X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Received: from poplet2.per.eftel.com ([203.24.100.45] verified) by logan.com (CommuniGate Pro SMTP 5.2.16) with ESMTP id 3879930 for flyrotary@lancaironline.net; Fri, 09 Oct 2009 00:22:28 -0400 Received-SPF: none receiver=logan.com; client-ip=203.24.100.45; envelope-from=lendich@aanet.com.au Received: from sv1-1.aanet.com.au (sv1-1.per.aanet.com.au [203.24.100.68]) by poplet2.per.eftel.com (Postfix) with ESMTP id 90E2B17393E for ; Fri, 9 Oct 2009 12:21:47 +0800 (WST) Received: from ownerf1fc517b8 (203.171.92.134.static.rev.aanet.com.au [203.171.92.134]) by sv1-1.aanet.com.au (Postfix) with SMTP id 3811ABEC005 for ; Fri, 9 Oct 2009 12:21:45 +0800 (WST) Message-ID: From: "George Lendich" To: "Rotary motors in aircraft" References: Subject: Re: [FlyRotary] Re: Your muffler Date: Fri, 9 Oct 2009 14:18:27 +1000 MIME-Version: 1.0 Content-Type: multipart/mixed; boundary="----=_NextPart_000_0009_01CA48EB.5ECE8E30" X-Priority: 3 X-MSMail-Priority: Normal X-Mailer: Microsoft Outlook Express 6.00.2900.5843 X-MimeOLE: Produced By Microsoft MimeOLE V6.00.2900.5579 X-Antivirus: avast! (VPS 091008-0, 10/08/2009), Outbound message X-Antivirus-Status: Clean This is a multi-part message in MIME format. ------=_NextPart_000_0009_01CA48EB.5ECE8E30 Content-Type: multipart/alternative; boundary="----=_NextPart_001_000A_01CA48EB.5ECE8E30" ------=_NextPart_001_000A_01CA48EB.5ECE8E30 Content-Type: text/plain; charset="iso-8859-1" Content-Transfer-Encoding: quoted-printable Al, Not tested yet, but have one almost complete for the single. The cones are there to stop the sound waves having a direct line of = sight out the rear end, the sound waves will be going all over the place = within the exhaust and I tried to replicate that with the zig zaggy = lines. There is no restriction as the area around the back to back cones, is = equal to the area of the 2" exhaust manifold area. However I do take your point on swirl restriction, but I don't see a = problem as it will swirl out the end, whereas sound waves travel in a = straight line ( I think). Bill did have me put in a reflector plate = opposite the incoming exhaust, but I don't know if this will interrupt = the swirl motion, I suspect it might. The reflector plate is on the LHS = of the parts count - photo attached. George ( down under) George; Nice design. Has anyone run one of these yet. My concern with the tangential muffler is something called 'swirl flow = choking' - discovered in connection with a similar attempt with gas = turbine exhaust. High circumferential velocity tends to keep the flow = from moving out the end, and consequent pressure buildup. I don't know = whether it applies to the pulsed flow, but it might, and your conical = restriction toward the outlet could make it worse.=20 To avoid that possibility in my tangential muffler I added internal = vanes at a 45 degree angle opposite the ports, and extended the header = pipes into muffler to a squared end. Disrupts the circumferential flow = and helps direct the exhaust toward the exit. Your depiction of the idealized sounds waves going axially; ah-h, = well; maybe/maybe notJ. Al G -----Original Message----- From: Rotary motors in aircraft [mailto:flyrotary@lancaironline.net] = On Behalf Of George Lendich Sent: Thursday, October 08, 2009 1:14 PM To: Rotary motors in aircraft Subject: [FlyRotary] Re: Your muffler Kelly There you go matey. All off the shelf SS cones and tube. George ( down under) ----- Original Message -----=20 From: Kelly Troyer=20 To: Rotary motors in aircraft=20 Sent: Thursday, October 08, 2009 9:32 PM Subject: [FlyRotary] Your muffler George, Do you have a photo or drawing available of your muffler = design..........I seem to remember seeing some design info in the past but do not know where = to find it...... Thanks, -- Kelly Troyer=20 "Dyke Delta"_13B ROTARY Engine=20 "RWS"_RD1C/EC2/EM2=20 "Mistral"_Backplate/Oil Manifold=20 =20 -------------- Original message from "George Lendich" = : --------------=20 > Ed,=20 > Cones are the GO.=20 >=20 > Any bare edge will take a battering from the heat and shock = waves. Cones=20 > formed back to back eliminate any edges.=20 >=20 > There must be supporting structure for the cones, I've used 1/4" = solid=20 > round bar welded into the exhaust skin.=20 > George (down under)=20 ------=_NextPart_001_000A_01CA48EB.5ECE8E30 Content-Type: text/html; charset="iso-8859-1" Content-Transfer-Encoding: quoted-printable
Al,
Not tested yet, but have one almost = complete for=20 the single.
 
The cones are there to stop the sound=20 waves having a direct line of sight out the rear end, the sound = waves will=20 be going all over the place within the exhaust and I tried to replicate = that=20 with the zig zaggy lines.
 
There is no restriction as the area = around the back=20 to back cones, is equal to the area of the 2" exhaust=20 manifold area.
 
However I do take your point on swirl = restriction,=20 but I don't see a problem as it will swirl out the end, whereas sound = waves=20 travel in a straight line ( I think).  Bill=20 did have me put in a reflector plate opposite the incoming exhaust, but = I don't=20 know if this will interrupt the swirl motion, I suspect it might. The = reflector=20 plate is on the LHS of the parts count - photo = attached.
 
George ( down under)

George;

 

Nice = design. =20 Has anyone run one of these yet.

My = concern with the=20 tangential muffler is something called =91swirl flow choking=92 =96 = discovered in=20 connection with a similar attempt with gas turbine exhaust.  High = circumferential velocity tends to keep the flow from moving out the = end, and=20 consequent pressure buildup.  I don=92t know whether it applies = to the=20 pulsed flow, but it might, and your conical restriction toward the = outlet=20 could make it worse.

 

To avoid = that=20 possibility in my tangential muffler I added internal vanes at a 45 = degree=20 angle opposite the ports, and extended the header pipes into muffler = to a=20 squared end. Disrupts the circumferential flow and helps direct the = exhaust=20 toward the exit.

 

Your = depiction of=20 the idealized sounds waves going axially; ah-h, well; maybe/maybe=20 notJ.

 

Al=20 G

 

-----Original=20 Message-----
From: = Rotary=20 motors in aircraft [mailto:flyrotary@lancaironline.net] On Behalf Of George = Lendich
Sent: Thursday, October 08, = 2009 1:14=20 PM
To: Rotary = motors in=20 aircraft
Subject: = [FlyRotary]=20 Re: Your muffler

 

Kelly

There you go matey. All = off the=20 shelf SS cones and tube.

George ( down=20 under)

----- Original Message = -----=20

From: Kelly = Troyer=20

To: Rotary motors in = aircraft=20

Sent:=20 Thursday, October 08, 2009 9:32 PM

Subject:=20 [FlyRotary] Your muffler

 

 =20 George,

   Do you have a = photo or=20 drawing available of your muffler design..........I seem=20 to

remember seeing some design = info in the=20 past but do not know where to find it......

 

 

Thanks,

--
Kelly=20 Troyer
"Dyke Delta"_13B ROTARY Engine
"RWS"_RD1C/EC2/EM2=20
"Mistral"_Backplate/Oil Manifold =


 

-------------- Original = message from=20 "George Lendich" <lendich@aanet.com.au>: --------------=20


> Ed,
> Cones are the GO.
>
> = Any bare=20 edge will take a battering from the heat and shock waves. Cones =
>=20 formed back to back eliminate any edges.
>
> There = must be=20 supporting structure for the cones, I've used 1/4" solid
> = round=20 bar welded into the exhaust skin.
> George (down under)=20 =

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