作者: Stephen A. Mascarella , Robert L. Brundrett , Franklin C. Christ , Lawrence F. Corio
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摘要: An electrically actuated aircraft brake (11) and method for its servicing is characterized by the use actuator modules (36) which can be easily quickly replaced as a unit. Quick easy replacement of effected without disassembly overall wheel assembly (10). Accordingly, manufacturing, repair costs, overhaul, parts stocking maintenance costs requirements are minimized and/or greatly simplified compared to integrated designs used in prior art. Also, malfunctioning module on an preferably enough allow remain scheduled service with minimum downtime.