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公开(公告)号：US20240271560A1
公开(公告)日：2024-08-15
申请号：US18641320
申请日：2024-04-19
申请人： William Todd Hodges
发明人： William Todd Hodges
CPC分类号： F02B55/04 , F02B53/10 , F02B53/12 , F02B55/08 , F02M25/028 , F02B2053/005
摘要： A rotary engine has a rotor with a rotor pocket for receiving air-fuel mixture that is combusted therein to propel the rotor within the housing. The rotary engine may have one or more intake spray injectors that spray fuel into the rotor pocket and onto the rotor face within the intake chamber to effectively cool the rotor pocket and rotor face. An air channel extension of the rotor pocket may be configured in the housing and/or in the rotor to extend from the compression chamber into the ignition-combustion chamber to relieve some pressure in the trailing compression chamber of a rotor face to minimize negative work. A supplemental air-fuel conduit may be configured to supply high-pressure gas from the compression chamber to an ignition injector(s). A thrust nozzle may be configured within the rotor pocket to direct combustion gases therethrough to propel the rotor and increase efficiency.
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公开(公告)号：US1531184A
公开(公告)日：1925-03-24
申请号：US60070822
申请日：1922-11-13
申请人： TODD HODGES HENRY
发明人： TODD HODGES HENRY
IPC分类号： A47C7/56
CPC分类号： A47C7/56
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公开(公告)号：US11506116B2
公开(公告)日：2022-11-22
申请号：US17734144
申请日：2022-05-02
申请人： William Todd Hodges
发明人： William Todd Hodges
摘要： A rotary engine has a rotor with a rotor pocket for receiving air-fuel mixture that is combusted therein to propel the rotor within the housing. The rotary engine may have one or more intake spray injectors that spray fuel into the rotor pocket and onto the rotor face within the intake chamber to effectively cool the rotor pocket and rotor face. An air channel extension of the rotor pocket may be configured in the housing and/or in the rotor to extend from the compression chamber into the ignition-combustion chamber to relieve some pressure in the trailing compression chamber of a rotor face to minimize negative work. A supplemental air-fuel conduit may be configured to supply high-pressure gas from the compression chamber to an ignition injector(s). A thrust nozzle may be configured within the rotor pocket to direct combustion gases therethrough to propel the rotor and increase efficiency.
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公开(公告)号：US20220260010A1
公开(公告)日：2022-08-18
申请号：US17734144
申请日：2022-05-02
申请人： William Todd Hodges
发明人： William Todd Hodges
摘要： A rotary engine has a rotor with a rotor pocket for receiving air-fuel mixture that is combusted therein to propel the rotor within the housing. The rotary engine may have one or more intake spray injectors that spray fuel into the rotor pocket and onto the rotor face within the intake chamber to effectively cool the rotor pocket and rotor face. An air channel extension of the rotor pocket may be configured in the housing and/or in the rotor to extend from the compression chamber into the ignition-combustion chamber to relieve some pressure in the trailing compression chamber of a rotor face to minimize negative work. A supplemental air-fuel conduit may be configured to supply high-pressure gas from the compression chamber to an ignition injector(s). A thrust nozzle may be configured within the rotor pocket to direct combustion gases therethrough to propel the rotor and increase efficiency.
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公开(公告)号：US11365706B2
公开(公告)日：2022-06-21
申请号：US17128080
申请日：2020-12-19
申请人： William Todd Hodges
发明人： William Todd Hodges
摘要： A turbine engine system utilizes one or more augmented combustion modules to produce an exhaust that is fed into the turbine portion of the engine and wherein power is produced by the augmented combustion module for use to drive the main shaft and/or for auxiliary purposes. An augmented combustion module is configured between the compressor and the turbine of the engine and receives compressed air from the compressor and ignites an air/fuel-mixture to turn a shaft that can be used to produce power. The shaft may be coupled with an electrical power generator, a pump, a hydraulic or pneumatic power generator and/or power conversion or transmission devices and/or coupled with the main shaft of the turbine engine. The power from a power generator may be stored in a battery, hydraulic accumulator or pneumatic accumulator and may be used to power auxiliary electrical, hydraulic or pneumatic devices.
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公开(公告)号：US20220136460A1
公开(公告)日：2022-05-05
申请号：US17128080
申请日：2020-12-19
申请人： William Todd Hodges
发明人： William Todd Hodges
IPC分类号： F02K5/02
摘要： A turbine engine system utilizes one or more augmented combustion modules to produce an exhaust that is fed into the turbine portion of the engine and wherein power is produced by the augmented combustion module for use to drive the main shaft and/or for auxiliary purposes. An augmented combustion module is configured between the compressor and the turbine of the engine and receives compressed air from the compressor and ignites an air/fuel-mixture to turn a shaft that can be used to produce power. The shaft may be coupled with an electrical power generator, a pump, a hydraulic or pneumatic power generator and/or power conversion or transmission devices and/or coupled with the main shaft of the turbine engine. The power from a power generator may be stored in a battery, hydraulic accumulator or pneumatic accumulator and may be used to power auxiliary electrical, hydraulic or pneumatic devices.
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公开(公告)号：US20070195975A1
公开(公告)日：2007-08-23
申请号：US11175629
申请日：2005-07-06
申请人： Davis Cotton , Ian Esten , Todd Hodges , Bobby Lombardi , Joseph Saracino , James West , David Willenbrink
发明人： Davis Cotton , Ian Esten , Todd Hodges , Bobby Lombardi , Joseph Saracino , James West , David Willenbrink
摘要： A gain reduction meter for dynamics processing provides information describing which part of a dynamics curve is affecting the input signal. In particular, the gain reduction meter displays an amount of gain reduction due to applying a dynamics processing operation in a manner that differentiates between gain reduction achieved by the different parts of the dynamics curve for that dynamics processing operation. The gain reduction meter has a plurality of display elements. Each display element corresponds to an amount of gain reduction. The illumination of the display elements is controlled such that the appearance of each illuminated display element is dependent on where on the dynamics curve the amount of gain reduction corresponding to that display element is produced.
摘要翻译： 用于动力学处理的增益减小表提供描述动态曲线的哪一部分影响输入信号的信息。 特别地，增益减小表显示出由于以对该动力学处理操作的动力学曲线的不同部分所获得的增益减小进行区分的方式应用动力学处理操作来显示增益减小量。 增益减小计具有多个显示元件。 每个显示元素对应于减少增益的量。 控制显示元件的照明，使得每个照亮的显示元件的外观取决于动态曲线上的哪个位置产生对应于该显示元件的增益减小量。
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公开(公告)号：US20230113272A1
公开(公告)日：2023-04-13
申请号：US17991230
申请日：2022-11-21
申请人： William Todd Hodges
发明人： William Todd Hodges
摘要： A rotary combustion engine, such as a Wankel engine has a rotor with a rotor pocket for receiving air-fuel mixture that is combusted therein to propel the rotor within the housing. Rotor air channels extend from an inlet that is configured in the compression chamber to an outlet configured in the rotor pocket to deliver compressed air-fuel mixture to said rotor pocket. The rotor air channels have an open portion, open on the face of the rotor and a closed portion extending as a conduit into the rotor to the rotor pocket. Fuel may be delivered to the rotor air channel from a rotor-gear fuel conduit that receives fuel from the fixed gear or a side-wall fuel conduit that receives fuel from a housing side-wall injector through a side-wall fuel transfer port. Rotor air channels may be configured to direct air-fuel streams to intercept one another to enhance combustion.
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公开(公告)号：US11619165B1
公开(公告)日：2023-04-04
申请号：US17991230
申请日：2022-11-21
申请人： William Todd Hodges
发明人： William Todd Hodges
摘要： A rotary combustion engine, such as a Wankel engine has a rotor with a rotor pocket for receiving air-fuel mixture that is combusted therein to propel the rotor within the housing. Rotor air channels extend from an inlet that is configured in the compression chamber to an outlet configured in the rotor pocket to deliver compressed air-fuel mixture to said rotor pocket. The rotor air channels have an open portion, open on the face of the rotor and a closed portion extending as a conduit into the rotor to the rotor pocket. Fuel may be delivered to the rotor air channel from a rotor-gear fuel conduit that receives fuel from the fixed gear or a side-wall fuel conduit that receives fuel from a housing side-wall injector through a side-wall fuel transfer port. Rotor air channels may be configured to direct air-fuel streams to intercept one another to enhance combustion.
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