AAWSAP DIRD, Materials for Advanced Aerospace Platforms, January 2010
DOW-UAP-D120 · page 18 of 27
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UNCLASSIFIED/;'FOR OFFl&IAl W&IE 9fslllf Figure 3. Micrograph Showing a Phase Formation at the Surface of a Ti Alloy That has Been Exposed to Air at Elevated Temperature The a case is harder than the matrix because oxygen is a potent a-phase solid-solution strengthener. As with almost all other strengthening reactions, the increased strength is accompanied by reduced ductility. Again, drawing on conventional wisdom, the presence of a case in sheet structures has been forbidden by specification, design practice, or whatever means a company uses to manage its hardware. Less clear is how truly detrimental a case is to properties. Essentially no effort has been made to determine whether it can be tolerated if the affected hardware is allowed to operate at a modestly reduced stress. The industry standard for a case has essentially been one of zero tolerance. Given the significant potential weight advantage associated with use of Ti alloys in portions of the TPS and warm structure, this conservative approach needs to be revisited. Several key questions related to this are: • Is a case truly detrimental to the load-bearing capability of Ti alloy sheet structures? • If so, is there a limiting amount that can be tolerated without significantly degrading the structural capability? • Which properties are the most severely degraded? • Are a case formation and property degradation alloy dependent? • If so, which alloys are the most tolerant of a case formation? 13 UNCLASSIFIED/ /FOR OFFI&IAl Wliliii QfslL¥