Advanced gas turbine cooling for the carbon-neutral era

K Takeishi, R Krewinkel - International Journal of Turbomachinery …, 2023 - mdpi.com
In the coming carbon-neutral era, industrial gas turbines (GT) will continue to play an
important role as energy conversion equipment with high thermal efficiency and as …

Component having a film cooling arrangement

M Kopmels - US Patent 7,273,351, 2007 - Google Patents
(57) ABSTRACT A component such as a turbine blade of a gas turbine engine includes a?
lm cooling arrangement Which is optimized by a process in Which a component is …

Effect of varying jet diameter on the heat transfer distributions of narrow impingement channels

A Terzis, P Ott, M Cochet… - Journal of …, 2015 - asmedigitalcollection.asme.org
The development of integrally cast turbine airfoils allows the production of narrow
impingement channels in a double-wall configuration, where the coolant is practically …

Detailed heat transfer distributions of narrow impingement channels for cast-in turbine airfoils

A Terzis, P Ott, J von Wolfersdorf… - Journal of …, 2014 - asmedigitalcollection.asme.org
The current capabilities of the foundry industry allow the production of integrally cast turbine
airfoils. Impingement cooling effectiveness can be then further increased due to the …

Turbine stator vane with near wall integrated micro cooling channels

G Liang - US Patent 8,414,263, 2013 - Google Patents
In a gas turbine engine, Such as a large frame heavy-duty industrial gas turbine (IGT)
engine, a hot gas stream gener ated in a combustor is passed through a turbine to produce …

Vortex cooling of turbine blades

G Liang - US Patent 6,981,846, 2006 - Google Patents
(57) ABSTRACT A near wall cooling technique for cooling the pressure and 21 Ap1. No.:
10,791,575 9. C g line p (21) Appl. No 1791, Suction sides of a turbine airfoil that includes a …

Turbine airfoil with near-wall leading edge multi-holes cooling

G Liang - US Patent 7,520,725, 2009 - Google Patents
A gas turbine engine includes a turbine section in which a hot gas flow passes through the
rotor blades and stationary vanes or nozzles to extract energy from the flow. The effi ciency …

Hole staggering effect on the cooling performance of narrow impingement channels using the transient liquid crystal technique

A Terzis, G Wagner… - Journal of …, 2014 - asmedigitalcollection.asme.org
This study examines experimentally the cooling performance of narrow impingement
channels as could be cast-in in modern turbine airfoils. Full surface heat transfer coefficients …

Turbine airfoil with mini-serpentine cooling passages

G Liang - US Patent 7,527,474, 2009 - Google Patents
A gas turbine engine burns a fuel to produce a hot gas flow which is passed through a
turbine to produce mechanical work. A compressor delivers compressed air to a combustor …

Turbine airfoil with near-wall cooling

G Liang - US Patent 7,857,589, 2010 - Google Patents
A turbine airfoil having a mini-serpentine flow cooling circuit on the leading edge portion to
provide both convective and film cooling for the leading edge portion. The mini-serpentine …