LIGHTWEIGHT MATERIALS FOR AIRCRAFT APPLICATIONS

被引:388
作者
IMMARIGEON, JP [1 ]
HOLT, RT [1 ]
KOUL, AK [1 ]
ZHAO, L [1 ]
WALLACE, W [1 ]
BEDDOES, JC [1 ]
机构
[1] CARLETON UNIV, DEPT MECH & AEROSP ENGN, OTTAWA, ON K1S 5B6, CANADA
关键词
D O I
10.1016/1044-5803(95)00066-6
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
Reducing structural weight is one of the major ways to improve aircraft performance. Lighter and/or stronger materials allow greater range and speed and may also contribute to reducing operational costs. The article reviews some recent developments in lightweight materials for airframe components (aluminum alloys, composites, and hybrid materials) and engine components (titanium aluminides and titanium-based composites). Emphasis is placed on microstructural characterization and the relationship between the microstructure and mechanical properties of specific materials systems being investigated at the National Research Council's Institute for Aerospace Research.
引用
收藏
页码:41 / 67
页数:27
相关论文
共 86 条
[1]  
ASHLEY S, 1993, MECH ENG, V115, P60
[2]  
BALDANTONI A, 1989, AGARD REPORT, V713, P162
[3]  
BANIA PJ, 1994, JOM-J MIN MET MAT S, V46, P16, DOI 10.1007/BF03220742
[4]   HIGH-TEMPERATURE COMPRESSION BEHAVIOR OF NEAR GAMMA-TITANIUM ALUMINIDES CONTAINING ADDITIONS OF CHROMIUM OR TUNGSTEN [J].
BEDDOES, J ;
ZHAO, L ;
WALLACE, W .
MATERIALS SCIENCE AND ENGINEERING A-STRUCTURAL MATERIALS PROPERTIES MICROSTRUCTURE AND PROCESSING, 1994, 184 (01) :L11-L15
[5]   THE ISOTHERMAL COMPRESSION RESPONSE OF A NEAR GAMMA-TIAL+W INTERMETALLIC [J].
BEDDOES, J ;
ZHAO, L ;
IMMARIGEON, JP ;
WALLACE, W .
MATERIALS SCIENCE AND ENGINEERING A-STRUCTURAL MATERIALS PROPERTIES MICROSTRUCTURE AND PROCESSING, 1994, 183 (1-2) :211-222
[6]  
BOYER RR, 1994, JOM-J MIN MET MAT S, V46, P20
[7]  
Brown M.V., 1989, US Patent, Patent No. [4,863,528, 4863528]
[8]  
BROWN MH, 1989, Patent No. 4832758
[9]  
BROWN MH, 1984, Patent No. 4477292
[10]  
CHELLMAN DJ, 1988, METALL POWDER REP, V43, P672