Development of Hydrogen Embrittlement Test Methods Which Reflect Realistic Maintenance Scenarios

983116

11/09/1998

Event
SAE Airframe/Engine Maintenance & Repair Conference & Exposition
Authors Abstract
Content
This paper compares several different test methods used to test maintenance chemicals for potential to induce hydrogen embrittlement in high-strength steel. The program was structured to accomplish three main objectives with regard to hydrogen embrittlement testing: 1) compare various test methods used to qualify maintenance chemicals, 2) compare various coatings used to protect high-strength steel parts such as landing gear, and 3) compare various high-strength steel substrates specified for aircraft landing gear. The coatings selected included electrodeposited cadmium (baseline), ion vapor deposited (IVD) aluminum, SermeTel 984, and Zinc-Nickel plate. Substrates tested included AISI 4340 (260-280 ksi HT), 300M (280-300 ksi HT), and AerMet 100 (minimum 290 ksi HT).
Meta TagsDetails
DOI
https://doi.org/10.4271/983116
Pages
8
Citation
McLaughlin, J., Weir, J., and Boodey, J., "Development of Hydrogen Embrittlement Test Methods Which Reflect Realistic Maintenance Scenarios," SAE Technical Paper 983116, 1998, https://doi.org/10.4271/983116.
Additional Details
Publisher
Published
Nov 9, 1998
Product Code
983116
Content Type
Technical Paper
Language
English