COMPACT AERO-THERMO MODEL BASED CONTROL SYSTEM

    公开(公告)号:US20190093566A1

    公开(公告)日:2019-03-28

    申请号:US16203995

    申请日:2018-11-29

    Abstract: Systems and methods for controlling a fluid-based system are disclosed. The systems and methods may include a model processor for generating a model output, the model processor including a set state module for setting dynamic states, the dynamic states input to an open loop model based on the model operating mode, where the open loop model generates current state derivatives, solver state errors, and synthesized parameters as a function of the dynamic states and a model input vector. A constraint on the state derivatives and solver state errors is based a series of utilities that are based on mathematical abstractions of physical laws that govern behavior of the component. The model processor may include an estimate state module for determining an estimated state of the model based on at least one of a prior state, the current state derivatives, the solver state errors, and the synthesized parameters.

    Compact aero-thermo model based engine material temperature control

    公开(公告)号:US10161313B2

    公开(公告)日:2018-12-25

    申请号:US14768002

    申请日:2014-03-14

    Abstract: Systems and methods for controlling a fluid based system are disclosed. The systems and methods may include a model processor for generating a model output, the model processor including a set state module for setting dynamic states, the dynamic states input to an open loop model based on the model operating mode, where the open loop model generates current state derivatives, solver state errors, and synthesized parameters as a function of the dynamic states and a model input vector. A constraint on the state derivatives and solver state errors is based on a material temperature utility for determining a material temperature associated with a component of the cycle of the control system. The model processor may include an estimate state module for determining an estimated state of the model based on at least one of a prior state, the current state derivatives, the solver state errors, and the synthesized parameters.

    COMPACT AERO-THERMO MODEL BASED CONTROL SYSTEM
    4.
    发明申请
    COMPACT AERO-THERMO MODEL BASED CONTROL SYSTEM 审中-公开
    基于AERO-THERMO模型的控制系统

    公开(公告)号:US20160003165A1

    公开(公告)日:2016-01-07

    申请号:US14770543

    申请日:2014-03-14

    Abstract: Systems and methods for controlling a fluid based engineering system are disclosed. The systems and methods may include a model processor for generating a model output, the model processor including a set state module for setting dynamic states of the model processor, the dynamic states input to an open loop model based on the model operating mode, wherein the open loop model generates a current state model as a function of the dynamic states and the model input, wherein a constraint on the current state model is based a series of cycle synthesis modules, each member of the series of cycle synthesis modules modeling a component of a cycle of the control system and including a series of utilities, the utilities are based on mathematical abstractions of physical properties associated with the component. The model processor may further include an estimate state module for determining an estimated state of the model based on a prior state model output and the current state model of the open loop model.

    Abstract translation: 公开了用于控制基于流体的工程系统的系统和方法。 系统和方法可以包括用于生成模型输出的模型处理器,模型处理器包括用于设置模型处理器的动态状态的设置状态模块,基于模型操作模式输入到开环模型的动态状态,其中, 开环模型生成作为动态和模型输入的函数的当前状态模型,其中对当前状态模型的约束基于一系列循环综合模块,该系列循环综合模块的每个成员对 控制系统的一个循环并且包括一系列实用程序,该实用程序基于与组件相关联的物理属性的数学抽象。 模型处理器还可以包括用于基于先前状态模型输出和开环模型的当前状态模型来确定模型的估计状态的估计状态模块。

    Compact Aero-Thermo Model Based Tip Clearance Management
    5.
    发明申请
    Compact Aero-Thermo Model Based Tip Clearance Management 审中-公开
    基于紧凑型航空 - 热模型的尖端间隙管理

    公开(公告)号:US20150378364A1

    公开(公告)日:2015-12-31

    申请号:US14765953

    申请日:2014-03-14

    Abstract: Systems and methods for controlling a fluid based engineering system are disclosed. The systems and methods may include a model processor for generating a model output, the model processor including a set state module for setting dynamic states of the model processor, the dynamic states input to an open loop model based on the model operating mode, wherein the open loop model generates a current state model as a function of the dynamic states and the model input, wherein a constraint on the current state model is based a series of cycle synthesis modules, each member of the series of cycle synthesis modules modeling a component of a cycle of the control system and including a series of utilities, the utilities are based on mathematical abstractions of physical properties associated with the component, the series of cycle synthesis modules including a rotary apparatus module which estimates a tip clearance between the rotor and the rotor case. The model processor may further include an estimate state module for determining an estimated state of the model based on a prior state model output and the current state model of the open loop model.

    Abstract translation: 公开了用于控制基于流体的工程系统的系统和方法。 系统和方法可以包括用于生成模型输出的模型处理器,模型处理器包括用于设置模型处理器的动态状态的设置状态模块,基于模型操作模式输入到开环模型的动态状态,其中, 开环模型生成作为动态和模型输入的函数的当前状态模型,其中对当前状态模型的约束基于一系列循环综合模块,该系列循环综合模块的每个成员对 该控制系统的循环并且包括一系列实用程序,该实用程序基于与该组件相关联的物理性质的数学抽象,所述一系列循环综合模块包括估计转子和转子之间的顶端间隙的旋转装置模块 案件。 模型处理器还可以包括用于基于先前状态模型输出和开环模型的当前状态模型来确定模型的估计状态的估计状态模块。

    Compact aero-thermo model based control system

    公开(公告)号:US10767563B2

    公开(公告)日:2020-09-08

    申请号:US16203995

    申请日:2018-11-29

    Abstract: Systems and methods for controlling a fluid-based system are disclosed. The systems and methods may include a model processor for generating a model output, the model processor including a set state module for setting dynamic states, the dynamic states input to an open loop model based on the model operating mode, where the open loop model generates current state derivatives, solver state errors, and synthesized parameters as a function of the dynamic states and a model input vector. A constraint on the state derivatives and solver state errors is based a series of utilities that are based on mathematical abstractions of physical laws that govern behavior of the component. The model processor may include an estimate state module for determining an estimated state of the model based on at least one of a prior state, the current state derivatives, the solver state errors, and the synthesized parameters.

    COMPACT AERO-THERMO MODEL BASED ENGINE MATERIAL TEMPERATURE CONTROL

    公开(公告)号:US20190107057A1

    公开(公告)日:2019-04-11

    申请号:US16205351

    申请日:2018-11-30

    Abstract: Systems and methods for controlling a fluid-based system are disclosed. The systems and methods may include a model processor for generating a model output, the model processor including a set state module for setting dynamic states, the dynamic states input to an open loop model based on the model operating mode, where the open loop model generates current state derivatives, solver state errors, and synthesized parameters as a function of the dynamic states and a model input vector. A constraint on the current state derivatives and solver state errors is based on mathematical abstractions of physical laws that govern behavior of a component using a material temperature utility. The model processor may further include an estimate state module for determining an estimated state of the model based on at least one of a prior state, the current state derivatives, the solver state errors, and the synthesized parameters.

    Compact aero-thermo model based tip clearance management

    公开(公告)号:US10190503B2

    公开(公告)日:2019-01-29

    申请号:US14765953

    申请日:2014-03-14

    Abstract: Systems and methods for controlling a fluid based engineering system are disclosed. The systems and methods may include a model processor for generating a model output, the model processor including a set state module for setting dynamic states of the model processor, the dynamic states input to an open loop model based on the model operating mode, wherein the open loop model generates a current state model as a function of the dynamic states and the model input, wherein a constraint on the current state model is based a series of cycle synthesis modules, each member of the series of cycle synthesis modules modeling a component of a cycle of the control system and including a series of utilities, the utilities are based on mathematical abstractions of physical properties associated with the component, the series of cycle synthesis modules including a rotary apparatus module which estimates a tip clearance between the rotor and the rotor case. The model processor may further include an estimate state module for determining an estimated state of the model based on a prior state model output and the current state model of the open loop model.

    Compact Aero-Thermo Model Based Engine Material Temperature Control
    9.
    发明申请
    Compact Aero-Thermo Model Based Engine Material Temperature Control 审中-公开
    基于紧凑型航空热模型的发动机材料温度控制

    公开(公告)号:US20160017814A1

    公开(公告)日:2016-01-21

    申请号:US14768002

    申请日:2014-03-14

    Abstract: Systems and methods for controlling a fluid based engineering system are disclosed. The systems and methods may include a model processor for generating a model output, the model processor including a set state module for setting dynamic states of the model processor, the dynamic states input to an open loop model based on the model operating mode, wherein the open loop model generates a current state model as a function of the dynamic states and the model input, wherein a constraint on the current state model is based a series of cycle synthesis modules, each member of the series of cycle synthesis modules modeling a component of a cycle of the control system and including a series of utilities, the utilities are based on mathematical abstractions of physical properties associated with the component. The series of utilities may include a material temperature utility for determining a material temperature associated with a component of the cycle of the control system The model processor may further include an estimate state module for determining an estimated state of the model based on a prior state model output and the current state model of the open loop model.

    Abstract translation: 公开了用于控制基于流体的工程系统的系统和方法。 系统和方法可以包括用于生成模型输出的模型处理器,模型处理器包括用于设置模型处理器的动态状态的设置状态模块,基于模型操作模式输入到开环模型的动态状态,其中, 开环模型生成作为动态和模型输入的函数的当前状态模型,其中对当前状态模型的约束基于一系列循环综合模块,该系列循环综合模块的每个成员对 控制系统的一个循环并且包括一系列实用程序,该实用程序基于与组件相关联的物理属性的数学抽象。 一系列实用程序可以包括用于确定与控制系统的循环的组件相关联的材料温度的材料温度实用程序。模型处理器还可以包括用于基于先前状态模型来确定模型的估计状态的估计状态模块 输出和开环模型的当前状态模型。

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