Creep properties of TiB Particulate-Reinforced Ti-22Al-27Nb Composites
Emura, Satoshi and Hausmann, Joachim and Liying, Zeng and Hagiwara, Masuo (2005) Creep properties of TiB Particulate-Reinforced Ti-22Al-27Nb Composites. XITC Xian International Titanium Conference, 2005-10-18 - 2005-10-20, Xian (China).
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The Ti2AlNb intermetallic alloys, based on the ordered orthorhombic (O) phase, have a higher specific strength, better creep resistance and better workability than conventional titanium aluminides, such as TiAl and Ti3Al. Typical alloy system so far studied is a Ti-22Al-27Nb (mol pct) alloy, consisting primarily of the (O+B2 (ordered BCC)) two-phase microstructure. However, the mechanical properties of these alloys must be improved before commercial applications are feasible. To further improve the mechanical properties of this Ti2AlNb alloy, a TiB particulate-reinforced Ti-22Al-27Nb matrix composite was prepared using the gas-atomized powder metallurgy method. Because of the rapid solidification during the gas atomization process, the TiB particulates dispersed in the composite were extremely fine, with an average diameter of less than 1 μm and lengths ranging up to 5 μm. This composite (PM composite) showed better creep properties at high temperatures than both an unreinforced Ti-22Al-27Nb matrix alloy and a Ti-22Al-27Nb/TiB composite produced using a conventional ingot metallurgy method (IM composite) with relatively coarse (average diameter 5 μm and average length 40 μm) TiB particulates. We have also found that the size of TiB particulate in the PM composite can be controlled by heat treatment at high temperature (around 1473 K), and investigated the effect of the size of dispersed TiB particulates on the creep properties of Ti-22Al-27Nb/TiB composites.
|Document Type:||Conference or Workshop Item (Speech)|
|Title:||Creep properties of TiB Particulate-Reinforced Ti-22Al-27Nb Composites|
|Date:||18 October 2005|
|In ISI Web of Science:||No|
|Keywords:||Titanium, Intermetallic, Orthorhombic, MMC, TiB|
|Event Title:||XITC Xian International Titanium Conference|
|Event Location:||Xian (China)|
|Event Type:||international Conference|
|Event Dates:||2005-10-18 - 2005-10-20|
|HGF - Research field:||Aeronautics, Space and Transport|
|HGF - Program:||Aeronautics|
|HGF - Program Themes:||L ER - Engine Research|
|DLR - Research area:||Aeronautics|
|DLR - Program:||L ER - Engine Research|
|DLR - Research theme (Project):||L - Fan and Compressor Technologies|
|Institutes and Institutions:||Institute of Materials Research > Light Metal Composites|
|Deposited By:||Dr.-Ing. Joachim Hausmann|
|Deposited On:||16 Dec 2005|
|Last Modified:||27 Apr 2009 04:46|
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