首页> 外国专利> DIVING DEPTH STABILIZER WITH HYDRODYNAMIC WING DRIVE BOOSTER

DIVING DEPTH STABILIZER WITH HYDRODYNAMIC WING DRIVE BOOSTER

机译:潜水深度稳定器与流体动力翼驱动助力器

摘要

FIELD: shipbuilding.;SUBSTANCE: invention relates to the field of shipbuilding, in particular to the development of technical means for the development and exploration of the ocean, methods of seismic exploration. The diving depth stabilizer with a hydrodynamic wing drive booster contains a head, a body equipped with suspension assemblies for a carrier of an underwater vehicle with mating sections and a float, elements of apparatus and equipment, a tail fairing, a wing pivotally connected to the head. The head, which is a receiver of hydrodynamic pressure from the flow, is located in the stabilizer body and is made with a central axial hole. A spring-membrane mechanism is introduced into the central axial hole of the head, consisting of a membrane, a spring, a depth gauge, and a rotary mechanism. The wing is pivotally connected to the bracket and located above the head, in addition, a membrane is introduced into the wing, dividing the internal volume of the wing into two cavities, upper and lower, a thrust is introduced, with the help of which the membrane is connected to the rotary mechanism. Channels are introduced into the head, one of which is connected to the upper cavity of the membrane, and the other to the lower one. A damper with windows is located in the cavity of the axial hole and is connected to a depth gauge, a spring, through a rod and is configured to combine the opening and closing of channels for deflecting and submerging the wing, and maintaining a stabilizing horizontal position.;EFFECT: invention increases active control of the wing mechanism and maintenance of its stabilizing horizontal position by expanding the functionality.;1 cl, 3 dwg
机译:领域:造船。物质:发明涉及造船领域,尤其涉及开发海洋的发展和探索的技术手段,地震勘探方法。具有流体动力翼驱动增压器的潜水深度稳定器包含头部,一个主体,其配备有用于水下车辆的载体的悬架组件,其配合部分和浮动装置和设备的元件,尾部整流器,枢转连接的机翼头。作为来自流动的流体动力学压力的接收器的头部位于稳定器主体中,并且由中心轴向孔制成。将春膜机构引入头部的中心轴向孔中,由膜,弹簧,深度计和旋转机构组成。翼枢转地连接到支架上并位于头部上方,另外,将膜引入机翼,将机翼的内部容积分成两个腔,上下腔,借助于哪个推力膜连接到旋转机构。通道被引入头部,其中一个连接到膜的上腔,另一个连接到下一个。具有窗户的阻尼器位于轴向孔的腔体中,并且通过杆连接到深度计,弹簧,弹簧,并且构造成将通道的开口和关闭用于偏转和浸入机翼,并保持水平稳定位置。;效果:通过扩展功能来增加机构的主动控制和其稳定水平位置的维护。; 1 CL,3 DWG

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