CN102085556A - Roll forming method of GH4033 high-temperature alloy thin-wall ring piece - Google Patents
Roll forming method of GH4033 high-temperature alloy thin-wall ring piece Download PDFInfo
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- CN102085556A CN102085556A CN 201010582194 CN201010582194A CN102085556A CN 102085556 A CN102085556 A CN 102085556A CN 201010582194 CN201010582194 CN 201010582194 CN 201010582194 A CN201010582194 A CN 201010582194A CN 102085556 A CN102085556 A CN 102085556A
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- 239000000956 alloy Substances 0.000 title claims abstract description 34
- 229910045601 alloy Inorganic materials 0.000 title claims abstract description 32
- 238000000034 method Methods 0.000 title claims abstract description 26
- 238000005096 rolling process Methods 0.000 claims abstract description 60
- 230000002093 peripheral effect Effects 0.000 claims description 16
- 238000007493 shaping process Methods 0.000 claims description 14
- 238000010438 heat treatment Methods 0.000 claims description 4
- 229910001069 Ti alloy Inorganic materials 0.000 abstract description 3
- 238000012360 testing method Methods 0.000 description 6
- 238000005242 forging Methods 0.000 description 4
- 238000009434 installation Methods 0.000 description 4
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 3
- 230000032683 aging Effects 0.000 description 2
- 238000001816 cooling Methods 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 238000009413 insulation Methods 0.000 description 2
- 230000007774 longterm Effects 0.000 description 2
- 238000004080 punching Methods 0.000 description 2
- 239000000243 solution Substances 0.000 description 2
- 229910000601 superalloy Inorganic materials 0.000 description 2
- 229910018487 Ni—Cr Inorganic materials 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 229910052729 chemical element Inorganic materials 0.000 description 1
- 239000011651 chromium Substances 0.000 description 1
- VNNRSPGTAMTISX-UHFFFAOYSA-N chromium nickel Chemical compound [Cr].[Ni] VNNRSPGTAMTISX-UHFFFAOYSA-N 0.000 description 1
- 238000000205 computational method Methods 0.000 description 1
- 230000008602 contraction Effects 0.000 description 1
- 239000013078 crystal Substances 0.000 description 1
- 230000002950 deficient Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 239000011159 matrix material Substances 0.000 description 1
- 229910052759 nickel Inorganic materials 0.000 description 1
- 239000006104 solid solution Substances 0.000 description 1
- 230000035882 stress Effects 0.000 description 1
- 239000010936 titanium Substances 0.000 description 1
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Abstract
The invention discloses a roll forming method of a GH4033 high-temperature alloy thin-wall ring piece, wherein the thin-wall ring piece is roll-formed and has high size precision and excellent structure and performance. The technical is as follows: sleeving a titanium alloy pre-rolled blank which is heated to a deforming temperature and a pre-heated follow-up mould sleeve into a ring rolling mill; sleeving the follow-up mould sleeve in the pre-rolled blank; positioning the two workpieces by utilizing a main roller, a core roller, holding rollers and upper and lower conical rollers of the ring rolling mill; and starting the ring rolling mill, wherein the core roller of the ring rolling mill performs radial feed motion toward the main roller and rolls the pre-rolled blank together with the main roller under the support of the follow-up mould sleeve with a rolling force of 220-4,200 KN so that the pre-rolled blank is widened radially at a speed of 5-8 mm/s and the wall thickness is gradually reduced; and after the deformation of the pre-rolled blank reaches 25-45%, the pre-rolled blank is rolled into a thin-wall ring piece. The minimum of the wall thickness of the titanium alloy thin-wall ring piece roll-formed by the method is 25 mm, and the maximum of the height-thickness ratio is 25 mm; and the ring piece is mainly applied to the rotational parts such as a cylindrical shell and the like used in the fields of aerospace and the like..
Description
Technical field
The present invention relates to a kind of roll-forming method of annular forging piece, particularly related to the method for rolling and shaping of GH4033 high temperature alloy thin-walled ring.
Background technology
The GH4033 high temperature alloy is to be the ni-base wrought superalloy of matrix with nickel-chromium, the revolving body parts such as barrel-type casing that use in the fields such as Aero-Space of adopting this alloy hoop to roll into shape, the thin-walled rings such as front housing of aero-engine for example, requirement has enough elevated temperature strengths when using for 700～750 ℃ long-term, have good non-oxidizability when long-term work below 900 ℃.When rolling, because the alloy deformation temperature range is narrower, deflection is less, and the forging wall thickness is thinner, and dimensional accuracy, performance and tissue are had relatively high expectations, and have increased the difficulty of roll forming.
On October 8th, 2008, disclosed Chinese invention patent specification CN 101279346A disclosed a kind of method for rolling and shaping of nickel-based high-temperature alloy special-shaped ring rolling spare, this method by the alloy bar of specification blanking through jumping-up, punching, roll ring base (not using the roll off mould) for twice, again blank is put into rolling and shaping in the machine for rolling ring roll off mould, by taking the mode of small deformation amount shaping and the deflection of precise control in each processing step, tissue and well behaved special-shaped ring have been rolled out double rolling in the ring base process.When adopting the thin GH4033 high temperature alloy thin-walled ring of the rolling wall thickness of this method, because the roll off mould is fixed on (being on home roll and the core roller) on the roll, produce fierce friction when rolling between the pass of roll off mould and the pre-strip plate and make not only that the operation of rolling is very unstable to impact production, but also cause pre-strip plate temperature to raise easily alloy organizing and performance are exerted an influence, as defectives such as tissue variation, crystal grain be thick occurring.
When the GH4033 high temperature alloy thin-walled ring of home roll that adopts said method and direct use machine for rolling ring and core rolling system (encircling base) thin-walled as rolling in the above-mentioned method, owing to be subjected to the influence of the parts rigidity such as core roller of machine for rolling ring, the rigidity of structure that adds the thin-walled ring is relatively poor less with allowance, easily cause pre-strip plate plastic instability to occur and produce phenomenons such as draw down, horn mouth in the operation of rolling, cause the ring shape and size not reach that design is used or machined requirement and scrapping, this loses bigger concerning expensive GH4033 high-temperature alloy material.
In the roll off process, pre-strip plate has just begun when rolling owing to embrace the roller skew to its rotation direction one side earlier, the roller of embracing to opposite side is offset again, make pre-strip plate that the phenomenon that swings towards armful roller of its both sides be arranged in the operation of rolling, be subjected to embrace roller and help the reaction force that produces to influence, ring is scrapped by draw down easily.
Summary of the invention
The technical problem to be solved in the present invention provides a kind of method for rolling and shaping that adopts the servo-actuated die sleeve to realize GH4033 high temperature alloy thin-walled ring, and it is high and have a thin-walled ring of good tissue and performance to adopt this method can roll out dimensional accuracy.
For solving the problems of the technologies described above, the method for rolling and shaping of GH4033 high temperature alloy thin-walled ring of the present invention, its technical scheme may further comprise the steps:
The deformation temperature of heating GH4033 high temperature alloy pre-strip plate to 1110 ℃～1130 ℃, the temperature of and preheating servo-actuated die sleeve to 280 ℃～330 ℃;
Described pre-strip plate and servo-actuated die sleeve are put into machine for rolling ring, make pre-strip plate entangle that servo-actuated die sleeve, servo-actuated die sleeve entangle the core roller and along distinguishing tangent the contact between the outer peripheral face of the pre-strip plate of centre-to-centre spacing direction of home roll and core roller and home roll, between the outer peripheral face of the inner ring surface of pre-strip plate and servo-actuated die sleeve and between the outer peripheral face of the inner ring surface of servo-actuated die sleeve and core roller, pre-strip plate is embraced roller by two and is helped at its outer peripheral face, and epicone roller and following awl roller are along these two workpiece of upper and lower end face clamping of servo-actuated die sleeve and pre-strip plate;
Starting machine for rolling ring makes its home roll rotation and drives pre-strip plate, servo-actuated die sleeve, core roller and two armfuls of rollers rotations, simultaneously by machine for rolling ring drive the epicone roller and down the awl roller clamp the servo-actuated die sleeve and pre-strip plate rotates together, the core roller is radially done feed motion and with roll-force under the support of servo-actuated die sleeve the roll off pre-strip plate of home roll with 220KN～4200KN towards the home roll direction, pre-strip plate is with the speed of 5mm/s～8mm/s broadening radially, wall thickness reduces gradually, and its deflection reaches 25%～45% back and become the thin-walled ring by roll off.
And described servo-actuated die sleeve is when design, and its minimum wall thickness (MINI W.) is calculated as follows:
D
0＝L-D
1-R
1-R
2
In the formula: D
0Minimum wall thickness (MINI W.) for the servo-actuated die sleeve;
L is the minimum centers-distance of home roll and core roller;
D
1Radially minimum wall thickness (MINI W.) for the thin-walled ring;
R
1Radius for home roll;
R
2Radius for the core roller.
Adopt the thin-walled ring of above-mentioned method for rolling and shaping roll forming, its wall thickness minimum of a value is 25mm, and the maximum of ratio of height to thickness is 25mm.
Compared with prior art, beneficial effect of the present invention is as follows:
The present invention is the pre-strip plate of GH4033 high temperature alloy that is heated to deformation temperature with after the servo-actuated die sleeve cover of preheating is put into the machine for rolling ring location, radially do feed motion and its distortion is shaped by its core roller, obtained the thin-walled ring of thin-walled and tissue and function admirable with home roll pre-strip plate of roll off under the support of servo-actuated die sleeve towards the home roll direction.
In the roll off process, because the servo-actuated die sleeve has only carried out The pre-heat treatment, it almost can not be out of shape in the operation of rolling.When rolling since between pre-strip plate and core roller every one deck servo-actuated die sleeve, and the servo-actuated die sleeve therewith rotates in pre-strip plate in the same way, overcome between pre-strip plate and the servo-actuated die sleeve owing to produce fierce friction and made the phenomenon that the operation of rolling is unstable and easily cause pre-strip plate temperature to raise, thereby helped that tissue is produced and the acquisition quality forging.
In the roll off process, because the inner ring surface of pre-strip plate is close on the outer peripheral face of servo-actuated die sleeve and therewith in the same way, rotate synchronously, avoided pre-strip plate to be subjected to the influence of core roller rigid parts, thereby avoid it plastic instability to occur and produce phenomenons such as draw down, horn mouth, and with pre-strip plate in the same way, the servo-actuated die sleeve that rotates synchronously also can carry out full circle to the inner ring surface of pre-strip plate and prevent its draw down and phenomenon such as horn mouth occurs, can realize the high ring of precision rolling forming dimension precision, save valuable titanium alloy material.
In the roll off process,, pre-strip plate has been played supported preferably and firm effect, thereby can effectively alleviate pre-strip plate phenomenon that roller swings of embracing towards its both sides in the operation of rolling, prevented that ring from being scrapped by draw down owing to be set with the servo-actuated die sleeve in the pre-strip plate.
The dimensional accuracy of this alloy thin-wall ring has after testing reached 3 ‰ (3/1000ths) of corresponding size.
The room temperature tensile performance of this alloy thin-wall ring after testing, its tensile strength is 1050MPa (greater than the 804MPa of design instructions for use), percentage elongation is that 0.2% o'clock yield strength is 730MPa (greater than the 588MPa of design instructions for use), elongation after fracture be 28% (greater than the design instructions for use 10%), the contraction percentage of area be 36% (greater than the design instructions for use 13%), ballistic work is 677J (greater than the 294J/ of design instructions for use).
The high temperature endurance performance of this alloy thin-wall ring after testing, this alloy rings are that 750 ℃, proof stress are to reach 343MPa, duration in 51 hours disconnectedly in test temperature, have satisfied the design instructions for use.
The metallographic structure of this alloy thin-wall ring has after testing reached the requirement of " aviation superalloy annular spare standard " (GJB 5301) standard.
Description of drawings
Below in conjunction with the drawings and specific embodiments the present invention is described in further detail.
Fig. 1 is the perspective view of the pre-strip plate of GH4033 high temperature alloy.
Fig. 2 is the installation location and the roll off view of servo-actuated die sleeve and pre-strip plate.
Fig. 3 is the perspective view that pre-strip plate roll off becomes the thin-walled ring.
The specific embodiment
The method for rolling and shaping of implementing GH4033 high temperature alloy thin-walled ring of the present invention need provide equipment such as forge furnace, forcing press, machine for rolling ring, manipulator.
The main chemical elements content (percentage by weight) of this alloy is: C content 0.03%～0.08%, contain Cr amount 19.0%～22.0%, contain Al amount 0.60%～1.00%, contain Ti amount 2.40%～2.80%, contain Fe amount≤4.0%, contain B amount≤0.010%, contain Ce amount≤0.010%, contain Mn amount≤0.35%, si content≤0.65%, P content≤0.015%, contain S amount≤0.007%, surplus is Ni.
This alloy is as follows to the processing step of producing qualified thin-walled ring from bar:
Step 1: base.
By the GH4033 high temperature alloy bar of specification blanking through heating, jumping-up, punching, pulling, produce 10 ° of pre-strip plates after rolling in advance, its shape is as shown in Figure 1.
Step 2: installation.
As shown in Figure 2,10 ° of pre-strip plates are heated in forge furnace put into machine for rolling ring after 1110 ℃～1130 ℃ the deformation temperature and lie in (not shown) on the chassis of this machine, pre-10 ° of core rollers 2 that pack into machine for rolling ring of strip plate, the home roll 1 of its outer peripheral face and machine for rolling ring and two tangent contacts of outer peripheral face of embracing rollers 3 are embraced 3 pairs of pre-strip plates of roller for two and are played supporting roles for 10 °; Simultaneously servo-actuated die sleeve 4 is preheating in forge furnace and puts into (not shown) on the chassis that lies in this machine after machine for rolling ring packs into the core roller 2 of machine for rolling ring and is enclosed within 10 ° of the pre-strip plates after 280 ℃～330 ℃, between the outer peripheral face that pre-strip plate is 10 ° and the outer peripheral face of home roll 1, between the outer peripheral face of the inner ring surface of 10 ° of pre-strip plates and servo-actuated die sleeve 4, between the outer peripheral face of the inner ring surface that reaches servo-actuated die sleeve 4 and core roller 2 all along tangent contact of centre-to-centre spacing direction of core roller 2 and home roll 4; Start machine for rolling ring and make its epicone roller 5 and bore roller 6 down, finish the installation location of these two workpiece along servo-actuated die sleeve 4 these two workpiece of upper and lower end face clamping with 10 ° of pre-strip plates.The shipment of workpiece is mainly finished by Robot actions during installation.
Step 3: roll off.
Starting machine for rolling ring makes its home roll 1 rotate by direction shown in Figure 2, home roll 1 drives 10 ° of pre-strip plates, servo-actuated die sleeve 4, core roller 2 and two armfuls of rollers 3 and rotates by direction shown in Figure 2, simultaneously by machine for rolling ring drive epicone roller 5 and down awl roller 6 rotate by direction shown in Figure 2 and in 10 ° of the pre-strip plates and servo-actuated die sleeve 4 operations of rolling upper and lower end face of these two workpiece of clamping, make two of machine for rolling ring to embrace the outer peripheral face that rollers 3 help 10 ° of pre-strip plates; Core roller 2 radially towards home roll 1 direction do feed motion and with home roll 1 with 10 ° of the pre-strip plates of roll-force roll off under the support of servo-actuated die sleeve 4 of 220KN～4200KN, 10 ° of pre-strip plates are with the speed of 5mm/s～8mm/s broadening radially, its wall thickness reduces gradually.
Pre-strip plate is produced the continuous local plastic distortion by roll off for 10 ° under the support of servo-actuated die sleeve 4, being rolled after its deflection reaches 25%～45% is shaped is thin-walled ring 10 (as shown in Figure 3), close machine for rolling ring, the machine for rolling ring cantilever of removing home roll 1, epicone roller 5 after all rotatable parts stop and boring roller 6, two armfuls of rollers 3 down and be pressed in core roller 2 tops takes out thin-walled ring 10 from core roller 2 tops.
Thin-walled ring 10 is carried out solid solution+Ageing Treatment after the finish to gauge, and solution treatment is that thin-walled ring 10 is heated to 1080 ℃, insulation 8h, air cooling; Ageing Treatment is that the thin-walled ring 10 of solution treatment is cooled to 775 ℃, insulation 16h, air cooling.
In above-mentioned steps 1 and step 3, the finish-forging of this alloy or finishing temperature are not less than 950 ℃.
The computational methods of described deflection are: deflection=[(10 ° of the pre-strip plates longitudinal section area along the longitudinal section area-thin-walled ring 10 of center line along center line)/pre-10 ° of longitudinal section areas along center line of strip plate] * 100%.
In the rolling process, can in this die sleeve, fully be out of shape shaping for 10 ° for guaranteeing servo-actuated die sleeve 4 indeformable and pre-strip plate in the operation of rolling, the minimum wall thickness (MINI W.) of this die sleeve carries out designing and calculating by following formula:
D
0＝L-D
1-R
1-R
2
In the formula: D
0Minimum wall thickness (MINI W.) for servo-actuated die sleeve 4;
L is the minimum centers-distance of home roll 1 and core roller 2;
D
1Radially minimum wall thickness (MINI W.) for thin-walled ring 10;
R
1Radius for home roll 1;
R
2Radius for core roller 2.
Adopt this rolling alloy thin-wall ring 10 of above-mentioned roll off method, its minimum wall thickness (MINI W.) can reach 25mm, and high thick (referring to wall thickness) can reach 25mm than maximum.
After testing, adopt the GH4033 high temperature alloy thin-walled ring 10 of said method rolling and shaping to have high dimension precision and good interior tissue and performance, satisfied the design instructions for use of this alloy rings fully.
Claims (3)
1. the method for rolling and shaping of a GH4033 high temperature alloy thin-walled ring is characterized in that, may further comprise the steps:
The deformation temperature of heating GH4033 high temperature alloy pre-strip plate to 1110 ℃～1130 ℃, the temperature of and preheating servo-actuated die sleeve to 280 ℃～330 ℃;
Described pre-strip plate and servo-actuated die sleeve are put into machine for rolling ring, make pre-strip plate entangle that servo-actuated die sleeve, servo-actuated die sleeve entangle the core roller and along distinguishing tangent the contact between the outer peripheral face of the pre-strip plate of centre-to-centre spacing direction of home roll and core roller and home roll, between the outer peripheral face of the inner ring surface of pre-strip plate and servo-actuated die sleeve and between the outer peripheral face of the inner ring surface of servo-actuated die sleeve and core roller, pre-strip plate is embraced roller by two and is helped at its outer peripheral face, and epicone roller and following awl roller are along these two workpiece of upper and lower end face clamping of servo-actuated die sleeve and pre-strip plate;
Starting machine for rolling ring makes its home roll rotation and drives pre-strip plate, servo-actuated die sleeve, core roller and two armfuls of rollers rotations, simultaneously by machine for rolling ring drive the epicone roller and down the awl roller clamp the servo-actuated die sleeve and pre-strip plate rotates together, the core roller is radially done feed motion and with roll-force under the support of servo-actuated die sleeve the roll off pre-strip plate of home roll with 220KN～4200KN towards the home roll direction, pre-strip plate is with the speed of 5mm/s～8mm/s broadening radially, wall thickness reduces gradually, and its deflection reaches 25%～45% back and become the thin-walled ring by roll off.
2. method for rolling and shaping according to claim 1 is characterized in that: the minimum wall thickness (MINI W.) of described servo-actuated die sleeve carries out designing and calculating by following formula:
D
0＝L-D
1-R
1-R
2
In the formula: D
0Minimum wall thickness (MINI W.) for the servo-actuated die sleeve;
L is the minimum centers-distance of home roll and core roller;
D
1Radially minimum wall thickness (MINI W.) for the thin-walled ring;
R
1Radius for home roll;
R
2Radius for the core roller.
3. method for rolling and shaping according to claim 1 is characterized in that: the wall thickness minimum of a value of described thin-walled ring is 25mm, and the maximum of ratio of height to thickness is 25mm.
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|---|---|---|---|
| CN2010105821942A CN102085556B (en) | 2010-12-10 | 2010-12-10 | Roll forming method of GH4033 high-temperature alloy thin-wall ring piece |
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|---|---|---|---|
| CN2010105821942A CN102085556B (en) | 2010-12-10 | 2010-12-10 | Roll forming method of GH4033 high-temperature alloy thin-wall ring piece |
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| CN102085556B CN102085556B (en) | 2012-08-15 |
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Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108907044A (en) * | 2018-07-27 | 2018-11-30 | 贵州航天新力铸锻有限责任公司 | The i shaped steel molding die of nuclear fusion stack magnet support |
| CN109530607A (en) * | 2018-12-28 | 2019-03-29 | 贵州航宇科技发展股份有限公司 | A kind of 718plus forging special-shape ring manufacturing process |
| CN111036808A (en) * | 2019-12-31 | 2020-04-21 | 王飞 | Processing method of Ti1023 alloy special-shaped ring piece |
| CN111215567A (en) * | 2019-12-06 | 2020-06-02 | 陕西宏远航空锻造有限责任公司 | Forging method for improving grain size of GH4099 high-temperature alloy thin-wall ring |
| CN112024795A (en) * | 2020-09-25 | 2020-12-04 | 洛阳Lyc轴承有限公司 | Profiling grinding and expanding method and device for inner diameter of large annular forging |
| CN113680933A (en) * | 2021-08-27 | 2021-11-23 | 中国兵器工业第五九研究所 | Forming method of thin-wall magnesium alloy ring piece |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| SU282280A1 (en) * | А. В. Крупин, В. Рощин, В. М. Изотов , Гщщп | |||
| GB1292216A (en) * | 1970-01-21 | 1972-10-11 | Franz Donatu Timmermans | A method of rolling a cylinder |
| JPS4826665A (en) * | 1971-08-12 | 1973-04-07 | ||
| CN101284296A (en) * | 2008-04-23 | 2008-10-15 | 贵州航宇科技发展有限公司 | Rolling and shaping method of titanium alloy taper ring forged piece |
-
2010
- 2010-12-10 CN CN2010105821942A patent/CN102085556B/en active Active
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| SU282280A1 (en) * | А. В. Крупин, В. Рощин, В. М. Изотов , Гщщп | |||
| GB1292216A (en) * | 1970-01-21 | 1972-10-11 | Franz Donatu Timmermans | A method of rolling a cylinder |
| JPS4826665A (en) * | 1971-08-12 | 1973-04-07 | ||
| CN101284296A (en) * | 2008-04-23 | 2008-10-15 | 贵州航宇科技发展有限公司 | Rolling and shaping method of titanium alloy taper ring forged piece |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108907044A (en) * | 2018-07-27 | 2018-11-30 | 贵州航天新力铸锻有限责任公司 | The i shaped steel molding die of nuclear fusion stack magnet support |
| CN109530607A (en) * | 2018-12-28 | 2019-03-29 | 贵州航宇科技发展股份有限公司 | A kind of 718plus forging special-shape ring manufacturing process |
| CN111215567A (en) * | 2019-12-06 | 2020-06-02 | 陕西宏远航空锻造有限责任公司 | Forging method for improving grain size of GH4099 high-temperature alloy thin-wall ring |
| CN111036808A (en) * | 2019-12-31 | 2020-04-21 | 王飞 | Processing method of Ti1023 alloy special-shaped ring piece |
| CN111036808B (en) * | 2019-12-31 | 2021-06-15 | 王飞 | Processing method of Ti1023 alloy special-shaped ring piece |
| CN112024795A (en) * | 2020-09-25 | 2020-12-04 | 洛阳Lyc轴承有限公司 | Profiling grinding and expanding method and device for inner diameter of large annular forging |
| CN113680933A (en) * | 2021-08-27 | 2021-11-23 | 中国兵器工业第五九研究所 | Forming method of thin-wall magnesium alloy ring piece |
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| CN102085556B (en) | 2012-08-15 |
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Address after: 550081 Bashang mountain road, Jinyang national hi tech Industrial Development Zone, Guizhou, Guiyang Applicant after: Guizhou Aviation Technical Development Co.,Ltd. Address before: 550081 Bashang mountain road, Jinyang national hi tech Industrial Development Zone, Guizhou, Guiyang Applicant before: Guizhou Aviation Technical Development Co.,Ltd. |
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Inventor after: Wu Yongan Inventor after: Lu Manyu Inventor after: Liu Chaohui Inventor after: Huang Pan Inventor after: Yang Lianghui Inventor before: Wu Yongan Inventor before: Zhang Hua Inventor before: Lu Manyu Inventor before: Liu Chaohui Inventor before: Huang Pan Inventor before: Yang Lianghui |
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Denomination of invention: Roll forming method of GH4033 high-temperature alloy thin-wall ring piece Effective date of registration: 20140516 Granted publication date: 20120815 Pledgee: Bank of Guiyang Limited by Share Ltd. high tech branch Pledgor: Guizhou Aviation Technical Development Co.,Ltd. Registration number: 2014990000363 |
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Denomination of invention: Roll forming method of GH4033 high-temperature alloy thin-wall ring piece Effective date of registration: 20170725 Granted publication date: 20120815 Pledgee: Bank of Guiyang Limited by Share Ltd. high tech branch Pledgor: Guizhou Aviation Technical Development Co.,Ltd. Registration number: 2017990000680 |
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Denomination of invention: Rolling forming method of GH4033 superalloy thin wall ring Effective date of registration: 20200930 Granted publication date: 20120815 Pledgee: Guanshanhu sub branch of Guiyang Bank Co.,Ltd. Pledgor: Guizhou Aviation Technical Development Co.,Ltd. Registration number: Y2020520000017 |
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