经测试，飞机的轴驱动升力风扇推进系统可产生超过性能需求的垂直推力比。
The aircraft’s shaft-driven lift fan propulsion system produced more vertical thrust than needed to meet performance requirements.
皮瓣或金属板驱动系统在飞机根据索赔1，不包括横向轴延伸线，通过机身表示，从一个到另一个的说翅膀。
The flap or slat drive system in the aircraft according to claim 1, not including a transverse shaft line that extends through said fuselage from one to another of said wings.
为了实现燃料电池电动客车的动力转向功能，提出了直流电机通过联轴机构直接驱动油泵的电动液压式动力转向系统。
In order to achieve power steering function in fuel cell bus, an electrohydraulic system is proposed, where the pump is directly driven by a DC motor through an axis coupler.
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