Accession Number:

AD0736022

Title:

Design Studies and Model Tests of the Stowed Tilt Rotor Concept. Volume 9. Value Engineering Report

Descriptive Note:

Final rept.

Corporate Author:

BOEING VERTOL CO PHILADELPHIA PA

Personal Author(s):

Report Date:

1971-10-01

Pagination or Media Count:

64.0

Abstract:

The report describes and compares the technical and cost issues of flush and edgewise folding of the rotor blades for a stowed tilt rotor aircraft. Four different folding actuation schemes are presented. A cost saving recommendation is also made for the hub costing.

Subject Categories:

  • VSTOL

Distribution Statement:

APPROVED FOR PUBLIC RELEASE