X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Received: from nk11p99mm-asmtpout008.mac.com ([17.158.233.229] verified) by logan.com (CommuniGate Pro SMTP 5.4.3) with ESMTP id 5367234 for flyrotary@lancaironline.net; Fri, 27 Jan 2012 13:23:36 -0500 Received-SPF: pass receiver=logan.com; client-ip=17.158.233.229; envelope-from=markmcclure@me.com MIME-version: 1.0 Content-transfer-encoding: 7BIT Content-type: text/plain; CHARSET=US-ASCII Received: from [192.168.1.5] ([75.80.168.134]) by nk11p03mm-asmtp998.mac.com (Oracle Communications Messaging Exchange Server 7u4-22.01 64bit (built Apr 21 2011)) with ESMTPSA id <0LYG002MRZ2COL30@nk11p03mm-asmtp998.mac.com> for flyrotary@lancaironline.net; Fri, 27 Jan 2012 18:23:01 +0000 (GMT) X-Proofpoint-Virus-Version: vendor=fsecure engine=2.50.10432:5.6.7361,1.0.211,0.0.0000 definitions=2012-01-27_06:2012-01-27,2012-01-27,1970-01-01 signatures=0 X-Proofpoint-Spam-Details: rule=notspam policy=default score=0 spamscore=0 ipscore=0 suspectscore=0 phishscore=0 bulkscore=0 adultscore=0 classifier=spam adjust=0 reason=mlx scancount=1 engine=6.0.2-1012030000 definitions=main-1201270200 Subject: Re: [FlyRotary] Re: engine exhaust From: Mark McClure In-reply-to: Date: Fri, 27 Jan 2012 10:22:59 -0800 Message-id: References: To: Rotary motors in aircraft X-Mailer: Apple Mail (2.1251.1) Let me first clarify, my reference was for a Turboprop or turboshaft. Tracy is correct that on TurboJets and TurboFans the 75% Air is routed around combustion chamber, cools it and then mixes with the hot gases to provide thrust. In a turboprop/shaft engine almost all of the heat energy is used up by the turbines that it passes through. In fact on the C-20J After a two hour flight you could put the exhaust covers on instantly because the exhaust tubes were not hot. A traditional auto turbo is a turbine wheel and a compressor. Take two of them and you almost have all the parts you need to build a cheap Turboprop putting out a few hp. Bob I think what you are saying is that it would be improbable to use the air to cool the oil or water temperatures and so I would have to route the air directly over the combustion chamber, just like in the turbine. Basically drilling additional holes in the rotor housings. So I guess my thought is to try and harness that exhaust energy we are producing to provide for something. Maybe have the turbine wheel turn a generator/alternator. Mark Glasair SII - 30% complete 13b MSP - 5% complete On Jan 27, 2012, at 9:26 AM, Rogers, Bob J. wrote: > If you add another turbo to capture the remaining exhaust gas, the > compressor portion will generate compressed air, which can be directed > to flow over an oil cooler or a radiator, but the air will be much > hotter than the outside air available for cooling. When the air is > compressed, it is heated by as much as 100 degrees. The temperature > rise is a function of the amount of compression. That is why you need > an intercooler before such air is routed to an engine intake for > combustion. I doubt that the air from a compressor stage of the turbo > would be cool enough to help reduce the water or oil temperature very > much (if at all) and the volume of air would not be significant compared > to the volume of air available in the free stream of outside air. Plus > you have the added weight of the turbo to deal with. In short, it would > not work. > > Bob Rogers > Mustang II, powered by Rotary 13B Turbo > > -----Original Message----- > From: Rotary motors in aircraft [mailto:flyrotary@lancaironline.net] On > Behalf Of Ernest Christley > Sent: Friday, January 27, 2012 11:09 AM > To: Rotary motors in aircraft > Subject: [FlyRotary] Re: engine exhaust > > Mark McClure wrote: >> >> The 13b MSP is putting out exhaust temps of 1600F. So using the same > principles in reverse, the remaining energy powers a compressor (turbo) > and that air is then used to assist in the cooling. >> >> So the question is: What have I oversimplified? >> >> Mark >> >> > There is so much about the rotary that is completely unexplored. An > option that I'm investigating with my installation is to have a blower > attached to the shaft between the engine and PSRU. The goals are: > - to make more of the propeller efficient by removing the high pressure > area from between it and the cowling > - remove that high pressure area at the nose and > - use it to increase manifold pressure > - increase the manifold pressure > - in a extremely simple and lightweight method. > > I've seen the videos of people making jets out of turbos. I've not run > a single number, but it seems like it would be possible to duct the > output of a really thick radiator to the input of a large turbo. The > pressurized air would cool the turbo and get heated in return, then > combined with the exhaust to produce thrust. I do seem to remember > someone on this list doing an analysis and coming to the conclusion that > a "rotary jet" was not viable, but if you're getting a list of drag > reducing benefits, dealing with the exhaust (one of the worst pain > points we've had to deal with), AND getting some measurable thrust ... > you'll get listed as a hairy chested hero. > > -- > Homepage: http://www.flyrotary.com/ > Archive and UnSub: > http://mail.lancaironline.net:81/lists/flyrotary/List.html > > -- > Homepage: http://www.flyrotary.com/ > Archive and UnSub: http://mail.lancaironline.net:81/lists/flyrotary/List.html