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    Compact aero-thermo model based control system
    1.
    发明授权
    Compact aero-thermo model based control system 有权

    公开(公告)号：US10767563B2

    公开(公告)日：2020-09-08

    申请号：US16203995

    申请日：2018-11-29

    Applicant: United Technologies Corporation

    Inventor： Boris Karpman ,  Thomas Niemczycki ,  Ian Michael Dinsmore ,  David Sembiante ,  Robert H. Luppold

    IPC: F02C7/26 ,  G05B17/02 ,  F02C9/20 ,  G05D7/06 ,  F01D21/00 ,  F02C9/16 ,  F02C3/04 ,  F04D29/32 ,  G05B13/04 ,  G05B23/02

    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 CONTROL SYSTEM
    2.
    发明申请
    COMPACT AERO-THERMO MODEL BASED CONTROL SYSTEM 审中-公开

    公开(公告)号：US20190093566A1

    公开(公告)日：2019-03-28

    申请号：US16203995

    申请日：2018-11-29

    Applicant: United Technologies Corporation

    Inventor： Boris Karpman ,  Thomas Niemczycki ,  Ian Michael Dinsmore ,  David Sembiante ,  Robert H. Luppold

    IPC: F02C7/26 ,  F02C9/16 ,  G05B13/04 ,  F04D29/32 ,  F02C3/04 ,  F02C9/20 ,  G05D7/06 ,  G05B17/02 ,  F01D21/00 ,  G05B23/02

    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.

    Leak detection, isolation and accommodation assembly for gas turbine engines
    6.
    发明授权
    Leak detection, isolation and accommodation assembly for gas turbine engines 有权

    公开(公告)号：US10260425B2

    公开(公告)日：2019-04-16

    申请号：US15147173

    申请日：2016-05-05

    Applicant: United Technologies Corporation

    Inventor： Timothy J. Crowley ,  Tyler J. Selstad ,  Sorin Bengea ,  Robert H. Luppold

    IPC: F02C7/22 ,  F02C7/232 ,  F02C7/236 ,  F02C9/00 ,  F02C9/28

    Abstract: A fuel system for a gas turbine engine includes, among other things, a plurality of components defining a plurality of localized nodes at distinct locations relative to a fuel flow path, each of the plurality of localized nodes characterized by a distinct set of failure parameters. One or more fuel sensors are configured to measure at least one fuel condition relating to flow through the fuel flow path. A fuel observation assembly is coupled to one or more engine sensors configured to measure at least one engine condition. The fuel observation assembly comprises an estimation module operable to calculate an expected condition of each of the plurality of localized nodes based upon the set of failure parameters, an observation module operable to calculate an observed condition of each of the plurality of localized nodes, the observed condition based on present values of the at least one fuel condition and the at least one engine condition, and a comparison module operable to determine an abnormality corresponding to a first one of the plurality of localized nodes based upon a comparison of the expected condition and the observed condition for each of the plurality of localized nodes.

    LEAK DETECTION, ISOLATION AND ACCOMMODATION ASSEMBLY FOR GAS TURBINE ENGINES
    7.
    发明申请
    LEAK DETECTION, ISOLATION AND ACCOMMODATION ASSEMBLY FOR GAS TURBINE ENGINES 审中-公开

    公开(公告)号：US20170321608A1

    公开(公告)日：2017-11-09

    申请号：US15147173

    申请日：2016-05-05

    Applicant: United Technologies Corporation

    Inventor： Timothy J. Crowley ,  Tyler J. Selstad ,  Sorin Bengea ,  Robert H. Luppold

    IPC: F02C7/22 ,  F02C7/232 ,  F02C7/236

    CPC classification number: F02C7/222 ,  F02C7/22 ,  F02C7/232 ,  F02C7/236 ,  F02C9/00 ,  F02C9/28 ,  F05D2220/32 ,  F05D2260/80

    Abstract: A fuel system for a gas turbine engine includes, among other things, a plurality of components defining a plurality of localized nodes at distinct locations relative to a fuel flow path, each of the plurality of localized nodes characterized by a distinct set of failure parameters. One or more fuel sensors are configured to measure at least one fuel condition relating to flow through the fuel flow path. A fuel observation assembly is coupled to one or more engine sensors configured to measure at least one engine condition. The fuel observation assembly comprises an estimation module operable to calculate an expected condition of each of the plurality of localized nodes based upon the set of failure parameters, an observation module operable to calculate an observed condition of each of the plurality of localized nodes, the observed condition based on present values of the at least one fuel condition and the at least one engine condition, and a comparison module operable to determine an abnormality corresponding to a first one of the plurality of localized nodes based upon a comparison of the expected condition and the observed condition for each of the plurality of localized nodes.

    COMPACT AERO-THERMO MODEL BASED CONTROL SYSTEM
    8.
    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

    Applicant: UNITED TECHNOLOGIES CORPORATION

    Inventor： Boris Karpman ,  Thomas Niemczycki ,  Ian Michael Dinsmore ,  David Sembiante ,  Robert H. Luppold ,  Matthew Donald

    IPC: F02C9/16 ,  G05B17/02

    CPC classification number: F02C7/26 ,  F01D21/003 ,  F02C3/04 ,  F02C9/16 ,  F02C9/20 ,  F04D29/321 ,  F04D29/325 ,  F05D2220/32 ,  F05D2240/35 ,  F05D2260/81 ,  F05D2260/85 ,  G05B13/04 ,  G05B17/02 ,  G05B23/0254 ,  G05D7/0629

    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。

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