作者: Charles D. Bateman
DOI:
关键词:
摘要: A weight and balance system for an aircraft or the like which measures bend in a structural member of aircraft, such as landing gear element wing fuselage section, by use inclinometers mounted to each having signal output representing angle with respect reference plane then summing outputs from incinometers determine provides indication weight. In one example, includes bends response pair inclinometers, form servoed accelerometers, are adjacent opposite ends thereof provide voltage relative plane, device said For tire pressure detection, plurality associated bogie beam two more pairs tires is underpressured.