Mailing List flyrotary@lancaironline.net Message #30055
From: Ed Anderson <eanderson@carolina.rr.com>
Subject: Re: [FlyRotary] Re: Six port bolt-on manfold progress (was: RX-8)
Date: Wed, 8 Feb 2006 08:41:45 -0500
To: Rotary motors in aircraft <flyrotary@lancaironline.net>
Ok, Bill - appears you have given this project a lot of thought (no surprise there). 
 
To produce maximum thrust at full power your tip speed should fall between .88 and .92 mach. To move between .88 and .92 mach usually takes a change of about 110 to 120 RPM. This of course varies depending on your particular propeller and the temperature.  The calculator on the website gives the tip speed as 0.889 Mach, so looks like you are right on the money with the prop.
 
Looking forward to progress reports
 
Ed
 
----- Original Message -----
To: "Rotary motors in aircraft" <flyrotary@lancaironline.net>
Sent: Wednesday, February 08, 2006 1:32 AM
Subject: [FlyRotary] Re: Six port bolt-on manfold progress (was: RX-8)

> In the car, all the intake valves are open at something like 6500 RPM
> (maybe even lower.) My manifold emulates the stock manifold in this
> condition. Should work OK for the expected RPM operating range.
>
>         With a 2:85 PSRU, the max prop RPM will be 3157. As I understand
> it, this should not be a problem for a 72 inch prop.  You just have to
> pitch it correctly to absorb 243 HP at that RPM (at altitude.)
>
>         I'm planning to rig up a dyno using a big disk brake (and a lot of
> water) to find out how  many HP the engine is actually making.
>
> Bill Dube'
>
>
>
> At 07:18 PM 2/7/2006, you wrote:
>>Boy, Bill, what an intake manifold project.  If it should not turn out to
>>work as you desire - it will sure make a nice piece of artwork! Sorry,
>>couldn't resist it - I know nice artwork is not what you are looking for.
>>Looks like a lot of work has gone into it already.  Will eagerly await its
>>production and test results.
>>
>>I am still curious as to how you plan to get the engine close to 9000 with
>>the prop load.  One of the problems that typically happens is that a
>>manifold may be designed and may give great performance at say 9000 rpm in
>>a car engine.  Because they can shift gears and regulate the engine load,
>>which of course we can not do ..... unless....Aha! you plan on using  a
>>constant speed/variable pitch prop - don't you.
>>
>>At least my experience with a fix pitch prop is that due to the prop load
>>the engine simply won't get up into the rpm promise land that the intake
>>design would seem to promise.  My very first intake manifold was being
>>used by the rotary racers at the time and producing 280+ HP at untold rpms
>>- I tried it and the engine could simply not get past a 5500-6000 rpm
>>range.  I replaced it with an intake of longer, much smaller diameter
>>intakes and have now hit as high as 6800 rpm.
>>
>>In any case, hopefully your results will everything you aim for.  In any
>>case, it should provide us with an expert on carbon fiber intakes - that
>>in itself would be great 3lbs vs my 11lb intake would be great.
>>
>>Ed A
>>
>>Ed Anderson
>>Rv-6A N494BW Rotary Powered
>>Matthews, NC
>>eanderson@carolina.rr.com
>>----- Original Message ----- From: "Bill Dube" <
william.p.dube@noaa.gov>
>>To: "Rotary motors in aircraft" <
flyrotary@lancaironline.net>
>>Sent: Tuesday, February 07, 2006 8:49 PM
>>Subject: [FlyRotary] Six port bolt-on manfold progress (was: RX-8)
>>
>>
>>>The six port will supposedly make 248 HP 100% stock. This is at about
>>>9000 RPM, however. The four port does not make as much HP stock.
>>>
>>>I am working on a carbon fiber composite manifold for the 6 port that
>>>(hopefully) will emulate the stock manifold with all the valves open.
>>>CNC machining of the molds will commence the beginning of March. We CNC
>>>machined a foam test mold a few months ago. We did a test layup of the
>>>carbon fiber about a month ago.
>>>
>>>Attached is a picture of the CAD rendition of the six-port manifold. As
>>>you can see, it will use the stock throttle body, stock injectors, stock
>>>injector rails, and will be 100% bolt-on. Should weigh about 3 pounds.
>>>(Stock manifold weighs 22 pounds.)  High temperature epoxy will easily
>>>withstand 300 F. Back-of-the envelope calculation says the burst presure
>>>on the carbon fiber tubes should be well over 10,000 psi.
>>>
>>>     The goal is to make a lightweight manifold that will hug the top of
>>>the engine and will simply bolt on.
>>>
>>>     It is going slower than I would like, but I am working on it in my
>>>spare time and trying to keep the costs down.
>>>
>>>     Bill Dube'
>>>
>>>
>>>randy echtinaw wrote:
>>>
>>>>Gentlemen,
>>>>    I have the opportunity to purchase a 4 port or a 6 port RX-8
>>>>engine. I thought I wanted a 4 port because I thought it would be
>>>>easier to muffel. I just heard a "rumor" that the 4 port is junk and
>>>>go with the 6 port. I need 220-230 hp using the 2.85 PSRU, no turbo.
>>>>I would consider P-porting if absolutely necessary to get the HP.
>>>>Obviously, I know very little about engines and want to start with
>>>>the best I can get so, considering my needs which one do I want?
>>>>Thank you,
>>>>Randy
>>>>
>>>>--
>>>>Homepage: 
http://www.flyrotary.com/
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>>>
>>
>>
>>--------------------------------------------------------------------------------
>>
>>
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>>
>>
>>--
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>
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