Return-Path: Sender: (Marvin Kaye) To: flyrotary Date: Thu, 19 Sep 2002 19:34:32 -0400 Message-ID: X-Original-Return-Path: Received: from pop017.verizon.net ([206.46.170.210] verified) by logan.com (CommuniGate Pro SMTP 4.0b7) with ESMTP id 1737346 for flyrotary@lancaironline.net; Thu, 19 Sep 2002 13:38:03 -0400 Received: from verizon.net ([4.63.177.7]) by pop017.verizon.net (InterMail vM.5.01.05.09 201-253-122-126-109-20020611) with ESMTP id <20020919173803.ODBV22486.pop017.verizon.net@verizon.net> for ; Thu, 19 Sep 2002 12:38:03 -0500 X-Original-Message-ID: <3D8A0B6A.84E85ACB@verizon.net> X-Original-Date: Thu, 19 Sep 2002 10:37:46 -0700 From: Rick Girard X-Mailer: Mozilla 4.77 [en] (Windows NT 5.0; U) X-Accept-Language: en MIME-Version: 1.0 X-Original-To: FLYROTARY Subject: Enlarging Trailing spark plug holes Content-Type: multipart/mixed; boundary="------------C6165FDF05BDF8139E91AD5B" X-Authentication-Info: Submitted using SMTP AUTH PLAIN at pop017.verizon.net from [4.63.177.7] using ID at Thu, 19 Sep 2002 12:37:57 -0500 This is a multi-part message in MIME format. --------------C6165FDF05BDF8139E91AD5B Content-Type: text/plain; charset=iso-8859-1 Content-Transfer-Encoding: 8bit I received this from Dennis Hayes of Hayes Rotary in regards to enlarging the trailing spark plug holes: R.E. Enlarging Trailing Spark Plug Hole I have 27 years experience working with the rotary engine, including full dynamometer facilities in-house. I am the largest remanufacturing facility for rotary engines in the United States. I have worked with NASA, US Energy Dept., US Coast Guard. I developed single rotary applications for pumps and generators and I have worked extensively in alternate fuel for the rotary engine which includes natural gas. Over the past two decades for experimental aircraft only, I have successfully opened up the trailing spark plug hole to allow for a TRUE dual ignition system. Dr. Michael Seals of Western Washington University, who heads up the Vehicle Research Development Program for the last three decades, and myself collaborated and developed the best running and reliability redundancies of a TRUE dual ignition for experimental aircraft. We have built over 100 engines with this modification. We have disassembled and inspected engines after actual aircraft usage and found no cracks in the spark plug holes, no pre ignition, nor destruction of rotor housings. Our findings were conclusive that there is certainly additional blow by when the trailing spark plug hole is enlarged, specifically at idle and low speeds. Understandably aircraft application does not rely on idle and low speeds for extended periods of time. Dr. Michael Seals and myself did not find any pre ignition conditions when running at higher RPM. After two decades of building experimental aircraft engine we have not seen any destruction to a rotor housing. The importance of this procedure is to have TRUE dual ignition systems, allowing for enough engine power if either the ignitions were to fail to be able to land the vehicle safely. Dr. Michael Seals and myself would recommend that if there is any concern about enlarging the trailing spark plug hole, we suggest to have a switch that if primary (leading) ignition were to fail you can turn on the trailing ignition. Without enlarging the trailing hole there will likely not be enough power to land the vehicle safely. We are troubled with the idea of someone using dual ignition on the leading plugs only. If a spark plug fouls then there is no TRUE dual ignition. Thank you Dennis Hayes Owner – Hayes Rotary Engineering --------------C6165FDF05BDF8139E91AD5B Content-Type: text/x-vcard; charset=us-ascii; name="fly.ez.vcf" Content-Transfer-Encoding: 7bit Content-Description: Card for Rick Girard Content-Disposition: attachment; filename="fly.ez.vcf" begin:vcard n:Girard;Rick x-mozilla-html:FALSE adr:;;;;;; version:2.1 email;internet:fly.ez@verizon.net end:vcard --------------C6165FDF05BDF8139E91AD5B--