FILTER APPARATUS WITH TORQUE LIMITING MECHANISM
    4.
    发明申请
    FILTER APPARATUS WITH TORQUE LIMITING MECHANISM 审中-公开
    带扭矩限制机构的过滤器

    公开(公告)号:US20160193554A1

    公开(公告)日:2016-07-07

    申请号:US15068130

    申请日:2016-03-11

    Abstract: A filter apparatus is described that has a torque limiting device, which may be a clutch mechanism, and which provides a protective function for a filter, so as to protect a filter from being over tightened and to thereby prevent damage to filter components. The clutch mechanism can also eliminate or reduce the need for torque measurement of certain filter components. The clutch mechanism can be located on one of the fluid filter, a filter head which engages the fluid filter, or a combination of both the fluid filter and the filter head.

    Abstract translation: 描述了一种过滤装置,其具有扭矩限制装置,该扭矩限制装置可以是离合器机构,并且其提供过滤器的保护功能,以便防止过滤器过度紧固,从而防止对过滤器部件的损坏。 离合器机构还可以消除或减少某些过滤器部件的扭矩测量的需要。 离合器机构可以位于流体过滤器中的一个上,接合流体过滤器的过滤器头,或流体过滤器和过滤器头的组合。

    Snap in place natural gas filter
    9.
    发明授权

    公开(公告)号:US11358089B2

    公开(公告)日:2022-06-14

    申请号:US16033729

    申请日:2018-07-12

    Abstract: A filter that is retained in a shell housing by the use of a snap connection. The filter includes an endplate having snap features that interact with a groove in an inner portion of the shell housing. The groove may extend 360 degrees around an inner circumference of the shell housing. Accordingly, when the shell is unthreaded from the head service (e.g., during a filter replacement service), the shell only needs to be displaced the length of the inner radial seal interface between the shell and the head, not the entire length of the filter media thereby minimizing the stroke length needed to service the filter assembly.

    Separation assembly with a two-piece impulse turbine

    公开(公告)号:US11352999B2

    公开(公告)日:2022-06-07

    申请号:US17044371

    申请日:2019-04-16

    Inventor: Chirag D. Parikh

    Abstract: A separation assembly comprises a housing, a jet that expels a fluid within the housing, and a turbine assembly positioned within the housing and positioned so as to be contacted by the fluid expelled from the jet. The fluid causes the turbine assembly to rotate about a center rotational axis within the housing. The turbine assembly comprises a first turbine portion and a second turbine portion that are separately formed from each other and attachable together. The first turbine portion comprises a plurality of first vanes and the second turbine portion comprises a plurality of second vanes.

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