CN1383943A - Superplastic forming process of titanium alloy corrugated pipe - Google Patents
Superplastic forming process of titanium alloy corrugated pipe Download PDFInfo
- Publication number
- CN1383943A CN1383943A CN 02121323 CN02121323A CN1383943A CN 1383943 A CN1383943 A CN 1383943A CN 02121323 CN02121323 CN 02121323 CN 02121323 A CN02121323 A CN 02121323A CN 1383943 A CN1383943 A CN 1383943A
- Authority
- CN
- China
- Prior art keywords
- pipe
- titanium alloy
- make
- superplastic forming
- mould
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
Images
Landscapes
- Shaping Metal By Deep-Drawing, Or The Like (AREA)
Abstract
The present invention relates to the fabrication of corrugated pipe and corrugated expansion joint. The corrugated pipe and corrugated expansion joint is fabricated through the following steps: making a sealed pipe blank with seamless or welded titanium alloy pipe; heating the pipe blank to 650-1000 inside a multilayer structure mold; filling the pipe blank with 0.1-1 MPa pressure gas to make the pipe blank expand and form; applying axial pressure to close molds; and forming by further increased pressure of 1.5-3.0 MPa and cooling and demolding to obtain product. The product can bear relatively higher inner pressure and has high precision.
Description
Technical field: type of the present invention relates to the manufacture method of a kind of bellows and corrugated-type expansion joint.
Background technology: titanium alloy is a kind of natural superplastic material, and many titanium alloys just have a stable fine grained texture that waits at industry supply of material state.With regard to present result of study, alpha titanium alloy, beta-titanium alloy and alpha+beta titanium alloys all can be realized superplasticity to some extent, wherein be best especially with the alpha+beta titanium alloys, the percentage elongation of Ti-6Al-4V can reach more than 1000%, but the cold-forming property of titanium alloy is very poor.At present, the preparation method of bellows and corrugated-type expansion joint has methods such as hydroforming, rolling forming, mechanical bulging, welding forming and deposition formation.The deposition formation method can only be produced the nickel material; The bellows of welding forming and corrugated-type expansion joint can not bear interior pressure, thereby are not suitable for using on the pressure vessel; Because the cold deformation drag of titanium is big, resilience serious, plasticity is not high, cold-forming property is poor, thereby is not suitable for the processing method of hydroforming, rolling forming and mechanical bulging.
Summary of the invention: the method that the invention provides a kind of titanium alloy corrugated pipe superplastic forming.This method is suitable for titanium alloy corrugated tube and corrugated-type expansion joint are processed, and bellows of being processed and corrugated-type expansion joint can bear bigger interior pressure, and the forming accuracy height.Manufacturing process of the present invention is undertaken by following step: a, making pipe, and titanium alloy seamless pipe or welded tube are made the pipe of a sealing, and at one end leave inflation inlet; B, heating process are packed pipe in the mould of multilayer film structure into, subsequently with heating of pipe blank to 650~1000 ℃ of the superplastic forming temperature of titanium alloy; C, bulging process charge into gas in pipe, the pressure that charges into gas is 0.1~1MPa, make the outside bulging of pipe; D, matched moulds process to applying compressive load, make each module pressing at mould shaft; E, forming process, continuing increases air pressure in pipe, make its pressure reach 1.5~3.0MPa, makes the complete mold filling of pipe, after cooling and demolding is promptly made finished product.The gas that charges in pipe in the bulging process is inert gas or nitrogen.After in above-mentioned bulging process, in pipe, charging into gas, need pressurize 10~60 minutes.In above-mentioned forming process, in pipe, after the pressurization, need pressurize 5~30 minutes.Bulging process and matched moulds process are carried out simultaneously.The objective of the invention is to utilize titanium alloy at high temperature to have this character of superplasticity, the method of the compound superplastic forming that adopts superplastic gas-bulging and axially load is produced titanium alloy corrugated pipe and corrugated-type expansion joint, thereby provides a kind of economy, effective, practical production technology for the shaping of titanium alloy corrugated pipe and corrugated-type expansion joint.The present invention is suitable for making and has superplastic titanium alloy U-shaped bellows and wave mode expansion joint, and its nominal pressure is less than 2.5MPa, and its diameter is unrestricted.The present invention is particularly suitable for processing the big expansion joint of depth of convolution parameter.Manufacturing process of the present invention is compared with welding forming, and can bear than imperial palace and press, and the forming accuracy height; Compare with mechanical bulging with rolling forming, equipment is simpler, yield rate is high, cost is low.In the process of the present invention, because the pressure of pressurization bulging process is generally greater than several times of operating pressure, so drip molding need not carry out pressure detecting, and do not have residual stress; Because the pressure when being shaped is less, so the long service life of mould.
Description of drawings: Fig. 1 is the structural representation of heating process in the specific embodiment one, Fig. 2 is the structural representation of bulging process in the specific embodiment one, Fig. 3 is the structural representation of matched moulds process and forming process in the specific embodiment one, Fig. 4 is the sectional view of bellows, and Fig. 5 is the A-A cutaway view of Fig. 1.
The specific embodiment one: the pipe of present embodiment is to adopt the thick Ti-6Al-4V annealed state thin plate of 1.28mm to make the pipe 6 of upper-lower seal, in pipe 6 lower ends inflation inlet 6-1 is arranged.Heating process is to carry out (consulting Fig. 1) in the superplastic forming machine, the superplastic forming machine by body of heater 2, the pressure head 1 that is located at body of heater 2 tops, the upper cover plate 8 that is connected with pressure head 1, be located at the bracing frame 11 of body of heater 2 inside and the base plates 9 that are connected above the bracing frame 11 are formed.Mould adopts the mould of multilayer film structure, and its module number adds 1 for the ripple number, and counterdie 5 is positioned on the base plate 9, and patrix 3 is installed in loam cake 8 times, and middle mould 4 adopts the split-type structure, so that the demoulding (referring to Fig. 5).Before the dress mould, pipe 6 outer surfaces are coated high-temperature anti-oxidant, at high temperature not oxidized with the protection titanium alloy, and on mould with bellows contact position graphite spraying powder, its purpose one is to reduce the friction of mould and pipe, improves evenness of wall thickness; The 2nd, be convenient to the drip molding demoulding.With pipe 6 installations, at first counterdie 5 and base plate 9 are welded together then, the inflation inlet 6-1 with pipe 6 welds together with breather pipe 10, and draws by groove between base plate.Middle mould 4 with the split-type structure is assembled together again, and is sleeved on the outside of pipe 6, and patrix 3 is installed at last, and with pull bar 12 patrix 3, middle mould 4 and counterdie 6 is connected.Pipe 6 after the assembling is sent in the superplastic forming machine.Next step is pipe 6 to be heated to 927 ℃ of the superplastic forming temperature of titanium alloy, and is incubated 1 hour.The gas that charges in pipe 6 in the bulging process is argon gas, and its pressure is 0.2MPa, and pressurize 30 minutes, makes pipe 6 produce suitable plastic deformation, and this moment, single ripple bus length of pipe 6 was slightly less than single ripple bus long (consulting Fig. 2) of institute's machining bellows.The size of bulging stage inner barrel forming pressure and will coordinating between pressing time, low as forming pressure, pressing time is short, then after the mould pressing, the ripple nose part continues bulging and causes local wall thickness attenuate amount excessive away from mould, and the bellows wall unevenness is even, otherwise long when shaping pressure height, pressing time, cause that like this barrel distortion amount is excessive so that can not matched moulds.The pressure head 1 that makes the superplastic forming machine in the matched moulds process makes patrix 3, middle mould 4, counterdie 5 pressings slowly to pressing down.In forming process, continuation aerating in pipe 6 is depressed into 3MPa, and pressurize 10 minutes, make the complete mold filling of pipe (consulting Fig. 3), last shaping stage air pressure is suitable, and is excessive as air pressure, it is not tight that the upper, middle and lower mould is closed, influence the precision of drip molding, too small as air pressure, then cause the high commissure of intensity mold filling deficiency.Last step is the argon gas of emitting in the bellows 7 of shaping, lifts forcing press, make in the body of heater 1 and be cooled to room temperature, and the demoulding of coming out of the stove.
The specific embodiment two: what present embodiment and the specific embodiment one were different is that it is undertaken by following step: a, make pipe, titanium alloy seamless pipe or welded tube are made the pipe of a sealing, and at one end leave inflation inlet; B, heating process are packed pipe in the mould of multilayer film structure into, subsequently with heating of pipe blank to 650~1000 ℃ of the superplastic forming temperature of titanium alloy; C, bulging matched moulds process charge into gas in pipe, the pressure that charges into gas is 0.1~1MPa, make the outside bulging of pipe, and simultaneously at mould shaft to applying compressive load, make each module pressing; D, forming process, continuing increases air pressure in pipe, make its pressure reach 1.5~3.0MPa, makes the complete mold filling of pipe, after cooling and demolding is promptly made finished product.Other method and parameter are identical with the specific embodiment one.
The size and dimension of above-mentioned mould inside is identical with the size and dimension of bellows, and the die joint place of each module is positioned at the crest place of each ripple of bellows.Distance L between each module is pressed following formula and is determined: L=π (r
1+ r
2+ t)+2a-2w; The size of pipe is determined by following formula: the height H of pipe=nf[π (r
1+ r
2+ t)+2a]+2L
4+ C, the wall thickness t of pipe
0=mt; W in the formula-bellows pitch of waves, n-corrugated tube wave number, t-bellows wall thickness, r
1-bellows crest radius, r
2-bellows trough radius, a-bellows crest, trough transition region vertical wall section length, L
4-bellows straight section length, C-(get 10~20mm), m-coefficient (getting 1.1~1.25), f-coefficient (getting 0.95~0.98) because of the allowance that end cap stayed of removing pipe.
Claims (7)
1, the method for titanium alloy corrugated pipe superplastic forming is characterized in that it is undertaken by following step: a, make pipe, titanium alloy seamless pipe or welded tube are made the pipe of a sealing, and at one end leave inflation inlet; B, heating process are packed pipe in the mould of multilayer film structure into, subsequently with heating of pipe blank to 650~1000 ℃ of the superplastic forming temperature of titanium alloy; C, bulging process charge into gas in pipe, the pressure that charges into gas is 0.1~1MPa, make the outside bulging of pipe; D, matched moulds process to applying compressive load, make each module pressing at mould shaft; E, forming process, continuing increases air pressure in pipe, make its pressure reach 1.5~3.0MPa, makes the complete mold filling of pipe, after cooling and demolding is promptly made finished product.
2, the method for titanium alloy corrugated pipe superplastic forming according to claim 1 after it is characterized in that charging into gas in pipe in above-mentioned bulging process, needs pressurize 10~60 minutes.
3, the method for titanium alloy corrugated pipe superplastic forming according to claim 1 is characterized in that in above-mentioned forming process, after the pressurization, needs pressurize 5~30 minutes in pipe.
4, the method for titanium alloy corrugated pipe superplastic forming according to claim 1, mould 4 adopts the split-type structure in it is characterized in that.
5, the method for titanium alloy corrugated pipe superplastic forming according to claim 1, it is characterized in that the dress mould before, pipe (6) outer surface is coated high-temperature anti-oxidant, and on mould with bellows contact position graphite spraying powder.
6, the method for titanium alloy corrugated pipe superplastic forming according to claim 1 is characterized in that the gas that charges in the bulging process is inert gas or nitrogen in pipe (6).
7, the method for titanium alloy corrugated pipe superplastic forming is characterized in that it is undertaken by following step: a, make pipe, titanium alloy seamless pipe or welded tube are made the pipe of a sealing, and at one end leave inflation inlet; B, heating process are packed pipe in the mould of multilayer film structure into, subsequently with heating of pipe blank to 650~1000 ℃ of the superplastic forming temperature of titanium alloy; C, bulging matched moulds process charge into gas in pipe, the pressure that charges into gas is 0.1~1MPa, make the outside bulging of pipe, and simultaneously at mould shaft to applying compressive load, make each module pressing; D, forming process, continuing increases air pressure in pipe, make its pressure reach 1.5~3.0MPa, makes the complete mold filling of pipe, after cooling and demolding is promptly made finished product.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CNB021213232A CN1193839C (en) | 2002-06-14 | 2002-06-14 | Superplastic forming process of titanium alloy corrugated pipe |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CNB021213232A CN1193839C (en) | 2002-06-14 | 2002-06-14 | Superplastic forming process of titanium alloy corrugated pipe |
Publications (2)
Publication Number | Publication Date |
---|---|
CN1383943A true CN1383943A (en) | 2002-12-11 |
CN1193839C CN1193839C (en) | 2005-03-23 |
Family
ID=4744927
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CNB021213232A Expired - Fee Related CN1193839C (en) | 2002-06-14 | 2002-06-14 | Superplastic forming process of titanium alloy corrugated pipe |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN1193839C (en) |
Cited By (22)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN101817031A (en) * | 2010-05-20 | 2010-09-01 | 什邡市明日宇航工业股份有限公司 | Method for manufacturing titanium alloy guiding pipe for aircraft engine |
CN101856687A (en) * | 2010-05-31 | 2010-10-13 | 哈尔滨工业大学 | Current-assisted titanium and titanium alloy corrugated pipe single-bellow continuous forming device and method |
CN101987340A (en) * | 2009-08-07 | 2011-03-23 | 大诚电子制品(深圳)有限公司 | Material folding equipment and method |
CN102672007A (en) * | 2012-05-08 | 2012-09-19 | 哈尔滨工业大学 | Internal heating and pressurizing pipe distortion rectification device and method |
CN102785062A (en) * | 2012-08-22 | 2012-11-21 | 南京德邦金属装备工程股份有限公司 | Titanium alloy plate expansion joint manufacturing method |
CN102873166A (en) * | 2012-10-19 | 2013-01-16 | 上海桦厦实业有限公司 | Aircraft spherical shell isothermal forming method and device |
CN103042085A (en) * | 2012-12-21 | 2013-04-17 | 山东恒通膨胀节制造有限公司 | Method for forming nonferrous metal corrugated pipes such as titanium, zirconium and hafnium corrugated pipes |
CN103042086A (en) * | 2012-12-21 | 2013-04-17 | 山东恒通膨胀节制造有限公司 | Method for lowering formation external pressure tonnage of bellows expansion joint by reducing sectional area of cylinder |
CN103292058A (en) * | 2013-05-31 | 2013-09-11 | 南京三邦金属复合材料有限公司 | Method for forming titanium and thin-wall stainless steel corrugated pipe |
CN103521588A (en) * | 2013-10-28 | 2014-01-22 | 哈尔滨工业大学 | Current-assisted titanium alloy bellows hot-forming tool and method |
CN104493436A (en) * | 2014-11-25 | 2015-04-08 | 北京航星机器制造有限公司 | Method for manufacturing cylindrical titanium alloy parts with two ends flanged inwards through forced supplementing |
CN105710181A (en) * | 2016-02-03 | 2016-06-29 | 中国科学院金属研究所 | Forming method of large-deformation small-fillet thin-wall hollow component |
CN106181237A (en) * | 2016-07-14 | 2016-12-07 | 西北工业大学 | The titanium alloy coated side manufacture method of aero-engine composite material fan blade |
CN107013767A (en) * | 2017-05-25 | 2017-08-04 | 江苏省埃迪机电设备实业有限公司 | A kind of metal bellows of superelevation wave mode |
CN109967590A (en) * | 2017-12-27 | 2019-07-05 | 航天海鹰(哈尔滨)钛业有限公司 | A kind of titanium alloy U-shaped bellows differential temperature progressive forming method |
CN110102643A (en) * | 2019-05-23 | 2019-08-09 | 南京林业大学 | A kind of disposable shaping dies of dual damascene shell and manufacturing process |
CN111438223A (en) * | 2020-04-03 | 2020-07-24 | 西安石油大学 | Integral forming method for rectangular metal corrugated pipe |
CN113102868A (en) * | 2021-04-20 | 2021-07-13 | 中国直升机设计研究所 | Helicopter main nozzle lobe machining method |
CN113926914A (en) * | 2021-09-02 | 2022-01-14 | 航天材料及工艺研究所 | Forming method of high-temperature alloy large-diameter shallow-wave thin-wall corrugated pipe |
CN114192603A (en) * | 2021-12-14 | 2022-03-18 | 上海航天精密机械研究所 | Method for controlling interlayer redundancy and eliminating interlayer gap of multilayer metal corrugated pipe |
CN114406062A (en) * | 2021-12-22 | 2022-04-29 | 济南海圣机电科技有限公司 | Mould is used in bellows production |
CN117358817A (en) * | 2023-12-07 | 2024-01-09 | 沈阳仪表科学研究院有限公司 | Plastic forming device and plastic forming method for metal corrugated pipe |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102359691B (en) * | 2011-08-31 | 2012-10-17 | 南京三邦金属复合材料有限公司 | TA9 expansion joint manufacturing method |
-
2002
- 2002-06-14 CN CNB021213232A patent/CN1193839C/en not_active Expired - Fee Related
Cited By (34)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN101987340B (en) * | 2009-08-07 | 2014-11-12 | 大诚电子制品(深圳)有限公司 | Material folding equipment and method |
CN101987340A (en) * | 2009-08-07 | 2011-03-23 | 大诚电子制品(深圳)有限公司 | Material folding equipment and method |
CN101817031B (en) * | 2010-05-20 | 2011-08-03 | 什邡市明日宇航工业股份有限公司 | Method for manufacturing titanium alloy guiding pipe for aircraft engine |
CN101817031A (en) * | 2010-05-20 | 2010-09-01 | 什邡市明日宇航工业股份有限公司 | Method for manufacturing titanium alloy guiding pipe for aircraft engine |
CN101856687A (en) * | 2010-05-31 | 2010-10-13 | 哈尔滨工业大学 | Current-assisted titanium and titanium alloy corrugated pipe single-bellow continuous forming device and method |
CN101856687B (en) * | 2010-05-31 | 2011-11-30 | 哈尔滨工业大学 | Current-assisted titanium and titanium alloy corrugated pipe single-bellow continuous forming device and method |
CN102672007A (en) * | 2012-05-08 | 2012-09-19 | 哈尔滨工业大学 | Internal heating and pressurizing pipe distortion rectification device and method |
CN102785062A (en) * | 2012-08-22 | 2012-11-21 | 南京德邦金属装备工程股份有限公司 | Titanium alloy plate expansion joint manufacturing method |
CN102873166A (en) * | 2012-10-19 | 2013-01-16 | 上海桦厦实业有限公司 | Aircraft spherical shell isothermal forming method and device |
CN102873166B (en) * | 2012-10-19 | 2014-12-24 | 上海桦厦实业有限公司 | Aircraft spherical shell isothermal forming method and device |
CN103042085A (en) * | 2012-12-21 | 2013-04-17 | 山东恒通膨胀节制造有限公司 | Method for forming nonferrous metal corrugated pipes such as titanium, zirconium and hafnium corrugated pipes |
CN103042086A (en) * | 2012-12-21 | 2013-04-17 | 山东恒通膨胀节制造有限公司 | Method for lowering formation external pressure tonnage of bellows expansion joint by reducing sectional area of cylinder |
CN103292058B (en) * | 2013-05-31 | 2015-11-11 | 南京三邦新材料科技有限公司 | A kind of titanium and thin-wall stainless steel corrugated pipe forming method |
CN103292058A (en) * | 2013-05-31 | 2013-09-11 | 南京三邦金属复合材料有限公司 | Method for forming titanium and thin-wall stainless steel corrugated pipe |
CN103521588A (en) * | 2013-10-28 | 2014-01-22 | 哈尔滨工业大学 | Current-assisted titanium alloy bellows hot-forming tool and method |
CN103521588B (en) * | 2013-10-28 | 2015-04-22 | 哈尔滨工业大学 | Current-assisted titanium alloy bellows hot-forming tool and method |
CN104493436A (en) * | 2014-11-25 | 2015-04-08 | 北京航星机器制造有限公司 | Method for manufacturing cylindrical titanium alloy parts with two ends flanged inwards through forced supplementing |
CN104493436B (en) * | 2014-11-25 | 2018-11-09 | 北京航星机器制造有限公司 | A kind of manufacturing method having the both ends in-flanges titanium alloy cylindrical part for forcing feed supplement |
CN105710181A (en) * | 2016-02-03 | 2016-06-29 | 中国科学院金属研究所 | Forming method of large-deformation small-fillet thin-wall hollow component |
CN105710181B (en) * | 2016-02-03 | 2017-12-15 | 中国科学院金属研究所 | A kind of manufacturing process of large deformation small round corner thin-wall hollow member |
CN106181237A (en) * | 2016-07-14 | 2016-12-07 | 西北工业大学 | The titanium alloy coated side manufacture method of aero-engine composite material fan blade |
CN106181237B (en) * | 2016-07-14 | 2018-01-12 | 西北工业大学 | The titanium alloy coated side manufacture method of aero-engine composite material fan blade |
CN107013767A (en) * | 2017-05-25 | 2017-08-04 | 江苏省埃迪机电设备实业有限公司 | A kind of metal bellows of superelevation wave mode |
CN109967590A (en) * | 2017-12-27 | 2019-07-05 | 航天海鹰(哈尔滨)钛业有限公司 | A kind of titanium alloy U-shaped bellows differential temperature progressive forming method |
CN110102643A (en) * | 2019-05-23 | 2019-08-09 | 南京林业大学 | A kind of disposable shaping dies of dual damascene shell and manufacturing process |
CN110102643B (en) * | 2019-05-23 | 2023-10-24 | 南京林业大学 | Disposable forming die and forming method for double-corrugated shell |
CN111438223A (en) * | 2020-04-03 | 2020-07-24 | 西安石油大学 | Integral forming method for rectangular metal corrugated pipe |
CN111438223B (en) * | 2020-04-03 | 2022-06-03 | 西安石油大学 | Integral forming method for rectangular metal corrugated pipe |
CN113102868A (en) * | 2021-04-20 | 2021-07-13 | 中国直升机设计研究所 | Helicopter main nozzle lobe machining method |
CN113926914A (en) * | 2021-09-02 | 2022-01-14 | 航天材料及工艺研究所 | Forming method of high-temperature alloy large-diameter shallow-wave thin-wall corrugated pipe |
CN114192603A (en) * | 2021-12-14 | 2022-03-18 | 上海航天精密机械研究所 | Method for controlling interlayer redundancy and eliminating interlayer gap of multilayer metal corrugated pipe |
CN114406062A (en) * | 2021-12-22 | 2022-04-29 | 济南海圣机电科技有限公司 | Mould is used in bellows production |
CN117358817A (en) * | 2023-12-07 | 2024-01-09 | 沈阳仪表科学研究院有限公司 | Plastic forming device and plastic forming method for metal corrugated pipe |
CN117358817B (en) * | 2023-12-07 | 2024-04-16 | 沈阳仪表科学研究院有限公司 | Plastic forming device and plastic forming method for metal corrugated pipe |
Also Published As
Publication number | Publication date |
---|---|
CN1193839C (en) | 2005-03-23 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN1193839C (en) | Superplastic forming process of titanium alloy corrugated pipe | |
CN101418878A (en) | Method for manufacturing titan and titan alloy bellows | |
CN111112526A (en) | Manufacturing method of IN718 alloy axial asymmetric multi-flange casing ring piece | |
CN110508737B (en) | Wheel hub extrusion forming method | |
CN105562516A (en) | Charging pressing forming method for variable-cross-section special-shaped pipe | |
CN109692911B (en) | Integral forming device and method for large-scale ring shell part | |
CN109396208B (en) | Synchronous extrusion forming method for steel H-shaped connecting pieces with different wall thicknesses | |
CN110560544B (en) | Large-section-difference hollow structural member axial compression expansion forging process method | |
CN108723162A (en) | A kind of method that Fluid pressure induction shapes tangential non-close variable cross-section tubular member | |
CN102228926A (en) | Liquid-charging and forming method of two-way pressurizing pipe | |
CN110000271B (en) | Electromagnetic pulse forming device and method for corrugated pipe | |
CN106670249B (en) | The flanged squeezed manufacturing process of flange wheel rim | |
CN103537509A (en) | Large-sized multi-nozzle pipe hot extrusion forming process formulation and mold design method | |
CN110052525B (en) | One-die multi-piece integral forming die and method for space axis thin-walled pipe | |
CN115780805A (en) | Vertical continuous additive extrusion equipment for alloy section and preparation method | |
CN106180519A (en) | Die-forging forming mould and manufacturing process thereof | |
CN102921791A (en) | Section-variable hollow component forming device and method | |
CN103586299A (en) | High-alloy steel flexible wheel blank warm-extrusion technology used for harmonic wave decelerator | |
CN106553026B (en) | Thin Walled Curved bus aluminum alloy liner forming method and molding die | |
CN114985500A (en) | Continuous swaging composite forming device and method | |
CN111112431B (en) | Method for liquid-filled extrusion forming and blade obtained thereby | |
CN108284170B (en) | A kind of straight flange spherical shell manufacturing process | |
CN217121614U (en) | Hot extrusion molding device for blank of oil cylinder barrel of engineering machinery | |
CN220050036U (en) | Be used for metal powder metallurgy former | |
CN114789250B (en) | Preparation method of powder superalloy cylindrical spur gear component |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
C06 | Publication | ||
PB01 | Publication | ||
C10 | Entry into substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
C19 | Lapse of patent right due to non-payment of the annual fee | ||
CF01 | Termination of patent right due to non-payment of annual fee |