X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Received: from inca.al.noaa.gov ([140.172.240.8] verified) by logan.com (CommuniGate Pro SMTP 5.0.8) with ESMTP id 974204 for flyrotary@lancaironline.net; Tue, 07 Feb 2006 20:39:06 -0500 Received-SPF: none receiver=logan.com; client-ip=140.172.240.8; envelope-from=william.p.dube@noaa.gov Received: from [140.172.241.126] (mungo.al.noaa.gov [140.172.241.126]) by inca.al.noaa.gov (8.12.11/8.12.1) with ESMTP id k181cKBK015587 for ; Tue, 7 Feb 2006 18:38:21 -0700 (MST) Message-ID: <43E94AA2.5080800@noaa.gov> Date: Tue, 07 Feb 2006 18:34:26 -0700 From: Bill Dube Reply-To: william.p.dube@noaa.gov Organization: NOAA Aeronomy Lab User-Agent: Mozilla Thunderbird 1.0.2 (Windows/20050317) X-Accept-Language: en-us, en MIME-Version: 1.0 To: Rotary motors in aircraft Subject: Re: [FlyRotary] Why?? Re: [FlyRotary] RX-8 References: In-Reply-To: Content-Type: text/plain; charset=ISO-8859-1; format=flowed Content-Transfer-Encoding: 7bit Here is what I posted to the other list: > I bought one of Rupert's RX-8 engines (6-port) on Ebay about 6 months > ago. At the time, the US dollar was a bit stronger, so the price was > $1800 USD. Now it is closer to $1900 USD. > > My engine arrived exactly as pictured. Complete with engine harness, > injectors, fuel rails, intake manifold, throttle body, alternator, and > sensors. Oil cooler lines are present, but bent close to the engine > for > shipping. > > It arrived nicely padded and strapped on a pallet about 2 months > after I > bought it. Shipping was about $300 to Denver. Paperwork fees were > about > $200. > > I have not run the engine yet, but it seems just fine from what I can > tell by inspection. I put a borescope in the ports. The rotors, seals, > and walls look fine. No scoring or hot spots were apparent. Seems to > have great compression turning by hand. I would take a very rough > guess > at 20,000 miles, judging from the minor carbon on the rotor faces and > exhaust ports. > > These engines have never been in a car. They were used by Mazda for > some > sort of dyno testing. I suspect emissions testing, but that is just a > wild guess. The clutch and pressure plate on mine had zero wear. > > I considered this engine from Rupert a super good deal. When I > bought it > for such a low price, I knew that I would still be way ahead even if I > had to rebuild it. The fact that it is in such good condition that I > won't likely have to do anything internally was a bonus, from my > perspective. > > Rupert is a good guy to deal with. Very helpful and a square dealer. > > Bill Dube' Ed Anderson wrote: > That's certainly interesting, Randy, in that the 6 port and 4 port > Rx-8 engine both use identical internal parts. True the induction > system and port openings on the castings is different due to the > number of ports - similar to the difference between the older 13B six > port and 4 port turbo engines. > > While the 6 port will reportedly produce higher HP, its only when you > get up into the 8500+ rpm range that is true. Then the better high > rpm breathing of the 6 port induction system gives it an edge in > producing power. However, I know of no one who has exceeded 7500 rpm > in aircraft application at this point. Tracy Crook as probably a > couple hundred hours on a 4 port . I believe his conclusion was that > the complexity of the six port intake Vs its potential adaptation for > aircraft use made the 4 port preferable. > > In any case, hard to understand why one engine would be junk when it > shares the same design and parts as the other engine - sure would like > to know some particulars about it. > > Ed > > > ----- Original Message ----- From: "randy echtinaw" > To: "Rotary motors in aircraft" > Sent: Tuesday, February 07, 2006 7:17 PM > Subject: [FlyRotary] RX-8 > > >> Gentlemen, >> I have the opportunity to purchase a 4 port or a 6 port RX-8 >> engine. I thought I wanted a 4 port because I thought it would be >> easier to muffel. I just heard a "rumor" that the 4 port is junk and >> go with the 6 port. I need 220-230 hp using the 2.85 PSRU, no turbo. >> I would consider P-porting if absolutely necessary to get the HP. >> Obviously, I know very little about engines and want to start with >> the best I can get so, considering my needs which one do I want? >> Thank you, >> Randy >> >> -- >> Homepage: http://www.flyrotary.com/ >> Archive and UnSub: http://mail.lancaironline.net/lists/flyrotary/ >> > > > > -- > Homepage: http://www.flyrotary.com/ > Archive and UnSub: http://mail.lancaironline.net/lists/flyrotary/ >