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 5.3.2) with ESMTP id 4127270 for flyrotary@lancaironline.net; Tue, 16 Feb 2010 16:29:10 -0500 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 (mail.aanet.com.au [203.24.100.34]) by poplet2.per.eftel.com (Postfix) with ESMTP id DBA431738E4 for ; Wed, 17 Feb 2010 05:28:26 +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 6F97CBEC04C for ; Wed, 17 Feb 2010 05:28:24 +0800 (WST) Message-ID: From: "George Lendich" To: "Rotary motors in aircraft" References: Subject: Re: [FlyRotary] Re: rpm vs Power was : Throttle limits was Re: N.A. Renesis to turbo Date: Wed, 17 Feb 2010 07:28:25 +1000 MIME-Version: 1.0 Content-Type: multipart/alternative; boundary="----=_NextPart_000_001D_01CAAFA2.CADFD570" 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 100216-1, 02/16/2010), Outbound message X-Antivirus-Status: Clean This is a multi-part message in MIME format. ------=_NextPart_000_001D_01CAAFA2.CADFD570 Content-Type: text/plain; charset="iso-8859-1" Content-Transfer-Encoding: quoted-printable Bryan, I'm hearing you, I guess you mean the Renesis manifold. Maybe someone = can duplicate that in carbon fiber, in a more compact form. I know - = another job for Bill Jepson. George (down under) George, It's a shame that the stock intake that does all this using a valve, = can't be used in our application. Bryan =20 -------------------------------------------------------------------------= ----- From: Rotary motors in aircraft [mailto:flyrotary@lancaironline.net] = On Behalf Of George Lendich Sent: Tuesday, February 16, 2010 3:54 AM To: Rotary motors in aircraft Subject: [FlyRotary] Re: rpm vs Power was : Throttle limits was Re: = N.A. Renesis to turbo =20 Bryan, I missed where the 43" came from, however from my calculations for = 44mm inlet tube, my calculations came to 21.36". That's for a straight = tube inlet manifold. That's interesting isn't it. George (down under) This is hard for me to visualize as well. Perhaps if you get a = chance, you could snap a picture from the top. Did you get 43 in. from #1 secondary to #2 secondary? Bryan =20 -------------------------------------------------------------------------= --- From: Rotary motors in aircraft [mailto:flyrotary@lancaironline.net] = On Behalf Of Bill Bradburry Sent: Monday, February 15, 2010 11:29 PM To: Rotary motors in aircraft Subject: [FlyRotary] Re: rpm vs Power was : Throttle limits was Re: = N.A. Renesis to turbo =20 Dennis, I just looked at your picture again.the secondary look much longer = than the primaries. It may be an optical illusion??? I bet you mean 1 = 1/8 id?? Bill B=20 =20 -------------------------------------------------------------------------= --- From: Rotary motors in aircraft [mailto:flyrotary@lancaironline.net] = On Behalf Of Dennis Haverlah Sent: Monday, February 15, 2010 11:03 PM To: Rotary motors in aircraft Subject: [FlyRotary] Re: rpm vs Power was : Throttle limits was Re: = N.A. Renesis to turbo All my tubes are the same length and the same diameters. I can = check but I think they were 1 1/4 id. and 1 1/4 od. Bill Bradburry wrote: Dennis, Aren't your primary and secondary tubes different lengths from rotor = face to rotor face? If so, what are the two lengths? Are they = different diameters? Bill B =20 -------------------------------------------------------------------------= --- =20 -------------------------------------------------------------------------= --- =20 ------=_NextPart_000_001D_01CAAFA2.CADFD570 Content-Type: text/html; charset="iso-8859-1" Content-Transfer-Encoding: quoted-printable
Bryan,
I'm hearing you, I guess you mean the = Renesis=20 manifold. Maybe someone can duplicate that in carbon fiber, in a more = compact=20 form. I know - another job for Bill Jepson.
George (down under)

George,

It=92s a = shame that the=20 stock intake that does all this using a valve, can=92t be used in our=20 application.

Bryan

 

From:=20 Rotary motors in aircraft = [mailto:flyrotary@lancaironline.net] On=20 Behalf Of George Lendich
Sent: Tuesday, February 16, = 2010 3:54=20 AM
To: = Rotary motors in aircraft
Subject: [FlyRotary] Re: rpm vs = Power was=20 : Throttle limits was Re: N.A. Renesis to turbo

 

Bryan,

I = missed where=20 the 43" came from, however from my calculations for 44mm inlet tube, = my=20 calculations came to 21.36". That's for a straight tube inlet = manifold. That's=20 interesting isn't it.

George (down=20 under)

This is = hard for me=20 to visualize as well.  Perhaps if you get a chance, you could = snap a=20 picture from the top.

Did you = get 43 in.=20 from #1 secondary to #2 secondary?

Bryan

 

From:=20 Rotary motors in = aircraft=20 [mailto:flyrotary@lancaironline.net] On=20 Behalf Of Bill Bradburry
Sent: Monday, February 15, = 2010 11:29=20 PM
To: = Rotary motors in aircraft
Subject: [FlyRotary] Re: rpm = vs Power=20 was : Throttle limits was Re: N.A. Renesis to = turbo

 

Dennis,

I just looked at your picture again=85the = secondary=20 look much longer than the primaries.  It may be an optical=20 illusion???  I bet you mean 1 1/8 = id??

Bill = B 

 

From:=20 Rotary motors in = aircraft=20 [mailto:flyrotary@lancaironline.net] On=20 Behalf Of Dennis Haverlah
Sent: Monday, February 15, = 2010 11:03=20 PM
To: = Rotary motors in aircraft
Subject: [FlyRotary] Re: rpm = vs Power=20 was : Throttle limits was Re: N.A. Renesis to=20 turbo

All my tubes = are the same=20 length and the same diameters.  I can check but I think they = were 1 1/4=20 id. and 1 1/4 od.

Bill Bradburry = wrote:

Denn= is,

Aren=92t your primary and secondary tubes = different=20 lengths from rotor face to rotor face?   If so, what are = the two=20 lengths?  Are they different = diameters?

Bill B

 

 

 

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