Design of Helicopter Transmission for “On-Condition” Maintenance

700587

02/01/1970

Event
9th Reliability and Maintainability Conference
Authors Abstract
Content
This paper considers the reduction of helicopter “cost of ownership” by the process of reducing the frequency of transmission overhaul. Reasons for time scheduled overhauls (TBO) and their validity to helicopter transmissions are explored. Failure functions for several transmissions are shown and individual failure modes explored for indications of failure function trends beyond the current operating regime.
The conclusion is reached that significant cost savings are possible with On-Condition maintenance.
The only valid reason for retaining a TBO in the mature transmission is the presence of wearout type non-detectable safety-affecting failure modes. These generally take the form of structural fatigue originating from fretted joints or surfaces or slow wear in internal spline and clutches. These modes may exist in some of today's transmissions and, if so, represent the limiting TBO. The full potential of On-Condition operation may not be realized without safety oriented changes.
These changes include concepts which minimize or eliminate fretting, provide fail safety via redundancy or are tolerant to damage. Further improvement in condition monitoring and early, concentrated, development testing are the necessary ingredients for On-Condition maintenance of tomorrow's helicopter transmissions.
Meta TagsDetails
DOI
https://doi.org/10.4271/700587
Pages
13
Citation
Harding, D., and Mack, J., "Design of Helicopter Transmission for “On-Condition” Maintenance," SAE Technical Paper 700587, 1970, https://doi.org/10.4271/700587.
Additional Details
Publisher
Published
Feb 1, 1970
Product Code
700587
Content Type
Technical Paper
Language
English