Qualifying of metallic materials and structures for aerospace applications

被引:20
|
作者
Frazier, WE [1 ]
Polakovics, D [1 ]
Koegel, W [1 ]
机构
[1] Naval Air Syst Command, Res & Engn Grp, Air Vehicle Dept, Patuxent River, MD 20670 USA
来源
JOM-JOURNAL OF THE MINERALS METALS & MATERIALS SOCIETY | 2001年 / 53卷 / 03期
关键词
Crack Initiation; Flight Safety; Aerospace Material Specification; Certification Driver; Corrosive Envi;
D O I
10.1007/s11837-001-0171-z
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
The U.S. Navy's certification and qualification process for materials and structures is undertaken to ensure the flight safety and full mission capability of naval aviation weapon systems. A building-block process is practiced in which validated engineering data and concepts provide the foundation for continued technological development and innovation. For example, prior to developing material-property standards, the manufacturing process is frozen and fully characterized. The customer's cost, schedule, and performance requirements must be carefully considered. Technologies are selected for immediate use or further R&D based upon a risk assessment that takes into account many factors, including technological maturity, lessons learned, the sponsor budget and schedule constraints, affordability, return on investment, and life-cycle cost impact. This paper explores the process that the navy uses to qualify its airframe alloys and structures.
引用
收藏
页码:16 / 18
页数:3
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