Return-Path: Received: from wind.imbris.com ([216.18.130.7]) by ns1.olsusa.com (Post.Office MTA v3.5.3 release 223 ID# 0-70783U4500L450S0V35) with ESMTP id com for ; Fri, 2 Mar 2001 11:05:09 -0500 Received: from regandesigns.com (cda131-247.imbris.com [216.18.131.247]) by wind.imbris.com (8.11.2/8.9.3) with ESMTP id f22GFXa73770 for ; Fri, 2 Mar 2001 08:15:33 -0800 (PST) Message-ID: <3A9FAA8B.E6129CA6@regandesigns.com> Date: Fri, 02 Mar 2001 08:13:31 -0600 From: Brent Regan To: Lancair List Subject: Re LIV Cabin Heat X-Mailing-List: lancair.list@olsusa.com Reply-To: lancair.list@olsusa.com Mime-Version: 1.0 <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> In order to understand the cabin heat system in a LIV you need understand what is going on in the engine. Ambient air passes through the air cleaner and then the compressor section of the turbocharger. The pressure between the discharge of the turbo and the inlet of the throttle is referred to the Deck Pressure. The pressure between the throttle butterfly and the intake valve is the Manifold Pressure. The sonic venturies are connected to the Deck Pressure. The turbocharger controller and waste gate maintain the deck pressure above the manifold pressure by several inches. Manifold pressure is set by the pilot. Under most conditions of flight, the deck pressure is above the ambient pressure regardless of the manifold pressure. The deck pressure cannot fall significantly below the ambient pressure so the sonic venturies cannot "suck". An excellent reference is the "Aircraft Turbocharger and Control Reference with Troubleshooting Guide" published by Garrett / Allied Signal (Publication # TP25-0111-3). Regards Brent Regan >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>> 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. >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>