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Dave,
I see no reason why your "proposed system" shouldn't work,
provided you can get the wp to prime. It is very close to my
system, which does work. One caveat, be sure to bleed the air from
the radiator and wp cavity.
Mark S.
At 09:46 AM 4/9/2004 -0700, you wrote:
OK,
I finally got around to making some drawings so it is a little easier to
discuss. When I was saying surge tank was probably meaning purge or
expansion tank. Omitted from the drawing is the connection to the
turbo which returns to the lower part of the Rad, and the purge opening I
have at the pump outlet for filling the system. I also have a purge
screw at the top of the rad to remove any bits of air which may
accumulate there.
From the discussion so far, it
sounds like I need some more continuous flow through the vent system so I
have attached a drawing of my proposed changes, submitted for your
[dis]approval.
Several of you have mentioned
tests having to do with a garden hose. Great Ideas but I have no
access to a hose at the airport that I know of.
Based on all the input so far,
I am also doing the following:
1) Drill or tap a vent
hole to allow the old thermostat bypass passage to fill with
coolant.
2) Flush out the Rad and
make sure it free-flows.
3) Flush out all the hoses to
make sure they free flow.
4) Modify the system to match
the attached drawing.
5) Inspect the impeller
clearance for excessive gap (compared to the gap on my stock water
pump).
6) Burp and re purge the high
points of the engine at least 6-7 times before doing any high power runs,
and only if I find the rad is finally getting warm when it runs.
7) Install the TES inner
coolant o-rings.
8) Weld over the EGR passage (I
found that the clay I used got pushed aside after only 30 min of run
time). This is the most likely cause of me being too lean in rotor
1 and the reason why I can t idle well.
Lastly, I want to take a
poll. I know there is no right answer so I am looking for everybody
s opinion. While I have the engine apart I am considering replacing
the 9.0:1 turbo rotors with the higher compression 9.7:1 n.a. rotors,
even thought I still plan to run the turbo. I understand that I may
will to limit the boost more (but where I don t know). I see the
advantages as slightly better fuel economy and needing to run less boost
to achieve the same h.p. The disadvantages are cost and possibly
playing with detonation in areas that are not well tested. Any
other considerations? Opinions? Suggestions on boost limits
with each type of fuel (ie. 87 vs. 91 vs. 100LL)?
Thanks for everyone s help with
this cooling issue. I never could have taken on this project
without everyone s help.
David (just started 2 weeks of
vacation) Leonard
The Rotary Roster:
http://members.aol.com/_ht_a/rotaryroster/index.html
-----Original Message-----
From: Rotary motors in aircraft
[mailto:flyrotary@lancaironline.net]
On Behalf Of Al Gietzen
Sent: Thursday, April 08, 2004 9:24 PM
To: Rotary motors in aircraft
Subject: [FlyRotary] Re: Dave's pump problems
> MessageThis may have already been suggested, but where
did you run the block vent from the top of flywheel end of engine?
Should be connected to high point of cooling system.
>
> Tracy
>
That vent is my only vent from the system. It goes to
a small surge can with a 16 psi cap which vent to 2 larger pressurized
cans on the firewall.
Dave Leonard
Unless I misunderstand (I remember this
happening once
J) this is like
no vent at all; unless the cap is off the surge tank. Yeah, I know
you know that, but we re kind of out in space here trying to figure
something out. It seems that without a vent at the exit from the
pump there will be some air trapped in the pump no?
A nice way to put in a vent at the pump
outlet is to install an AN plug with an o-ring seal. Drill into the
bottom of the plug, and then right angle to the side just below the
o-ring. Back off the plug a couple of turns when you fill to bleed
air, tighten it down to run. (Photo attached) I have a second
one that has a shrader (sp?) valve welded into it so if I need to
pressure test the system, I can just swap plugs.
Al
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