Return-Path: Received: from mail10.syd.optusnet.com.au ([211.29.132.191] verified) by logan.com (CommuniGate Pro SMTP 4.3c1) with ESMTP-TLS id 724780 for flyrotary@lancaironline.net; Fri, 11 Feb 2005 04:51:12 -0500 Received-SPF: none receiver=logan.com; client-ip=211.29.132.191; envelope-from=lendich@optusnet.com.au Received: from george (d211-29-165-181.dsl.nsw.optusnet.com.au [211.29.165.181]) by mail10.syd.optusnet.com.au (8.12.11/8.12.11) with SMTP id j1B9oFPC031937 for ; Fri, 11 Feb 2005 20:50:16 +1100 Message-ID: <002b01c5101f$64cbb6f0$b5a51dd3@george> From: "George Lendich" To: "Rotary motors in aircraft" References: Subject: Re: [FlyRotary] Re: PSRU - hub/prop end Date: Fri, 11 Feb 2005 19:52:26 +1000 MIME-Version: 1.0 Content-Type: text/plain; charset="iso-8859-1" Content-Transfer-Encoding: 7bit X-Priority: 3 X-MSMail-Priority: Normal X-Mailer: Microsoft Outlook Express 6.00.2800.1106 X-MimeOLE: Produced By Microsoft MimeOLE V6.00.2800.1106 Ernst, Be careful there are different sizes and the gears don't all interchange with each other. George (down under). > George Lendich wrote: > > > Tracy, > > I guess that was directed at me, and that's a Yes! > > I had requested that info from the Chief Engineer at Timken Australia, > > who provide those figures. If memory serves me I quoted 3,000 RPM. > > > > Butch suggested that 250,000 hrs was way overkill ! > > That's not to say they are the best bearing for the job, but they are > > a very robust bearing - that's for sure. > > > > The big problem for any bearing is cooling, so a TRB with much larger > > surface area than ( for instance) a plain ball bearing, requires more > > cooling. > > > > I had originally wanted to use TRB on my own Aussie design, as an > > engineer mate explained - their so robust, but have been since coerced > > by Butch to consider other options. > > George ( down under) > > > I'd like to share as much of the details of this design with y'all as I > can. The more I look at it, the more I realize how ingenious and how > much overkill it is. I think it would probably drive a B-52 to an > aerobatic championship. It's heavy at around 45lbs, but a lot of that > weight was for cosmetic purposes. Joe was trying to emulate the center > section of a radial, AND need to add weight to the nose for CG purposes, > so the housing is about 2" thick at the rear. The wheel axle 'thingy' > (feel free to correct my terminology) is welded directly to the gearset > housing, and carries ALL of the flight loads. The prop shaft does > nothing but actually turn the propeller (not that that is a small job). > The hollow shaft that the hub rides on is 1.98" in diameter and has a > .2010" thick wall. > > The ball bearing at the rear can probably handle the reaction thrust, > but I'm going to add a plain bearing anyway. I have to supply oil to > the center of the sun gear, and the easiest way for me to do that is to > pump it forward through the sun gear shaft (vs backward through the prop > shaft as Tracy does). I'll only have to drill about 1" through a > hardened shaft, vs the 10" to do it the other way. I'll drill an oil > gallery in the plain bearing, and make it just large enough to backup > the inner race of the ball bearing. > > I'll feed oil at the rear in this method, and then I'll block off the > oil gallery at the other end so that it's supply will only feed > forward. It will be forced to travel down the inside of the hub and > return back between the propeller drive shaft and it's housing to a > single return at a low point in the planet gear housing. The front > bearings will ride in an oil bath about 1/3 of it's diameter; oil that > has just come through the cooler. This, combined with the hub spinning > out in the 200mph wind, should keep it cool. > > The only part that worries me is that it uses a 3-planet gearset. I > believe I can swap in a 4-planet set without further modification, but > that is still under investigation. > > >> Homepage: http://www.flyrotary.com/ > >> Archive: http://lancaironline.net/lists/flyrotary/List.html >