CN104690198A - Forming method of large GH4169 alloy direct aging disc forging - Google Patents
Forming method of large GH4169 alloy direct aging disc forging Download PDFInfo
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- CN104690198A CN104690198A CN201310666925.5A CN201310666925A CN104690198A CN 104690198 A CN104690198 A CN 104690198A CN 201310666925 A CN201310666925 A CN 201310666925A CN 104690198 A CN104690198 A CN 104690198A
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Abstract
The invention discloses a technology of 'die forging for blank forming plus die forging for forming plus direct aging' for the forming problem of the large GH4169 alloy direct aging disc forging. Since the traditional 'free forging for blank forming' is changed into the 'die forging for blank forming', uncontrollable factors of larger heating number and deformation in a free forging procedure are eliminated; the control of heating and the deformation in a forging technology are guaranteed; a forging after final direct aging treatment can stably meet requirements of a level ten grain size; the production efficiency is improved; and the cost is lowered.
Description
Technical field:
The present invention relates to the method for forging and molding of large-scale GH4169 alloy direct aging dish forging part, particularly projected area is greater than 0.2m
2and grain size requires the disk forge piece of 10 grades.
Background technology:
GH4169 alloy is a kind of with the nickel base superalloy of the γ " of body-centered tetragonal and face-centred cubic γ ' phase precipitation strength, be mainly used in the crucial load part of Aero-Space equipment, when these crucial load parts manufacture, forging used has very high requirement to performance, for the crucial load part at some engine core position, require that the grain size after the complete heat treatment of GH4169 alloy forging reaches 10 grades, and conventional forged after, solid-solution and aging heat treatment does not almost reach the grain size requirement of 10 grades, even if adopt direct aging Technology for Heating Processing, also the open die forging base moderate heat due to routine is secondary more, the uncontrollable reason of deflection and cause technique instability (key of grain refinement is the control to heating and deflection in Forging Technology, and open die forging is difficult to control), therefore according to the technique of traditional " open die forging base+die-forging forming+direct aging ", end product quality is unstable, can not be stable reach 10 grades of grain size requirements.
Traditional GH4169 alloy disc class takes the mode of " open die forging base+die forging " to complete at direct aging forging part before treatment, usually following two kinds of typical process route: Yi Zhongshi are had: upsetting cake → punching → horse expansion → reaming (ring base) → die forging, this technique due to Forging Technology link and fire time more, and horse is expanded the repeatedly small deformation of process and can cause the uneven of blank tissue, more difficultly reach more than the 8 grades grain size requirements of ring base.The second is: upsetting cake → punching → reaming (ring base) → die forging, and this scheme advantage eliminates horse to expand operation, raises the efficiency, and that simultaneously improves ring base due to the increase of reaming link deflection organizes level; Shortcoming is that after removing horse expansion, add the difficulty of reaming, namely reaming one fire completes the deflection of more than 40%, and capacity of equipment requires higher, and the operability of technique needs to consider; Above two kinds of process programs, owing to relating to free forging process, are affected by human factors comparatively large, unstable product quality, therefore are difficult to meet forging ' s block dimension and integrative organization's performance requirement.
The invention discloses the technique of one " die forging base+die-forging forming+direct aging ", by traditional " open die forging base " is changed into " die forging base ", eliminate open die forging operation moderate heat secondary more, the uncontrollable factor of deflection, ensure that the control to heating and deflection in Forging Technology, ensure that the forging after final direct aging process can stablize the grain size requirement reaching 10 grades, improve production efficiency, reduce cost.
Technical problem of the present invention is:
For the forging molding of large-scale GH4169 alloy direct aging dish forging part, according to the technique of traditional " open die forging base+die-forging forming+direct aging ", end product quality is unstable, can not be stable reach 10 grades of grain size requirements.
Technical scheme:
Step 1 prefabricated blank, is adopted the mode of die-forging forming to complete upsetting cake and punching operation, by mould controlling distortion amount between 50% to 55%, is added remove punching core material by machine, improve ring base size and metallurgical quality uniformity;
Step 2 preformed, adopts the swollen hole of die forging to complete reaming operation, by mould controlling distortion amount between 20% to 25%;
Step 3 die-forging forming, utilizes finish-forging die one pyrogene type, by mould controlling distortion amount between 30% to 35%;
In 30s, enter water after step 4 die forging final molding, be chilled to room temperature, complete direct aging process.
The invention has the beneficial effects as follows:
Adopt die-forging forming to replace open die forging upsetting cake, punching, improve technology stability; Adopt the swollen hole of die forging to replace looping mill rolling, reasonable distribution and controlling distortion amount, improve ring base performance;
On the whole, by traditional " open die forging base " is changed into " die forging base ", eliminate open die forging operation moderate heat secondary more, the uncontrollable factor of deflection, ensure that the control to heating and deflection in Forging Technology, ensure that the forging after final direct aging process can stablize the grain size requirement reaching 10 grades, improve production efficiency, reduce manufacturing cost.
Concrete case embodiment
Below with reference to embodiment, technical solution of the present invention is further described:
Large-scale GH4169 alloy direct aging dish forging of the present invention, external diameter φ 681mm, internal diameter φ 374mm, projected area is about 0.25m
2, all round properties index of forging and grain size require the requirement (grain size requires 10 grades) that should meet xx-0515 standard.
Its forging step is as follows in detail:
The pattern of first step design upsetting cake, increase drift in the centre up and down of pattern, directly put in pattern by bar, hammering, to certain height, makes blank just be full of die cavity (not going out burr), completes prefabricated blank shaping.
The web portion extension set at prefabricated blank center adds to fall by the mode that second step is added by machine, so far realizes upsetting cake in traditional handicraft, work that punching two operations will complete, and this operation deflection reaches more than 50%, and grain size can improve 2 ~ 2.5 grades.
3rd step design preforming tool, the counterdie of this mould has the fuse of a taper, fuse has two kinds of gradients, top is 15 degree, and below is 10 degree, and object comes swollen hole by the gradient of taper fuse, realize the work that traditional reaming operation will complete, this operation deflection is less, by mould controlling distortion amount between 20% to 25%, mainly makes crystal grain no longer grow up.
After 4th step completes preforming operation, finish-forging die die cavity directly put into by waste base, completes die forging final molding, and this operation deflection reaches more than 30%, crystal grain energy refinement 1 ~ 1.5 grade.
In 30s, enter water after 5th step die forging final molding, be chilled to room temperature, complete direct aging process.
The homogeneous fire of forging process of this technique completes, and is meeting on the shaping basis of forging, after tested, finally can stablize the microscopic structure (10 grades of grain sizes) being met standard-required.
Claims (1)
1. a forming method for large-scale GH4169 alloy direct aging dish forging, is characterized in that, comprise the steps,
Step 1 prefabricated blank, is adopted the mode of die-forging forming to complete upsetting cake and punching operation, by mould controlling distortion amount between 50% to 55%, is added remove punching core material by machine, improve ring base size and metallurgical quality uniformity;
Step 2 preformed, adopts the swollen hole of die forging to complete reaming operation, by mould controlling distortion amount between 20% to 25%;
Step 3 die-forging forming, utilizes finish-forging die one pyrogene type, by mould controlling distortion amount between 30% to 35%;
In 30s, enter water after step 4 die forging final molding, be chilled to room temperature, complete direct aging process.
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Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
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CN106111862A (en) * | 2016-08-29 | 2016-11-16 | 中航动力股份有限公司 | A kind of forging method of GH4901 sleeve spacer ring |
CN107175306A (en) * | 2017-07-18 | 2017-09-19 | 中国第二重型机械集团德阳万航模锻有限责任公司 | The large-scale forging part forging method of fine grain AF1410 steel |
CN107913963A (en) * | 2017-12-07 | 2018-04-17 | 陕西宏远航空锻造有限责任公司 | A kind of GH4169 alloy annulars forging forming method |
CN108160887A (en) * | 2016-12-07 | 2018-06-15 | 陕西宏远航空锻造有限责任公司 | A kind of forming method of large size GH4169 alloy annular forging |
CN108246947A (en) * | 2017-12-07 | 2018-07-06 | 陕西宏远航空锻造有限责任公司 | A kind of GH4169 alloy die forgings improve the forging method of flaw detection bottom damage |
CN110976740A (en) * | 2019-12-19 | 2020-04-10 | 陕西宏远航空锻造有限责任公司 | Method for manufacturing drum shaft forging |
CN111659842A (en) * | 2020-05-27 | 2020-09-15 | 四川工程职业技术学院 | Die forging processing method for variable-section titanium alloy frame type forge piece |
CN112719180A (en) * | 2020-12-18 | 2021-04-30 | 陕西宏远航空锻造有限责任公司 | Forming method of large GH4169 alloy disc-shaped forge piece |
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CN101036931A (en) * | 2007-03-05 | 2007-09-19 | 贵州安大航空锻造有限责任公司 | Method for smithing GH4169 alloy plate shaped forgeable piece in air at an approximately equal temperature |
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CN103341586A (en) * | 2013-06-07 | 2013-10-09 | 北京科技大学 | Method for achieving forming of GH4738 nickel-base superalloy turbine discs |
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CN101036931A (en) * | 2007-03-05 | 2007-09-19 | 贵州安大航空锻造有限责任公司 | Method for smithing GH4169 alloy plate shaped forgeable piece in air at an approximately equal temperature |
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Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN106111862A (en) * | 2016-08-29 | 2016-11-16 | 中航动力股份有限公司 | A kind of forging method of GH4901 sleeve spacer ring |
CN108160887A (en) * | 2016-12-07 | 2018-06-15 | 陕西宏远航空锻造有限责任公司 | A kind of forming method of large size GH4169 alloy annular forging |
CN107175306A (en) * | 2017-07-18 | 2017-09-19 | 中国第二重型机械集团德阳万航模锻有限责任公司 | The large-scale forging part forging method of fine grain AF1410 steel |
CN107913963A (en) * | 2017-12-07 | 2018-04-17 | 陕西宏远航空锻造有限责任公司 | A kind of GH4169 alloy annulars forging forming method |
CN108246947A (en) * | 2017-12-07 | 2018-07-06 | 陕西宏远航空锻造有限责任公司 | A kind of GH4169 alloy die forgings improve the forging method of flaw detection bottom damage |
CN110976740A (en) * | 2019-12-19 | 2020-04-10 | 陕西宏远航空锻造有限责任公司 | Method for manufacturing drum shaft forging |
CN111659842A (en) * | 2020-05-27 | 2020-09-15 | 四川工程职业技术学院 | Die forging processing method for variable-section titanium alloy frame type forge piece |
CN112719180A (en) * | 2020-12-18 | 2021-04-30 | 陕西宏远航空锻造有限责任公司 | Forming method of large GH4169 alloy disc-shaped forge piece |
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