X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Received: from rwcrmhc14.comcast.net ([216.148.227.154] verified) by logan.com (CommuniGate Pro SMTP 5.0.9) with ESMTP id 1085468 for flyrotary@lancaironline.net; Sat, 29 Apr 2006 10:05:09 -0400 Received-SPF: none receiver=logan.com; client-ip=216.148.227.154; envelope-from=rlwhite@comcast.net Received: from Quail (c-68-35-160-229.hsd1.nm.comcast.net[68.35.160.229]) by comcast.net (rwcrmhc14) with SMTP id <20060429140423m1400rr0j1e>; Sat, 29 Apr 2006 14:04:23 +0000 Date: Sat, 29 Apr 2006 08:05:20 -0600 From: Bob White To: "Rotary motors in aircraft" Subject: Re: [FlyRotary] Re: Engine Run and Static RPM Report Message-Id: <20060429080520.cf8f2073.rlwhite@comcast.net> In-Reply-To: References: X-Mailer: Sylpheed version 2.2.4 (GTK+ 2.8.3; i686-pc-linux-gnu) Mime-Version: 1.0 Content-Type: text/plain; charset=US-ASCII Content-Transfer-Encoding: 7bit Hi Ed, Yes, it's the 2.85:1 so no secrets. I have a "street" port and 9.7:1 rotors. What I'm wondering now is what would I turn if I could get some air to it, like by reducing my elevation 6000 ft. If I might ask, who made the 74x88 and about how much was it? I would much rather have a cruise prop as the climb performance is pretty good anyway. I'll see what other molds Steve Hill has also. I can get this prop to 76x78 but that's still somewhat short of your 74x88. I do like the appearance of Steve's props. They are a beautiful carbon fiber. He would make a new mold, but he needs to sell about 5 props to make it cost effective. BTW, congratulations on the new hanger. It looks great. Bob W. On Sat, 29 Apr 2006 05:57:12 -0400 "Ed Anderson" wrote: > Bob, I presume you are using a 2.85:1 PSRU to get 6600 with your 68x78 prop > which would give you approx 2300 prop rpm. I flew with a 68x72 and a static > of 5600 would give me a prop rpm of 2580. At 7000 rpm your prop would be > swinging at 2456 rpm. My point is that assuming your are using the 2.85 > then I agree with your assessment, you are a bit "under propped", if you > are using a 2.17:1 then I want to know your secret {:>). > > I found that with a 2.85 gear box and going to a 74x88 prop, the take off > and climb out performance improved tremendously over using the 2.17 and my > 68x72 prop. > > Also if my old 68x72 would turn 2580 at 5600 engine rpm and yours 2456 at > 7000 rpm then I think you will find that your fuel burn is going to be a bit > higher for the same prop rpm. > > Ed > > ----- Original Message ----- > From: "Bob White" > To: "Rotary motors in aircraft" > Sent: Friday, April 28, 2006 9:24 PM > Subject: [FlyRotary] Engine Run and Static RPM Report > > > > I've been trying to finish up all the little nitpicking details and a > > few big details so I haven't ran my engine for quite a while. I made > > up my mind to get some time on it today. The weather was a bit nasty > > today with the winds kicking up to 20-30 kts (it wasn't that bad when I > > started). I fired it up, and the first problem showed up - No > > charging. The new alternator mount from Pineapple racing is power > > coated and insulating the alternator from the block. I rigged up a > > jumper to fix that problem, and started the engine again. All was > > well. After taxiing around for 1/2 hour or so, I hit 4 hours run > > time. Bruce T.'s break in instructions was to run the engine 5 hours > > below 4500, but I couldn't stand the suspense any longer. I really > > wanted to find out what my static RPM was. So, I stopped it heading > > into the wind and gave it full throttle. I saw 6400 RPM and backed off. > > The mixture was going a little lean, so I turned up the mixture and got > > 6600 RPM. Max manifold pressure was a little over 23. (Don't forget > > that I'm at 6000 ft.) That's a little over the 6000 RPM limit Bruce has > > for the 5 to 15 hour segment, but his regime seems quite a bit more > > conservative that some of the other break-in schemes I've heard on > > here. :) With this prop, I suspect I could exceed my RPM redline of > > 7500. If everything is looking OK, I may increase that to 7700. > > > > It seems like I'm a little under propped. This prop is 68 in. dia, with > > a 78 in. pitch. > > > > I also found out that a little air flowing over the rads is a good > > thing. As I mentioned earlier, the wind was kicking up to about 30 > > knots toward the end. While taxiing downwind, the water temp started > > climbing above 200 F. I shut the engine down, got out and pushed the > > plane around into the wind. After starting the engine back up, the > > temps dropped down to 160F. > > > > Now the next big question is how badly will my new cowling and cooling > > plenum screw up the cooling. I'm only about 1/2 done with the cowling > > mods and getting ready to jump back into some more fiberglass work. > > Apparently according to the checklist my DAR sent, I need to do a high > > speed taxi test. I'm not going to do that until I think the plane is > > airworthy, even if I don't have the paperwork!! > > > > Bob W. > > > > -- > > http://www.bob-white.com > > N93BD - Rotary Powered BD-4 (first engine start 1/7/06) > > Custom Cables for your rotary installation - > > http://www.roblinphoto.com/shop/ > > > > -- > > 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/ -- http://www.bob-white.com N93BD - Rotary Powered BD-4 (first engine start 1/7/06) Custom Cables for your rotary installation - http://www.roblinphoto.com/shop/