X-Virus-Scanned: clean according to Sophos on Logan.com X-SpamCatcher-Score: 1 [X] Return-Path: Received: from ispmxmta06-srv.windstream.net ([166.102.165.167] verified) by logan.com (CommuniGate Pro SMTP 5.1.4) with ESMTP id 1731888 for flyrotary@lancaironline.net; Tue, 02 Jan 2007 23:16:48 -0500 Received-SPF: pass receiver=logan.com; client-ip=166.102.165.167; envelope-from=montyr2157@alltel.net Received: from ispmxaamta08-gx.windstream.net ([67.141.68.94]) by ispmxmta06-srv.windstream.net with ESMTP id <20070103041552.ZXDB4563.ispmxmta06-srv.windstream.net@ispmxaamta08-gx.windstream.net> for ; Tue, 2 Jan 2007 22:15:52 -0600 Received: from Thorstwin ([67.141.68.94]) by ispmxaamta08-gx.windstream.net with SMTP id <20070103041552.RITB4808.ispmxaamta08-gx.windstream.net@Thorstwin> for ; Tue, 2 Jan 2007 22:15:52 -0600 Message-ID: <000d01c72eed$eb4c4700$01fea8c0@Thorstwin> From: "Monty Roberts" To: "Rotary motors in aircraft" References: Subject: Re: EM2 Data Logger pix Date: Tue, 2 Jan 2007 22:16:19 -0600 MIME-Version: 1.0 Content-Type: text/plain; format=flowed; charset="iso-8859-1"; reply-type=original Content-Transfer-Encoding: 7bit X-Priority: 3 X-MSMail-Priority: Normal X-Mailer: Microsoft Outlook Express 6.00.2900.3028 X-MimeOLE: Produced By Microsoft MimeOLE V6.00.2900.3028 Tracy, Thanks for the data. Wow! The inertia in this system is much greater than I thought it would be. The Lag time between the maximum fuel burn and the max rad inlet temp is almost 1 min. Really brings the duty cycle thing home! Anybody wanting to make really big power continuously should study this very carefully. I would solely attribute the difference in rise time to the exhaust inserts in the Renesis side housings. Not too surprising considering the additional cooling problems you had with this engine. The lower EGT had to go somewhere. Some to expansion and work; the rest to the coolant. Transient data is no good for doing heat balance work. If you already have steady state data it can be useful to give you the thermal mass/resistance of the engine/coolers etc, but otherwise is pretty useless. Too many things going on. Metal heating up in the block and the coolers. That is why all the lags in the various temps. A big gulp of fuel makes heat. Heat conducts through rotor housings, rotors, side housings etc, finally makes it to coolant. Coolant begins to heat rad. Rad begins to heat air. A large portion of that fuel heats the coolant more directly through the side port exhaust than the al rotor housing apparently. Seems a little strange.....but must be less resistance there. To really get a good comparison here you are going to have to get some steady state data. The best approach is probably to see what the max fuel burn you can get at some egt at 15Kft is. Fly in this condition long enough for the transients to stabilize in a reasonable fashion. Then repeat at the same fuel burn at 2000 ft or so and maybe one intermediate altitude like 6K with the egt in the same approximate place (Peak EGT is probably the easiest). From that I can figure out some things.....hopefully. If you send me raw data in Excel or some sort of delimited format I can even crunch on it a little and see what shakes out. Monty