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    SPHERICAL INVOLUTE GEAR COUPLING
    71.
    发明申请
    SPHERICAL INVOLUTE GEAR COUPLING 审中-公开
    球形相关齿轮联轴器

    公开(公告)号：WO2012151699A1

    公开(公告)日：2012-11-15

    申请号：PCT/CA2012/050303

    申请日：2012-05-09

    Applicant: EXPONENTIAL TECHNOLOGIES, INC. ,  PATTERSON, Curtis ,  JUAN, Alejandro ,  GOTTFRIED, Kristjan

    Inventor： PATTERSON, Curtis ,  JUAN, Alejandro ,  GOTTFRIED, Kristjan

    IPC: F16H1/24 ,  F03C2/08 ,  F04C2/08 ,  F16D3/18 ,  F16H1/10 ,  F16H1/12 ,  F16H55/02 ,  F16H57/12

    CPC classification number: F04C2/084 ,  F04C3/08 ,  F16D3/185 ,  Y10T74/1966

    Abstract: Disclosed herein are several embodiments of rotors (gears) which utilize spherical involute curves to determine the surfaces of the lobes (teeth). In some embodiments the contact surfaces are radial projections of spherical involute surfaces. In other embodiments the contact surfaces have a root and/or tip of a spherical involute curve, but are barreled or otherwise curved to reduce the point stress on each rotor. The rotors may also be configured where torque transfer is provided at a first set of lobes (teeth) and backlash removal is provided on teeth radially opposed to the first set of lobes (teeth). As the apparatus rotates, the position of torque transfer remains substantially the same, as does backlash prevention/removal, but the teeth providing these operations vary. The rotors may also be used for fluid flow.

    Abstract translation: 本文公开了使用球形渐开线曲线来确定凸角（齿）的表面的转子（齿轮）的若干实施例。 在一些实施例中，接触表面是球形渐开线表面的径向突起。 在其他实施例中，接触表面具有球形渐开线曲线的根部和/或尖端，但是被套管或以其它方式弯曲以减小每个转子上的点应力。 转子还可以被配置成在第一组叶片（齿）处提供扭矩传递，并且在与第一组叶片（齿）径向相对的齿上提供齿隙移除。 当设备旋转时，转矩传递的位置保持基本相同，防止/去除齿隙，但提供这些操作的齿不同。 转子也可用于流体流动。

    MULTITUBE VALVELESS PULSE DETONATION ENGINE
    73.
    发明申请
    MULTITUBE VALVELESS PULSE DETONATION ENGINE 审中-公开
    多功能气动脉冲爆震发动机

    公开(公告)号：WO2011156923A2

    公开(公告)日：2011-12-22

    申请号：PCT/CA2011/050362

    申请日：2011-06-15

    Applicant: EXPONENTIAL TECHNOLOGIES, INC. ,  GOTTFRIED, Kristjan ,  JUAN, Alejandro

    Inventor： GOTTFRIED, Kristjan ,  JUAN, Alejandro

    CPC classification number: F02K7/04 ,  F02C5/11 ,  F02K7/067 ,  F23C15/00 ,  F23C2900/03004

    Abstract: Disclosed herein is a valveless multitube pulse detonation engine including: a plurality of detonation tubes, wherein each detonation tube comprises an independent discharge outlet, and the plurality of detonation tubes interconnected at a common air/fuel mixture intake port. In the disclosed engine, an air and fuel mixture is detonated in the detonation tubes simultaneously, and the common air/fuel mixture intake port minimizes back-pressure caused by detonating the air/fuel mixture by directing multiple reverse shock waves into one another and effectively using the back-pressures as reacting surfaces for one another and effectively reducing the effect of back flowing shock waves moving towards upstream. The detonation tubes may be non-linear, and may have independent discharges. The independent discharges may be coupled to an adapter nozzle terminating in a combined exhaust outlet.

    Abstract translation: 本文公开了一种无阀多管脉冲爆震发动机，其包括：多个爆管，其中每个爆管包括独立的排放口，并且多个引爆管在公共空气/燃料混合物进气口处相互连接。 在所公开的发动机中，空气和燃料混合物同时在引爆管中引爆，并且公共空气/燃料混合物进气口通过将多个反向冲击波相互引导并有效地使由空气/燃料混合物引爆引起的背压最小化 使用背压作为彼此的反应表面，并且有效地减少向上游移动的回流冲击波的影响。 引爆管可以是非线性的，并且可以具有独立的放电。 独立放电可以连接到终止于组合排气出口的适配器喷嘴。

    PRESSURE-GAIN COMBUSTION APPARATUS AND METHOD
    75.
    发明申请
    PRESSURE-GAIN COMBUSTION APPARATUS AND METHOD 审中-公开

    公开(公告)号：US20190093880A1

    公开(公告)日：2019-03-28

    申请号：US16110722

    申请日：2018-08-23

    Applicant: EXPONENTIAL TECHNOLOGIES, INC.

    Inventor： ALEJANDRO JUAN

    IPC: F23C3/00 ,  F23C15/00 ,  F23R7/00

    Abstract: A pressure gain combustor comprises a detonation chamber, a pre-combustion chamber, an oxidant swirl generator, an expansion-deflection (E-D) nozzle, and an ignition source. The detonation chamber has an upstream intake end and a downstream discharge end, and is configured to allow a supersonic combustion event to propagate therethrough. The pre-combustion chamber has a downstream end in fluid communication with the detonation chamber intake end, an upstream end in communication with a fuel delivery pathway, and a circumferential perimeter between the upstream and downstream ends with an annular opening in communication with an annular oxidant delivery pathway. The oxidant swirl generator is located in the oxidant delivery pathway and comprises vanes configured to cause oxidant flowing past the vanes to flow tangentially into the pre-combustion chamber thereby creating a high swirl velocity zone around the annular opening and a low swirl velocity zone in a central portion of the pre-combustion chamber. The E-D nozzle is positioned in between the pre-combustion chamber and detonation chamber and provides a diffusive fluid pathway therebetween. The ignition source is in communication with the low swirl velocity zone of the pre-combustion chamber. This configuration is expected to provide a combustor with a relatively low total run-up DDT distance and time, thereby enabling high operating frequencies and corresponding high combustor performance.

    Segmented Positive Displacement Rotor Housing
    78.
    发明申请
    Segmented Positive Displacement Rotor Housing 审中-公开
    分段正位移转子壳体

    公开(公告)号：US20150260184A1

    公开(公告)日：2015-09-17

    申请号：US14215609

    申请日：2014-03-17

    Applicant: Exponential Technologies, Inc.

    Inventor： Erik Farrell ,  Alejandro Juan ,  Curtis Patterson ,  Stephen F. Scott ,  Kyle Fiolka

    IPC: F04C3/08 ,  F04C15/00

    CPC classification number: F04C3/08 ,  F04C2/084 ,  F04C15/0003 ,  F04C15/0057 ,  F04C15/0076 ,  Y10T29/53

    Abstract: This disclosure concerns an advanced nutating positive displacement device having a high power to mass ratio and low production cost. This device in one example forms an exemplary pump as will be discussed in detail. The examples disclosed herein are of the rotary positive displacement type, but in a class by themselves. The devices are formed by a nutating rotor having a face comprising lobes and valleys, and a fixed stator also having a face with lobes and valleys. The face of the rotor opposes and cooperates with the face of the stator. The opposing faces define chambers that change volume with rotation of the rotor.

    Abstract translation: 本公开涉及具有高功率质量比和低生产成本的先进的章动正位移装置。 在一个示例中，该装置形成示例性泵，如将在下面详细讨论的。 本文公开的实例是旋转正位移型，但是在一个类中。 这些装置由具有包括裂片和谷部的面的章动转子和固定的定子构成，该定子还具有带有凸起和谷部的面。 转子的表面与定子的表面相反并配合。 相对的面限定了随转子旋转而改变体积的室。

    Pressure balancing system for a fluid pump
    80.
    发明授权
    Pressure balancing system for a fluid pump 有权

    公开(公告)号：US11168683B2

    公开(公告)日：2021-11-09

    申请号：US16817049

    申请日：2020-03-12

    Applicant: Exponential Technologies, Inc.

    Inventor： Kristjan Gottfried ,  Erik Farrell ,  Michael Sereda-Mohr

    IPC: F04C3/06 ,  F04C29/00 ,  F04C15/00

    Abstract: A pressure balancing system for a pump. In one example, the pressure balancing system has: a housing; a first rotor a first shaft, a first face surface; a second rotor, a second face surface adjacent the first face surface of the first rotor; the face of the first rotor, the face of the second rotor, and an inner surface of the housing forming at least one working fluid chamber; an annular ring fitted around a shaft, adjacent a first pressure chamber having a fluid connection through the housing; the annular ring configured to bias the first rotor toward the second rotor when fluid is supplied under pressure to the first pressure chamber; a fluid conduit is configured to convey fluid to a pressure chamber between the housing and the annular ring to bias the annular ring thus biasing the first rotor toward the second rotor.

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