X-Virus-Scanned: clean according to Sophos on Logan.com From: Received: from omr-a015e.mx.aol.com ([204.29.186.63] verified) by logan.com (CommuniGate Pro SMTP 6.1.10) with ESMTPS id 8728169 for flyrotary@lancaironline.net; Mon, 13 Jun 2016 23:48:25 -0400 Received-SPF: pass receiver=logan.com; client-ip=204.29.186.63; envelope-from=Lehanover@aol.com Received: from mtaomg-aae02.mx.aol.com (mtaomg-aae02.mx.aol.com [172.27.1.100]) by omr-a015e.mx.aol.com (Outbound Mail Relay) with ESMTP id 534CB3800088 for ; Mon, 13 Jun 2016 23:48:08 -0400 (EDT) Received: from core-mla04c.mail.aol.com (core-mla04.mail.aol.com [172.27.37.4]) by mtaomg-aae02.mx.aol.com (OMAG/Core Interface) with ESMTP id 2A1F538000081 for ; Mon, 13 Jun 2016 23:48:08 -0400 (EDT) Full-name: Lehanover Message-ID: <671264.4b47dc7f.4490d877@aol.com> Date: Mon, 13 Jun 2016 23:48:08 -0400 Subject: Re: [FlyRotary] Re: Mistral To: flyrotary@lancaironline.net MIME-Version: 1.0 Content-Type: multipart/alternative; boundary="part1_671264.4b47dc7f.4490d877_boundary" X-Mailer: AOL 9.8 sub 2019 X-Originating-IP: [74.140.106.236] x-aol-global-disposition: G DKIM-Signature: v=1; a=rsa-sha256; c=relaxed/relaxed; d=mx.aol.com; s=20150623; t=1465876088; bh=dZZA6lfG4a9VKT3d9Pd7pl3L7Lh2YH8NIGTJN8a31zw=; h=From:To:Subject:Message-ID:Date:MIME-Version:Content-Type; b=RqDYEhIpejof7xC82YIBig5gESyQMWDK0ihvjs7IkQ3nQZuNcccgEcNfqv+wRNgTi zzYe8O/dQVI3Z/s6w/LLpc9EVc22fp6ZcQU/jY/HHd08EwgN/1fYV7D++IQDbUaDLx nN3LbBb8gb/ZhtrDpmiTmPh9DEBpFAcqouPBWLgA= x-aol-sid: 3039ac1b0164575f7e7843c2 --part1_671264.4b47dc7f.4490d877_boundary Content-Type: text/plain; charset="US-ASCII" Content-Transfer-Encoding: 7bit The intake was designed to fit the mid 80s style13B intake ports in both 2 rotor and 3 rotor engines. Runner length tuned to cruise RPM. intake design well done. Reduction gearbox very well designed with power take off pulleys and hydraulic propeller governor mount. Versions of both engines also ran on jet A. Tried for years to get engines certified in Europe and US. Probably not possible so as to maintain the status of current 1920s technology aircraft engines. I was offered an job with them. I helped all I could via Email. Test Piper landed short when test muffler decomposed blocking exit flow. Destroyed Piper. They tune like dirt bikes. Sensitive to exhaust flow and back pressure. Lynn E. Hanover In a message dated 6/13/2016 3:00:33 P.M. Eastern Daylight Time, flyrotary@lancaironline.net writes: www.mistral-engines.com --part1_671264.4b47dc7f.4490d877_boundary Content-Type: text/html; charset="US-ASCII" Content-Transfer-Encoding: quoted-printable
The intake was designed to fit the mid 80s style13B intake ports in= both 2=20 rotor and 3 rotor engines. Runner length tuned to cruise RPM. intake desig= n well=20 done. Reduction gearbox very well designed with power take off pulleys and= =20 hydraulic propeller governor mount.
 
Versions of both engines also ran on jet A. Tried for years to get en= gines=20 certified in Europe and US. Probably not possible so as to maintain the st= atus=20 of current 1920s technology aircraft engines.
I was offered an job with them. I helped all I could via Email. Test= Piper=20 landed short when test muffler decomposed blocking exit flow. Destroyed Pi= per.=20 They tune like dirt bikes. Sensitive to exhaust flow and back pressure.
 
Lynn E. Hanover
 
In a message dated 6/13/2016 3:00:33 P.M. Eastern Daylight Time,=20 flyrotary@lancaironline.net writes:
www.mistral-engines.com
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