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 -----
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/ >>>>Archive and UnSub: http://mail.lancaironline.net/lists/flyrotary/ >>> >> >> >>-------------------------------------------------------------------------------- >> >> >>>-- >>>Homepage:
http://www.flyrotary.com/ >>>Archive and UnSub: http://mail.lancaironline.net/lists/flyrotary/ >> >> >> >>-- >>Homepage:
http://www.flyrotary.com/ >>Archive and UnSub: http://mail.lancaironline.net/lists/flyrotary/ > > > -- > Homepage: http://www.flyrotary.com/ > Archive
and UnSub: http://mail.lancaironline.net/lists/flyrotary/ >
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