X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Received: from imf21aec.mail.bellsouth.net ([205.152.59.69] verified) by logan.com (CommuniGate Pro SMTP 5.0.8) with ESMTP id 1033434 for flyrotary@lancaironline.net; Tue, 14 Mar 2006 02:46:52 -0500 Received-SPF: pass receiver=logan.com; client-ip=205.152.59.69; envelope-from=bobperk@bellsouth.net Received: from ibm63aec.bellsouth.net ([68.19.241.183]) by imf21aec.mail.bellsouth.net with ESMTP id <20060314074607.MRTI26992.imf21aec.mail.bellsouth.net@ibm63aec.bellsouth.net> for ; Tue, 14 Mar 2006 02:46:07 -0500 Received: from HpPavilion310n ([68.19.241.183]) by ibm63aec.bellsouth.net with ESMTP id <20060314074607.JOTX1948.ibm63aec.bellsouth.net@HpPavilion310n> for ; Tue, 14 Mar 2006 02:46:07 -0500 From: "Bob Perkinson" To: "Rotary motors in aircraft" Subject: RE: [FlyRotary] Re: heat output Date: Tue, 14 Mar 2006 01:46:06 -0600 Message-ID: MIME-Version: 1.0 Content-Type: multipart/alternative; boundary="----=_NextPart_000_0064_01C64709.0FB7F670" X-Priority: 3 (Normal) X-MSMail-Priority: Normal X-Mailer: Microsoft Outlook IMO, Build 9.0.2416 (9.0.2910.0) X-MimeOLE: Produced By Microsoft MimeOLE V6.00.2600.0000 Importance: Normal In-Reply-To: This is a multi-part message in MIME format. ------=_NextPart_000_0064_01C64709.0FB7F670 Content-Type: text/plain; charset="iso-8859-1" Content-Transfer-Encoding: 7bit Ed didn't you build a turbo in your exhaust system, and Tracy went and welded it up so that it wouldn't turn? {:>) Bob Perkinson Hendersonville, TN. RV9 N658RP Reserved If nothing changes Nothing changes Thomas, while there is probably more hydrocarbon (fuel) being ejected from the combustion chamber ports of a rotary than a non-race reciprocating engine , I think you will find that its already being burned in the header pipes - that is one of the reasons for the Rotary's hotter exhaust. So great idea, but I believe you will find its already ignited in the 1700F+ temps of the exhaust. Humm, so if its already ignited, then all we need to do is shape a rocket reaction chamber shape and get additional thrust...... On the other hand, I think a turbo charger would probably be a more effective use of that exhaust energy. But, that's just my opinion and it might be interesting to see if any thrust would result. Monty???. Ed ------=_NextPart_000_0064_01C64709.0FB7F670 Content-Type: text/html; charset="iso-8859-1" Content-Transfer-Encoding: quoted-printable
Ed didn't you=20 build a turbo in your exhaust system, and Tracy went and welded it up so = that it=20 wouldn't turn? {:>)
 

Bob Perkinson
Hendersonville, TN.
RV9 N658RP=20 Reserved
If nothing changes
Nothing = changes
 


 
Thomas, while there is probably more = hydrocarbon (fuel)=20 being ejected from the combustion chamber ports of a rotary than a = non-race=20  reciprocating engine , I think you will find that its already = being=20 burned in the header pipes - that is one of the reasons for the = Rotary's=20 hotter exhaust.  So great idea, but I believe you will find its = already=20 ignited in the 1700F+ temps of the exhaust. 
 
Humm, so if its already ignited, then all we = need to do=20 is shape a rocket reaction chamber shape and get additional = thrust...... =20 On the other hand, I think a turbo charger would probably be a more = effective=20 use of that exhaust energy.  But, that's just my opinion and it = might be=20 interesting to see if any thrust would result.  = Monty???.
 
Ed
 
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