Exact(1)
The turbine blade temperature and the compressor surge margin could be recovered to the reference values by either under-firing or compressor air bleeding, which are effective for blade temperature control and surge margin control, respectively.
Similar(7)
This leads to increased blade and vane temperatures and therefore to enhanced oxidation and corrosion attack of the coatings on these components.
Performance optimization of a gas turbine engine can be expressed in terms of minimizing fuel consumption while maintaining nominal thrust output, maximizing thrust for the same fuel consumption and minimizing turbine blade temperature.
A thermodynamic cooling model was used to estimate the reasonable amount of turbine coolant needed to maintain the turbine blade temperature of each stage at a feasible level.
Propulsion engines and the vast majority of auxiliary generator engines running at speeds below 1000 rev/min will be turbocharged and will be designed to allow a generous through flow of scavenge air at this point in order to control the turbine blade temperature.
Clearance gap between blade and casing causes secondary leakage flow with high tip wall heat fluxes and local high blade temperatures.
The purpose of this study is to determine if an educational model during a surgical skills laboratory results in a significant reduction in cast saw blade temperatures generated during cast removal.
The optimal split of fuel to be burned between the adiabatic and isothermal segments is determined to be a function of turbomachinery irreversibilities and the turbine-blade temperature limit.
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