X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Received: from qmta15.westchester.pa.mail.comcast.net ([76.96.59.228] verified) by logan.com (CommuniGate Pro SMTP 6.0.5) with ESMTP id 6291582 for flyrotary@lancaironline.net; Sun, 26 May 2013 20:58:11 -0400 Received-SPF: none receiver=logan.com; client-ip=76.96.59.228; envelope-from=gordon@acumen-ea.com Received: from omta10.westchester.pa.mail.comcast.net ([76.96.62.28]) by qmta15.westchester.pa.mail.comcast.net with comcast id gobf1l0020cZkys5Foxd0s; Mon, 27 May 2013 00:57:37 +0000 Received: from HPElitebook ([76.123.51.236]) by omta10.westchester.pa.mail.comcast.net with comcast id goxd1l00Q55mGuc3WoxdMx; Mon, 27 May 2013 00:57:37 +0000 From: "Gordon Alling" To: "'Rotary motors in aircraft'" References: In-Reply-To: Subject: RE: [FlyRotary] oil cooler mount question Date: Sun, 26 May 2013 20:57:37 -0400 Message-ID: <004501ce5a75$2e940890$8bbc19b0$@com> MIME-Version: 1.0 Content-Type: text/plain; charset="us-ascii" Content-Transfer-Encoding: 7bit X-Mailer: Microsoft Office Outlook 12.0 Thread-index: Ac5aPK3BmtJH7cliTy+zUyq7h6anUQAGKX3A Content-Language: en-us DKIM-Signature: v=1; a=rsa-sha256; c=relaxed/relaxed; d=comcast.net; s=q20121106; t=1369616257; bh=ZiKuF1Kke5GHzqCGFW6LkHCIJpGMXVd0QPvHTXdtYBo=; h=Received:Received:From:To:Subject:Date:Message-ID:MIME-Version: Content-Type; b=aZVCRmy/YZjUmthnU2JE8rDzUCg2cJ5pQ/v5iNmCKwNlOgqE1Xxtjc72aqmnHkmOD 64rz63BIWwXg4i8n8R849IsEjhLyScJpn2xOmSli9CyqdQeKc66TsfwkDhiC2GBUW7 /BLu9iIYbjBe/Nyq1IkoH/FOZEuXzPUrKPZOvni8HbWNF1PrvNqLo8tk5/fW43sTod 0NgKm7i4WUZFoB+cdT50yDmEDOQvCMx9eJqZ5v3vFhfnIEnpVDMs2AvznZmxZpt1H1 1Kzyp3wEphTUUirHacVvX2cIqE15PFPYLvaH/Dr1MVbs3uq5/AGNwCl/PU+j6F4OJp lJ0W/wdEkpFkw== Charlie, Do I understand the photo shows a baffle between the cowl air inlet and the oil cooler face? If that is correct, is it intended to distribute the inlet air across the face of the heat exchanger? Does it work? Have you measured temps across the face of the HX? My intuition says that that baffle will shield a large portion of the HX face and reduce the effectiveness. But my intuition is notoriously bad (that's why I haven't made gobs of money on the stock market). Let us know how effective the heat transfer is. Gordon C. Alling, Jr., PE President acumen Engineering/Analysis, Inc. 540-786-2200 www.acumen-ea.com -----Original Message----- From: Rotary motors in aircraft [mailto:flyrotary@lancaironline.net] On Behalf Of Charlie England Sent: Sunday, May 26, 2013 1:13 PM To: Rotary motors in aircraft Subject: [FlyRotary] oil cooler mount question I've started design/fabrication/redesign of my oil cooler mount/diffuser. Just as I had a 'final' answer on the mount & was contemplating the diffuser, it occurred to me that I didn't have any shock mount provisions for the heat exchanger. For those who have been flying for a while, have any of you hard mounted the cooler to its support structure? As the photo shows, the primary mount is direct to the reduction drive plate. I would simply add the shock mounts, but if I use this particular cooler (a CX Racing 30 row unit like the one on Tracy's 20B), I won't have any room. I do have the option of buying a 25 row or using the 19 row I already have on hand, but I'd rather have a bit too much capacity & throttle the exit air than start with too little & have to rebuild everything. Thanks, Charlie