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Don't forget to add the speed of the airplane to
your numbers.
Bill Schertz
KIS Cruiser #4045
N343BS
Phase I testing
----- Original Message -----
Sent: Tuesday, July 07, 2009 8:45
PM
Subject: [FlyRotary] Re: INJECTION OIL IN
FUEL
This is
what I figured out as my "formula":
Max Prop RPM & Speed of Sound
1 Mile = 5,280 Feet
Speed of Sound = 768 mph (I think
this is at sea level barometric pressure, I haven't figured out what happens
with altitude.)
pi = 3.1429
6 FT (72") D (Diameter) Prop
CIRCUMFERENCE = pi X D = 3.1429 X 6 ft
= 18.857 ft Circumference
1 RPM = 18.857 ft/Minute at prop tip
With 2:1 PSRU Reduction, calculate by prop RPM and Circumference:
Prop RPM 3,000 (Engine RPM 6,000) = 56,571 ft/Minute = 10.714
miles/minute = 642.84 MPH
(768 MPH - 642.84 MPH = 125.16 MPH under
Speed of Sound)
Prop RPM 3,500 (Engine RPM 7,000) = 66,000 ft/Minute
= 12.5 miles/minute = 750 MPH
(768 MPH - 750 MPH = 18 MPH under
Speed of Sound)
================================================
I
paid enough attention in my math classes to think I've got it right.
Here's one for you: Does a cogbelt PSRU's powerlimit increase with a
wider belt? Like, for example, if a two incher can handle 150 HP, then you
might need a four inch belt to handle 300 HP. Something like that?
Here's
another: One maker put an engine RPM limit on the PSRU, and I'm thinking it
has to do with the capability of the bearing at the input end. Maybe because
these bearings are sealed - they don't run in an oil bath.
Thank you,
Bernie.
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