X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Received: from sj-iport-3.cisco.com ([171.71.176.72] verified) by logan.com (CommuniGate Pro SMTP 5.2.3) with ESMTPS id 2929355 for flyrotary@lancaironline.net; Mon, 19 May 2008 15:39:20 -0400 Received-SPF: softfail receiver=logan.com; client-ip=171.71.176.72; envelope-from=echristley@nc.rr.com X-IronPort-AV: E=Sophos;i="4.27,511,1204531200"; d="scan'208";a="69800097" Received: from sj-dkim-2.cisco.com ([171.71.179.186]) by sj-iport-3.cisco.com with ESMTP; 19 May 2008 12:38:34 -0700 Received: from sj-core-4.cisco.com (sj-core-4.cisco.com [171.68.223.138]) by sj-dkim-2.cisco.com (8.12.11/8.12.11) with ESMTP id m4JJcYsO013483 for ; Mon, 19 May 2008 12:38:34 -0700 Received: from xbh-rtp-201.amer.cisco.com (xbh-rtp-201.cisco.com [64.102.31.12]) by sj-core-4.cisco.com (8.13.8/8.13.8) with ESMTP id m4JJcNbj006950 for ; Mon, 19 May 2008 19:38:34 GMT Received: from xfe-rtp-202.amer.cisco.com ([64.102.31.21]) by xbh-rtp-201.amer.cisco.com with Microsoft SMTPSVC(6.0.3790.1830); Mon, 19 May 2008 15:38:25 -0400 Received: from [64.102.38.155] ([64.102.38.155]) by xfe-rtp-202.amer.cisco.com with Microsoft SMTPSVC(6.0.3790.1830); Mon, 19 May 2008 15:38:25 -0400 Message-ID: <4831D740.5010507@nc.rr.com> Date: Mon, 19 May 2008 15:38:40 -0400 From: Ernest Christley Reply-To: echristley@nc.rr.com User-Agent: Thunderbird 2.0.0.12 (X11/20080227) MIME-Version: 1.0 To: Rotary motors in aircraft Subject: Re: [FlyRotary] Self-repairing Aircraft References: In-Reply-To: Content-Type: text/plain; charset=ISO-8859-1; format=flowed Content-Transfer-Encoding: 7bit X-OriginalArrivalTime: 19 May 2008 19:38:25.0606 (UTC) FILETIME=[E7B54660:01C8B9E7] Authentication-Results: sj-dkim-2; header.From=echristley@nc.rr.com; dkim=neutral Schemmel, Grant wrote: > Self-repairing composite airframes anyone? > > > www.sciencedaily.com/releases/2008/05/080519105052.htm > > > No. Self damage reporting. SURE!! I don't think it would make sense to carry around extra epoxy to heal possible future damage. All epoxies I've ever heard about have relative short shelf lifes, and the weight could be better spent beefing up the part in the first place. I also don't care for the mindset that we can make the part thinner, because we'll know when it gets damaged. I'd rather keep the mindset that we build the part stout enough that any damage severe enough to compromise the part will be discernable on a normal visual inspection. A layer of "bleeding glass" in the layup schedule would be great (if not expensive) during the annual, but I would hate to think that I was depending on some oozing epoxy to keep the wings on when I hit the turbulent air.