Return-Path: Received: from imf16aec.mail.bellsouth.net ([205.152.59.64] verified) by logan.com (CommuniGate Pro SMTP 4.2b2) with ESMTP id 3180774 for flyrotary@lancaironline.net; Tue, 20 Apr 2004 12:05:11 -0400 Received: from bellsouth.net ([68.153.79.163]) by imf16aec.mail.bellsouth.net (InterMail vM.5.01.06.08 201-253-122-130-108-20031117) with ESMTP id <20040420160511.ZHQV1714.imf16aec.mail.bellsouth.net@bellsouth.net> for ; Tue, 20 Apr 2004 12:05:11 -0400 Message-ID: <40854A2F.9080808@bellsouth.net> Date: Tue, 20 Apr 2004 12:05:03 -0400 From: Mike Robert User-Agent: Mozilla/5.0 (Windows; U; Windows NT 5.1; en-US; rv:1.7b) Gecko/20040316 X-Accept-Language: en-us, en MIME-Version: 1.0 To: Rotary motors in aircraft Subject: Re: [FlyRotary] Re: intake ideas? References: In-Reply-To: Content-Type: text/plain; charset=ISO-8859-1; format=flowed Content-Transfer-Encoding: 7bit Tracy Crook wrote: > One more comment on intake manifolds & race results. Do not ignore > the benefits of a really clean air inlet with ram air recovery BEFORE > the manifold. At 1125 ft msl, 220 IAS, I saw manifold pressures > around 31.8" Hg. Ignore this factor and you throw away about 6% > "free" horsepower. > > Al, I forgot to comment on your last note about your MAP tap in > manifold. I think it is highly possible you were seeing errors > induced by air stream eddies or some other unpredictable factors > caused by that location. It is a challenge to get MAP > measurements when you have no real plenum, only runners with high > velocity air. > > Tracy I have personally encountered this problem in a ground-bound rotary. Solved by connecting taps from each runner and running the resulting single line through a cheap plastic generic fuel filter(C) and MIG jet(R) before the MAP sensor. Basically, a physical RC network. -Mike