Mark,
I didn't see where the screws were placed, are they
at the outer corners of the plate?
George ( down under)
George,
What I like about the plate is that if it leaks you can remove
it, clean it up, and re-seal it. You can't do that if it is welded in
place. Besides, it is held in place with four 1/4-20 screws.
Mark
On Mon, Sep 21, 2009 at 9:03 PM, George Lendich <lendich@aanet.com.au>
wrote:
Mark,
I like that plate, it gives added support to
the manifold. It may be better welded on- then again there's the distortion
issue.
George ( down under)
No, they're plates that fit over the 2" SS tubes and bolt to the
rotor housing. You use RTV to make a seal between the sealing
plate, rotor housing and SS tube. Look closely at the picture I
posted, and then check the web link. The web page shows the entire
process start to finish. http://www.rotaryeng.net/Welded-steel-p-port.html
Mark
On Mon, Sep 21, 2009 at 8:39 PM, George Lendich
<lendich@aanet.com.au> wrote:
Mark,
What are PL's sealing plates are these
the sides plates he uses to pressure the sealant?
George ( down under)
Kelly,
Yes, I TIG welded them to the inner liner, then used PL's sealing
plates and Ultra Grey RTV to seal off the coolant. I plan
to pressure test them prior to assembly.
Mark
On Mon, Sep 21, 2009 at 2:41 PM, Kelly Troyer
<keltro@att.net> wrote:
Mark,
Have you made any decisions on the retension/sealing
method for your 20B "P" port inserts ??
-- Kelly Troyer "Dyke Delta"_13B ROTARY Engine
"RWS"_RD1C/EC2/EM2 "Mistral"_Backplate/Oil Manifold
--------------
Original message from Mark Steitle <msteitle@gmail.com>: --------------
Bill,
I'm not sure what's changed, but my oil temps are up from
what I reported earlier. I routinely see 220-225 on
climbout, then they settle down to 200 in cruise. Maybe I'm
producing more hp now, or maybe the earlier temperature report was
not in mid-summer, or possibly my system is not cooling as well as
it did earlier. I'm just glad that I installed TES
o-rings throughout.
My cowl flap initially had an aluminum lip,
that protruded into the airstream about 1". This
was a quick and dirty test to see the result. I
couldn't open or close it, it was open all the time. I have
since replaced the 1" lip with a servo-controlled door so I
can open/close as desired. When closed it is the same as a
stock cowl. This is very helpful in cooler climates, not so
much during triple-digit Texas summer months.
I also added an "airfoil shaped" piece on the firewall
directly above the cowl flap opening. This was done in
the hope of helping coax the heated air out of the
cowl. But I didn't detect any great improvement in
cooling. Oh, well. Next thing I plan on adding is
small air dams on each end of the flap door. The idea here
is to promote more efficient airflow out of the cowl flap.
I've heard that these make a big difference. We'll
see.
If you are considering installing a cowl flap, you may want
to consider locating it on the side, or possibly install
one on each side, back near the firewall. This would
allow you to make the opening larger, and this
location may be in a lower pressure area
than the bottom, especially during climbout. Just a
thought.
Cooling is still marginal in the Texas heat, and it
will be worse with the new P-port 20B engine. So, I may
be forced to make some major changes to get the more
powerful engine to cool, or else be forced to throttle back
during climbout. I've been considering relocating
the radiator from under the engine to the cool side of the
engine (fore/aft). This would allow me to use a slightly
larger radiator. It would clean up the plumbing and
significantly shorten the cooling lines
too.
No, I haven't experienced SAG. But then I'm running
Renesis type irridium spark plugs. I'm at 143 hours
now. Personally, I won't use anything else.
Mark
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