Return-Path: Received: from lanfear.nidlink.com ([216.18.128.7]) by truman.olsusa.com (Post.Office MTA v3.5.1 release 219 ID# 0-52269U2500L250S0V35) with ESMTP id com for ; Sun, 11 Jul 1999 13:31:17 -0400 Received: from enaila.nidlink.com (root@enaila.nidlink.com [216.18.128.8]) by lanfear.nidlink.com (8.9.0/8.9.0) with ESMTP id KAA24565 for ; Sun, 11 Jul 1999 10:34:27 -0700 (PDT) Received: from regandesigns.com (tnt132-26.nidlink.com [216.18.132.26]) by enaila.nidlink.com (8.9.0/8.9.0) with ESMTP id KAA11227 for ; Sun, 11 Jul 1999 10:34:26 -0700 (PDT) Message-ID: <3788D578.D7D6E03E@regandesigns.com> Date: Sun, 11 Jul 1999 10:33:44 -0700 From: Brent Regan To: lancair.list@olsusa.com Subject: Re:Engines References: <19990711040154.AAA27489@truman.olsusa.com> X-Mailing-List: lancair.list@olsusa.com Mime-Version: 1.0 <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> Bill's comments about "feeding the dinosaurs" are spot on, but the fantasy of an inexpensive, high performance engine is just that. The markets are too small, the development costs are too high, and the liability is too great to make it a possibility. Suppose it takes $10M (low estimate) to develop and certify a new engine (a jet fuel burning, 400 hp, 500 pound system with a 30K foot critical altitude). Over 5 years you might sell 1000 engines. With cost of money factored in, that is $15K PER ENGINE. If you were really good, you could build each engine for another $15K (parts and labor). Add a 40% gross margin and you are at $50K. Now add warranty reserve, liability reserve, world wide training and support. Spending $150 to $200 per installed horsepower is about right. The GA market doesn't have the volumes required to reduce the costs by an order of magnitude to automobile levels. Until some market perturbation comes along, like a war or an av gas shortage or both, the high performance aircraft engine will continue to obey the laws of the market and will always obey the laws of physics. The bulk of the AGATE $s will end up in the pockets of the usual suspects, and be used to make minor advances in existing technology (with a few notable exceptions). FYI, in the everything old is new again category the Zoche engine is virtually identical to an engine designed at Continental in the mid 70s and the Orenda engine first flew in 1986. My favorite is that a 700 Hp diesel aircraft engine was making regular flights across the Atlantic in the 1930's! Holly Junkers Jumo, Batman! In the mid 80s I was involved in an (unsuccessful) effort to buy the Stratified Charge Rotary Combustion Engine technology from Curtis Wright. I believe that the "what the market needs" requirements have remained the same since then. That is a Jet A burning 500 to 750 Hp engine with a .32 BSFC and a FL400 service ceiling with an operation cost of %50 that of a turbine engine. I buy "farm diesel" for my tractor at about $0.85 per gallon (no road tax) which is about $0.13 a pound. Running 450 Hp in my Lancair would put my cruise at around 330 KTAS at FL240 and cost $18/hour in fuel or $0.055/ KM. Currently I consume $40/hour at 275 KTAS or $0.15 per mile. 20% faster at 1/3 the cost. Now there are some numbers I like ;) Anybody out there got a spare $10M?? I'm ready to start designing. Regards Brent Regan >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>> LML homepage: http://www.olsusa.com/Users/Mkaye/maillist.html