REAL TIME MODEL BASED COMPRESSOR CONTROL

Patent №

US 9,540,944

Granted

2017-01-10

Filed 2012

Owner

UNITED TECHNOLOGIES CORPORATION

Lab

AI components

1

planning

Assignment

Recorded

Dataset

AIPD

2023_r1 edition

Application

13631436

A gas turbine engine comprises a compressor, a combustor, a turbine, and an electronic engine control system. The compressor, combustor, and turbine are arranged in flow series. The electronic engine control system is configured to generate a real-time estimate of compressor stall margin from an engine model, and command engine actuators to correct for the difference between the real time estimate of compressor stall margin and a required stall margin.

PlanningF01D 17/00F02C 9/52F01D 17/08F02C 9/54F04D 27/001F02C 9/18F05D 2270/101

AI classification

Planning1.00
Evolutionary computation0.08
Machine learning0.00
Natural language0.00
Speech0.00
Knowledge representation0.00
AI hardware0.00
Vision0.00

Ownership

UNITED TECHNOLOGIES CORPORATION

assignment · 290500328

Assignors

MEISNER, RICHARD P., WINEBRENNER, BRIAN V., FEULNER, MATTHEW R., KARPMAN, BORIS, MARCOS, JUAN A., MA, DAVID L.

On an employer assignment, the assignors are typically the inventors.

From the same owner

© 2026 NYSGPT2525 LLC