X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Received: from imo-d21.mx.aol.com ([205.188.144.207] verified) by logan.com (CommuniGate Pro SMTP 5.2c1) with ESMTP id 2603946 for flyrotary@lancaironline.net; Tue, 18 Dec 2007 14:41:29 -0500 Received-SPF: pass receiver=logan.com; client-ip=205.188.144.207; envelope-from=WRJJRS@aol.com Received: from WRJJRS@aol.com by imo-d21.mx.aol.com (mail_out_v38_r9.3.) id q.d1d.1b76bc4f (37130) for ; Tue, 18 Dec 2007 14:40:26 -0500 (EST) Received: from WEBMAIL-DG02 (webmail-dg02.sim.aol.com [205.188.171.66]) by cia-ma02.mx.aol.com (v121.4) with ESMTP id MAILCIAMA024-910a4768222a3c1; Tue, 18 Dec 2007 14:40:26 -0500 References: To: flyrotary@lancaironline.net Subject: Re: [FlyRotary] Re: Supercharging Date: Tue, 18 Dec 2007 14:39:54 -0500 X-AOL-IP: 65.161.241.3 In-Reply-To: X-MB-Message-Source: WebUI MIME-Version: 1.0 From: wrjjrs@aol.com X-MB-Message-Type: User Content-Type: multipart/alternative; boundary="--------MB_8CA0FC4E626BDA2_E14_7E9B_WEBMAIL-DG02" X-Mailer: AOL Webmail 33161-STANDARD Received: from 65.161.241.3 by WEBMAIL-DG02 (205.188.171.66) with HTTP (WebMailUI); Tue, 18 Dec 2007 14:39:54 -0500 Message-Id: <8CA0FC4E626BDA2-E14-3E57@WEBMAIL-DG02> X-Spam-Flag: NO ----------MB_8CA0FC4E626BDA2_E14_7E9B_WEBMAIL-DG02 Content-Transfer-Encoding: 7bit Content-Type: text/plain; charset="us-ascii" Ernest, No that isn't true. I agree that any supercharging method certainly adds complication. The MAJOR difference is that a SUPERcharger, rather than a turbo requires additional careful engineering to enable the DRIVE for the blower to survive. A turbo must be mounted itself, but the drive is simple, even if the plumbing isn't. Cheers, Bill -----Original Message----- From: Ernest Christley To: Rotary motors in aircraft Sent: Tue, 18 Dec 2007 8:31 am Subject: [FlyRotary] Re: Supercharging wrjjrs@aol.com wrote:? > Greg,? > Superchargers are sometimes simpler to implement, but there are other > reasons they aren't as popular on aircraft. First they are a power > robbing device. There is a net gain in power of course, but the > charger can require 10-15 HP to drive it at WOT and it makes the > engine less efficient. The other problem is you must be sure the unit > is up to continous use in the boost RPM range. Lastly the mount must > be solid enough to hold up to continous use as well.? > Bill Jepson Doesn't the same apply to all intake charging devices?? ? --? Homepage: http://www.flyrotary.com/? Archive and UnSub: http://mail.lancaironline.net:81/lists/flyrotary/List.html? ________________________________________________________________________ More new features than ever. Check out the new AOL Mail ! - http://webmail.aol.com ----------MB_8CA0FC4E626BDA2_E14_7E9B_WEBMAIL-DG02 Content-Transfer-Encoding: 7bit Content-Type: text/html; charset="us-ascii"
Ernest, No that isn't true. I agree that any supercharging method certainly adds complication. The MAJOR difference is that a SUPERcharger, rather than a turbo requires additional careful engineering to enable the DRIVE for the blower to survive. A turbo must be mounted itself, but the drive is simple, even if the plumbing isn't.
Cheers,
Bill


-----Original Message-----
From: Ernest Christley <echristley@nc.rr.com>
To: Rotary motors in aircraft <flyrotary@lancaironline.net>
Sent: Tue, 18 Dec 2007 8:31 am
Subject: [FlyRotary] Re: Supercharging

wrjjrs@aol.com wrote: 
> Greg, 
> Superchargers are sometimes simpler to implement, but there are other > reasons they aren't as popular on aircraft. First they are a power > robbing device. There is a net gain in power of course, but the > charger can require 10-15 HP to drive it at WOT and it makes the > engine less efficient. The other problem is you must be sure the unit > is up to continous use in the boost RPM range. Lastly the mount must > be solid enough to hold up to continous use as well. 
> Bill Jepson Doesn't the same apply to all intake charging devices? 
 
-- 
Homepage: http://www.flyrotary.com/ 
Archive and UnSub: http://mail.lancaironline.net:81/lists/flyrotary/List.html 

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