I seems to me one could make a variable load
dynamometer out of a torque converter. My guess is that the internals of a
water break and a torque converter look a lot alike. This is purely
speculation. To vary the load on a traditional
water break one vary the quantity of fluid in the water break. So vary the
quantity of the fluid in the torque converter. Some sort of cooling of the torque
convent would be needed (this is where all the engine power goes- Heat) I will
consult one of my friends who know a lot a about cars see what he thinks.
Warning: Large Dynos are dangerous when
under load due to the danger of water break rupture (high pressure water and steel
shrapnel). There should always be a protective barrier between you ad the water
break when it is under load.
Alex Madsen
From: Rotary motors in aircraft
[mailto:flyrotary@lancaironline.net] On
Behalf Of David Staten
Sent: Saturday, January 22, 2005
11:30 PM
To: Rotary
motors in aircraft
Subject: [FlyRotary] Re: Dynos II
(was Re: changed to Octane)
Well... The RD1-B is at a 2.17:1 gear ratio.. so
2700-3000 rpm would be the high end coming out of the PSRU gearbox. I know that
some cars their top gear in the tranny is a 1:1, so 3000 rpm at the engine is
transmitted to the wheels.. so i would expect (er.. HOPE) the
"drivetrain" to handle it..
After looking at the PL plans, it seems feasible to build the dyno he
describes, but it would involve mounting the engine to a separate test stand
and then putting a prop on it.. I was hoping to figure out some way to not have
to put the prop on (or if we did, use a loaner prop) so that we could figure
out exactly what our engine was capable of doing, THEN getting the prop matched
to the known power available, rather than guessing.
I guess it would be possible to rig up an axle brake as a load device and
couple that with a PL style dyno (measuring torque with a sidearm).. Wouldnt be
able to measure static thrust that way.. but hey.. its not a major factor until
the right prop is on there.
Dont know if practical or not, but a load cell on a trailer hitch might be able
to measure static thrust if the whole thing was trailer mounted. For what its
worth I swung by the airport and got the cardboard template for the firewall. I
may see how practical this will be to build or not.. If the bennies dont
outweigh the cost, it may not be worth it.. but it would be nice to get a good
breakin on the engine and test under load without having to do it during the
flight test.. Might be able to address cooling issues up front too, and insure
that what we have is adequate.
Dave
Jack Ford wrote:
How's about adapting a flange-style u-joint to the output of the engine and
running a driveshaft? 'Course the driveshaft might get launched spinning at
9k or so, and so might the truck axle pinion and bearings.
Might be a better arrangement to use a stick-shift transmission (in granny)
between the engine and the truck axle, use the axle for brakes and measure
torque at the engine mount. Same cat.
Jack Ford
----- Original Message -----
From: <Lehanover@aol.com>
To: "Rotary motors in aircraft" <flyrotary@lancaironline.net>
Sent: Saturday, January 22, 2005 11:10 AM
Subject: [FlyRotary] Re: Dynos II (was Re: changed to Octane)
In a message dated 1/22/2005 12:08:34 PM Central Standard Time,
dale.r@cox.net writes:
Build a disc to bolt to the companion flange of a truck differential and
the
flywheel of a rotary.
How about elongating half of the bolt holes in the backing plate, in an
arc
to conform with the bolt circle diameter. Use smaller bolts and drop in a
small
needle bearing around each bolt/stud. Now the backing plate can articulate
a
bit around the centerline of the axle. Mount the transducer to a bracket
welded to the housing, and the other end to the backing plate. Calibrate
the output
with a torque wrench.
There you go. A truck axle dyno.
Don't forget the math to take out the effect of the differential ratio,
lest
you report some giant numbers.
Lynn E. Hanover
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