Return-Path: Received: from fed1rmmtao06.cox.net ([68.230.241.33] verified) by logan.com (CommuniGate Pro SMTP 4.3c2) with ESMTP id 766024 for flyrotary@lancaironline.net; Wed, 02 Mar 2005 01:17:16 -0500 Received-SPF: none receiver=logan.com; client-ip=68.230.241.33; envelope-from=ALVentures@cox.net Received: from BigAl ([68.7.14.39]) by fed1rmmtao06.cox.net (InterMail vM.6.01.04.00 201-2131-118-20041027) with ESMTP id <20050302061628.LOZT1497.fed1rmmtao06.cox.net@BigAl>; Wed, 2 Mar 2005 01:16:28 -0500 From: "Al Gietzen" To: "'Rotary motors in aircraft'" , "'kevin lane'" Subject: RE: [FlyRotary] Re: 20B exhaust (so far) Date: Tue, 1 Mar 2005 22:16:43 -0800 Message-ID: <000001c51eef$67d2c350$6400a8c0@BigAl> MIME-Version: 1.0 Content-Type: multipart/alternative; boundary="----=_NextPart_000_0001_01C51EAC.59AF8350" X-Priority: 3 (Normal) X-MSMail-Priority: Normal X-Mailer: Microsoft Outlook, Build 10.0.6626 Importance: Normal In-Reply-To: X-MimeOLE: Produced By Microsoft MimeOLE V6.00.2900.2180 This is a multi-part message in MIME format. ------=_NextPart_000_0001_01C51EAC.59AF8350 Content-Type: text/plain; charset="us-ascii" Content-Transfer-Encoding: quoted-printable Kevin; =20 You may be able to get by without bellows in that configuration; but = there will be some thermal and support stresses, and at our exhaust temps, = stress corrosion occurs in 321 (ask David Atkins what happened to his SS = exhaust). So when you do it over you may want to go to inconel. =20 Also, I believe the most reliable weld at the exhaust flange would be = with a slip fit of the pipe through the flange, and the weld on the other side. This allows the stress due to the expansion of the pipe relative to the flange to be carried against the flange rather than by the weld.=20 =20 FWIW, =20 Al =20 -----Original Message----- From: Rotary motors in aircraft [mailto:flyrotary@lancaironline.net] On Behalf Of kevin lane Sent: Tuesday, March 01, 2005 9:03 PM To: Rotary motors in aircraft Subject: [FlyRotary] Re: 20B exhaust (so far) =20 Buly - I discussed this very point with my welder at great length. He = has a lot of experience fabricating exhaust for race cars, including rotaries. = We decided to chance not using the slip joints based on other cases where = he didn't use them. They can always be added if deemed necessary. I will = have a ball joint ahead of the muffler. I hope to have some dedicated = airflow over the manifold also. My guess is that this whole system will be = changed as I learn more of what I really need. Kevin Lane Portland, OR e-mail-> n3773@comcast.net web-> http://home.comcast.net/~n3773 (browse w/ internet explorer) ----- Original Message -----=20 From: Bulent Aliev=20 To: Rotary motors in aircraft=20 Sent: Tuesday, March 01, 2005 6:06 PM Subject: [FlyRotary] Re: 20B exhaust (so far) =20 Hi Kevin, I believe you must have some slip joints there to allow for expansion. Without them you may get some cracking. Buly On 3/1/05 7:45 PM, "kevin lane" wrote: I have my engine upside down right now while I work out oil cooler = location. My welder gave me some 321, so that's why the front rotor has an = additional weld. That plywood box is a spintech muffler mock-up, although it's not = in place. I plan to run it against the fire wall. With my belly scoop I = can't run the exhaust down there (damn!), so it will go out the side, a la = turbine engine I guess. I was lucky to have the welded up part able to slide on around the engine mount, easy to forget when you are playing with = individual pieces. Kevin Lane Portland, OR e-mail-> n3773@comcast.net web-> http://home.comcast.net/~n3773 (browse w/ internet explorer) =20 ------=_NextPart_000_0001_01C51EAC.59AF8350 Content-Type: text/html; charset="us-ascii" Content-Transfer-Encoding: quoted-printable Re: [FlyRotary] 20B exhaust (so far)

Kevin;

 

You may be able to get by without bellows in that configuration; but there will be some thermal and = support stresses, and at our exhaust temps, stress corrosion occurs in 321 (ask = David Atkins what happened to his SS exhaust).  So when you do it over = you may want to go to inconel.

 

Also, I believe the most reliable = weld at the exhaust flange would be with a slip fit of the pipe through the = flange, and the weld on the other side.  This allows the stress due to the expansion of the pipe relative to the flange to be carried against the = flange rather than by the weld.

 

FWIW,

 

Al

 

-----Original = Message-----
From: Rotary motors in = aircraft [mailto:flyrotary@lancaironline.net] On Behalf Of kevin lane
Sent: Tuesday, March 01, = 2005 9:03 PM
To: Rotary motors in = aircraft
Subject: [FlyRotary] Re: = 20B exhaust (so far)

 

Buly - I = discussed this very point with my welder at great length.  He has a lot of = experience fabricating exhaust for race cars, including rotaries.  We decided = to chance not using the slip joints based on other cases where he didn't = use them.  They can always be added if deemed necessary.  I will have a ball = joint ahead of the muffler.  I hope to have some dedicated airflow over = the manifold also.  My guess is that this whole system will be changed = as I learn more of what I really need.

=

----- Original Message = -----

Sent: Tuesday, March 01, 2005 6:06 PM

Subject: [FlyRotary] Re: 20B exhaust (so far)

 

Hi Kevin, I believe you must have some slip joints there to allow for = expansion. Without them you may get some cracking.
Buly


On 3/1/05 7:45 PM, "kevin lane" <n3773@comcast.net> wrote:

I have my engine = upside down right now while I work out oil cooler location.  My welder = gave me some 321, so that's why the front rotor has an additional weld. =  That plywood box is a spintech muffler mock-up, although it's not in place. =  I plan to run it against the fire wall.  With my belly scoop I can't = run the exhaust down there (damn!), so it will go out the side, a la turbine = engine I guess.  I was lucky to have the welded up part able to slide on = around the engine mount, easy to forget when you are playing with individual = pieces.
Kevin Lane  Portland, OR
e-mail-> n3773@comcast.net
web-> http://home.comcast.net/~n3773
(browse w/ internet explorer)

 

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