X-Junk-Score: 0 [] X-Cloudmark-Score: 0 [] X-Cloudmark-Analysis: v=2.3 cv=H+OlPNQi c=1 sm=1 tr=0 a=eFBQFpTHgAL+VL8MZ9Ce/g==:117 a=xycr6CVXJRVtFs4WRGOeRA==:17 a=jpOVt7BSZ2e4Z31A5e1TngXxSK0=:19 a=MeAgGD-zjQ4A:10 a=DAwyPP_o2Byb1YXLmDAA:9 a=pGLkceISAAAA:8 a=uPiJfPnwKj-UgTLIOWgA:9 a=QEXdDO2ut3YA:10 a=yMhMjlubAAAA:8 a=SSmOFEACAAAA:8 a=qFyOwGBB6rmy3wURi98A:9 a=d0xzhFdqDXg5IzUW:21 a=gKO2Hq4RSVkA:10 a=UiCQ7L4-1S4A:10 a=hTZeC7Yk6K0A:10 a=frz4AuCg-hUA:10 a=pHzHmUro8NiASowvMSCR:22 a=6VlIyEUom7LUIeUMNQJH:22 From: "Marc Wiese cardmarc@charter.net" Received: from [47.43.20.26] (HELO impout002.msg.chrl.nc.charter.net) by logan.com (CommuniGate Pro SMTP 6.2.14) with ESMTPS id 13135382 for flyrotary@lancaironline.net; Sat, 02 Nov 2019 18:34:22 -0400 Received-SPF: pass receiver=logan.com; client-ip=47.43.20.26; envelope-from=cardmarc@charter.net Received: from HomeDesktop ([97.94.202.172]) by cmsmtp with ESMTP id R1y9iA2KEh15uR1y9iNo7f; Sat, 02 Nov 2019 22:34:06 +0000 Authentication-Results: charter.net; none X-Authority-Analysis: v=2.3 cv=etJrMbhX c=1 sm=1 tr=0 a=xycr6CVXJRVtFs4WRGOeRA==:117 a=xycr6CVXJRVtFs4WRGOeRA==:17 a=jpOVt7BSZ2e4Z31A5e1TngXxSK0=:19 a=DAwyPP_o2Byb1YXLmDAA:9 a=pGLkceISAAAA:8 a=uPiJfPnwKj-UgTLIOWgA:9 a=QEXdDO2ut3YA:10 a=yMhMjlubAAAA:8 a=SSmOFEACAAAA:8 a=qFyOwGBB6rmy3wURi98A:9 a=d0xzhFdqDXg5IzUW:21 a=gKO2Hq4RSVkA:10 a=UiCQ7L4-1S4A:10 a=hTZeC7Yk6K0A:10 a=frz4AuCg-hUA:10 To: "'Rotary motors in aircraft'" References: In-Reply-To: Subject: RE: [FlyRotary] Re: stock manifold Date: Sat, 2 Nov 2019 17:34:06 -0500 Message-ID: <00dc01d591cd$a32b1310$e9813930$@charter.net> MIME-Version: 1.0 Content-Type: multipart/alternative; boundary="----=_NextPart_000_00DD_01D591A3.BA575500" X-Mailer: Microsoft Outlook 16.0 Thread-Index: AQLDOzXQ1oaF7ywgpn1yFarRT26NdKWdJC3A Content-Language: en-us X-CMAE-Envelope: MS4wfJLBaC6KNR7SU7OAkJRxwuv/TUGNyQADRYUJe0xfInLzVYVFz0xjMEkSsRLhGPA8UZToSVf7CBdr0FzCcVRnQHNokPT+W2pJNyLcCMMw4SS2IwWFnoub Hh6RQKIzjZaVnFj59/5zFnPrMlkoC5tsLvYgwd4vtOKhZnhff5NaINqvOFFsk2lRwLc0H9WnpfZpdQ== This is a multipart message in MIME format. ------=_NextPart_000_00DD_01D591A3.BA575500 Content-Type: text/plain; charset="UTF-8" Content-Transfer-Encoding: quoted-printable All the FD 3rd gen (TT) engine turbo exhaust parts are Inconel, even the = nuts, studs, and bolts. The manifold is cast Inconel, I was told way = back. FYIW. Expensive to source replacements. Marc =20 Inconel? Really? I did a similar cut and welded it together with SS rod and my Henrob = 2000. I think I used the insert as the 45* elbow. (the PVC pipe has been replaced with 0.036 SS pipe) Finn On 11/1/2019 5:10 PM, Neil Unger 12348ung@gmail.com = wrote: Can anyone tell m,e the exact metal used in the stock exhaust manifold? = I have cut one in half to reverse the direction and it appears to be S/S = outer with inconel inserts. It will help to know before I weld back = together with the correct rod. As shown the weight is now approx 10 lbs = and I am impressed with the build of the manifold, --- much better than = my version, and will be not much heavier.=20 Neil Unger=20 =20 ------=_NextPart_000_00DD_01D591A3.BA575500 Content-Type: text/html; charset="UTF-8" Content-Transfer-Encoding: quoted-printable

All the FD = 3rd gen (TT) engine turbo exhaust parts are Inconel, even the = nuts, studs, and bolts. The manifold is cast Inconel, I was told way = back. FYIW. Expensive to source replacements.

Marc

 

Inconel? Really?

I did a similar cut and welded = it together with SS rod and my Henrob 2000.
I think I used the insert = as the 45* elbow.
(the PVC pipe has been replaced with 0.036 SS = pipe)

Finn

On 11/1/2019 5:10 PM, Neil Unger 12348ung@gmail.com = wrote:

Can = anyone tell m,e the exact metal used in the stock exhaust = manifold?  I have cut one in half to reverse the direction and it = appears to be S/S outer with inconel inserts.   It will help = to know before I weld back together with the correct rod.  As shown = the weight is now approx 10 lbs and I am impressed with the build of the = manifold, --- much better than my version, and will be not much heavier. =

Neil Unger =

 

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