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Lynn,
I think you are right about bolt material, I looked up grade 8 steel, it's only rated to 450 degrees F. 18-8 (304) stainless, although much weaker, has incredible temperature range . It's rated for pressure vessel service to about 1300F and general use to 1690F.
So I just broke off a 1/16" drill in the head of an 18-8 stainless bolt, trying to make it accept safety wire. I'll keep working on that.
I'm considering Inconel 600 hardware for the turbo inlet flange, it's rated to 2000F, but I'll try the stainless there for now, and watch it a lot.
I plan to trim large diameter washers to fit tight against the turbo and header bodies, then after tightening the bolts, bend the washer edge up to act as a lock tab.
-----Original Message-----
From: shipchief shipchief@aol.com
To: Rotary motors in aircraft <flyrotary@lancaironline.net>
Sent: Mon, Jan 27, 2014 7:22 pm
Subject: [FlyRotary] Re: Exhaust Leak at Turbo Outlet Flange
Dave;
you pretty well summarized the problem.
Ross the Subaru guy over on the VANs air force forum had valuable input as well.
After I cleaned up and inspected the mess, installed grade 8 bolts and grade C high temp lock nuts on the turbo mount flange. I used the stainless embossed shim type gasket.
I assembled the turbine exhaust - to - exhaust pipe flange W/O gasket, using 1" grade 5 bolts that I had on hand. I used grade 8 washers, stacked based on the hole depth, they are not all the same depth.
I removed the Kevlar exhaust pipe wrap, cut off an undamaged section, and stuffed it into the burned thru hole in the turbo blanket.
I made exhaust pipe heat shields out of cut offs from galvanized building studs, left over from building my hangar.
N89SE ran like a top, and made the 32 minute flight back to the Home Drome with no trouble.
Today I shopped at the local specialty fastener store and picked up more Grade 8 hardware and some 1/16" cobalt drill bits, no one seems to carry drilled head grade 8 bolts around here.
I brought the top cowl home to repair the heat damaged spot over the turbo. The repair might be an aluminum inspection door.
Oh, one last thing; today I post flight inspected the repair, and all eight fasteners took 1/12th of a turn to re-tighten. I figure that's just thermal setting. Even if safety wired, they would need to be un-wired and re-torqued at least once?
(I posted similar on the VANs forum, so you might see this over there too)
-----Original Message-----
From: Lehanover < Lehanover@aol.com>
To: Rotary motors in aircraft < flyrotary@lancaironline.net>
Sent: Mon, Jan 27, 2014 10:59 am
Subject: [FlyRotary] Re: Exhaust Leak at Turbo Outlet Flange
If you use locking nuts like Jet nuts that grip the stud, you just back out
the stud on removal. Use the stock nuts or stainless nuts and safety wire them
in the tightening direction. They never come loose and can be removed without
drama. On my NA engines I use no exhaust gasket. Just a bead of GE 100% silicone
tub and tile calk. Keep it well away from the ports. Never had a leak, but I had
no back pressure from a turbo hot section either. Might be worth a try.
Lynn E. Hanover
I believe Mazda
uses some Inconel hardware on the 93+ 13Brew engines…………found this out the
hard and expensive way.
Marc
From: Rotary motors in
aircraft [mailto:flyrotary@lancaironline.net] On Behalf Of David
Leonard
Sent: Saturday, January 25, 2014 8:14 PM
To:
Rotary motors in aircraft
Subject: [FlyRotary] Re: Exhaust Leak at
Turbo Outlet Flange
Bummer! Glad you are safe.
I use the stock steel nuts. Locknuts might be an
improvement but not if there is any non-steel component. I did loose one
of those nuts once without to-do. Not sure how long it was gone.
The other 2 held everything together.
Be very careful with what gaskets you choose. I found
some nice-looking aftermarket turbo manifold gaskets for about $20 while the
stock versions are about $90 each, so I installed one. It lasted about
30 hours until it disintegrated. The resulting exhaust leak burned
through a coolant line and I dead sticked onto a local airport (departing
from a formation routine at an airshow!.. complete with a cloud of
steam).
Sigh, the stock ones are nothing but stainless steel
layer, not some sort of fiber stuff in the after market
ones.
On another occasion I was using some very nice and
expensive exhaust clamps that were steel but I didnt notice that part of the
block holding the nuts was aluminum. About 50 hrs in something caused
the alumimum to get too hot, which created an exhaust leak, which accelerated
the process. It burned a hole in the cowl and splatered molten aluminum
everywhere - some of it is still around.
Another time I was using some fancy exhaust
wrap. It slowly disintigrated over the course of 100+ hours and was
generally an annoyance.
I tried a flowmaster hushpower muffler but melted most
of the stuffing out of it on the first flight. Luckily it melted pretty
cleanly and didnt clog the exhaust.
Moral of the story.. as if it didn't take me long
enough to beat this through my skull.. NOTHING that is not made of
steel or better goes into any part of the exhaust system. Particularly
gaskets and nuts.
Guess I should have passed that one along sooner.
Glad you got back safely. Good job.
I had the nuts
come loose on my turbo manifold on the block, I'm using with out
the turbo, so I drilled the nuts and secured them with wire.
JohnD
Thanks for keeping us all informed , helps us all to make
sure we look for often simple overlooked areas.
Renises 13 b rv7
Sent from my
iPad
During the 8th
flight of my RV8 with 13B Turbo, I experienced an exhaust leak at the
turbo exhaust flange. I mistakenly used brass exhaust nuts which are
twice as tall as regular nuts. They work great on most engines. I should
have know better, as the temperature at the turbo outlet, under the
insulation is much higher.
The brass nuts
softened and deformed into a flange face at the washer! Once the tension
was gone, the heat & vibration did the
rest.
The exhaust gasket
blew where the gap was widest, at the top.
The escaping heat
burned thru the insulating jacket and the stick on reflective
aluminum. Then the fiberglass cowl charred, I smelled
that!
I was close to my
destination, and high, so I was able to pull off the power, put down the
nosed and get on the ground without
incident.
I'm disassembling
it now, looks like I need 4 high temperature lock nuts and a TO-4
exhaust flange gasket. I should review and improve the insulation over the
turbine housing. Also I need to repair the charred area of the cowl, which
might be in the form of an aluminum access
hatch.
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