公开(公告)号：US20160230677A1

公开(公告)日：2016-08-11

申请号：US14616369

申请日：2015-02-06

Applicant: United Technologies Corporation

Inventor： Matthew R. Feulner ,  Roxanne M. Bochar ,  Stefan M. Poth, JR.

IPC: F02C9/28 ,  F02C7/042

CPC classification number: F02C9/28 ,  F01D17/08 ,  F01D17/162 ,  F02C7/042 ,  F02C9/20 ,  F04D27/0246 ,  F05D2270/096 ,  F05D2270/311 ,  F05D2270/312 ,  F05D2270/313

Abstract: A variable-geometry system for a gas turbine engine can be used to improve operations in various inclement weather conditions. This may be achieved by varying the orientation of an element in a gas turbine engine flowpath in response to a comparison between sensor-gathered parameter data and stored parameter values and ranges using a pre-programmed algorithm. The orientation of the element may be infinitely variable within a range of orientations.

Abstract translation: 用于燃气涡轮发动机的可变几何系统可用于改善各种恶劣天气条件下的操作。 这可以通过响应于使用预编程算法的传感器收集的参数数据与存储的参数值和范围之间的比较来改变燃气涡轮发动机流路中的元件的取向来实现。 该元件的取向可以在取向范围内无级变化。

公开(公告)号：US20180238243A1

公开(公告)日：2018-08-23

申请号：US15899486

申请日：2018-02-20

Applicant: United Technologies Corporation

Inventor： Stefan M. Poth, JR.

IPC: F02C9/48 ,  F02C9/26 ,  G05B17/02 ,  F02C9/00 ,  G05B15/02 ,  F02C9/16 ,  G05B19/02 ,  G06Q10/00 ,  G06Q10/06

CPC classification number: F02C9/48 ,  F02C9/00 ,  F02C9/16 ,  F02C9/26 ,  G05B15/02 ,  G05B17/02 ,  G05B19/02 ,  G06Q10/00 ,  G06Q10/06 ,  G06Q10/0631

Abstract: A disclosed control system and method of controlling a gas turbine engine utilizes a thrust rating schedule generated from airframe selected requirements. The system utilizes a generic logic structure for ratings combined with simple selection logic to customize rating schedules for multiple airframe customers. The use of a common generic logic structure to generate rating schedules for different airframe manufacturers reduces software design effort, memory consumption, and processor throughput requirements.

公开(公告)号：US20150275767A1

公开(公告)日：2015-10-01

申请号：US14430589

申请日：2013-03-15

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： Stefan M. Poth, JR.

IPC: F02C9/00 ,  G05B15/02

CPC classification number: F02C9/48 ,  F02C9/00 ,  F02C9/16 ,  F02C9/26 ,  G05B15/02 ,  G05B17/02 ,  G05B19/02 ,  G06Q10/00 ,  G06Q10/06

Abstract: A disclosed control system and method of controlling a gas turbine engine utilizes a thrust rating schedule generated from airframe selected requirements. The system utilizes a generic logic structure for ratings combined with simple selection logic to customize rating schedules for multiple airframe customers. The use of a common generic logic structure to generate rating schedules for different airframe manufacturers reduces software design effort, memory consumption, and processor throughput requirements.

Abstract translation: 公开的控制系统和控制燃气涡轮发动机的方法利用从机体选择的要求产生的推力额定表。 该系统利用通用逻辑结构进行评级，并结合简单的选择逻辑来为多个机身客户定制评级计划。 使用通用通用逻辑结构为不同的机身制造商生成额定计划减少了软件设计工作量，内存消耗和处理器吞吐量要求。

公开(公告)号：US20140090456A1

公开(公告)日：2014-04-03

申请号：US13631359

申请日：2012-09-28

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： Richard P. Meisner ,  Alexandra I. Britten ,  Stefan M. Poth, JR. ,  Boris Karpman

IPC: G01M15/14

CPC classification number: G01M15/14 ,  G05B23/0254 ,  G05B23/0297

Abstract: A gas turbine engine inlet sensor fault detection and accommodation system comprises an engine model, an engine parameter comparison block, an inlet condition estimator, control laws, and a fault detection and accommodation system. The engine model is configured to produce a real-time model-based estimate of engine parameters. The engine parameter comparison block is configured to produce residuals indicating the difference between the real-time model-based estimate of engine parameters and sensed values of the engine parameters. The inlet condition estimator is configured to iteratively adjust an estimate of inlet conditions based on the residuals. The control laws are configured to produce engine control parameters for control of gas turbine engine actuators based on the inlet conditions. The fault detection and accommodation system is configured to detect faults in inlet condition sensors, select sensed inlet conditions for use by the control laws in the event of no fault, and select estimated inlet conditions for use by the control laws in the event of inlet condition sensor fault.

Abstract translation: 燃气涡轮发动机入口传感器故障检测和调节系统包括发动机模型，发动机参数比较块，入口状态估计器，控制规律以及故障检测和调节系统。 引擎模型被配置为产生基于实时模型的发动机参数估计。 引擎参数比较块被配置为产生指示基于实时模型的发动机参数估计与发动机参数的感测值之间的差异的残差。 入口条件估计器被配置为基于残差迭代地调整入口条件的估计。 控制规则被配置为基于入口条件来生成用于控制燃气涡轮发动机执行器的发动机控制参数。 故障检测和调试系统被配置为检测入口状态传感器中的故障，选择在无故障情况下由控制规则使用的感应入口条件，并在入口条件下选择控制规则使用的估计入口条件 传感器故障。