APU Already On Turbo Charged Engines

DOT or DOE wants to save billions in fuel every year by prohibiting semi rigs from idling at stops. All they need to do is get some cops to go to fuel centers and bang on cabs at 3 am.

Auxilary power units are considered too expensive for many owners so the regulations stay off the books. Here's something that might be cheaper and possibly aftermarket:

Instead of running the entire engine of large turbo diesel or gas engines bypass the cylinders with ducting that goes straight from the turbo compressor to the turbine then run the turbo part of the engine to power a generator.

You would need to install:

  1. bypass valves and ducting

  1. a combuster w/fuel line

  2. high speed air or electric starter

  1. reducer gearing to power the ac compressor and/or alternator

  2. possibly a regenerator

The thermo efficiency might not be too great but it'll last longer than batteries and be more reliable than a small gas engine..

Bret Cahill

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Bret Cahill
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I couldn't find anything on the web or the US patent office.

Bret Cahill

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Bret Cahill

Consider what reduction ratio you would need to drive a reciprocating compressor using the gas turbine.

N. Shamsundar University of Houston

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N. Shamsundar

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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MLD
< Consider what reduction ratio you would need to drive a reciprocating

< compressor using the gas turbine.

It might be easier to have the turbine run a high rpm generator as well as the centrifugal compressor then power everything electrically.

I just saw a system where the main engine was on line as usual but the turbine powered a generator as well as the turbo compressor.

That engine would be easy to convert to APU only power. All you need is a combustor, 2 bypass valves and some ducting.

Bret Cahill

Reply to
Bret Cahill
< 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).

That's larger than the 3 - 10 hp size APU that would be useful on semi rigs. Vehicle turbo chargers run at somewhat higher rpms -- 50 - 100K. Tip speeds of flow machinery are typically in the transonic range regardless of diameter. If you increase the diameter you reduce the rpm.

Bret Cahill

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Bret Cahill

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