AGMA 2000FTM1-2000
Minimization of In-Process Corrosion of Aerospace Gears

Standard No.
AGMA 2000FTM1-2000
Release Date
2000
Published By
American Gear Manufacturers Association
Scope
This study was conducted in two phases: Phase I was to identify root causes of in-process corrosion by conducting a comprehensive study, using manufacturing process bench marking, at two gear production facilities. The Phase I study was augmented by controlled laboratory experiments. The desired end product of Phase I was to understand the sources of corrosion on gears during the manufacturing process and to identify solutions to minimize the corrosion problem. Phase II was to implement the identified solutions to a restricted area of the manufacturing floor to test them in a production environment. Phase I involved defining the boundaries of the gear making process, developing detailed process maps that describe all of the steps required to produce the gears, veriiing the actual inputs at each process step, and perfoming the Failure Mode and Effects Analysis (FMEA) to assess priority of the process parameters. After the process conditions that could potentially be contributing to corrosion initiation were identified and prioritized, the design of experiments (DOE) were planned and performed.



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