Return-Path: Received: from pop3.olsusa.com ([63.150.212.2] verified) by logan.com (CommuniGate Pro SMTP 3.4.5) with ESMTP id 780025 for rob@logan.com; Mon, 14 May 2001 19:18:58 -0400 Received: from imo-r17.mx.aol.com ([152.163.225.71]) by pop3.olsusa.com (Post.Office MTA v3.5.3 release 223 ID# 0-71175U5500L550S0V35) with ESMTP id com for ; Mon, 14 May 2001 19:11:40 -0400 Received: from RWolf99@aol.com by imo-r17.mx.aol.com (mail_out_v30.10.) id k.41.b7528bd (18561) for ; Mon, 14 May 2001 19:17:56 -0400 (EDT) From: RWolf99@aol.com Message-ID: <41.b7528bd.2831c1a4@aol.com> Date: Mon, 14 May 2001 19:17:56 EDT Subject: Chicken Rivets To: lancair.list@olsusa.com MIME-Version: 1.0 Content-Type: text/plain; charset="US-ASCII" Content-Transfer-Encoding: 7bit X-Mailing-List: lancair.list@olsusa.com Reply-To: lancair.list@olsusa.com <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> In a message dated 5/13/2001 9:46:18 PM Pacific Daylight Time, lancair.list@olsusa.com writes: << In commercial aircraft you will often see metal bonding in primary load carrying structures. The bond is often backed up with a few fasteners "just in case". These fasteners are affectionately known as "chicken rivets". >> Umm, I don't think that's really what's going on here. Quite often adhesives are strong in shear and tension but weak in peel (kinda like velcro). The purpose of those little rivets is NOT to take the shear and/or tension loads, but just the peel forces. This allows the adhesive to do the work in shear and tension, but not be subjected to peel. - Rob Wolf >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>> LML website: http://www.olsusa.com/Users/Mkaye/maillist.html LML Builders' Bookstore: http://www.buildersbooks.com/lancair Please send your photos and drawings to marvkaye@olsusa.com. >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>