Return-Path: Received: from imf23aec.mail.bellsouth.net ([205.152.59.71] verified) by logan.com (CommuniGate Pro SMTP 4.1.8) with ESMTP id 2782779 for flyrotary@lancaironline.net; Wed, 03 Dec 2003 22:35:45 -0500 Received: from TOSHIBAjhr ([209.214.14.176]) by imf23aec.mail.bellsouth.net (InterMail vM.5.01.06.05 201-253-122-130-105-20030824) with SMTP id <20031204033544.ECHE1942.imf23aec.mail.bellsouth.net@TOSHIBAjhr> for ; Wed, 3 Dec 2003 22:35:44 -0500 From: "John Slade" To: "Rotary motors in aircraft" Subject: Expansion Chambers Date: Wed, 3 Dec 2003 22:35:44 -0500 Message-ID: MIME-Version: 1.0 Content-Type: text/plain; charset="iso-8859-1" Content-Transfer-Encoding: 7bit X-Priority: 3 (Normal) X-MSMail-Priority: Normal X-Mailer: Microsoft Outlook IMO, Build 9.0.2416 (9.0.2910.0) Importance: Normal In-Reply-To: X-MimeOLE: Produced By Microsoft MimeOLE V6.00.2800.1165 Fellow Rotarians: I've come to the point where I need to set up the expansion / overflow system. My engine guy is saying I can just have an overflow reservoir since the pressure cap is at the top of the engine. I've read that some 13B flyers (if not all) have expansion chambers which, in turn, have their own overflow reservoirs. My understanding of a reservoir is a bottle that holds excess coolant which is expelled from the pressure cap. The coolant is then sucked back in as the fluid cools. An expansion chamber is a pressurized bottle, usually made of aluminum. I beleive it should be 1.5 qts or more. Could someone please correct my understanding where wrong, discuss the pros and cons of these systems for our purposes, and point me in the right direction for obtaining / constructing the parts I need? Regards, John Slade