So, if I take a stand alone gas turbine compressor, say an axial compressor shaft driven by other parts of the turbine engine train and put an after cooler on it and in line with it, axially, so that the shaft from the driver passes through the aftercooler (shaped like a donut), and connect it to the compressor with ducting or diffusers, is it a part of the engine or is it a stand alone Hx subject to the PV code? The compressor is clearly a piece of rotating equipment easily identifiable by certain features and the Hx is clearly a Hx, tubes, fins, etc, capable of being moved off axis and having the compressor discharge ducted to it but otherwise functioning the same. Nothing about it has the appearance of the other engine parts. Is it part of the engine, or is it a stand alone Hx that happens to coupled in line with a turbine?
This is a serious question made deliberately vague, sorry.
rmw