique for producing runner hub with runner hub core of large-scale bulb through-flow type hydro-turbo generator set | |
| CN115709262A (en) | Double-spoke-plate turbine disc structure and investment casting centering method thereof | |
| CN205967569U (en) | Shaping special milling cutter cutter of titanium alloy compressor dish tongue -and -groove | |
| CN201979303U (en) | Clamp for broaching super-large-dimension dovetail type mortise of heavy type gas turbine compressor | |
| CN105057992A (en) | Low-rigidity turbine blade milling clamp and use method thereof | |
| RU2749240C2 (en) | Method of manufacturing or repairing a part of a rotary machine, as well as a part manufactured or repaired using such a method | |
| CN216370331U (en) | Special disc milling machine for upper and lower large faces of tile cover | |
| CN117124029B (en) | Integral manufacturing process method of multistage blisk | |
| CN207447890U (en) | A kind of HSK locks tool holder | |
| CN210024570U (en) | Tool for automatically correcting center of guide vane | |
| CN207858307U (en) | A kind of nonstandard guide vane processing unit (plant) | |
| CN210208679U (en) | Special machine tool for crankshaft |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant |