Home > Archive>Volume 45, Issue 1, 2015 >
PDF HTML XML Export Cite reminder
Microstructure and Property Analysis of the Vacuum Brazed Carbon-CarbonComposites and High Temperature Alloys Joint
DOI:
CSTR:
[cstr]
Author:
Affiliation:

Clc Number:

TG407

Fund Project:

  • Article
    • |
  • Figures
    • |
  • Metrics
    • |
  • Reference
    • |
  • Related
    • |
  • Cited by
    • |
  • Materials
    • |
  • Comments
    Abstract:

    Joining samples of carbon/ carbon composites (C/ C composites) and Ni based high temperature alloy
    (GH600) were fabricated by vacuum brazing with the powder of BNi68CrWB as the interlayer material. The mechanical
    properties and microstructure of the joints between C/ C composite and GH600 were investigated by scanning electron
    microscopes and universal material testing machines. The results show that the joining of C/ C composites to Ni
    based high temperature alloy is successfully achieved by vacuum brazing process. The fracture of the joint occurs in
    the C/ C composites. The shear strength at high temperature of the brazed joints rapidly decreases above 700 ℃.

    Reference
    Related
    Cited by
Get Citation

Copy
Share
Article Metrics
  • Abstract:
  • PDF:
  • HTML:
  • Cited by:
History
  • Received:
  • Revised:
  • Adopted:
  • Online: November 28,2016
  • Published:
Article QR Code

You are the visitor

Beijing Public Network Security：11010602060147号 京ICP备06019415号-2

Address：P.O.Box 9200-73, Beijing 100076, P.R.China

Postcode：100076 Fax：010-68383237

ServiceTel：010-68383269 E-mail：703@china.com

Copyright：Aerospace Materials ＆ Technology ® 2025 All Rights Reserved