Mailing List flyrotary@lancaironline.net Message #54377
From: Thomas Giddings <tom@midwestaviation.net>
Subject: Re: [FlyRotary] Re: Fw: [FlyRotary] Re: intersting video
Date: Sat, 26 Mar 2011 19:02:40 -0400
To: Rotary motors in aircraft <flyrotary@lancaironline.net>
Greg: Is your Turbo set up  a GT4088 non bb unit ?
Tom Giddings
VP Avionics Sales
MIDWEST AVIONICS
200 Hardy Roberts Dr
PO Box 219
West Paducah,KY 42086
877-904 9966
Cell; 727 858-1772
FAX:270 744 3466
tom@midwestaviation.net
Online Store
www.midwest-avionics.com

Image
Midwest Aviation Avionics Logo.jpg


On Mar 26, 2011, at 12:36 AM, Greg Ward wrote:

> Hey Tom:
> Around 450 HP at take-off.  Tracy says I am on my own at that HP, so we will see.
> Greg
>
> ----- Original Message ----- From: "Thomas Giddings" <tom@midwestaviation.net>
> To: "Rotary motors in aircraft" <flyrotary@lancaironline.net>
> Sent: Friday, March 25, 2011 8:15 PM
> Subject: [FlyRotary] Re: Fw: [FlyRotary] Re: intersting video
>
>
> Greg: Thanks the for pics of your project. How much power do you estimate making with that turbo set up...
>
> Tom
>
> On Mar 25, 2011, at 2:38 PM, Greg Ward wrote:
>
>> First 2 photos
>>
>> Subject: Re: [FlyRotary] Re: intersting video
>>
>>
>> Hey Tom;
>> Couple more shots of a very long process.  As you can see, we got the Grifin
>> radiator mounted behind the oil cooler, with separate cowl flaps. The one
>> shot with the blue plastic is the part of the opening we calculated would be
>> open all the time, with the main flap adjustable for hot taxi days.  The oil
>> cooler we can shut off entirely, for those cold high altitude days.  The one
>> weird shot was shot upside down, trying to get an idea what it would look
>> like when we were done.....(:-)
>>
>> Greg Ward
>> Lancair Legacy N178RG, Still in progress
>>
>>
>>
>>
>> ----- Original Message ----- From: "Thomas Giddings" <tom@midwestaviation.net>
>> To: "Rotary motors in aircraft" <flyrotary@lancaironline.net>
>> Sent: Friday, March 25, 2011 4:54 AM
>> Subject: [FlyRotary] Re: intersting video
>>
>>
>> Greg: I also thought about the P51 style scoop. I do think it is a great
>> idea. I have a landing gear that retracts into the fuselage and there really
>> is not much room for a belly scoop. Could you post some Pics of how you did
>> this. How Big is the Radiator and scoop and where did you place the oil
>> cooler. By the way if any of you are at Sun N Fun next week . Please stop by
>> and say Hi. I will be in Building A booth 67 all week. I plan on getting out
>> and looking at some flying examples if possible. and maybe  see some of you
>> folks then.
>>
>> Tom Giddings
>>
>> On Mar 25, 2011, at 12:43 AM, Greg Ward wrote:
>>
>>> Hey Tom;
>>> We looked at this scenario when we were laying out our Legacy, and
>>> determined that it was packing too much into a cowling that already had a
>>> large intercooler, and a turbo that was guaranteed to be radiating about
>>> 1400 to 1900 degrees of heat.  So, the question was, where to put a
>>> radiator, oil cooler, etc. outside of the cowling?  We settled on a P-51
>>> scoop for both, and built it exactly like the original, hoping for a
>>> little thrust return.  Difference was, we kept the radiator out of the
>>> fuselage, because we didn't want a leak in the cockpit at 20+K feet, with
>>> all that entails.  We are also looking at installing a hot water heating
>>> system, with valves both in and out for the very same reasons.  So, what
>>> we have left is, the engine, intercooler, turbo, and whatever goes on the
>>> firewall, with a lot of air going through, to hopefully keep everything
>>> happy.  The flaps on the scoop should enable us to keep temps under
>>> control, a' la P-51, so we'll see.
>>>
>>> Greg Ward
>>> Lancair Legacy N178RG, Still in progress
>>>
>>>
>>> ----- Original Message ----- From: "Thomas Giddings"
>>> <tom@midwestaviation.net>
>>> To: "Rotary motors in aircraft" <flyrotary@lancaironline.net>
>>> Sent: Thursday, March 24, 2011 8:59 PM
>>> Subject: [FlyRotary] intersting video
>>>
>>>
>>> Here is a youtube engine test run of an LS1 V8. Watch it long enough to
>>> see how the dual radiators are plumbed. This system for engine cooling
>>> includes two radiators which appear to be in series. It  seems to be going
>>> from the thermostat housing to the top of the first radiator then is taken
>>> out the bottom of the first one and crosses over to number two at the top
>>> inlet and back out the bottom into the pump and back through the block
>>> .They are both dual pass radiators . They feed this air from two outside
>>> the cowl scoops. Bud Warren claims this cools very well. In fact he claims
>>> it is the only way to cool the 300HP LS1 V8's . I wanted to original
>>> install a LS3 into my Questair, but could quite get it stuffed in there .
>>> http://www.youtube.com/watch?v=CUSbOAZRRtg. If this link does not work
>>> search youtube for Franks Bearhawk Test run. Incidently they claim they
>>> need 1256 Sq In of radiator surface to keep the V8 running at 190 in
>>> cruise and 200 max in the climb. Also if you to geared drives yahoo forum
>>> there is a very interesting read on the subject on cooling requirements
>>> for the LS1.
>>>
>>> Tom Giddings
>>> VP Avionics Sales
>>> MIDWEST AVIONICS
>>> 200 Hardy Roberts Dr
>>> PO Box 219
>>> West Paducah,KY 42086
>>> 877-904 9966
>>> Cell; 727 858-1772
>>> FAX:270 744 3466
>>> tom@midwestaviation.net
>>> Online Store
>>> www.midwest-avionics.com
>>>
>>> <Image00010.jpg><P1010273.jpg><Mail Attachment.txt>
>>
>>
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