Invention Grant
- Patent Title: Compact aero-thermo model based control system
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Application No.: US16203995Application Date: 2018-11-29
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Publication No.: US10767563B2Publication Date: 2020-09-08
- Inventor: Boris Karpman , Thomas Niemczycki , Ian Michael Dinsmore , David Sembiante , Robert H. Luppold
- Applicant: United Technologies Corporation
- Applicant Address: US CT Farmington
- Assignee: RAYTHEON TECHNOLOGIES CORPORATION
- Current Assignee: RAYTHEON TECHNOLOGIES CORPORATION
- Current Assignee Address: US CT Farmington
- Agency: Cantor Colburn LLP
- Main IPC: F02C7/26
- 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.
Public/Granted literature
- US20190093566A1 COMPACT AERO-THERMO MODEL BASED CONTROL SYSTEM Public/Granted day:2019-03-28
Information query
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