X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Received: from simmts7-srv.bellnexxia.net ([206.47.199.165] verified) by logan.com (CommuniGate Pro SMTP 5.2.10) with ESMTP id 3320465 for flyrotary@lancaironline.net; Thu, 27 Nov 2008 18:32:56 -0500 Received-SPF: pass receiver=logan.com; client-ip=206.47.199.165; envelope-from=lacombr@nbnet.nb.ca Received: from simip10-ac.srvr.bell.ca ([206.47.199.89]) by simmts7-srv.bellnexxia.net (InterMail vM.5.01.06.13 201-253-122-130-113-20050324) with ESMTP id <20081127233214.VBIL2983.simmts7-srv.bellnexxia.net@simip10-ac.srvr.bell.ca> for ; Thu, 27 Nov 2008 18:32:14 -0500 X-IronPort-Anti-Spam-Filtered: true X-IronPort-Anti-Spam-Result: AhkGAIO8LkmOp11o/2dsb2JhbACCRCzPBoJ9 Received: from fctnnbsc14w-142167093104.pppoe-dynamic.nb.aliant.net (HELO PCdeRita) ([142.167.93.104]) by simip10-ac.srvr.bell.ca with SMTP; 27 Nov 2008 18:29:21 -0500 Message-ID: From: "Rino" To: "Rotary motors in aircraft" References: In-Reply-To: Subject: Renesis fuel burn Date: Thu, 27 Nov 2008 19:32:13 -0400 MIME-Version: 1.0 Content-Type: multipart/alternative; boundary="----=_NextPart_000_0080_01C950C6.D9061150" X-Priority: 3 X-MSMail-Priority: Normal X-Mailer: Microsoft Windows Mail 6.0.6000.16480 X-MimeOLE: Produced By Microsoft MimeOLE V6.0.6000.16669 This is a multi-part message in MIME format. ------=_NextPart_000_0080_01C950C6.D9061150 Content-Type: text/plain; charset="iso-8859-1" Content-Transfer-Encoding: quoted-printable Where can I get information on fuel burn and power for the renesis? The maximum fuel burn I can get on takeoff is 11.7 gph (reading on the = EM2) at 64 00 rpm. The EM2 is not fully calibrated yet! I think I = should be able to get a higher fuel burn than that. The other part of the problem. What should be the intake manifold = runner length on the Renesis. Best power has to be between 6000 and = 6500 rpm limited by the propeller and redrive configuration. I cannot = use more than 65" dia. prop. The present runner length is 17" and I think it is not enough. Rino Lacombe Renesis powered Glass Goose ------=_NextPart_000_0080_01C950C6.D9061150 Content-Type: text/html; charset="iso-8859-1" Content-Transfer-Encoding: quoted-printable

Where = can I get=20 information on fuel burn and power for the renesis?

The = maximum fuel burn=20 I can get on takeoff is 11.7 gph (reading on the EM2) at 64 00 = rpm. =20 The EM2 is not fully calibrated yet! I think I should be = able to get=20 a higher fuel burn than that.

The = other part of the=20 problem. What should be the intake manifold runner length on the=20 Renesis. Best power has to be between 6000 and 6500 rpm = limited=20 by the propeller and redrive configuration. I cannot use = more than=20 65" dia. prop.

The = present runner=20 length is 17" and I think it is not enough.

Rino=20 Lacombe

Renesis = powered Glass=20 Goose

------=_NextPart_000_0080_01C950C6.D9061150--