Return-Path: Sender: "Marvin Kaye" To: lml@lancaironline.net Date: Sat, 12 Mar 2005 10:14:59 -0500 Message-ID: X-Original-Return-Path: Received: from mta10.adelphia.net ([68.168.78.202] verified) by logan.com (CommuniGate Pro SMTP 4.3c2) with ESMTP id 790304 for lml@lancaironline.net; Sat, 12 Mar 2005 09:25:45 -0500 Received-SPF: pass receiver=logan.com; client-ip=68.168.78.202; envelope-from=glcasey@adelphia.net Received: from worldwinds ([70.32.213.236]) by mta10.adelphia.net (InterMail vM.6.01.04.01 201-2131-118-101-20041129) with SMTP id <20050312142452.CJXL7277.mta10.adelphia.net@worldwinds> for ; Sat, 12 Mar 2005 09:24:52 -0500 From: "Gary Casey" X-Original-To: "lancair list" Subject: Vacuum supply for backup gyros X-Original-Date: Sat, 12 Mar 2005 06:20:38 -0800 X-Original-Message-ID: MIME-Version: 1.0 Content-Type: text/plain; charset="Windows-1252" 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 X-MimeOLE: Produced By Microsoft MimeOLE V6.00.2800.1106 I'm thinking that at least some turbocharged engine users would like to use non-electric (vacuum) gyros as a backup for their fancy glass panels. I have a design (patented, in fact) that allows a turbocharged engine to supply the required differential pressure to vacuum instruments under all operating conditions without the necessity of a vacuum pump. This could also be used to supply the primary flight instruments, but perhaps some people would be reluctant to go that far. For a backup source it would be ideal as it is lighter than a vacuum pump and has no wear parts. I personally like the idea of using vacuum gyros as a backup as they have no electrical requirement at all - potentially eliminating the need for a redundant electrical system in a glass-panel plane. The device is basically a pressure regulator that automatically selects pressure from 3 or 4 sources and picks the appropriate pair of sources to produce the required differential pressure. It picks from the intake manifold, compressor discharge, atmospheric and cabin pressure(in the case of a pressurized aircraft). It starts from the lowest and picks whichever supply is necessary to get the appropriate pressure. Any interest? Comments?