CN102029342B - Method for rolling and forming TC11 titanium alloy thin-walled rings - Google Patents
Method for rolling and forming TC11 titanium alloy thin-walled rings Download PDFInfo
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- CN102029342B CN102029342B CN201010582213A CN201010582213A CN102029342B CN 102029342 B CN102029342 B CN 102029342B CN 201010582213 A CN201010582213 A CN 201010582213A CN 201010582213 A CN201010582213 A CN 201010582213A CN 102029342 B CN102029342 B CN 102029342B
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- 238000005096 rolling process Methods 0.000 title claims abstract description 61
- 238000000034 method Methods 0.000 title claims abstract description 27
- 229910001069 Ti alloy Inorganic materials 0.000 title claims abstract description 23
- 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
- 230000009466 transformation Effects 0.000 claims description 4
- 230000008520 organization Effects 0.000 abstract 1
- 239000000956 alloy Substances 0.000 description 19
- 229910045601 alloy Inorganic materials 0.000 description 17
- 238000005242 forging Methods 0.000 description 5
- 238000009434 installation Methods 0.000 description 4
- 230000008602 contraction 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
- 238000004080 punching Methods 0.000 description 2
- 208000004350 Strabismus Diseases 0.000 description 1
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical group [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 1
- 238000000137 annealing Methods 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 229910052729 chemical element Inorganic materials 0.000 description 1
- 238000000205 computational method Methods 0.000 description 1
- 239000013078 crystal Substances 0.000 description 1
- 230000002950 deficient Effects 0.000 description 1
- 238000001514 detection method Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000007774 longterm Effects 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 239000010936 titanium Substances 0.000 description 1
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Abstract
The invention discloses a method for rolling and forming TC11 titanium alloy thin-walled rings, which is used for rolling and forming thin-walled rings with high size precision and good organization and performance. The method comprises the following steps: firstly, nesting a pre-rolled titanium alloy billet which is heated to a deformation temperature and a preheated follow-up die sleeve into a ring rolling mill, and positioning the follow-up die sleeve and pre-rolled billet by a main roller, a core roller, a holding roller, an upper cone roller and a lower cone roller of the ring rolling mill, wherein the follow-up die sleeve is nested in the pre-rolled billet; and then, starting up the ring rolling mill to enable the core roller to make a feed motion radially towards the direction of the main roller and roll the pre-rolled billet together with the main roller by the rolling force of 200KN-4000KN under the support of the follow-up die sleeve, so that the width of the pre-rolled billet is expanded radially at aspeed of 5-10mm/s, the wall thickness of the pre-rolled billet is gradually reduced, and after the deformation of the pre-rolled billet reaches 25%-45%, the pre-rolled billet is rolled into a thin-walled ring. The minimum value of the wall thickness of the titanium alloy thin-walled ring rolled by the method is 25, and the maximum value of the height-to-thickness ratio thereof is 25 mm. The ring is mainly used for components of revolved bodies such as cylindrical shells and the like used in the fields of aviation 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 TC11 titanium alloy thin wall ring.
Background technology
The TC11 titanium alloy is the good diphasic titanium alloy of a kind of combination property; 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; Thin-walled ring such as aero-engine drum barrel for example, require when long-term work below 500 ℃, to have excellent heat resistance can and higher room temperature strength.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 101279345A disclosed a kind of method for rolling and shaping of alloy special-shaped titanium ring; This method by the alloy bar of specification blanking through jumping-up, punching, roll ring base (not using the roll off mould) for twice; Put into rolling and shaping in the machine for rolling ring roll off mould to blank again; Through 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 TC11 titanium alloy thin wall 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; The pass of roll off mould and produce in advance fierce friction between the strip plate and make not only that the operation of rolling is very unstable to impact production when rolling; But also cause preparatory strip plate temperature to raise easily alloy organizing and performance are exerted an influence, like defectives such as tissue occurring and make a variation, crystal grain is thick.
When the TC11 titanium alloy thin wall ring of home roll that adopts said method and direct use machine for rolling ring and core rolling system (encircling base) thin-walled like rolling in the above-mentioned method; Owing to receive 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; Be prone to cause preparatory 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 TC11 titanium alloy material.
In the roll off process; In advance 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 squints again; Make preparatory strip plate that the phenomenon that roller swings of embracing towards its both sides arranged in the operation of rolling, receive 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 that the present invention will solve provides a kind of method for rolling and shaping that adopts the servo-actuated die sleeve to realize TC11 titanium alloy thin wall 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 TC11 titanium alloy thin wall ring according to the invention, its technical scheme may further comprise the steps:
Heating TC11 titanium alloy preparatory strip plate is to 20 ℃～30 ℃ deformation temperature below the transformation temperature, the temperature of and preheating servo-actuated die sleeve to 250 ℃～300 ℃;
Put into machine for rolling ring to said preparatory strip plate and servo-actuated die sleeve; Make preparatory strip plate entangle that servo-actuated die sleeve, servo-actuated die sleeve entangle the core roller and along between the outer peripheral face of the preparatory strip plate of centre-to-centre spacing direction of home roll and core roller and home roll, distinguish tangent the contact between the outer peripheral face of inner ring surface and the servo-actuated die sleeve of strip plate and between the outer peripheral face of the inner ring surface of servo-actuated die sleeve and core roller in advance; Strip plate is embraced roller in its outer peripheral face support by two in advance, epicone roller and the upper and lower end face clamping servo-actuated die sleeve and preparatory strip plate of following awl roller along servo-actuated die sleeve and preparatory strip plate;
Starting machine for rolling ring makes its home roll rotation and drives preparatory strip plate, servo-actuated die sleeve, core roller and two armfuls of rollers rotations; Grasping the servo-actuated die sleeve by machine for rolling ring driving epicone roller and following awl roller simultaneously rotates with preparatory strip plate together; The core roller is radially done feed motion and with roll-force under the support of servo-actuated die sleeve the roll off preparatory strip plate of home roll with 200KN～4000KN towards the home roll direction; In advance strip plate is with the speed of 5mm/s～10mm/s broadening radially; Wall thickness reduces gradually, and its deflection reaches 25%～45% back and become the thin-walled ring by roll off.
And said 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 25.
Compared with prior art, beneficial effect of the present invention is following:
The present invention is the preparatory strip plate of TC11 titanium 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 preparatory 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 in advance between strip plate and the core roller at a distance from one deck servo-actuated die sleeve; And the servo-actuated die sleeve is therewith rotating in the strip plate in advance in the same way; Overcome between preparatory strip plate and the servo-actuated die sleeve since produce fierce friction make the operation of rolling unstable with the phenomenon that is prone to cause preparatory strip plate temperature to raise, thereby help that tissue is produced and the acquisition quality forging.
In the roll off process; Because in advance the inner ring surface of strip plate is close on the outer peripheral face of servo-actuated die sleeve and therewith in the same way, rotate synchronously; Avoided preparatory strip plate to receive 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 preparatory 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 preparatory 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, saves valuable titanium alloy material.
In the roll off process,, preparatory strip plate has been played supported preferably and firm effect, thereby can effectively alleviate preparatory 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 in advance be set with the servo-actuated die sleeve in the strip plate.
Through detecting the dimensional accuracy of this alloy thin-wall ring, 3 ‰ (3/1000ths) of corresponding size have been reached.
Through detecting the room temperature tensile performance of this alloy thin-wall ring; Its tensile strength is 1060MPa～1100MPa (having satisfied the design instructions for use); Percentage elongation is that 0.2% o'clock yield strength is 955MPa～1000MPa (greater than the 910MPa of design instructions for use); Elongation after fracture be 12%～16% (greater than the design instructions for use 8%), the contraction percentage of area be 23.5%～27% (greater than the design instructions for use 23%), ballistic work is 48～61J (greater than the 23.5J of design instructions for use).
Through the high temperature tensile properties of this alloy thin-wall ring of detection at 500 ℃; Its tensile strength is 725MPa～770MPa (greater than the 715MPa of design instructions for use); Elongation after fracture be 14%～19.5% (greater than the design instructions for use 12%), the contraction percentage of area be 52%～70.5% (greater than the design instructions for use 40%).
Through detecting the enduring quality of this alloy thin-wall ring, this alloy forged piece is that 500 ℃, proof stress are to reach 640MPa, duration in 36 hours disconnectedly in test temperature, has satisfied the design instructions for use.
Through detecting the metallographic structure of this alloy thin-wall ring, reached the requirement of " annular titanium alloy forging " (HB 7238) aviation industry standards.
Description of drawings
Below in conjunction with the accompanying drawing and the specific embodiment the present invention is done further explain.
Fig. 1 is the perspective view of the preparatory strip plate of TC11 titanium alloy.
Fig. 2 is the installation location and the roll off view of servo-actuated die sleeve and preparatory strip plate.
Fig. 3 is the perspective view that preparatory strip plate roll off becomes the thin-walled ring.
The specific embodiment
The method for rolling and shaping of the described TC11 titanium alloy thin wall of embodiment of the present invention ring 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: contain Al amount 5.8%～7.0%, contain Mo amount 2.8%～3.8%, contain Zr amount 0.8%～2.0%, si content 0.2%～0.35%, contain Fe amount≤0.25%, C content≤0.10%, contain N amount≤0.05%, contain H amount≤0.012%, contain O amount≤0.15%, other elements are single≤0.10% and summation≤0.40%, surplus be Ti.
This alloy is following to the processing step of producing qualified thin-walled ring from bar:
Step 1: base.
By the TC11 titanium alloy bar of specification blanking through heating, jumping-up, punching, pulling, produce 10 ° of preparatory strip plates after rolling in advance, its shape is as shown in Figure 1.
Step 2: installation.
As shown in Figure 2; In forge furnace, be heated to 10 ° of preparatory strip plates below the transformation temperature and put into machine for rolling ring after 20 ℃～30 ℃ the deformation temperature and to lie in (not shown) on the chassis of this machine; Preparatory 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 preparatory strip plates of roller for two and are played supporting roles for 10 °; In forge furnace, be preheating to servo-actuated die sleeve 4 simultaneously and put 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 preparatory strip plates after 250 ℃～300 ℃, in advance between the outer peripheral face of the outer peripheral face of 10 ° of strip plates and home roll 1, in advance between the outer peripheral face of inner ring surface and the servo-actuated die sleeve 4 of 10 ° of strip plates, 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; The startup machine for rolling ring makes its epicone roller 5 and the upper and lower end face clamping servo-actuated die sleeve 4 and preparatory strip plate 10 ° of following awl roller 6 along servo-actuated die sleeve 4 and 10 ° of preparatory strip plates, the installation location of accomplishing servo-actuated die sleeve 4 and 10 ° of preparatory strip plates.The shipment of workpiece is mainly accomplished through 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 preparatory 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 drive by machine for rolling ring that epicone roller 5 rotates by direction shown in Figure 2 with awl roller 6 down and in 10 ° of strip plates in advance 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 preparatory strip plates; Core roller 2 radially towards home roll 1 direction do feed motion and with home roll 1 with 10 ° of the preparatory strip plates of roll-force roll off under the support of servo-actuated die sleeve 4 of 200KN～4000KN; In advance 10 ° of strip plates are with the speed of 5mm/s～10mm/s broadening radially, and its wall thickness reduces gradually.
Strip plate is produced the continuous local plastic distortion by roll off for 10 ° under the support of servo-actuated die sleeve 4 in advance; After its deflection reaches 25%～45%, being rolled 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 the double annealing processing after the finish to gauge, promptly is heated to 950 ℃ to thin-walled ring 10, presses wall thickness insulation 1～2h; With stove air cooling to 530 ℃, insulation 6h, air cooling.
In above-mentioned steps 1 and step 3, the finish-forging of this alloy or finishing temperature are not less than 850 ℃; In the present embodiment, it is 1005 ℃ through the transformation temperature that detects this alloy.
The computational methods of said deflection are: deflection=[(in advance 10 ° of the strip plates longitudinal section area along the longitudinal section area-thin-walled ring 10 of center line along center line)/in advance 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 preparatory 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 25 than maximum.
Through detecting, adopt the TC11 titanium alloy thin wall 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 forged piece fully.
Claims (3)
1. the method for rolling and shaping of a TC11 titanium alloy thin wall ring is characterized in that, may further comprise the steps:
Heating TC11 titanium alloy preparatory strip plate is to 20 ℃～30 ℃ deformation temperature below the transformation temperature, the temperature of and preheating servo-actuated die sleeve to 250 ℃～300 ℃;
Put into machine for rolling ring to said preparatory strip plate and servo-actuated die sleeve; Make preparatory strip plate entangle the servo-actuated die sleeve, the servo-actuated die sleeve entangles the core roller; And centre-to-centre spacing direction along home roll and core roller; In advance between the outer peripheral face of strip plate and home roll, distinguish tangent the contact between the outer peripheral face of the inner ring surface of 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 in advance; Strip plate is embraced roller in its outer peripheral face support by two in advance, epicone roller and the upper and lower end face clamping servo-actuated die sleeve and preparatory strip plate of following awl roller along servo-actuated die sleeve and preparatory strip plate;
Starting machine for rolling ring makes its home roll rotation and drives preparatory strip plate, servo-actuated die sleeve, core roller and two armfuls of rollers rotations; Simultaneously driving the special servo-actuated die sleeve of living of epicone roller and awl roller folder down by machine for rolling ring rotates with strip plate in advance together; The core roller is radially done feed motion and with roll-force under the support of servo-actuated die sleeve the roll off preparatory strip plate of home roll with 200KN～4000KN towards the home roll direction; In advance strip plate is with the speed of 5mm/s～10mm/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 said 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 said thin-walled ring is 25mm, and the maximum of ratio of height to thickness is 25.
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201010582213A CN102029342B (en) | 2010-12-10 | 2010-12-10 | Method for rolling and forming TC11 titanium alloy thin-walled rings |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201010582213A CN102029342B (en) | 2010-12-10 | 2010-12-10 | Method for rolling and forming TC11 titanium alloy thin-walled rings |
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| CN102029342A CN102029342A (en) | 2011-04-27 |
| CN102029342B true CN102029342B (en) | 2012-09-05 |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105396998A (en) * | 2015-12-02 | 2016-03-16 | 贵州安大航空锻造有限责任公司 | Rolling method of isotropic alpha-phase titanium alloy rectangular ring piece |
| CN105382156A (en) * | 2015-12-02 | 2016-03-09 | 贵州安大航空锻造有限责任公司 | Isotropic rolling method for alpha-beta two-phase titanium alloy rectangular ring piece |
| CN114289677A (en) * | 2021-12-15 | 2022-04-08 | 陕西宏远航空锻造有限责任公司 | Rolling forming method for titanium alloy non-uniform-thickness special-shaped thin-wall ring piece |
Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB1292216A (en) * | 1970-01-21 | 1972-10-11 | Franz Donatu Timmermans | A method of rolling a cylinder |
| 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 |
Family Cites Families (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS4826665A (en) * | 1971-08-12 | 1973-04-07 |
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Patent Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB1292216A (en) * | 1970-01-21 | 1972-10-11 | Franz Donatu Timmermans | A method of rolling a cylinder |
| 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 |
Non-Patent Citations (1)
| Title |
|---|
| JP特开昭48-26665A 1973.04.07 |
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Denomination of invention: Method for rolling and forming TC11 titanium alloy thin-walled rings Effective date of registration: 20140516 Granted publication date: 20120905 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: Method for rolling and forming TC11 titanium alloy thin-walled rings Effective date of registration: 20170725 Granted publication date: 20120905 Pledgee: Bank of Guiyang Limited by Share Ltd. high tech branch Pledgor: Guizhou Aviation Technical Development Co.,Ltd. Registration number: 2017990000682 |
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Date of cancellation: 20200924 Granted publication date: 20120905 Pledgee: Bank of Guiyang Limited by Share Ltd. high tech branch Pledgor: Guizhou Aviation Technical Development Co.,Ltd. Registration number: 2017990000682 |
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Denomination of invention: Rolling forming method of TC11 titanium alloy thin wall ring Effective date of registration: 20200930 Granted publication date: 20120905 Pledgee: Guanshanhu sub branch of Guiyang Bank Co.,Ltd. Pledgor: Guizhou Aviation Technical Development Co.,Ltd. Registration number: Y2020520000016 |
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Date of cancellation: 20230322 Granted publication date: 20120905 Pledgee: Guanshanhu sub branch of Guiyang Bank Co.,Ltd. Pledgor: Guizhou Aviation Technical Development Co.,Ltd. Registration number: Y2020520000016 |