1300cc
per rotor.
Bobby
From: Rotary motors in
aircraft [mailto:flyrotary@lancaironline.net] On Behalf Of Bill
Bradburry
Sent: Wednesday, June 13, 2012 10:56 AM
To:
Rotary motors in aircraft
Subject: [FlyRotary] Re: IVO Prop
Users...
Elsewhere
on this same site he claims”
You can roughly calculate the VE of an engine if hp is known
with:
VE = 5600 X HP divided by (RPM X Displacement in cubic
inches)
This
would indicate that the rotary, with a VE of 1 would require a
displacement of 160 cu in to get a HP of 180 at 6300 rpm or 200 at 7000
rpm.
So
what is the deal on the 1300 cc? that is about 80 cu in. about
half what would be required to produce the HP we hope to
get.
Bill
B
I
would highly recommend that any of you running an IVO in-flight
adjustable prop to take a few minutes of your time and read Ross's write up on
his SDS site...some great information found at:
One
thing I found interesting for instance was his use of a
dedicated AMP meter on his IVO circuit which then allows him to set
his pitch based on the amount of amps he is
pulling...