X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Received: from qmta06.westchester.pa.mail.comcast.net ([76.96.62.56] verified) by logan.com (CommuniGate Pro SMTP 5.4.4) with ESMTP id 5432571 for flyrotary@lancaironline.net; Wed, 07 Mar 2012 15:33:58 -0500 Received-SPF: none receiver=logan.com; client-ip=76.96.62.56; envelope-from=gordon@acumen-ea.com Received: from omta22.westchester.pa.mail.comcast.net ([76.96.62.73]) by qmta06.westchester.pa.mail.comcast.net with comcast id ihNs1i0011ap0As56kZS3J; Wed, 07 Mar 2012 20:33:26 +0000 Received: from GordonHPelite ([76.27.173.182]) by omta22.westchester.pa.mail.comcast.net with comcast id ikZR1i00j3wUsn83ikZRQ1; Wed, 07 Mar 2012 20:33:26 +0000 From: "Gordon Alling" To: "'Rotary motors in aircraft'" References: In-Reply-To: Subject: RE: [FlyRotary] Re: Radiators Date: Wed, 7 Mar 2012 15:33:22 -0500 Message-ID: <001a01ccfca1$8a68cd00$9f3a6700$@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: Acz8nsu7SnE1lK2jRDCfhDsH0Bu+oAAAI4JQ Content-Language: en-us Yes, I'm running two 13Bs. One rule of thumb I use is for a typical gas engine, the total fuel energy is distributed roughly 1/3 to the shaft, 1/3 to the coolant and 1/3 to the exhaust. Assuming an even 200 HP shaft power, that puts approximately 200 HP = 510,000 BTU/hr into the coolant. I don't know how this distribution changes for a rotary vs. a piston engine. My approach is to look for an automotive radiator for an engine with roughly the same shaft power as the 13B and see how it works. That aside, I noted that several of the auto radiators that I am looking at integrate an oil cooler for transmission fluid and/or engine oil. This strikes me as rather slick if the ratio of radiator area to oil cooler area works for the distribution of cooling load in the coolant vs. the engine oil. Assuming that 1/3 of the cooling load is in the oil, as a starting point, I will look for a radiator that has 1/3 of its face area dedicated to oil cooling. In the end, I will have to test is and see. Thanks for the input. 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 Mark Steitle Sent: Wednesday, March 07, 2012 3:13 PM To: Rotary motors in aircraft Subject: [FlyRotary] Re: Radiators Bill, I don't think Gordon is running a rotary, so the 2/3 - 1/3 rule probably doesn't apply. I have no idea what the water-oil ratio of is for a 4.3L Chevy V-6, but I'd bet that info is available somewhere on the internet. Mark On 3/7/12, William Jepson wrote: > Gordon, the oil cooling required in a rotary is higher than a standard > I.c.e. The oil cooling is about 1/3 of the total cooling. There are lots of > "rules of thumb" on cooling. Typically about 3 ci of heat exchanger per hp. > That would be divided 2/3 water and 1/3 oil cooling. Ducting changes things > dramatically but that is a start. > Bill Jepson > On Mar 7, 2012 7:20 AM, "Gordon Alling" wrote: > >> I'm thinking about radiators for my 13B Defiant. I've noted some >> automotive radiators integrate oil and transmission fluid cooling with the >> engine coolant heat exchanger. Has anyone looked at these as a means of >> integrating the oil and water cooler for an aircraft application? Does >> anyone have an estimate of the oil and transmission heat load in a typical >> GMC 4.3 L Jimmy?**** >> >> ** ** >> >> Gordon C. Alling, Jr., PE**** >> >> President**** >> >> *acumen* *Engineering/Analysis, Inc.***** >> >> ** ** >> >> 540-786-2200**** >> >> www.acumen-ea.com**** >> >> ** ** >> > -- Homepage: http://www.flyrotary.com/ Archive and UnSub: http://mail.lancaironline.net:81/lists/flyrotary/List.html