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公开(公告)号：WO2018191082A1
公开(公告)日：2018-10-18
申请号：PCT/US2018/026124
申请日：2018-04-04
Applicant: SWIFT ENGINEERING, INC.
Inventor： STREETT, Andrew , ROCKLINGER, Marc , LIU, Xuewu
Abstract: A system for measuring water quality parameters, such as pH, CO2, alkalinity, and so forth, includes sensors or other measuring components integrated onto a circuit board. The circuit board may be contained within a submersible, watertight housing. A spectrophotometer may be located on the circuit board to measure the wavelength and intensity of light transmitted through the water being tested. Sensors for measuring salinity, pressure, temperature, or other properties may also be included on or near the circuit board. A microcontroller for processing these measurements is located on the circuit board. System components used to direct and filter the water, such as certain pumps, filters, and so forth, may be included in the housing off of the circuit board. Integrating the sensors and other measuring components onto a circuit board allows for a compact, low-cost water-quality-measuring system that is capable of making very accurate and precise measurements.
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公开(公告)号：WO2007149654A3
公开(公告)日：2008-12-04
申请号：PCT/US2007068846
申请日：2007-05-14
Applicant: SWIFT ENGINEERING INC , MCCUE MATTHEW R , SCHAFER DON
Inventor： MCCUE MATTHEW R , SCHAFER DON
IPC: F02M37/04
Abstract: The present invention provides a fuel injection system in which fuel is delivered to the engine by varying the fuel pump pressure creating a variable flow rate through a fuel injector. The system comprises an engine control unit, a variable DC brushless motor fuel pump, and a fuel injector, wherein the engine control unit drives and varies the pump rate of the fuel pump to vary the fuel flow rate to the engine.
Abstract translation: 本发明提供一种燃料喷射系统，其中燃料通过改变燃料泵压力而被输送到发动机，从而产生通过燃料喷射器的可变流量。 该系统包括发动机控制单元，可变直流无刷电动机燃料泵和燃料喷射器，其中发动机控制单元驱动和改变燃料泵的泵送速率以改变对发动机的燃料流量。
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公开(公告)号：WO2007149654A2
公开(公告)日：2007-12-27
申请号：PCT/US2007/068846
申请日：2007-05-14
Applicant: SWIFT ENGINEERING, INC. , McCUE, Matthew, R. , SCHAFER, Don
Inventor： McCUE, Matthew, R. , SCHAFER, Don
Abstract: The present invention provides a fuel injection system in which fuel is delivered to the engine by varying the fuel pump pressure creating a variable flow rate through a fuel injector. The system comprises an engine control unit, a variable DC brushless motor fuel pump, and a fuel injector, wherein the engine control unit drives and varies the pump rate of the fuel pump to vary the fuel flow rate to the engine.
Abstract translation: 本发明提供一种燃料喷射系统，其中燃料通过改变燃料泵压力而被输送到发动机，从而产生通过燃料喷射器的可变流量。 该系统包括发动机控制单元，可变直流无刷电动机燃料泵和燃料喷射器，其中发动机控制单元驱动和改变燃料泵的泵送速率以改变对发动机的燃料流量。
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公开(公告)号：WO2004044544A2
公开(公告)日：2004-05-27
申请号：PCT/US2003/036215
申请日：2003-11-13
Applicant: SWIFT ENGINEERING, INC.
Inventor： PAGE, Mark , ROBERTS, Neil , HUSCHILT, Tom , KANE, Brian , WINKLER, John
IPC: G01M9/02
Abstract: A positioning system is provided for use in a wind tunnel that results in accurate and dynamic orientation for a model while reducing aerodynamic interference. The system includes a pitch-yaw sleeve having a generally cylindrical shape and a torque tube disposed askew within the sleeve and rotatable about its longitudinal axis to drive a shaft. The shaft is generally elongated and crooked. The sting, to which a model is affixed, is rotatably attached to a distal end of the shaft. Rotation of the pitch-yaw tube and/or the pitch-yaw sleeve provides precise pitch and yaw orientation of the model, and rotation of the sting relative to the shaft provides precise roll orientation.
Abstract translation: 提供了一种在风洞中使用的定位系统，其导致模型的精确和动态取向，同时减少空气动力学干扰。 该系统包括具有大致圆柱形形状的俯仰偏航套管和扭矩管，该扭矩管在套筒内设置成歪斜并能围绕其纵向轴线旋转以驱动轴。 轴通常是细长的和弯曲的。 固定有模型的刺刺可旋转地附接到轴的远端。 俯仰偏转管和/或俯仰偏航套筒的旋转提供了模型的精确俯仰和偏转方位，并且刺刺相对于轴的旋转提供了精确的滚动方向。
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公开(公告)号：WO2015108578A3
公开(公告)日：2015-09-03
申请号：PCT/US2014060166
申请日：2014-10-10
Applicant: SWIFT ENGINEERING INC
Inventor： GODLASKY ROBERT , OGAWA NATE , STREETT ANDREW
CPC classification number: B64D27/02 , B64C29/02 , B64C39/024 , B64C2201/021 , B64C2201/088 , B64C2201/102
Abstract: A VTOL aircraft includes at least one puller rotor and at least one pusher rotor. The VTOL aircraft, for example, may include three puller rotors and one pusher rotor. The combination of static puller and pusher rotors allows the rotors to remain in a fixed orientation (i.e., no moving mechanical axes are required) relative to the wings and fuselage of the VTOL aircraft, while being able to transition the aircraft from a substantially vertical flight path to a substantially horizontal flight path.
Abstract translation: 垂直起落飞行器包括至少一个牵引转子和至少一个推动器转子。 例如，VTOL飞机可以包括三个牵引转子和一个推动器转子。 静态牵引器和推动器转子的组合允许转子相对于垂直起降飞机的机翼和机身保持在固定方向（即，不需要移动的机械轴），同时能够使飞机从基本垂直的飞行 到达基本水平的飞行路径的路径。
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Patent Agency Ranking
公开(公告)号：WO2004044544A3
公开(公告)日：2005-05-19
申请号：PCT/US0336215
申请日：2003-11-13
Applicant: SWIFT ENGINEERING INC
Inventor： PAGE MARK , ROBERTS NEIL , HUSCHILT TOM , KANE BRIAN , WINKLER JOHN
Abstract: A positioning system (10) is provided for use in a wind tunnel (12) that results in accurate and dynamic orientation for a model (14) while reducing aerodynamic interference. The system includes a pitch-yaw sleeve (36) having a generally cylindrical shape and a torque tube disposed askew within the sleeve and rotatable about its longitudinal axis to drive a shaft. The shaft is generally elongated and crooked. The sting, to which a model is affixed, is rotatably attached to a distal end of the shaft. Rotation of the pitch-yaw tube (38) and/or the pitch-yaw sleeve (36) provides precise pitch and yaw orientation of the model (14), and rotation of the sting relative to the shaft provides precise roll orientation.
Abstract translation: 提供了一种用于风洞（12）中的定位系统（10），其导致模型（14）的精确和动态取向，同时减少空气动力学干扰。 该系统包括具有大致圆柱形形状的俯仰偏转套筒（36）和扭矩管，扭矩管在套筒内倾斜设置，并可围绕其纵向轴线旋转以驱动轴。 轴通常是细长的和弯曲的。 固定有模型的刺刺可旋转地附接到轴的远端。 俯仰偏转管（38）和/或俯仰偏转套管（36）的旋转提供了模型（14）的精确俯仰和偏转定向，并且刺刺相对于轴的旋转提供了精确的滚动取向。
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公开(公告)号：EP3057867A2
公开(公告)日：2016-08-24
申请号：EP14878419.2
申请日：2014-10-10
Applicant: Swift Engineering, Inc.
Inventor： GODLASKY, Robert , OGAWA, Nate , STREETT, Andrew
CPC classification number: B64D27/02 , B64C29/02 , B64C39/024 , B64C2201/021 , B64C2201/088 , B64C2201/102
Abstract: A VTOL aircraft includes at least one puller rotor and at least one pusher rotor. The VTOL aircraft, for example, may include three puller rotors and one pusher rotor. The combination of static puller and pusher rotors allows the rotors to remain in a fixed orientation (i.e., no moving mechanical axes are required) relative to the wings and fuselage of the VTOL aircraft, while being able to transition the aircraft from a substantially vertical flight path to a substantially horizontal flight path.
Abstract translation: 垂直起降飞机包括至少一个牵引转子和至少一个推动器转子。 例如，VTOL飞机可以包括三个牵引转子和一个推动器转子。 静态牵引器和推动器转子的组合允许转子相对于垂直起降飞机的机翼和机身保持在固定的方向（即，不需要移动的机械轴），同时能够使飞机从基本垂直的飞行 到大致水平的飞行路径的路径。
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公开(公告)号：EP3439951A2
公开(公告)日：2019-02-13
申请号：EP17786296.8
申请日：2017-03-14
Applicant: Swift Engineering, Inc.
Inventor： MOSHE, Jonathan
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公开(公告)号：EP3631479A1
公开(公告)日：2020-04-08
申请号：EP18806797.9
申请日：2018-05-18
Applicant: Swift Engineering, Inc.
Inventor： STREETT, Andrew , BROWN, Bryan
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公开(公告)号：EP3610255A1
公开(公告)日：2020-02-19
申请号：EP18784390.9
申请日：2018-04-04
Applicant: Swift Engineering, Inc.
Inventor： STREETT, Andrew , ROCKLINGER, Marc , LIU, Xuewu
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