作者: Jr. Jay W. Carter
DOI:
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摘要: A rotor aircraft has an adjusting mechanism that controls the sensitivity of control stick relative to fore and aft tilt rotor. The is pivotable between directions as well laterally about a pivot point. linkage connected head. assembly tilts head in response tilting movement stick. point rotates at radius An member located can be moved change corresponds amount make while moves full forward positions. also ailerons horizontal stabilizer but these services are not affected by member.