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Wide and multiple apex seals for the rotary engine (Abbr.: Multi-Apex-Seals for the Rotary Engine)

机译:旋转发动机的宽和多个顶部密封件(缩写:旋转发动机的多顶部密封件)

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摘要

Conventional rotary engines are based on a trochoidal-type housing bore profile and its inside envelope is the basis of the rotor profile. To seal the chambers, spring-loaded apex seals are used in place of the designed rotor apexes. The conventional design method is limited to an epitrochoidal-based housing and does not consider the apex seal profile. Previously the authors presented the complete theory and algorithm of the deviation-function (DF) method of rotary engine design based on the apex seal profile. By using the DF method, the apex seal and engine housing bore are conjugate kinematic pairs, which enable the design of a variety of apex seals that conform to the bore, including wider apex seals and multiple seals at each rotor apex. The wide apex seal design has better rotor-to-housing conformity and therefore improves sealing. The multi-apex-seal grid assembly improves sealing capability and also reduces the forces on the apex seals. The incorporation of apex seal profiles into the rotary engine design process also makes possible a larger variety of new rotary engine profiles.
机译:常规的旋转发动机基于摆线型壳体孔轮廓,并且其内包络线是转子轮廓的基础。为了密封腔室,使用弹簧加载的顶点密封件代替设计的转子顶点。常规的设计方法仅限于基于摆线的壳体,并且不考虑顶点密封轮廓。以前,作者基于顶点密封轮廓介绍了旋转发动机设计的偏差函数(DF)方法的完整理论和算法。通过使用DF方法,顶点密封和发动机壳体孔是共轭运动学对,这使得能够设计与孔相符的各种顶点密封,包括更宽的顶点密封和每个转子顶点处的多个密封。宽尖的密封设计具有更好的转子到壳体的一致性,因此改善了密封性。多顶点密封栅组件提高了密封能力,还减少了在顶点密封件上的作用力。将顶点密封型材结合到旋转发动机设计过程中,还可以使更多种类的新型旋转发动机型材成为可能。

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