Return-Path: Received: from mxsf20.cluster1.charter.net ([209.225.28.220] verified) by logan.com (CommuniGate Pro SMTP 4.2.5) with ESMTP id 563674 for flyrotary@lancaironline.net; Sat, 11 Dec 2004 19:54:44 -0500 Received-SPF: none receiver=logan.com; client-ip=209.225.28.220; envelope-from=cardmarc@charter.net Received: from mxip04.cluster1.charter.net (mxip04a.cluster1.charter.net [209.225.28.134]) by mxsf20.cluster1.charter.net (8.12.11/8.12.11) with ESMTP id iBC0sCAH011146 for ; Sat, 11 Dec 2004 19:54:14 -0500 Received: from unknown (HELO homeoffice) (68.191.212.162) by mxip04.cluster1.charter.net with ESMTP; 11 Dec 2004 19:54:15 -0500 X-Ironport-AV: i="3.87,136,1099285200"; d="scan'208"; a="490670678:sNHT13473284" From: "Marc Wiese" To: "'Rotary motors in aircraft'" Subject: RE: [FlyRotary] Re: CS psru development Date: Sat, 11 Dec 2004 18:53:40 -0600 Message-ID: <002001c4dfe5$17a23df0$6502a8c0@homeoffice> MIME-Version: 1.0 Content-Type: text/plain; charset="US-ASCII" Content-Transfer-Encoding: 7bit X-Priority: 3 (Normal) X-MSMail-Priority: Normal X-Mailer: Microsoft Outlook, Build 10.0.2627 X-MimeOLE: Produced By Microsoft MimeOLE V6.00.2900.2180 In-Reply-To: Importance: Normal Hi Ed, No, this will utilize the typical oil driven type cs prop governors found on 99% of aircraft now. It will be fed and will supply oil to the prop hub just like most typical cs props-just like Mistral's unit and the Marcotte unit (but much more economical, if we can pull it off). I want to use a Whirlwind type prop-they use Hartzell type cs hubs. It will have a typical SAE cs type prop flange. Use any cs prop. It is based on a planetary reduction in production for other uses (helicopters) in Eastern Europe. Marc Wiese -----Original Message----- From: Rotary motors in aircraft [mailto:flyrotary@lancaironline.net] On Behalf Of Ed Anderson Sent: Thursday, December 09, 2004 9:19 AM To: Rotary motors in aircraft Subject: [FlyRotary] Re: CS psru development Marc, I assume this is an electrically controlled CS PSRU rather than a hydraulic type? Just Curious. Ed Anderson ----- Original Message ----- From: To: "Rotary motors in aircraft" Sent: Thursday, December 09, 2004 10:08 AM Subject: [FlyRotary] CS psru development > I have some preliminary information on the cs planetary psru I am helping develop. Reduction ratio presently 2.92! Great reduction ration for rx8s. > It looks like the actual position of the propeller governor from the propeller shaft centerline to the top of the governor is 290 millimeters (11.5 inches) and the angle is 35 degrees from the vertical position. The reducer length from the propeller shaft flange to the engine would be about 400 millimeters (15.75 inches) and the weight of the reducer will be about 32 kilograms (70.5 lbs). > > Please ask questions so I can figure out the most flexible package. > > Does anyone know the Marcotte weight or the Mechanir weight of their cs psru's? I know Tracy's non cs is about 45 lbs. > Marc Wiese > > > >> Homepage: http://www.flyrotary.com/ > >> Archive: http://lancaironline.net/lists/flyrotary/List.html > >> Homepage: http://www.flyrotary.com/ >> Archive: http://lancaironline.net/lists/flyrotary/List.html