Miku the Based wrote:The Corparation wrote:[.
The expansion of that air as it heats is what is actually drives the turbine. .
Isn't that a given in any reactor, coal and nuclear power plants uses water to turn into water vapor to do the work of pushing the mechanical and electrical turbine. So in these aircraft reactors they use air instead. Never heard of these air reactors, is it a open system that requires a air intake?
There were designs for direct cycle air cooled reactors analogous to boiling water reactors where air was both the primary coolant and the working fluid, which did have air intakes and exhausts to the core. A good specific example (and an example of why they no longer see use) is the heat transfer reactor experiment, which had an overpower and partial meltdown, leading to a radiological accident.
As for your question about efficiency with regards to temperature differential, every heat engine operates by converting a portion of heat input to work. This transfer can be simplified to a proportionality, where work output (W) is proportional to the difference in energy of the input heat (Qin) and the output heat (Qout). Combined with the general use efficiency equation (usable output/total input, in this case W/Qin), we get the equation for a heat engine’s efficiency as (Qin-Qout)/Qin. A drop in input heat (Qin) caused by a lowering of temperature, or a rise in output heat caused by a rise in heat sink temperature will therefore cause a lowering of the engine’s total efficiency.