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    Method for regulating a thermodynamic process by means of neural networks
    11.
    发明申请
    Method for regulating a thermodynamic process by means of neural networks 审中-公开
    通过神经网络调节热力学过程的方法

    公开(公告)号：US20050137995A1

    公开(公告)日：2005-06-23

    申请号：US11058111

    申请日：2005-02-15

    Applicant: Franz Wintrich ,  Volker Stephan ,  Dirk Tiedtke

    Inventor： Franz Wintrich ,  Volker Stephan ,  Dirk Tiedtke

    IPC: G05B13/02 ,  G06N3/08 ,  G06F15/00 ,  G06F15/18 ,  G06F17/00 ,  G06N3/10 ,  G06N5/02

    CPC classification number: G05B13/027

    Abstract: In a method for regulating a thermodynamic process, in which process variables in the system are measured, predictions are calculated in a neural network on the basis of a trained, current process model and compared with optimization objectives and actions suitable for regulating the process are carried out in the system, at the same time the process is automatically analyzed and at least one new process model is formed, trained and compared with the current process model with respect to the predictions.

    Abstract translation: 在一种用于调节热力学过程的方法中，其中测量系统中的过程变量，在神经网络中基于训练有素的当前过程模型计算预测，并与适用于调节过程的优化目标和动作进行比较 在系统中，同时自动分析过程，并形成至少一个新的过程模型，并对与预测相关的当前过程模型进行训练和比较。

    Method for the control of aero gas turbine engines
    12.
    发明授权
    Method for the control of aero gas turbine engines 失效
    用于控制航空燃气涡轮发动机的方法

    公开(公告)号：US06712314B2

    公开(公告)日：2004-03-30

    申请号：US10012376

    申请日：2001-12-12

    Applicant: Volker Stephan

    Inventor： Volker Stephan

    IPC: B64D3100

    CPC classification number: F02C9/42 ,  B64C11/50 ,  B64D31/12 ,  Y02T50/671

    Abstract: The exchange, removal or addition, as applicable, of media and/or power is provided between the individual shafts of an engine, between individual engines and between the engines and the aircraft. Thus, additional degrees of freedom are provided, enabling engine parameters to be addressed in terms of a reduction or avoidance of negative resonances or beats. It also provides an ability to alter thrust from engines of a multi-engined aircraft to reduce rudder trim.

    Abstract translation: 在发动机的单个轴之间，在各个发动机之间以及发动机和飞行器之间提供介质和/或动力的交换，移除或添加（如适用）。 因此，提供了额外的自由度，使发动机参数能够在减少或避免负的共振或节拍方面得到解决。 它还提供了改变多发发动机发动机的推力以减少方向舵装饰的能力。

    CONTROL SYSTEM
    13.
    发明申请
    CONTROL SYSTEM 失效
    控制系统

    公开(公告)号：US20120065746A1

    公开(公告)日：2012-03-15

    申请号：US13279012

    申请日：2011-10-21

    Applicant: Franz Wintrich ,  Volker Stephan ,  Erich Schaffernicht ,  Frank-Florian Steege

    Inventor： Franz Wintrich ,  Volker Stephan ,  Erich Schaffernicht ,  Frank-Florian Steege

    IPC: G05B13/02

    CPC classification number: G05B13/04 ,  F01K13/02 ,  F23G5/50 ,  F23N5/00 ,  F23N2023/44 ,  F23N2023/48 ,  F23N2900/05006 ,  G05B13/027 ,  G05B2219/31354 ,  Y02E20/12

    Abstract: A control system (1) for a complex process, particularly for controlling a combustion process in a power plant, a waste incinerator plant, or a cement plant, has a controlled system (14) and at least one controller (36), wherein the control system (1) is divided hierarchically into various levels (10, 20, 30, 40). The first level (10) represents the complex, real process to be controlled and is implemented by the controlled system (14). The second level (20) represents an interface to the process and is implemented by a process control system. The third level (30) represents the control of the process and is implemented by the at least one active controller (36). The fourth level (40) represents a superordinate overview and is implemented by a principal controller (44).

    Abstract translation: 用于复杂过程的控制系统（1）具有控制系统（14）和至少一个控制器（36），特别是用于控制发电厂，废物焚化炉设备或水泥厂的燃烧过程的控制系统（1） 控制系统（1）被分成不同的层次（10,20,30,40）。 第一级（10）表示被控制的复杂的实际过程，并由受控系统（14）实现。 第二级（20）表示该过程的接口，并由过程控制系统实现。 第三级（30）表示该过程的控制，并由至少一个主动控制器（36）实现。 第四级（40）表示上级概览，由主控制器（44）实现。

    Control loop for regulating a combustion process
    14.
    发明授权
    Control loop for regulating a combustion process 失效
    用于调节燃烧过程的控制回路

    公开(公告)号：US08019446B2

    公开(公告)日：2011-09-13

    申请号：US12074271

    申请日：2008-02-29

    Applicant: Franz Wintrich ,  Volker Stephan

    Inventor： Franz Wintrich ,  Volker Stephan

    IPC: G05B13/02

    CPC classification number: F23G5/50 ,  F23N2029/20 ,  Y02E20/12

    Abstract: In a control loop for regulating a combustion process in a plant (e.g., a power-generating plant, a waste incineration plant or a cement works) having a controlled system for converting material by way of the combustion process while supplying air, with at least one flame body being formed, and having at least one observation device for imaging the flame body, other sensors for determining the input data, at least one adjustment device that can be controlled by output data for supplying at least material and/or air, and a computer for evaluating the input data in relation to target values and for determining the output data by using a current process model, the computer has a feature extraction module that extracts features from the input data using an information measure. The features are informative for the target values, and are for use in an alternative process model.

    Abstract translation: 在用于调节工厂（例如，发电厂，废物焚化厂或水泥厂）中的燃烧过程的控制回路中，具有用于在供应空气的同时通过燃烧过程转换材料的受控系统，至少 形成一个火焰体，并具有至少一个用于使火焰体成像的观察装置，用于确定输入数据的其它传感器，至少一个调节装置，其可由用于至少供应材料和/或空气的输出数据进行控制;以及 用于评估与目标值相关的输入数据并通过使用当前过程模型来确定输出数据的计算机，该计算机具有特征提取模块，其使用信息测量从输入数据中提取特征。 这些特征对于目标值是有用的，并且用于替代过程模型。

    Method for the control of aero gas turbine engines
    16.
    发明授权
    Method for the control of aero gas turbine engines 有权
    用于控制航空燃气涡轮发动机的方法

    公开(公告)号：US07100868B2

    公开(公告)日：2006-09-05

    申请号：US10773182

    申请日：2004-02-09

    Applicant: Volker Stephan

    Inventor： Volker Stephan

    IPC: B64D31/00 ,  B64C11/50

    CPC classification number: F02C9/42 ,  B64C11/50 ,  B64D31/12 ,  Y02T50/671

    Abstract: The exchange, removal or addition, as applicable, of media and/or power between the individual shafts of an engine, between individual engines and between the engines and the aircraft provides for additional degrees of freedom, enabling engine parameters to be addressed in terms of a reduction or avoidance of negative resonances or beats. It also provides an ability to alter thrust from engines of a multi-engined aircraft to reduce rudder trim.

    Abstract translation: 发动机的单个轴之间，发动机之间以及发动机和飞机之间的介质和/或动力的交换，移除或添加提供了额外的自由度，使发动机参数能够被解决 减少或避免负共振或节拍。 它还提供了改变多发发动机发动机的推力以减少方向舵装饰的能力。

    Control loop for regulating a combustion process
    17.
    发明申请
    Control loop for regulating a combustion process 失效
    用于调节燃烧过程的控制回路

    公开(公告)号：US20080215165A1

    公开(公告)日：2008-09-04

    申请号：US12074271

    申请日：2008-02-29

    Applicant: Franz Wintrich ,  Volker Stephan

    Inventor： Franz Wintrich ,  Volker Stephan

    IPC: G05B13/04

    CPC classification number: F23G5/50 ,  F23N2029/20 ,  Y02E20/12

    Abstract: In a control loop for regulating a combustion process in a plant (e.g., a power-generating plant, a waste incineration plant or a cement works) having a controlled system for converting material by way of the combustion process while supplying air, with at least one flame body being formed, and having at least one observation device for imaging the flame body, other sensors for determining the input data, at least one adjustment device that can be controlled by output data for supplying at least material and/or air, and a computer for evaluating the input data in relation to target values and for determining the output data by using a current process model, the computer has a feature extraction module that extracts features from the input data using an information measure. The features are informative for the target values, and are for use in an alternative process model.

    Abstract translation: 在用于调节工厂（例如，发电厂，废物焚化厂或水泥厂）中的燃烧过程的控制回路中，具有用于在供应空气的同时通过燃烧过程转换材料的受控系统，至少 形成一个火焰体，并具有至少一个用于使火焰体成像的观察装置，用于确定输入数据的其它传感器，至少一个调节装置，其可由用于至少供应材料和/或空气的输出数据进行控制;以及 用于评估与目标值相关的输入数据并通过使用当前过程模型来确定输出数据的计算机，该计算机具有特征提取模块，其使用信息测量从输入数据中提取特征。 这些特征对于目标值是有用的，并且用于替代过程模型。

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