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<DIV>Excellent example Earl. Underestimation of the loads generated is an issue; one should consider what happens to a cantilevered load of about 1 lb with a moment arm of about 2", when that load experiences even moderate Gs (10).</DIV>
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<DIV>It seems that many have opted out of using a firewall in the electric set-ups. Actually, a firewal per se' may not really be necessary but a bulkhead should be used in the nose, just behind the motor. 1/8" lite ply would probably work fine, or better yet, carbon tow epoxied in place completely around the inside circumference of the fuselage. A carbon tow "X" could then be run from the bulkhead to the nose ring to allow load transfer. </DIV>
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<DIV>Bulkheads add great column strength for minimal weight. Shorter columns result between the support of the bulkhead, enhancing torsional and compresssive strengths of the otherwise existing structure.</DIV>
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<DIV>A similar structural failure was occuring with the Impacts several months back, where oscillations of the tail forces were ripping the tails off the models. The definitive fix for that was never really implemented at the factory so the folks resorted to all sorts of ladders, etc to fix a design flaw.</DIV>
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<DIV>Matt</DIV>
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<DIV>In a message dated 8/13/2006 11:15:35 AM Eastern Standard Time, ehaury@houston.rr.com writes:</DIV>
<BLOCKQUOTE style="PADDING-LEFT: 5px; MARGIN-LEFT: 5px; BORDER-LEFT: blue 2px solid"><FONT face=Arial>An example of the forces involved. I had (automotive) engine dynamometer <BR>stands fitted with inertial flywheels that were cantilevered behind the rear <BR>support. Shaft dia was 2 1/2", flywheel (350 # ft sq) mounted about 6" <BR>behind rear bearing, the shaft continued forward about 3' to another support <BR>with a dyno rotor (60 # ft sq) between the supports. A very small imbalance <BR>(<1/2 oz) would impart a wobble at 3500 rpm of several inches at the <BR>flywheel O.D. Watched with a strobe - the steel shaft looked like a rubber <BR>hose flexing! A much better system placed a support immediately before and <BR>after the flywheel.<BR><BR>So - scale that down and it's apparent the forces we're dealing with are <BR>easily underestimated. While cantilevered mounting of props is the norm (and <BR>only practical) - it's not the best situation and leads to all sorts of <BR>twisting forces when gyroscopic precession is included (changing the plane <BR>of rotation in pattern maneuvers). Mounting of an outrunner offers all sorts <BR>of complications compounded by the rotational forces of the motor housing / <BR>magnets (mass) - firewall mount it and the lever arm is long allowing any <BR>flex in the firewall to translate into a good deal of freedom of movement <BR>(oscillation) at the prop. Center mount it and - while the moments are <BR>shorter - the twisting forces fore / aft of the mounting also exert twisting <BR>to the mount, now in a weaker location (nose-ring). The long geared motors <BR>are a bit better in that they obviously demand a rear support and have the <BR>(motor) rotating mass closer to the centerline (shorter moment). But, add to <BR>all this a fuselage designed for power loading in the normal region of a <BR>firewall (light forward) and there's little structural rigidity to withstand <BR>the twisting forces on the more forward E mount.<BR><BR>Certainly mounting an outrunner with mid and rear support is a start. Adding <BR>structural strength to the fuse nose also seems prudent. Some have seen the <BR>(wing) foam I've installed in the nose of my E airplanes. I primarily did <BR>this for air ducting - however I quickly noticed a noise reduction. <BR>Obviously from reducing resonance of the composite of the fuse nose - <BR>certainly stiffening the composite structure lessens onset of fatigue <BR>failure of the composite. Likely an overall strength addition to the fuse <BR>nose also. An easy / light retrofit with a some foam and poly glue.<BR><BR>Best fix is appears to be a combination of strengthening the fuse nose and <BR>limiting movement / twisting by two point (fore / aft) support of the motor.<BR><BR>Earl<BR><BR><BR><BR><BR>----- Original Message ----- <BR>From: "Jerry Stebbins" <JAStebbins@worldnet.att.net><BR>To: <chad@f3acanada.org>; "NSRCA Mailing List" <BR><nsrca-discussion@lists.nsrca.org><BR>Sent: Sunday, August 13, 2006 9:17 AM<BR>Subject: Re: [NSRCA-discussion] Outrunners and structural failures<BR><BR><BR>> Chad we are getting ready to try the EVO in the spinner mount. My guess is<BR>> the location of the prop relative to the rear mount-plus all the prop<BR>> related influences is the primary generation source. With the prop right <BR>> at<BR>> the mount (in the spinner) there would be a very moment short arm. I guess <BR>> I<BR>> need to look at Jerry B's whirl flutter info trail and see what I find. <BR>> Hope<BR>> he finds his lost parts and then has time to educate us on what he has<BR>> found.<BR>> Jerry S<BR>> ----- Original Message ----- <BR>> From: "Chad Northeast" <chad@f3acanada.org><BR>> To: "NSRCA Mailing List" <nsrca-discussion@lists.nsrca.org><BR>> Sent: Saturday, August 12, 2006 10:46 PM<BR>> Subject: Re: [NSRCA-discussion] Outrunners and structural failures<BR>><BR>><BR>>> Very interesting...and here I was going to get Pletty to make me a front<BR>>> mounted 30-10 Evo....I guess there goes that idea :)<BR>>><BR>>> What is being used for the front mount?<BR>>><BR>>> I have always rear mounted (without a front support), and you can always<BR>>> hear some vibration when you get large AOA changes...like in snaps, or<BR>>> hard corners with slight rudder application. Always figured it was the<BR>>> prop deflecting and vibrating the motor since is cantilivered so far<BR>>> away from the rotational axis. I had figured a front mount would solve<BR>>> this.<BR>>><BR>>> I did grab a couple of front mount setups while at the Nats and they all<BR>>> felt like they had more movement than my rear mount setup has, which<BR>>> surprised me somewhat.<BR>>><BR>>> Chad<BR>>><BR>>> Chris Moon wrote:<BR>>><BR>>>>Several of us have been collecting info on the many (upwards of a dozen)<BR>>>>fuse structural failures with people running the larger outrunners. The<BR>>>>common theme is that they are all front mounted to the nose ring without<BR>>>>any support at the rear of the motor. There have been some who have<BR>>>>mounted their motors this way that have not had failures, but all that<BR>>>>have failed were nose ring mounted without support for the back. Except<BR>>>>for one, and that looks like it was a problem with the fuse<BR>>>>manufacturer. In that case (today) the seam split due to a poorly glued<BR>>>>seam without good adhesion by the fiberglass seam tape. The problem<BR>>>>seems to be explained by a phenomenon called "whirl flutter" and<BR>>>>basically is caused by an outside force causing the prop and motor to<BR>>>>oscillate to the point where the structure will fail. Here is a video<BR>>>>of the phenomenon:<BR>>>><BR>>>>http://www.airspacemag.com/ASM/Web/Site/QT/PWFlutter.html<BR>>>><BR>>>>(Thanks to Jerry Budd for the research and video link)<BR>>>><BR>>>>So, if you are planning to use the big outrunners like the Axi or Hacker<BR>>>>A60, the evidence is showing that a rear support of some kind is<BR>>>>necessary to prevent failure. I had 2 failures with my A60 set up until<BR>>>>I added a rear support. My first failure was on the 2nd flight and the<BR>>>>2nd failure was on the 15th flight (at the NATS).I now have almost 20<BR>>>>flight with the rear support and everything seems fine now. Of course<BR>>>>you can also mount the Axi to a firewall and we have not heard of any<BR>>>>failures with that set up. I spoke with Jerry Budd and he is planning<BR>>>>to be making a rear support available for the outrunners similar to the<BR>>>>one he now makes for the Hacker C50. Please if you are planning on using<BR>>>>a front mount outrunner consider the rear support before you get too far<BR>>>>along. I was going to write a KFactor article on this, but it seems<BR>>>>like a better idea to get this out more quickly via the mail list.<BR>>>><BR>>>><BR>>>><BR>>>>Chris Moon<BR>>>>D5 VP<BR>>>></FONT></BLOCKQUOTE></DIV>
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