Accession Number:

AD0904766

Title:

Titanium 3Al-2.5V CW Hydraulic Tubing Development

Corporate Author:

BOEING COMMERCIAL AIRPLANE CO SEATTLE WA

Report Date:

1972-10-01

Abstract:

This report contains the fatigue, metallurgical, and bend test results on titanium alloy 3Al-2.5V cold worked and stress relieved tubing procured during the prototype supersonic transport test program, and the new texture-controlled tubing. The tubing procured for the prototype program was tested with three different inside-diameter finishes developed by Boeing, Grumman Aerospace, and McDonnell-Douglas. The texture-controlled tubing was developed during this program, and its requirements are defined in the new Boeing-proposed specification, which is included in this report.

Descriptive Note:

Final rept. on Task 2

Supplementary Note:

Report on SST Technology Follow-On Program-Phase 1.

Pages:

0153

Communities Of Interest:

Modernization Areas:

Distribution Statement:

Approved for public release; distribution is unlimited.

Contract Number:

DOT-FA-SS-71-12

File Size:

4.74MB