Flight control technology for 8000 psi has emerged almost simultaneously with new fire-resistant hydraulic fluids, such as MIL-H-83282 and CTFE. A proliferation of industry recommendations has resulted in a wide variety of mechanisms for solving associated actuator design problems, including tighter clearances, special seals, finishes, materials, and many others. As there are few common agreements on the issues, an extensive three-phase test program was undertaken to attempt to corroborate some of these approaches or suggest others that may be better or more cost effective.
8000 psi Hydraulic System Seals and Materials Test Program-A Progress Report
Sae Technical Papers
Aerospace Technology Conference and Exposition ; 1985
01.10.1985
Aufsatz (Konferenz)
Englisch
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