a 43% efficient gas turbine won't give 61% on combined cyclegruntguru wrote: ↑30 Mar 2020, 00:33That is a gas turbine plus a steam powerplant heated by the turbine exhaust. (Combined cycle)subcritical71 wrote: ↑30 Mar 2020, 00:01GE’s H class gas turbine has >61% thermal efficiency https://www.ge.com/content/dam/gepower ... -oct15.pdf. Guinness has it at 63.08%
The gas turbine alone would be about 43%.
you need a 50% efficient gas turbine to reach or exceed 60% on combined cycle
43% is about the best an aviation gas turbine can do
the biggest gas turbines for power generation are about 50% efficient
(though velocities at the blade tips are significantly supersonic)
there was a German company that proposed cars using piston-engine ICEs on combined cycle
the BMW TurboSteamer
btw
traditionally a 50% efficient heat engine was called 50% efficient (not 50% thermally efficient)
thermal efficiency TE is the % conversion efficiency of in-cylinder heat to work
of course there's indicated thermal efficiency ITE and brake thermal efficiency BTE
ITE seems to be what many posters intend when they (wrongly) speak of combustion efficiency
in F1 ITE is about 50% but CE is about 95%
BTE (even if called thermal efficiency) is anyway a somewhat skewed measure
eg the combustion of (most) fuels 'traps' heat primarily as the latent heat in the water vapour content of the exhaust
eg gasoline traps about 7%, methane traps about 10%, and hydrogen traps about 15%
this trapping is by engineering convention ignored (ie in using the lower calorific value LCV)