X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Received: from mail01.syd.optusnet.com.au ([211.29.132.182] verified) by logan.com (CommuniGate Pro SMTP 5.2.6) with ESMTPS id 3102621 for flyrotary@lancaironline.net; Sun, 31 Aug 2008 17:15:12 -0400 Received-SPF: pass receiver=logan.com; client-ip=211.29.132.182; envelope-from=lendich@optusnet.com.au Received: from george (d211-31-70-177.dsl.nsw.optusnet.com.au [211.31.70.177]) by mail01.syd.optusnet.com.au (8.13.1/8.13.1) with SMTP id m7VLEQhp023400 for ; Mon, 1 Sep 2008 07:14:28 +1000 Message-ID: <003101c90bae$90a83e90$6400a8c0@george> From: "George Lendich" To: "Rotary motors in aircraft" References: Subject: Re: [FlyRotary] Re: Composite instruction Date: Mon, 1 Sep 2008 07:14:31 +1000 MIME-Version: 1.0 Content-Type: text/plain; format=flowed; charset="iso-8859-1"; reply-type=original Content-Transfer-Encoding: 7bit X-Priority: 3 X-MSMail-Priority: Normal X-Mailer: Microsoft Outlook Express 6.00.2900.3138 X-MimeOLE: Produced By Microsoft MimeOLE V6.00.2900.3350 X-Antivirus: avast! (VPS 080831-0, 31/08/2008), Outbound message X-Antivirus-Status: Clean Mike/ Randy, I am building a Vision with composite core and although most cowls are thin fiberglass, they could be stiffer and lighter with a composite construction. As the core foam is quite stiff, it will hold a shape, when heated, shaped then cooled, a thin section of core about 3/16 would be sufficient, with 2 layers of light glass (5 oz). Because the foam might distort when working on it in-situ, you could support it with some backing material - this would save making moulds. Once you have the outside glassed then take it off and glass the inside. The Vision is make completely from this method. This is how I will do my cowl. Hope that helps. George (down under) > Randy, > > You are setting yourself up for a ton of work. I built a custom cowl for > my > RV-4 out of carbon fiber (got a really good deal on the fabric). When I > built it it was lighter than the then current RV-4 cowl and stiffer too. > It > has now been hacked/patched so many times to accomodate changes to cooling > systems, exhaust, etc.... that it has gained weight. It weighs about the > same as the fiberglass RV-6A cowling from the airplane I'm flying. > > I built a plug from foam directly on the airplane. Carved to shape, > covered > with fiberglass cloth and then body worked and painted to get it smooth. > Once I was happy with it I waxed the crap out of it and shot a couple of > coats of PVA (mold release) on it. I laid the carbon up directly on this. > I > used 4 layers of 8 ounce standard weave cloth. Once cured I split it > lengthwise and removed it from the plug. I then removed the plug from the > fuselage. > > Obviously this leaves a smooth interior surface (good for cleaning) and a > rough exterior (lots of filler and sanding). Once its all smoothed up then > fitment to the airplane was standard Vans (combination of piano hinge and > screws/nutplates for attachment). > > No idea how much time this tookbut it was definitely multiple 100s of > hours. > And this is not the lightest/best way. If you really wanted the best > method, > build the plug as described and then lay up a female mold on the plug. > Make > your cowl pieces in the female mold. This saves the time/effort/weight of > the filling and sanding. It also provides a means to use composite > sandwich > core construction where there is some sort of core material installed > between inner and outer layers of glass. This makes the cowl MUCH stiffer > and allows you to use fewer layers of cloth. But the additional work of > making a female mold was too much for me. Glad in the end that I didnt go > this route as I would have been pissed if I'd gone to all the effort and > then had to hack the finished cowl as I did. > > The guys building composite planes will probably have other ideas on how > to > do this but this is what worked for me. Good Luck. > > Mike Wills > RV-4 N144MW > > > ----- Original Message ----- > From: "randy echtinaw" > To: "Rotary motors in aircraft" > Sent: Sunday, August 31, 2008 7:37 AM > Subject: [FlyRotary] Composite instruction > > >>I am eventually going to have to build a custom composite radiator/oil >>cooler pod ala P-51 and possibly a cowling if I cannot get aluminum to >>work around my RX-8 engine. I am looking for some good reference books on >>how to do this especially concerning making male molds - release agents - >>cloth to use - number of layers required - etc.?? >> My plane is wood/tube/fabric - thought I might as well use a little >> fiberglass too :)) >> My biggest concern is making them as light as possible but still having >> the needed strength and stiffness. >> Thanks >> >> -- >> 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 >