Ed,
Excellent take on throttle travel. You
have a good knack for explaining things that simple minds can grasp.
Oh, and a belated Happy Birthday from Georgia!
Bryan
From: Rotary motors in aircraft
[mailto:flyrotary@lancaironline.net] On
Behalf Of Ed Anderson
Sent: Friday, February 12, 2010
4:38 PM
To: Rotary
motors in aircraft
Subject: [FlyRotary] Throttle
limits was Re: N.A. Renesis to turbo
Bill, if Dennis had a TB just big enough that it exactly
provided 100% power at sea level,
then as he increases in altitude, he will find more and more throttle travel
that does nothing to increase power. This is because it takes less and
less throttle plate opening to provide sufficient airflow for the pressure/air
density in the manifold to reach the ambient pressure/air density (ambient
density is decreasing with altitude). Since that air density is less than
at sea level, it requires less throttle opening to reach than at sea level.
The position of the throttle plate affects
only the air flow volume (not the density of that air airflow), but the amount
of air flow volume does determine the air density in the manifold. The external
atmospheric pressure is of course what is forcing the air through the throttle
body – The less air pressure at altitude means less air is flowing
through the TB as you gain altitude. Remember even though to simply the
verbiage - we often talk of the engine “sucking” but of course it
does not. The engine simply opens its ports and whatever pressure is in
the manifold forces that air into the essentially empty combustion
chamber.
Think of it this way, there are two ways
you can have ambient air density in your intake manifold. Those two ways are
with the throttle open or the throttle closed – a contradiction?
Not, so. You may have ambient air pressure/density in the manifold when
the engine is running and TB open sufficiently to provide ambient pressure in
the manifold OR when the engine is
not running.
When the engine is stopped - you also have
ambient pressure in your intake even with your throttle 99.99 % closed because
the engine is not “sucking” any air out of the manifold when
stopped. So a small leak in the throttle bottle is sufficient for the
manifold pressure to reach and maintain ambient when the engine is not running.
What Dennis has done with his DIE intake
does not change this factor, but what the pulse in the intake does when it
reaches the other end of the intake manifold (note how his intakes are tied
together so the pulse can travel from one intake port of one rotor to the
intake port of the second rotor) is briefly create a localized pressure
increase in the intake manifold right at the intake port as it is open.
This in effect shoves more mixture into the combustion chamber – in
effect it is a very brief supercharger effect. It only lasts for
milliseconds and therefore you don’t get the same power increase that you
would if you had a turbocharger pushing in denser air the entire time the
intake is open. On the other hand you don’t have 30-50 lbs
more weight and for basically no more than fabricating your intake different
– it’s basically a free lunch.
But, as Dennis will tell you - doing
the analysis to get the equations so you get dimension correct for the effect
– can give you a headache {:>) – right Dennis??.
So, anyhow, back the throttle travel, if
your TB is larger than needed to
reach 100% power at sea level, then
you would also find “excess” throttle travel sitting on the ground
with the engine running at WOT. Once the throttle is opened sufficient
for manifold pressure to reach ambient, then opening it further will provide no
increase in power. You have in the vernacular- “Maxed Out!” {:>)
Once the throttle plate is open sufficient
to permit the manifold pressure/air density to reach ambient conditions –
no further opening will produce any more power even though you may have
5” of throttle travel and 50% more throttle plate opening to go.
Ed
From: Rotary motors in aircraft
[mailto:flyrotary@lancaironline.net] On
Behalf Of Bill Bradburry
Sent: Friday, February 12, 2010
3:33 PM
To: Rotary
motors in aircraft
Subject: [FlyRotary] Re: rpm vs
Power was : Throttle limits was Re: N.A. Renesis to turbo
Thanks, Dennis,
It sounds like you still have a little unused throttle
travel even with the new intake.
Can you provide design measurements for your new
intake? I ask only if you have no plans to make and sell it.
Bill B
From: Rotary motors in aircraft
[mailto:flyrotary@lancaironline.net] On
Behalf Of Dennis Haverlah
Sent: Friday, February 12, 2010
2:20 PM
To: Rotary
motors in aircraft
Subject: [FlyRotary] Re: rpm vs
Power was : Throttle limits was Re: N.A. Renesis to turbo
I used the same 65 mm
Mustang throttle body on both my original and new intakes. If I
remember correctly, I believe I had a longer unused throttle travel with
the original intake but I never measured it. I don't know the static rpm
increase with the new intake - probably have that in my notes some where but my
max. rpm at high altitude (8,000 - 10,000) increased 400-500 rpm. I
estimated I went from 165 -170 HP with the old intake to about 185 HP with the
new intake. This in in line with Ed Anderson's recent note that Mazda got
about a 16% power increase at 6000 rpm with the DIE effect. I felt much
improved acceleration the first time I took off with the new intake.
the new intake is based on dynamic intake
effect (DIE) where the closing of an intake valve caused the
moving intake air to bounce off the valve creating a pressure wave. The
wave travels at the speed of sound to the other intake valve and arrives there
just before that valve closes. This increases the amount of air and fuel
that enters the combustion chamber. (As we know the rotary has no valves
but uses the sides of the rotor for opening and closing the intakes.) I
designed my intake to give max. performance at 6300 rpm.
If I had cut down my prop to 74" it would give me more clearance for the
prop on my RV-7A and increase my top end rpm. Max rpm is about 6400
rpm with the new intake and the 76" prop. I'm really not needing
higher RPM now.
Dennis Haverlah
Bill Bradburry wrote:
Dennis,
Did your static rpm increase with the new
manifold? How much? Did you before and do you now have any unused
throttle travel like Mike describes? Are you using the same
throttle body on the new manifold? What is the MM opening of the Mustang
body?
My manifold is very similar to your old one. My
tubes are cut just above the injector bosses, which makes them a little (maybe
an inch) shorter than your old ones. I have a 76 X 88 Performance prop
which I am considering having cut down to 74” like Tracy and Ed when I
send it in for final finish. I am using an aftermarket throttle body that
is 75MM in throat diameter. This is the same size as the stock Renesis
throttle body which is why I picked it. I had intended to use the Renesis
body, but didn’t wait for Tracy
to get the fly by wire done. I am not flying, but my static is 52-5300
rpm and I have a lot of throttle left at that rpm. The last probably ¼ of
the travel is not used.
Bill B
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