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Message-ID: <003601c83abe$477b0160$7c771fd3@george>
From: "George Lendich"
To: "Rotary motors in aircraft"
References:
Subject: Re: [FlyRotary] Re: PP Timing
Date: Mon, 10 Dec 2007 09:50:27 +1000
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Subject: [FlyRotary] Re: PP Timing
In a message dated 12/9/2007 4:32:22 AM Eastern Standard Time, =
lendich@optusnet.com.au writes:
The inlet timing would be the same ( 85 degrees) - but later, but =
not so late as to get into the compression stage, which might cause =
further issues.
=20
I remember discussing this with someone (it might have been Lynn) =
but I can't remember what the negatives are with such a late PP.
=20
Can someone put me straight on this again!
I hope I got those degrees right!
George (down under)
Port Timing
IO =3D Intake opens
IC =3D Intake closes
EO =3D Exhaust opens
EC =3D Exhaust closes
US Model First Generation RX-7
IO 32=B0 ATDC
IC 40=B0 ABDC
EO 75=B0 BBDC
EC 38=B0 ATDC
European Model Model First Generation RX-7
IO 32=B0 ATDC
IC 50=B0 ABDC
EO 75=B0 BBDC
EC 48=B0 ATDC
First and Second Generation 6-Port 13BPrimary intake (Part =
throttle/cruise)
IO 32=B0 ATDC
IC 40=B0 ABDC
Secondary intake (Part to full throttle)
IO 32=B0 ATDC
IC 30=B0 ABDC
Auxiliary high speed ports (Full throttle above approximately 4000 =
rpm)
IO 45=B0 ATDC
IC 70=B0 ABDC
EO 71=B0 BBDC
EC 48=B0 ATDC
Second and Third Generation Turbo 13B
IO 32=B0 ATDC
IC 50=B0 ABDC
EO 71=B0 BBDC
EC 48=B0 ATDC
Racing Beat "Street Port"
IO 25=B0 ATDC
IC 60=B0 ABDC
EO 84=B0 BBDC
EC 48=B0 ATDC
Racing Beat "J-Bridge Port"
IO 115=B0 BTDC
IC 72=B0 ABDC
EO 88=B0 BBDC
EC 57=B0 ATDC
Mazda Factory Peripheral Port
IO 86=B0 BTDC
IC 75=B0 ABDC
EO 73=B0 BBDC
EC 65=B0 ATDC
This information was copied from Paul Yaws very informative web site =
at:
WWW.Yawpower.com.=20
You cannot spend too much time reading on this site.
I could not get my mind around some of the numbers you cited. I am =
setting up a new house in Zephyrhills Florida, and will be building a =
new shop here as money becomes available. I have none of my stuff here, =
and had to refer to Paul's web page to see the open and close numbers. =
This is my wife's computer, and she has nothing about rotaries on it.
We will be in Ohio for Christmas and we will keep that house for =
summer time.=20
Of the 4 events called out in both piston and rotary engines, the =
intake port (or valve) in the piston case, closing point have the =
greatest effect on lower to middle range power. This also applies to the =
Pport engine. =20
Note: that even the exotic high speed ports on the 6 port engine close =
at 70 degrees ABDC.
My Bridgeported engine closes at 80 degrees, techically, but is =
flowing very little at that point. (big radius and polish job on the =
closing line). Extending the closing point to gain HP higher up the RPM =
range is fine for a car, or an application where torque can be =
mulitplied by some sort of transmission, but the fixed loading of a =
propeller may not allow you to wind up to your ideal or near to your =
ideal power RPM. So a robust mid range is a must.=20
The side ported engines (even street ported) open the intake port =
After BDC. So exhaust dilution is nil. In the Pport engine, this is not =
possible. The big hole in the housing will be opening long before the =
exhaust port is closed off to any extent, and dilution is going to =
happen.=20
From this fact alone I deduce that the intake port should close just =
after 70 degrees. That the intake port should open as late as it is =
possible to build. The intake port would have a near rectangular shape, =
not far removed from a tall looking exhaust port. Even so, the round =
port may be flowing so poorly near the open and close points that very =
little affect may be noticed. The top of the exhaust port I would leave =
stock. I would widen and radius the sides of the port. I would open the =
port just a bit early with a slight bow to the centerline, and a =
generous radius.=20
The idea here is to minimize overlap.=20
The Pport engine has the pointed rotor tip to open and close the port =
/vice the flat side of the rotor. The flow is uninteruped in effect, =
with the down side being that the flow is directed right out the exhaust =
port, producing the giant fireballs the racers love to generate.
The RPM where this shuts off is controlled by the overlap period.=20
Airplane engines operate in the low to middle of the RPM range of the =
engine. My bridgeport idles at 2,200 RPM. The hint here is that =
automotive like closing points will produce the best airplane engines.
A poorly done Pport engine will massively outperform a side port =
engine. The Pport will be less happy with exhaust system problems. More =
thought to header lengths and muffler design. A function of overlap. =
Smaller header tubes rather than larger. Same exact length a must. Same =
angle into a collector. Longer rather than shorter.=20
The idea here is to have the port close before a reflected wave can =
get back to it.
The port numbers I could give you from home are from Mandeville =
modified housings that were used up to 10,700 RPM, and that data would =
probably be of no value.
Sorry.
Lynn E. Hanover=20
Thanks Lynn,
It goes without saying that I always appreciate your contribution. I =
may have to refer back to what you were saying to clarify some points.
I now understand the closing event has the most effect on the mid =
range power we need in Aviation (why is that? and why is your BP closing =
of 80 degrees flowing very little - there seems to be plenty of suction =
still going on?) and that closing event should not exceed 70 degrees =
ABDC. This is probably something you told me previously and I hadn't =
remembered ( or understood properly). However the Mazda Factory PP is 75 =
degree IC, perhaps allowing for higher HP at the higher RPM range. =
Whereas the Leman's engine seems to be about 70 degrees ABDC.
Secondly, the later the opening event the better ( I understood that =
one) because of overlap and contamination of the inlet charge at lower =
RPM. Now if we could just close it before we open it, we would be way =
ahead - but of course that is not possible, so the squat PP is the next =
best shape and timing.
So the opening later is better; but the closing later is not good! As =
we say in Australia - BUGGER!!
Anyhow there is another reference in your response which I don't quite =
understand and that is "So even with red lines at or above 8,000 RPM =
this modest port closing is more than adequate (this is understood). If =
I remember correctly (this becomes less likely with time) " Can you =
explain the last sentence about (less likely with time). Do you mean =
later openings gave better higher RPM, HP in the racing industry.
TIA
George (down under)
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Subject: [FlyRotary] Re: PP =
Timing
In a message dated 12/9/2007 =
4:32:22 AM Eastern=20
Standard Time, lendich@optusnet.com.au=20
writes:
The inlet timing would be the same ( 85 degrees) - but =
later,=20
but not so late as to get into the compression stage, which might =
cause=20
further issues.
I remember =
discussing this=20
with someone (it might have been Lynn) but I can't remember what the =
negatives are with such a late PP.
=
Can someone put =
me straight on=20
this again!
I hope I got those degrees right!
George (down=20
under)
Port Timing
IO =3D =
Intake=20
opens
IC =3D Intake closes
EO =3D Exhaust opens
EC =3D =
Exhaust=20
closes
US Model=20
First Generation RX-7
IO 32=B0 ATDC
IC 40=B0 ABDC
EO 75=B0 BBDC
EC =
38=B0=20
ATDC
European=20
Model Model First Generation RX-7
IO 32=B0 =
ATDC
IC 50=B0 ABDC
EO=20
75=B0 BBDC
EC 48=B0 ATDC
First and Second =
Generation=20
6-Port 13BPrimary=20
intake (Part throttle/cruise)
IO 32=B0 ATDC
IC 40=B0 =
ABDC
Secondary=20
intake (Part to full throttle)
IO 32=B0 ATDC
IC 30=B0 =
ABDC
Auxiliary high=20
speed ports (Full throttle above approximately 4000 rpm)
IO 45=B0 =
ATDC
IC=20
70=B0 ABDC
EO 71=B0 BBDC
EC 48=B0 ATDC
Second and Third =
Generation=20
Turbo 13B
IO 32=B0=20
ATDC
IC 50=B0 ABDC
EO 71=B0 BBDC
EC 48=B0 =
ATDC
Racing Beat =
"Street=20
Port"
IO 25=B0=20
ATDC
IC 60=B0 ABDC
EO 84=B0 BBDC
EC 48=B0 =
ATDC
Racing Beat =
"J-Bridge=20
Port"
IO 115=B0=20
BTDC
IC 72=B0 ABDC
EO 88=B0 BBDC
EC 57=B0 =
ATDC
Mazda Factory =
Peripheral=20
Port
IO 86=B0=20
BTDC
IC 75=B0 ABDC
EO 73=B0 BBDC
EC 65=B0 ATDC
This =
information was=20
copied from Paul Yaws very informative web site at:
WWW.Yawpower.com.
You cannot =
spend too=20
much time reading on this site.
I could not get my mind =
around some=20
of the numbers you cited. I am setting up a new house in Zephyrhills =
Florida,=20
and will be building a new shop here as money becomes available. I =
have none=20
of my stuff here, and had to refer to Paul's web page to see the open =
and=20
close numbers. This is my wife's computer, and she has nothing about =
rotaries=20
on it.
We will be in Ohio for Christmas and we will keep that house =
for=20
summer time.
Of the 4 events called out in both piston and =
rotary=20
engines, the intake port (or valve) in the piston case, closing point =
have the=20
greatest effect on lower to middle range power. This also applies to =
the Pport=20
engine.
Note: that even the exotic high speed ports on =
the 6=20
port engine close at 70 degrees ABDC.
My Bridgeported engine closes =
at 80=20
degrees, techically, but is flowing very little at that point. (big =
radius and=20
polish job on the closing line). Extending the closing point to gain =
HP higher=20
up the RPM range is fine for a car, or an application where torque can =
be=20
mulitplied by some sort of transmission, but the fixed loading of a =
propeller=20
may not allow you to wind up to your ideal or near to your ideal power =
RPM. So=20
a robust mid range is a must.
The side ported engines (even =
street=20
ported) open the intake port After BDC. So exhaust dilution is nil. In =
the=20
Pport engine, this is not possible. The big hole in the housing will =
be=20
opening long before the exhaust port is closed off to any extent, and =
dilution=20
is going to happen.
From this fact alone I deduce that the =
intake port=20
should close just after 70 degrees. That the intake port should open =
as late=20
as it is possible to build. The intake port would have a near =
rectangular=20
shape, not far removed from a tall looking exhaust port. Even so, the =
round=20
port may be flowing so poorly near the open and close points that very =
little affect may be noticed. The top of the exhaust port I =
would leave=20
stock. I would widen and radius the sides of the port. I would open =
the port=20
just a bit early with a slight bow to the centerline, and a generous =
radius.=20
The idea here is to minimize overlap.
The Pport =
engine=20
has the pointed rotor tip to open and close the port /vice the flat =
side of=20
the rotor. The flow is uninteruped in effect, with the down side being =
that=20
the flow is directed right out the exhaust port, producing the giant =
fireballs=20
the racers love to generate.
The RPM where this shuts off is =
controlled=20
by the overlap period.
Airplane engines operate in the low to =
middle=20
of the RPM range of the engine. My bridgeport idles at 2,200 =
RPM. The=20
hint here is that automotive like closing points will produce the best =
airplane engines.
A poorly done Pport engine will massively =
outperform=20
a side port engine. The Pport will be less happy with exhaust system =
problems.=20
More thought to header lengths and muffler design. A function of =
overlap.=20
Smaller header tubes rather than larger. Same exact length a must. =
Same angle=20
into a collector. Longer rather than shorter.
The idea here is =
to have=20
the port close before a reflected wave can get back to it.
The =
port=20
numbers I could give you from home are from Mandeville modified =
housings that=20
were used up to 10,700 RPM, and that data would probably be of no=20
value.
Sorry.
Lynn E. Hanover
Thanks =
Lynn,
It goes=20
without saying that I always appreciate your contribution. I may have =
to refer=20
back to what you were saying to clarify some points.
I now=20
understand the closing event has the most effect on the mid range =
power we=20
need in Aviation (why is that? and why is your BP closing of =
80=20
degrees flowing very little - there seems to be plenty of suction =
still going=20
on?) and that closing event should not exceed 70 degrees =
ABDC. This=20
is probably something you told me previously and I hadn't remembered ( =
or=20
understood properly). However the Mazda Factory PP is 75 degree IC, =
perhaps=20
allowing for higher HP at the higher RPM range. Whereas the =
Leman's=20
engine seems to be about 70 degrees ABDC.
Secondly, the =
later the opening=20
event the better ( I understood that one) because of overlap and =
contamination=20
of the inlet charge at lower RPM. Now if we could just close it before =
we open=20
it, we would be way ahead - but of course that is not possible, so the =
squat PP is the next best shape and =
timing.
So the opening later is better; but the closing later =
is not=20
good! As we say in Australia - BUGGER!!
Anyhow there is another reference in your response =
which I=20
don't quite understand and that is "So even with red lines at or above =
8,000=20
RPM this modest port closing is more than adequate (this is=20
understood). If I remember correctly (this becomes less =
likely with=20
time) " Can you explain the last sentence about (less likely with =
time). Do=20
you mean later openings gave better higher RPM, HP in the racing=20
industry.
TIA
George (down under)
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