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本文针对方向舵液压助力器,提出的初步设计观点。在通用航空飞机飞行过程中安全性,稳定性起到作用。如付诸现实将降低安全成本。
This article aims at the rudder hydraulic booster, put forward the preliminary design point of view. In the general aviation aircraft flight safety, stability play a role. Reality will reduce security costs.