X-Virus-Scanned: clean according to Sophos on Logan.com From: "Bill Bradburry" Received: from vms173019pub.verizon.net ([206.46.173.19] verified) by logan.com (CommuniGate Pro SMTP 6.1.6) with ESMTPS id 8113991 for flyrotary@lancaironline.net; Fri, 30 Oct 2015 00:33:48 -0400 Received-SPF: pass receiver=logan.com; client-ip=206.46.173.19; envelope-from=bbradburry@verizon.net Received: from Desktop ([108.19.210.50]) by vms173019.mailsrvcs.net (Oracle Communications Messaging Server 7.0.5.32.0 64bit (built Jul 16 2014)) with ESMTPA id <0NX0006BMNBGUG20@vms173019.mailsrvcs.net> for flyrotary@lancaironline.net; Thu, 29 Oct 2015 23:33:17 -0500 (CDT) X-CMAE-Score: 0 X-CMAE-Analysis: v=2.1 cv=WcjxEBVX c=1 sm=1 tr=0 a=zPnTPV6VkIgwbpPgU2rZ+A==:117 a=o1OHuDzbAAAA:8 a=oR5dmqMzAAAA:8 a=kj9zAlcOel0A:10 a=5lJygRwiOn0A:10 a=Ia-xEzejAAAA:8 a=7g1VtSJxAAAA:8 a=-eX8OwzTMr-WdqzcjAYA:9 a=CjuIK1q_8ugA:10 a=Qa1je4BO31QA:10 a=JDB6nq5jwKAA:10 To: "'Rotary motors in aircraft'" References: In-reply-to: Subject: RE: [FlyRotary] Re: 20B with RD-1C Prop Options Date: Thu, 29 Oct 2015 23:33:18 -0500 Message-id: <59BE85B22A1F49E7BBF3C3051541FC1F@Desktop> MIME-version: 1.0 Content-type: text/plain; charset=US-ASCII Content-transfer-encoding: 7bit X-Mailer: Microsoft Office Outlook 11 Thread-index: AdESubLkMFUUHUqZSOGJZG7WMwW74wADdaTQ X-MIMEOLE: Produced By Microsoft MimeOLE V6.0.6002.18463 James, There could be some slip involved, but it is mostly the change in angle of attack as the prop disc is moved forward thru the air. If you can stand the expense, I recommend you get some kind of in flight adjustable prop. The rotary power output is really affected by rpm and being able to adjust it in flight is very helpful. I also recommend you set a max take off rpm target of 2500 prop and 7125 engine. There are several good reasons for this not the least of which is that the EC-2/3 has a cutoff at 7500 rpm. (Tracy can straighten me out here if needed) If you dyno the engine be sure and let us know what you get. I don't think you will be anywhere near those HP numbers you quote. Also when you get up to altitude and cut the rpm back to 48-5200, you will really be reducing the output. If you leave the engine at 7125 rpm and climb to 8000 ft, you will be producing 75%, if you then reduce the rpm to 4800, I don't know what your percent power might be...but a heck of a lot lower than 75%. Do you plan to try and buy a completed airframe? It sometimes takes a surprising length of time to build one. Ask me how I know. :>) Bill -----Original Message----- From: Rotary motors in aircraft [mailto:flyrotary@lancaironline.net] Sent: Thursday, October 29, 2015 9:20 PM To: Rotary motors in aircraft Subject: [FlyRotary] Re: 20B with RD-1C Prop Options Thanks for the input Tracy! So is the difference between top speed rpm and static rpm the "slip"? > On Oct 29, 2015, at 6:32 PM, Tracy wrote: > > Hi James, > HP targets sound doable, but those rpm numbers are probably off. Remember that with a fixed pitch prop, hp varies as the CUBE of rpm. Would recommend propping for a max power at top speed rpm of about 7000. That will give you a static rpm of around 6000. > > Will get those instruction manuals you asked about to you next time I'm in the office. > > Tracy > > Sent from my iPad > >> On Oct 29, 2015, at 16:22, James R. Osborn wrote: >> >> Hi guys, >> >> So I am going to be building an RV-10. I sourced Bobby's spare 20B / RD-1C combo and my plan is to work on the motor first, kind of bass-ackward but that is what I am doing. My plan is to build a motor/mount test stand and work everything out on the ground before I ever put it in an airframe. I plan to set it up NA using the existing side port configuration. I don't know if it is ported - I am going to attempt to determine this by inspection without cracking it open and doing a dynamic compression test to evaluate the health of the motor. If it is necessary to entirely rebuild the motor, I would probably go PP. So I am thinking the target HP as it is would be in the 275 HP range and probably 325 HP if it ends up being a PP. How do these numbers sound to you all? >> >> I will be looking for a way to dyno it, hopefully borrow one to get some data. But I was also thinking about just getting an appropriate fixed pitch prop and working through the bugs based on static run ups. I like the idea of a three blade prop. I like the idea of optimizing for cruise at 75%, say 5800 rpm which would put full throttle at 7733 rpm on the 20B. At 5800 rpm, the prop would be spinning 2035 rpm and at full throttle 2713 rpm (using the 2.85 ratio RD-1C PSRU). Do all these numbers sound about right? >> >> If so, then how do I choose a prop that will result in 2713 rpm static run up at full throttle, but be tuned for efficiency at 2035 rpm cruise? I am assuming at these reasonable RPMs that it will be a larger swing and the three blade makes sense - what do you think? Is there a convenient way to find props out there that will work at the target full throttle HP of 275 or 325? Also if you guys have any good resources to learn about how to figure these things out (books, web pages, online calculators, etc.) that would be great! >> >> Another option might be to go with something like the IVOPROP Magnum, either ground adjustable or electric inflight adjustable. What do you guys think of these? Would the adjustability really help me adapt to however my power plant turns out? Would the extra complexity be worth it? For the ground adjustable one, I am thinking the process would be: 1. select the "correct" swing (how?) and go for three blades, 2) use ground adjustability and work up to THE pitch while I tune the motor until I achieve full throttle static run up around 7700 RPM. Will this result in a reasonably efficient setting for 75% cruise? Am I thinking about this clearly? All opinions are welcome. >> >> There's a lot for you to chew on! >> >> - James >> >> >> -- >> Homepage: http://www.flyrotary.com/ >> Archive and UnSub: http://mail.lancaironline.net:81/lists/flyrotary/List.html > > -- > Homepage: http://www.flyrotary.com/ > Archive and UnSub: http://mail.lancaironline.net:81/lists/flyrotary/List.html -- Homepage: http://www.flyrotary.com/ Archive and UnSub: http://mail.lancaironline.net:81/lists/flyrotary/List.html