X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Sender: To: lml@lancaironline.net Date: Tue, 24 May 2011 13:23:22 -0400 Message-ID: X-Original-Return-Path: Received: from qmta01.emeryville.ca.mail.comcast.net ([76.96.30.16] verified) by logan.com (CommuniGate Pro SMTP 5.4c3j) with ESMTP id 4991836 for lml@lancaironline.net; Mon, 23 May 2011 11:26:22 -0400 Received-SPF: pass receiver=logan.com; client-ip=76.96.30.16; envelope-from=j.hafen@comcast.net Received: from omta11.emeryville.ca.mail.comcast.net ([76.96.30.36]) by qmta01.emeryville.ca.mail.comcast.net with comcast id n3MN1g0010mlR8UA13Rn0T; Mon, 23 May 2011 15:25:47 +0000 Received: from [10.0.1.5] ([24.17.111.171]) by omta11.emeryville.ca.mail.comcast.net with comcast id n3Rm1g0093hvfg88X3Rmzg; Mon, 23 May 2011 15:25:47 +0000 Content-Type: text/plain; charset=us-ascii Mime-Version: 1.0 (Apple Message framework v1084) Subject: Re: [LML] Re: L-IV Choice of Engine From: John Hafen In-Reply-To: X-Original-Date: Mon, 23 May 2011 08:25:45 -0700 Content-Transfer-Encoding: quoted-printable X-Original-Message-Id: References: X-Original-To: "Lancair Mailing List" X-Mailer: Apple Mail (2.1084) Correct me if I'm wrong, please, but I seem to remember that the WWII = Merlins were designed to last 200 hours. And that was overkill based on = the circumstances. =20 John Hafen IVP 413AJ TSIO 550, 300 hours On May 23, 2011, at 7:49 AM, Ted Noel wrote: Brent, I am always amazed and amused at your erudition and elocution. Your = comments are well-considered. As one who took a different route (the Eagle V8) I have discovered the = myriad trials of incorporating that engine into my airframe. It's = horribly expensive and time-consuming. At the same time, it promises = some advantages. As for the design compromises (Cheetah vs. Draft Horse), those are = generally issues of cam profiles, bore vs. stroke, and similar internal = issues. Those are well known and understood. Note the differences = between load haulers (see your note below), stationary engines, and = cars. Designing a piston engine for various tasks isn't all that = difficult for a competent engineer. After all, our 1930's boat anchors = are... drum roll please... piston engines. Probably the greatest challenge after internal design is cooling. Liquid = cooling is heavy, and has hoses that can fail. Air cooling is lighter, = and has exhaust valves that famously fail. Computer ignition is highly = reliable, while magneto ignition is heavy and failure-prone. Perhaps the best illustration of newer technology is the rapid demise of = vacuum-driven instruments in favor of all-electric panels. So the issue = is not the technology, it's the implementation. Liquid cooling = eliminates certain internal compromises so that engines can live longer = and produce more power per cubic inch, offsetting the apparent weight = penalty of liquid cooling. They can have higher fuel efficiency. And = they're more reliable, the key reason I went liquid. Of course, that = last sentence hangs on the effectiveness of the cooling system... Lest anyone think that the ideas I've listed above are pie-in-the-sky, = remember the P-51, P40, P38, and Spitfire. They all flew with liquid = cooled Allison or Merlin engines. It's not the idea. It's the execution. Ted Noel On 5/23/2011 8:03 AM, Brent Regan wrote: > Market forces require that, to be successful and survive, consumer = products must be designed to satisfy a selection of requirements imposed = by the consumer. Over time and competition, natural selection refines = the design so that it is either better optimized and competes or it = falls into the dustbin of history. >=20 > Engines, while simple in concept, are spectacularly diverse in = implementation. When you think "engine" think "mammal" and then imagine = all the different species of mammals. Most all are successfully = reproducing. Each is optimized for a particular set of conditions that = allows them to dominate in a specific niche. The same is true for = engines. Every mass produced engine is optimized for a specific set of = requirements and no two requirement sets are the same. Taking an engine = from one application and inserting it in another results, de facto, in a = sub optimal situation. You could couple the 350 Hp diesel engine from my = truck to a weed whacker and it would indeed whack weeds but the = portability requirement would not be met. >=20 > Aircraft engines are designed with the primary requirements of light = weight, low speed, high continuos percentage power, high reliability and = a narrow power band. Think "Draft Horse". >=20 > Automotive engines are designed for low cost, high speed, low = emissions, high peak power and wide torque range. Think "Cheetah". >=20 > What would happen if you hitched four Cheetas to your plow? >=20 > Modern automobile engines have benefited in billions of dollars in = development with the ONLY goal of making them more attractive to = automobile buyers. The corollary is that all that effort has been = expended to make automobile engines that deliberately do not directly = satisfy the requirements of aircraft. >=20 > The landscape is littered, both figuratively and literally, with well = meaning, would be aircraft engine designers who share a common inability = to learn from history. Perhaps driven by the false assumption that = desirable automobile engine characteristics can be selectively = transplanted into an aircraft with the simple transposition of hardware. = The problem, of course is that all the "not desirable" for aircraft = characteristics are part of the bargain. Eating the brains of your enemy = won't give you their wisdom but it may give you Mad Cow disease. >=20 > People who know enough to design an aircraft engine are wise enough = not to. >=20 > Brent Regan >=20 > --=20 > For archives and unsub = http://mail.lancaironline.net:81/lists/lml/List.html >=20 >=20 > ----- > No virus found in this message. > Checked by AVG - www.avg.com > Version: 10.0.1375 / Virus Database: 1509/3654 - Release Date: = 05/22/11 >=20 >=20 -- For archives and unsub = http://mail.lancaironline.net:81/lists/lml/List.html