Mailing List flyrotary@lancaironline.net Message #59339
From: Stephen Izett <steveizett@me.com>
Subject: Re: [FlyRotary] Re: turbo manifold
Date: Wed, 02 Jan 2013 14:43:26 +0800
To: Rotary motors in aircraft <flyrotary@lancaironline.net>
Steve

So are we observing that the lower plot of the Renesis NA and the Renesis TC as being pretty much the same implies that the TC back pressure appeared to have no significant effect?

What did the intake manifolds for both NA engines look like.
Power output seems a little low. However I'm not familiar with what HorsePower to MP you could expect.

Thanks

Steve Izett




On 02/01/2013, at 2:24 PM, Steven W. Boese wrote:

Based on the relative insensitivity of the Renesis to backpressure, a turbo was installed on the test stand Renesis.  I had previously installed the same stock 1988 RX7 turbo on the test stand 13B and observed a large penalty in efficiency at cruise power levels.  As a result, I had lost interest in a turbo option.  At the rotary gathering this fall, Bobby expressed an interest in how the Renesis would respond to a turbo.  So some data was collected in this regard.  Those present at the rotary gathering may recognize the plot of data that is attached.  It showed the power generated with a 13Bnormally aspirated (NA, red), supercharged (SC, black), and turbocharged (TC, lighter blue).  Data from the normally aspirated (NA, green) and turbocharged (TC, darker blue) Renesis has been added to this plot.  The results seem remarkable in that there appears to be no penalty at cruise power for the turbo installation on the Renesis other than weight and complexity.

 

The data by no means represents an extensive study, but the difference in response of the Renesis to the turbo compared to the 13B seems worthy of reporting.  Field elevation here is 7200 ft with DA normally above 8000 ft which limits normally aspirated MAP to 23" Hg at WOT.  An intercooler was installed on the test stand for both engines.  No attempt to boost the Renesis above 30" MAP was made.  It is also unlikely that the turbo tested would be the best match for this application.  Any thoughts on identifying an appropriate turbo would be welcome.

 

Steve Boese
RV6A, 1986 13B NA, RD1A, EC2

     


From: Rotary motors in aircraft [flyrotary@lancaironline.net] on behalf of Stephen Izett [steveizett@me.com]
Sent: Tuesday, January 01, 2013 7:23 PM
To: Rotary motors in aircraft
Subject: [FlyRotary] Re: turbo manifold

Steve

Did that engine end up turboed?
I have a Renesis, hopefully flying in the next 6 months but am seriously interested in turboing it down the road.

Cheers

Steve Izett
Glasair SIIS RG Renesis
 

<Renesis turbo.jpg>--
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