Re: APU Already On Turbo Charged Engines


"N. Shamsundar" <shamsundar_at_@xxxxxx> wrote in message
news:dlikfm$cla$1@xxxxxxxxxxxxxxxxxxx
> Bret Cahill wrote:
> > I couldn't find anything on the web or the US patent office.
> >
> >
> > Bret Cahill
> >
> Consider what reduction ratio you would need to drive a reciprocating
> compressor using the gas turbine.
>
> N. Shamsundar
> University of Houston

Can't come up with anything specific but in general----the (free) turbine of
a gas generator (jet engine) could run in the vicinity of 17000 rpm (at
100% speed).
MLD


.

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