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The magnitude of recoverable performance loss is determined by site environment and character of operations.
13 List of Figures.The ISO rating temperature corresponds to the curve for an estimated 25,000 hours between hot-section repairs when burning natural gas fuel.Gas fuel control system Figure.4 LM2500 Gas Turbine.During low speed operation, the inlet guide vanes are closed to limit the amount of air flowing through the compressor, and provisions for bleeding air from the compressor are provided at one or more stages.Consistent with GEs evolutionary design philosophy, the 6C incorporates technologies that have been validated in service worldwide.If an EX2000 Generator Excitation System is controlling the generator, then 3 phase PT and CT data is communicated to the Mark VI on the network rather than using the vgen card.In models with air-cooled turbine buckets, the last-stage wheel has been adapted to provide an extraction to supply the necessary cooling air for the turbine and rotor buckets (Fig.
Compressor discharge pressure for constant firing temperature.
Since the general nature of material behavior variability has been addressed, it is appropriate now to discuss several specific material behavior topics that are significant to the gas turbine design engineer and the user.
The extent of this kind of diagnostics has been greatly increased in speedtronic Mark V control over previous generations.The wiring has been made more accessible for ease of installation.The new design dissipates less power than previous generations for equivalent panels.Redundancy has been achieved by using a two coil type servo valve and in most cases, two lvdts.This has been offset by a more efficient cooling system and by reducing the surface area (length) of the liner.
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