Matches 301 - 320 out of 320 < 1 2 3 4 5 6 7


Match Document Document Title
US20160146107 Variable Supersonic Engine Inlet  
Systems and methods for generating an oblique shock in a supersonic inlet are disclosed. The system can comprise an inlet with a slot disposed at an oblique angle to the main incoming air stream....
US20160138483 APPLICATION OF FUEL FLOW-BASED PROBABILISTIC CONTROL IN GAS TURBINE TUNING UNDER PART LOAD, RELATED CONTROL SYSTEMS, COMPUTER PROGRAM PRODUCTS AND METHODS  
Various embodiments include a system having: at least one computing device configured to tune a set of gas turbines (GTs) by performing actions including: commanding each GT in the set of GTs to a...
US20160138482 APPLICATION OF PROBABILISTIC CONTROL IN GAS TURBINE TUNING WITH MEASUREMENT ERROR, RELATED CONTROL SYSTEMS, COMPUTER PROGRAM PRODUCTS AND METHODS  
Various embodiments include a system having: at least one computing device configured to tune a set of gas turbines (GTs) by performing actions including: commanding each GT in the set of GTs to a...
US20160138481 DEGRADED GAS TURBINE TUNING AND CONTROL SYSTEMS, COMPUTER PROGRAM PRODUCTS AND RELATED METHODS  
Various embodiments include a system having: at least one computing device configured to tune a set of gas turbines (GTs) by performing actions including: commanding each GT in the set of GTs to a...
US20160130974 COMPRESSOR MONITORING METHOD  
A method of predicting the condition of a compressor with respect to rotating stall is disclosed. The method comprises the steps of: i) comparing the difference between the largest and smallest...
US20160025014 HIGH TEMPERATURE DISK CONDITIONING SYSTEM  
A gas-circulation system for conditioning a disk of an aircraft may comprise a first takeoff port configured to extract a combusted gas and a second takeoff port configured to extract an...
US20160017805 IGNITER TIP WITH COOLING PASSAGE  
A combustor cap for a combustor chamber of a combustion system is provided. The combustor cap includes a plate member including: a plurality of openings for accommodating a plurality of fuel...
US20160010495 METHOD FOR THE CONTROL AND PROTECTION OF A GAS TURBINE AND GAS TURBINE USING SUCH METHOD  
In a method for the control and protection of a gas turbine a gas turbine performance and lifetime indicative process quantity is estimated from a set of available process signals. The gas turbine...
US20150369138 ENGINE HEALTH MONITORING AND POWER ALLOCATION CONTROL FOR A TURBINE ENGINE USING ELECTRIC GENERATORS  
A control for a turbine engine using electrical machines monitors engine health and allocates power extraction between the electrical machines.
US20150346059 VEHICLE MISSION CAPABILITY PREDICTION SYSTEM AND METHOD  
A system method for predicting vehicle mission capability for a vehicle that is propelled by an engine includes collecting engine degradation data for the engine. Location independent engine...
US20150345403 Model-Based Optimal Control For Stall Margin Limit Protection in an Aircraft Engine  
A control system for a gas turbine engine, a method for controlling a gas turbine engine, and a gas turbine engine are disclosed. The control system may include a hybrid model predictive control...
US20150330310 METHODS AND APPARATUS TO DETERMINE AIRFLOW CONDITIONS AT AN INLET OF AN ENGINE  
Methods and apparatus to determine airflow conditions at an inlet of an engine are disclosed herein. An example apparatus disclosed herein includes a sensor disposed at an inlet of an engine to...
US20150291286 MULTIPLE AIRCRAFT ENGINE CONTROL SYSTEM AND METHOD OF COMMUNICATING DATA THEREIN  
The multiple aircraft engine control system having a corresponding engine controller associated with each one of the engines, each one of the engine controllers having at least two independent...
US20150285159 METHOD AND A DEVICE FOR ADJUSTING A SETPOINT VALUE OF A PARAMETER THAT INFLUENCES THRUST FROM A GAS TURBINE ENGINE  
A method of adjusting a setpoint value of at least one parameter that has an influence on thrust of a gas turbine engine propelling an aircraft during a stage of flight of the aircraft, the method...
US20150268131 METHOD AND A DEVICE FOR NORMALIZING VALUES OF OPERATING PARAMETERS OF AN AEROENGINE  
The normalization method comprises: normalizing a current value of each operating parameter relative to exogenous variables with the help of a first regression model defined on a space generated...
US20150267620 DYNAMIC AND AUTOMATIC TUNING OF A GAS TURBINE ENGINE USING EXHAUST TEMPERATURE AND INLET GUIDE VANE ANGLE  
Methods and systems are provided for dynamically auto-tuning a gas turbine engine. Initially, parameters of the gas turbine engine are monitored to determine that they are within predefined upper...
US20150267619 GAS TURBINE ENGINE PERFORMANCE SEEKING CONTROL  
A gas turbine engine control system is disclosed having a model and an observer that together can be used to adjust a command issued to the gas turbine engine or associated equipment to improve...
US20150006058 SYSTEM AND METHOD FOR CONDITIONING NOISY SIGNALS  
There is provided a system and method for conditioning a noisy signal. A sensing signal is received during each one of a plurality of successive control cycles, the sensing signal comprising a...
US20110119032 ANOMALOUS DATA DETECTION METHOD  
An example data assessment method for a diagnostic system includes receiving a set of initialization data, analyzing the set of initialization data to identify a data outlier in the set of...
US20100324799 TURBINE ENGINE SPEED AND VIBRATION SENSING SYSTEM  
A turbo machine includes a speed probe that is configured to detect a speed of a rotating feature. Engine controls are used by a processor to control operation of the turbo machine. The processor...

Matches 301 - 320 out of 320 < 1 2 3 4 5 6 7