High-Temperature Polyimide Hydraulic Actuator Rod Seals for Advanced Aircraft 700790
This paper summarizes the results and findings of a program to design, develop, and evaluate actuator rod seals for use in advanced aircraft high-temperature hydraulic systems. The rod seals are intended to function efficiently and reliably for 3000 hr in the temperature range of -40-500 F. Preliminary studies of various material and design combinations showed that a polyimide low-pressure second-stage V-seal in a two-stage configuration had the greatest potential in long-term duty cycle testing in a simulated actuator test system. Modifications of this seal that provided for improved fatigue life and more efficient loading met the test objectives of 20 X 106 short-stroke cycles of operation at 500 F. Severity of this testing was equivalent to 3000 hr of duty cycle operation. The validity of design techniques used to achieve performance goals was shown.
Citation: Loomis, W., Johnson, R., and Lee, J., "High-Temperature Polyimide Hydraulic Actuator Rod Seals for Advanced Aircraft," SAE Technical Paper 700790, 1970, https://doi.org/10.4271/700790. Download Citation
Author(s):
William R. Loomis, Robert L. Johnson, John Lee
Affiliated:
Lewis Research Center, NASA, Tetrafluor Div., Royal Industries
Pages: 10
Event:
National Aeronautic and Space Engineering and Manufacturing Meeting
ISSN:
0148-7191
e-ISSN:
2688-3627
Related Topics:
Hydraulic systems
Seals and gaskets
Aircraft
Sensors and actuators
Fatigue
SAE MOBILUS
Subscribers can view annotate, and download all of SAE's content.
Learn More »