Research on integrated forming process of three-roll reducing and thickening of necking section for thin-walled tube of aluminum alloy 2A12

Aircraft joystick pipe is the key part of aircraft hard control system. In this paper, a hollow necking rod pipe made of aluminum alloy 2A12 is taken as the research object. The tapered roller with extrusion cone on one side of the roller surface is designed. Simufact.Forming14.0 was used to analyze...
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Autor*in:	Y. X. Xia [verfasserIn] X. D. Shu [verfasserIn] S. Zhang [verfasserIn] J. T. Wang [verfasserIn] C. Q. Ye [verfasserIn]

Format:	E-Artikel
Sprache:	Englisch

Erschienen:	2022

Schlagwörter:	aluminum alloy 2A12 three-roll forming thin-walled pipe thickening

Übergeordnetes Werk:	In: Metalurgija - Croatian Metallurgical Society, 2007, 61(2022), 3-4, Seite 733-736
Übergeordnetes Werk:	volume:61 ; year:2022 ; number:3-4 ; pages:733-736

Links:	Link aufrufen Link aufrufen Journal toc Journal toc

Katalog-ID:	DOAJ075812304

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520			\|a Aircraft joystick pipe is the key part of aircraft hard control system. In this paper, a hollow necking rod pipe made of aluminum alloy 2A12 is taken as the research object. The tapered roller with extrusion cone on one side of the roller surface is designed. Simufact.Forming14.0 was used to analyze. It was found that the radial rolling force at the end of the thickening section in the second pass increased sharply. At this time, the retaining part inhibited the axial extension of the metal and realized the accumulation in the thickness direction. The thickening rate and effect were favorable at 120 rpm, which provide a theoretical basis to realize integrated forming of aeronautical thin-walled aluminum alloy tube.
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spelling	(DE-627)DOAJ075812304 (DE-599)DOAJ6b9aabb2409440be8e31aa207c2e7281 DE-627 ger DE-627 rakwb eng TN1-997 Y. X. Xia verfasserin aut Research on integrated forming process of three-roll reducing and thickening of necking section for thin-walled tube of aluminum alloy 2A12 2022 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier Aircraft joystick pipe is the key part of aircraft hard control system. In this paper, a hollow necking rod pipe made of aluminum alloy 2A12 is taken as the research object. The tapered roller with extrusion cone on one side of the roller surface is designed. Simufact.Forming14.0 was used to analyze. It was found that the radial rolling force at the end of the thickening section in the second pass increased sharply. At this time, the retaining part inhibited the axial extension of the metal and realized the accumulation in the thickness direction. The thickening rate and effect were favorable at 120 rpm, which provide a theoretical basis to realize integrated forming of aeronautical thin-walled aluminum alloy tube. aluminum alloy 2A12 three-roll forming thin-walled pipe thickening Mining engineering. Metallurgy X. D. Shu verfasserin aut S. Zhang verfasserin aut J. T. Wang verfasserin aut C. Q. Ye verfasserin aut In Metalurgija Croatian Metallurgical Society, 2007 61(2022), 3-4, Seite 733-736 (DE-627)523860609 (DE-600)2268647-2 13342576 nnns volume:61 year:2022 number:3-4 pages:733-736 https://doaj.org/article/6b9aabb2409440be8e31aa207c2e7281 kostenfrei https://hrcak.srce.hr/file/397076 kostenfrei https://doaj.org/toc/0543-5846 Journal toc kostenfrei https://doaj.org/toc/1334-2576 Journal toc kostenfrei GBV_USEFLAG_A SYSFLAG_A GBV_DOAJ GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_95 GBV_ILN_105 GBV_ILN_110 GBV_ILN_151 GBV_ILN_161 GBV_ILN_170 GBV_ILN_206 GBV_ILN_213 GBV_ILN_230 GBV_ILN_285 GBV_ILN_293 GBV_ILN_602 GBV_ILN_2005 GBV_ILN_2009 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2055 GBV_ILN_2108 GBV_ILN_2111 GBV_ILN_2119 GBV_ILN_4012 GBV_ILN_4037 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4249 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4335 GBV_ILN_4338 GBV_ILN_4367 GBV_ILN_4700 AR 61 2022 3-4 733-736
allfields_unstemmed	(DE-627)DOAJ075812304 (DE-599)DOAJ6b9aabb2409440be8e31aa207c2e7281 DE-627 ger DE-627 rakwb eng TN1-997 Y. X. Xia verfasserin aut Research on integrated forming process of three-roll reducing and thickening of necking section for thin-walled tube of aluminum alloy 2A12 2022 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier Aircraft joystick pipe is the key part of aircraft hard control system. In this paper, a hollow necking rod pipe made of aluminum alloy 2A12 is taken as the research object. The tapered roller with extrusion cone on one side of the roller surface is designed. Simufact.Forming14.0 was used to analyze. It was found that the radial rolling force at the end of the thickening section in the second pass increased sharply. At this time, the retaining part inhibited the axial extension of the metal and realized the accumulation in the thickness direction. The thickening rate and effect were favorable at 120 rpm, which provide a theoretical basis to realize integrated forming of aeronautical thin-walled aluminum alloy tube. aluminum alloy 2A12 three-roll forming thin-walled pipe thickening Mining engineering. Metallurgy X. D. Shu verfasserin aut S. Zhang verfasserin aut J. T. Wang verfasserin aut C. Q. Ye verfasserin aut In Metalurgija Croatian Metallurgical Society, 2007 61(2022), 3-4, Seite 733-736 (DE-627)523860609 (DE-600)2268647-2 13342576 nnns volume:61 year:2022 number:3-4 pages:733-736 https://doaj.org/article/6b9aabb2409440be8e31aa207c2e7281 kostenfrei https://hrcak.srce.hr/file/397076 kostenfrei https://doaj.org/toc/0543-5846 Journal toc kostenfrei https://doaj.org/toc/1334-2576 Journal toc kostenfrei GBV_USEFLAG_A SYSFLAG_A GBV_DOAJ GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_95 GBV_ILN_105 GBV_ILN_110 GBV_ILN_151 GBV_ILN_161 GBV_ILN_170 GBV_ILN_206 GBV_ILN_213 GBV_ILN_230 GBV_ILN_285 GBV_ILN_293 GBV_ILN_602 GBV_ILN_2005 GBV_ILN_2009 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2055 GBV_ILN_2108 GBV_ILN_2111 GBV_ILN_2119 GBV_ILN_4012 GBV_ILN_4037 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4249 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4335 GBV_ILN_4338 GBV_ILN_4367 GBV_ILN_4700 AR 61 2022 3-4 733-736
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allfieldsSound	(DE-627)DOAJ075812304 (DE-599)DOAJ6b9aabb2409440be8e31aa207c2e7281 DE-627 ger DE-627 rakwb eng TN1-997 Y. X. Xia verfasserin aut Research on integrated forming process of three-roll reducing and thickening of necking section for thin-walled tube of aluminum alloy 2A12 2022 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier Aircraft joystick pipe is the key part of aircraft hard control system. In this paper, a hollow necking rod pipe made of aluminum alloy 2A12 is taken as the research object. The tapered roller with extrusion cone on one side of the roller surface is designed. Simufact.Forming14.0 was used to analyze. It was found that the radial rolling force at the end of the thickening section in the second pass increased sharply. At this time, the retaining part inhibited the axial extension of the metal and realized the accumulation in the thickness direction. The thickening rate and effect were favorable at 120 rpm, which provide a theoretical basis to realize integrated forming of aeronautical thin-walled aluminum alloy tube. aluminum alloy 2A12 three-roll forming thin-walled pipe thickening Mining engineering. Metallurgy X. D. Shu verfasserin aut S. Zhang verfasserin aut J. T. Wang verfasserin aut C. Q. Ye verfasserin aut In Metalurgija Croatian Metallurgical Society, 2007 61(2022), 3-4, Seite 733-736 (DE-627)523860609 (DE-600)2268647-2 13342576 nnns volume:61 year:2022 number:3-4 pages:733-736 https://doaj.org/article/6b9aabb2409440be8e31aa207c2e7281 kostenfrei https://hrcak.srce.hr/file/397076 kostenfrei https://doaj.org/toc/0543-5846 Journal toc kostenfrei https://doaj.org/toc/1334-2576 Journal toc kostenfrei GBV_USEFLAG_A SYSFLAG_A GBV_DOAJ GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_95 GBV_ILN_105 GBV_ILN_110 GBV_ILN_151 GBV_ILN_161 GBV_ILN_170 GBV_ILN_206 GBV_ILN_213 GBV_ILN_230 GBV_ILN_285 GBV_ILN_293 GBV_ILN_602 GBV_ILN_2005 GBV_ILN_2009 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2055 GBV_ILN_2108 GBV_ILN_2111 GBV_ILN_2119 GBV_ILN_4012 GBV_ILN_4037 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4249 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4335 GBV_ILN_4338 GBV_ILN_4367 GBV_ILN_4700 AR 61 2022 3-4 733-736
language	English
source	In Metalurgija 61(2022), 3-4, Seite 733-736 volume:61 year:2022 number:3-4 pages:733-736
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authorswithroles_txt_mv	Y. X. Xia @@aut@@ X. D. Shu @@aut@@ S. Zhang @@aut@@ J. T. Wang @@aut@@ C. Q. Ye @@aut@@
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callnumber-first	T - Technology
author	Y. X. Xia
spellingShingle	Y. X. Xia misc TN1-997 misc aluminum alloy 2A12 misc three-roll forming misc thin-walled pipe misc thickening misc Mining engineering. Metallurgy Research on integrated forming process of three-roll reducing and thickening of necking section for thin-walled tube of aluminum alloy 2A12
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topic_title	TN1-997 Research on integrated forming process of three-roll reducing and thickening of necking section for thin-walled tube of aluminum alloy 2A12 aluminum alloy 2A12 three-roll forming thin-walled pipe thickening
topic	misc TN1-997 misc aluminum alloy 2A12 misc three-roll forming misc thin-walled pipe misc thickening misc Mining engineering. Metallurgy
topic_unstemmed	misc TN1-997 misc aluminum alloy 2A12 misc three-roll forming misc thin-walled pipe misc thickening misc Mining engineering. Metallurgy
topic_browse	misc TN1-997 misc aluminum alloy 2A12 misc three-roll forming misc thin-walled pipe misc thickening misc Mining engineering. Metallurgy
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title	Research on integrated forming process of three-roll reducing and thickening of necking section for thin-walled tube of aluminum alloy 2A12
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title_full	Research on integrated forming process of three-roll reducing and thickening of necking section for thin-walled tube of aluminum alloy 2A12
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title_sort	research on integrated forming process of three-roll reducing and thickening of necking section for thin-walled tube of aluminum alloy 2a12
callnumber	TN1-997
title_auth	Research on integrated forming process of three-roll reducing and thickening of necking section for thin-walled tube of aluminum alloy 2A12
abstract	Aircraft joystick pipe is the key part of aircraft hard control system. In this paper, a hollow necking rod pipe made of aluminum alloy 2A12 is taken as the research object. The tapered roller with extrusion cone on one side of the roller surface is designed. Simufact.Forming14.0 was used to analyze. It was found that the radial rolling force at the end of the thickening section in the second pass increased sharply. At this time, the retaining part inhibited the axial extension of the metal and realized the accumulation in the thickness direction. The thickening rate and effect were favorable at 120 rpm, which provide a theoretical basis to realize integrated forming of aeronautical thin-walled aluminum alloy tube.
abstractGer	Aircraft joystick pipe is the key part of aircraft hard control system. In this paper, a hollow necking rod pipe made of aluminum alloy 2A12 is taken as the research object. The tapered roller with extrusion cone on one side of the roller surface is designed. Simufact.Forming14.0 was used to analyze. It was found that the radial rolling force at the end of the thickening section in the second pass increased sharply. At this time, the retaining part inhibited the axial extension of the metal and realized the accumulation in the thickness direction. The thickening rate and effect were favorable at 120 rpm, which provide a theoretical basis to realize integrated forming of aeronautical thin-walled aluminum alloy tube.
abstract_unstemmed	Aircraft joystick pipe is the key part of aircraft hard control system. In this paper, a hollow necking rod pipe made of aluminum alloy 2A12 is taken as the research object. The tapered roller with extrusion cone on one side of the roller surface is designed. Simufact.Forming14.0 was used to analyze. It was found that the radial rolling force at the end of the thickening section in the second pass increased sharply. At this time, the retaining part inhibited the axial extension of the metal and realized the accumulation in the thickness direction. The thickening rate and effect were favorable at 120 rpm, which provide a theoretical basis to realize integrated forming of aeronautical thin-walled aluminum alloy tube.
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title_short	Research on integrated forming process of three-roll reducing and thickening of necking section for thin-walled tube of aluminum alloy 2A12
url	https://doaj.org/article/6b9aabb2409440be8e31aa207c2e7281 https://hrcak.srce.hr/file/397076 https://doaj.org/toc/0543-5846 https://doaj.org/toc/1334-2576
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Research on integrated forming process of three-roll reducing and thickening of necking section for thin-walled tube of aluminum alloy 2A12

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