Return-Path: Received: from imf20aec.mail.bellsouth.net ([205.152.59.68] verified) by logan.com (CommuniGate Pro SMTP 4.3c1) with ESMTP id 744214 for flyrotary@lancaironline.net; Fri, 18 Feb 2005 10:01:09 -0500 Received-SPF: pass receiver=logan.com; client-ip=205.152.59.68; envelope-from=sqpilot@bellsouth.net Received: from [209.214.44.51] by imf20aec.mail.bellsouth.net (InterMail vM.5.01.06.11 201-253-122-130-111-20040605) with ESMTP id <20050218150022.PFQS1977.imf20aec.mail.bellsouth.net@[209.214.44.51]> for ; Fri, 18 Feb 2005 10:00:22 -0500 Received: from 127.0.0.1 (AVG SMTP 7.0.300 [265.8.8]); Fri, 18 Feb 2005 09:00:14 -0600 Message-ID: <006f01c515ca$8b856740$332cd6d1@paul52u7f5qyav> From: "Paul" To: "Rotary motors in aircraft" References: Subject: Re: [FlyRotary] Re: I found the power Date: Fri, 18 Feb 2005 09:00:11 -0600 X-Priority: 3 X-MSMail-Priority: Normal X-Mailer: Microsoft Outlook Express 6.00.2900.2180 X-MimeOLE: Produced By Microsoft MimeOLE V6.00.2900.2180 Mime-Version: 1.0 Content-Transfer-Encoding: 7bit Content-Type: text/plain; format=flowed; charset=iso-8859-1; reply-type=response Hi, Jim....yes, I am looking at scoops similar to Velocity, and what Al Gietzen posted. Regarding the prop, this is the prop that Ron Gowan had on his rotary powered LongEZ. It is designed for 160 hp (rather than 120hp). It is similar to what the 0320 LongEZ guys are using. Ron Gowan got 195 mph in his rotary powered LongEZ with this prop at 6000 rpm's. I was initially unable to get above 5100 rpm's (until I removed the cowling and found the REAL power problem). Now that I am getting 5600 rpm's static, it is very likely that I would be able to get that elusive 6000 rpms once the prop unloads, and my engine is getting cold ram air instead of heated cowling air. Paul Conner ----- Original Message ----- From: "Jim Sower" To: "Rotary motors in aircraft" Sent: Thursday, February 17, 2005 1:39 PM Subject: [FlyRotary] Re: I found the power > Paul, > I'm inquiring into the adequacy of the NACA duct(s) you want to use to > feed your throttle body. If I wasn't really confident that they would > perform as advertised (it's hard to make them work really well in the low > pressure areas of the fuselage) I'd be inclined to use a P-51 type > external scoop like you see under right wing of Velocitys or something > like that. > > As to the prop, I would not use a prop designed for a 120 HP engine to > make power estimates on a rotary. I would not fly the airplane until I > was getting at least 5000 rpm on a prop comparable to the one ED used when > he was running his 2.17 PSRU. Someone with a Lyc O-360 should be able to > lend you a prop to test with for a while if your prop is a little radical. > > 5200 rpm on a 62 x 66 prop is not useful for power determination. If you > look at prop rpm (2390) it tells you that you have about the same power as > an O-235 - about 110 - 115 hp. Somehow you've got to extract a lot more > power out of that machine. Maybe check out your fuel flow on your high > power turn ups and ponder that for a while. > > I would not fly that airplane until I was getting good rpm with a REAL > prop ... Jim S. > > Paul wrote: > >> Hi, Jim....I still had the smaller 62 x 66 prop on at the time. Regarding >> the size of the NACA duct, are you referring to the large one on the >> bottom of the fuselage, or the proposed two smaller ones for bringing in >> air to my throttlebody? Take care. Paul Conner >> >> ----- Original Message ----- From: "Jim Sower" >> To: "Rotary motors in aircraft" >> Sent: Wednesday, February 16, 2005 11:30 PM >> Subject: [FlyRotary] Re: I found the power >> >> >>> Paul, >>> What size prop is this that gives you 5600 rpm now? Is it still the one >>> off of the O-235 or have you gone back to your original? What's the >>> total area of the NACA duct (like top view)? >>> Just wonderin' ... Jim S. >>> >>> Paul wrote: >>> >>>> Today I finished installing the firesleeve on the remaing fuel lines, >>>> made some stand-offs so that the fuel lines would not be right up >>>> against the engine, and finished hooking up and securing a few other >>>> items. With the top cowling off, I ran the pumps for a minute, then >>>> checked for leaks...none found. Then I started the engine and ran it >>>> for 20 or so seconds and shut it down and reinspected for fuel leaks. >>>> None found. I restarted and taxiied away from the hangar a bit so as >>>> to not be as loud for others in and near the hangar and did a full >>>> power runup. I hit 5600 static rpm's. In the past, the best I could >>>> hope for was 5200, most of the time settling for 5100 rpm's. I taxiied >>>> back in and installed the top cowling....max rpm's 5100. Took the top >>>> cowling back off....max rpm's 5600. One more try....5100 with the >>>> cowling back on. It is beginning to become more clear to me, that one >>>> of two things are affecting rpm's. Option one is that with the top >>>> cowling on the engine is ingesting heated air and just cannot develop >>>> the same power as when it ingests outside unheated air. Option two is >>>> the muffler bearing may be worn. I'm kinda leaning toward option one. >>>> I was thinking of installing two small NACA ducts on the bottom of >>>> my cowling with two hoses coming up to feed air to my TWM throttlebody. >>>> The NACA ducts I purchased from Van's RV (made for cowling ventilation) >>>> already have a male outlet already molded in the assembly, so you just >>>> slide a hose over it and secure with a clamp. Very simple >>>> installation.(Works well for my cabin ventillation) If I recall >>>> correctly, they are about the same size as my throttle body bore. I >>>> wonder if I will loose much efficiency as the air goes through the >>>> corregated hose, and if the Van's RV ventillation NACA ducts will >>>> provide a sufficient volume of air. Of course while flying, I would >>>> have the advantage of a little bit of ram effect as well as the ability >>>> to suck in fresh outside air that has not been heated inside the >>>> cowling during taxi/takeoff run. Any opinions/suggestions would of >>>> course be much appreciated. I will discuss the vapor lock issue in the >>>> next post, so as to not complicate responses, etc. Thanks to all who >>>> reply. Paul Conner >>>> >>>> ------------------------------------------------------------------------ >>>> >>>> >>>> No virus found in this outgoing message. >>>> Checked by AVG Anti-Virus. >>>> Version: 7.0.300 / Virus Database: 265.8.8 - Release Date: 2/14/2005 >>>> >>>> ------------------------------------------------------------------------ >>>> >>>> >>>> >>>>>> Homepage: http://www.flyrotary.com/ >>>>>> Archive: http://lancaironline.net/lists/flyrotary/List.html >>>>>> >>> >>>>> Homepage: http://www.flyrotary.com/ >>>>> Archive: http://lancaironline.net/lists/flyrotary/List.html >>>> >>> >>> >>> -- >>> No virus found in this incoming message. >>> Checked by AVG Anti-Virus. >>> Version: 7.0.300 / Virus Database: 265.8.8 - Release Date: 2/14/2005 >>> >>> >> >> >> >> > >>> Homepage: http://www.flyrotary.com/ >>> Archive: http://lancaironline.net/lists/flyrotary/List.html > > > -- > No virus found in this incoming message. > Checked by AVG Anti-Virus. > Version: 7.0.300 / Virus Database: 265.8.8 - Release Date: 2/14/2005 > > -- No virus found in this outgoing message. Checked by AVG Anti-Virus. Version: 7.0.300 / Virus Database: 265.8.8 - Release Date: 2/14/2005