Microstructure and Mechanical Properties of Wide-gap Brazed Joints of K465 Alloy Using Cobalt-base Brazing Alloy

Vacuum brazing of K465 superalloy was carried out by using Co45NiCrWB cobalt-base filler metal at 1220 ℃ for different holding time, and the joint clearance was 0.5 mm pre-filled with FGH95 nickel-base superalloy powder. The effect of the structural constitution of brazed different holding time of t...

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Main Authors: PAN Hui, ZHAO Haisheng
Format: Article
Language:zho
Published: Journal of Aeronautical Materials 2017-06-01
Series:Journal of Aeronautical Materials
Subjects:
Online Access:http://jam.biam.ac.cn/CN/Y2017/V37/I3/50
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spelling doaj-a712a53d577749c1b63698843c4bd7962020-11-25T00:40:34ZzhoJournal of Aeronautical MaterialsJournal of Aeronautical Materials1005-50531005-50532017-06-01373505510.11868/j.issn.1005-5053.2016.000205201703000205Microstructure and Mechanical Properties of Wide-gap Brazed Joints of K465 Alloy Using Cobalt-base Brazing AlloyPAN Hui0ZHAO Haisheng1Welding and Plastic Forming Division, Beijing Institute of Aeronautical Materials, Beijing 100095, ChinaWelding and Plastic Forming Division, Beijing Institute of Aeronautical Materials, Beijing 100095, ChinaVacuum brazing of K465 superalloy was carried out by using Co45NiCrWB cobalt-base filler metal at 1220 ℃ for different holding time, and the joint clearance was 0.5 mm pre-filled with FGH95 nickel-base superalloy powder. The effect of the structural constitution of brazed different holding time of temperature on the brazed joint microstructure and properties. The results show that the brazing seam is composed of alloy powder particles and borides among them. It is two-phase structure of γ and γ' with a few small blocks of borides in the powder particles, and there exists phases rich in Cr, W and Nb elements. The powder particles are growing along the holding time during the brazing process, while their combination is expanded. It is good for stress rapture properties of joints that borides was fine in brazing seam with more superalloy powder and proper holding time. And the joints brazed for 30-60 min show higher stress rapture properties.http://jam.biam.ac.cn/CN/Y2017/V37/I3/50brazingnickel-base superalloymicrostructuremechanical property
collection DOAJ
language zho
format Article
sources DOAJ
author PAN Hui
ZHAO Haisheng
spellingShingle PAN Hui
ZHAO Haisheng
Microstructure and Mechanical Properties of Wide-gap Brazed Joints of K465 Alloy Using Cobalt-base Brazing Alloy
Journal of Aeronautical Materials
brazing
nickel-base superalloy
microstructure
mechanical property
author_facet PAN Hui
ZHAO Haisheng
author_sort PAN Hui
title Microstructure and Mechanical Properties of Wide-gap Brazed Joints of K465 Alloy Using Cobalt-base Brazing Alloy
title_short Microstructure and Mechanical Properties of Wide-gap Brazed Joints of K465 Alloy Using Cobalt-base Brazing Alloy
title_full Microstructure and Mechanical Properties of Wide-gap Brazed Joints of K465 Alloy Using Cobalt-base Brazing Alloy
title_fullStr Microstructure and Mechanical Properties of Wide-gap Brazed Joints of K465 Alloy Using Cobalt-base Brazing Alloy
title_full_unstemmed Microstructure and Mechanical Properties of Wide-gap Brazed Joints of K465 Alloy Using Cobalt-base Brazing Alloy
title_sort microstructure and mechanical properties of wide-gap brazed joints of k465 alloy using cobalt-base brazing alloy
publisher Journal of Aeronautical Materials
series Journal of Aeronautical Materials
issn 1005-5053
1005-5053
publishDate 2017-06-01
description Vacuum brazing of K465 superalloy was carried out by using Co45NiCrWB cobalt-base filler metal at 1220 ℃ for different holding time, and the joint clearance was 0.5 mm pre-filled with FGH95 nickel-base superalloy powder. The effect of the structural constitution of brazed different holding time of temperature on the brazed joint microstructure and properties. The results show that the brazing seam is composed of alloy powder particles and borides among them. It is two-phase structure of γ and γ' with a few small blocks of borides in the powder particles, and there exists phases rich in Cr, W and Nb elements. The powder particles are growing along the holding time during the brazing process, while their combination is expanded. It is good for stress rapture properties of joints that borides was fine in brazing seam with more superalloy powder and proper holding time. And the joints brazed for 30-60 min show higher stress rapture properties.
topic brazing
nickel-base superalloy
microstructure
mechanical property
url http://jam.biam.ac.cn/CN/Y2017/V37/I3/50
work_keys_str_mv AT panhui microstructureandmechanicalpropertiesofwidegapbrazedjointsofk465alloyusingcobaltbasebrazingalloy
AT zhaohaisheng microstructureandmechanicalpropertiesofwidegapbrazedjointsofk465alloyusingcobaltbasebrazingalloy
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