NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Fully Integral, Flexible Composite DriveshaftAn all-composite driveshaft incorporating integral flexible diaphragms was developed for prime contractor testing. This new approach makes obsolete the split lines required to attach metallic flex elements and either metallic or composite spacing tubes in current solutions. Subcritical driveshaft weights can be achieved that are half that of incumbent technology for typical rotary wing shaft lengths. Spacing tubes compose an integral part of the initial tooling but remain part of the finished shaft and control natural frequencies and torsional stability. A concurrently engineered manufacturing process and design for performance competes with incumbent solutions at significantly lower weight and with the probability of improved damage tolerance and fatigue life.
Document ID
20150005320
Acquisition Source
Glenn Research Center
Document Type
Other
Authors
Lawrie, Duncan
(Lawrie Technology, Inc. Girard, PA, United States)
Date Acquired
April 10, 2015
Publication Date
November 1, 2014
Publication Information
Publication: An Overview of SBIR Phase 2 Airbreathing Propulsion Technologies
Subject Category
Mechanical Engineering
Aircraft Design, Testing And Performance
Distribution Limits
Public
Copyright
Public Use Permitted.
No Preview Available