摘要:
Certain embodiments of the invention may include systems and methods for controlling an integrated drive train. According to an example embodiment of the invention, a method for controlling a gas turbine drive train (100) includes measuring speed (311) associated with the drive train (100), controlling fuel flow to a turbine (328) based at least in part on a speed command (506) and the measured speed (311), controlling one or more guide vanes associated with a torque converter (326) based at least in part on the speed command (506) and an expected power output (514) of the torque converter (326), and selectively coordinating respective torque contributions from the torque converter (326) and the turbine (328).
摘要:
A system and method implements machine performance, most preferably for gas ' turbine engines. The system and method implement a control law (118) that ' receives sensed operational parameter feedback signals (124). For each sensed engine operational parameter (108, 114), the feedback signals (124) that are supplied to the control law (118) selectively (122) comprise the sensor signal (114) representative of the engine operational parameter, if the sensor (108) signal is valid, or an observer (120) estimate (126) of the sensed engine operational parameter, if the sensor signal is invalid.
摘要:
Method for detecting faults in a device comprising the steps of receiving a plurality of performance parameters, applying the plurality of performance parameters to a first model (21) to produce a plurality of estimated performance parameters, applying the plurality of performance parameters to a second model (24) to produce a plurality of estimated device parameters, computing a plurality of residuals from the plurality of estimated device parameters, computing a plurality of distance measuring from the plurality of residuals, detecting at least one parameter deviation using the plurality of residuals and the plurality of estimated performance parameters, and setting at least one detection flag if the detected at least one parameter deviation is persistent.
摘要:
A method for determining a target exhaust temperature (70) for a gas turbine (10) including: determining a target exhaust temperature (70) based on a compressor pressure condition; determining a temperature adjustment to the target exhaust temperature based on at least one parameter of a group of parameters consisting of specific humidity (68), compressor inlet pressure loss (52) and turbine exhaust back pressure (56); and adjusting the target exhaust temperature by applying the temperature adjustment.
摘要:
A method of performing diagnostics on a system comprises receiving a plurality of measurement parameters, each corresponding to one of a plurality of parameters at a time k, forming a deviation vector from the plurality of measurement parameters, calculating an initial deviation vector from an initial fault vector, calculating a multiple fault isolation deviation vector using the initial deviation vector and the deviation vector, determining if an event is in progress using the multiple fault isolation deviation vector, performing statistical data validity to set a present inhibit flag and a past inhibit flag, and performing module performance analysis according to the present inhibit flag and the past inhibit flag.
摘要:
A gas turbine engine (20) includes a first (86) and second (90) pump driven by a spool (30). An air-oil cooler (88) is located downstream of the first pump (86). An air-air precooler (92) is located downstream of the second pump (90) and the air-oil cooler (88).
摘要:
A gas turbine engine (20) includes a first (86) and second (90) pump driven by a spool (30). An air-oil cooler (88) is located downstream of the first pump (86). An air-air precooler (92) is located downstream of the second pump (90) and the air-oil cooler (88).