X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Sender: To: lml@lancaironline.net Date: Thu, 17 Nov 2011 11:44:03 -0500 Message-ID: X-Original-Return-Path: Received: from nm2-vm3.bullet.mail.ne1.yahoo.com ([98.138.91.132] verified) by logan.com (CommuniGate Pro SMTP 5.4.2) with SMTP id 5203965 for lml@lancaironline.net; Thu, 17 Nov 2011 11:38:34 -0500 Received-SPF: none receiver=logan.com; client-ip=98.138.91.132; envelope-from=casey.gary@yahoo.com Received: from [98.138.90.54] by nm2.bullet.mail.ne1.yahoo.com with NNFMP; 17 Nov 2011 16:37:58 -0000 Received: from [98.138.89.161] by tm7.bullet.mail.ne1.yahoo.com with NNFMP; 17 Nov 2011 16:37:58 -0000 Received: from [127.0.0.1] by omp1017.mail.ne1.yahoo.com with NNFMP; 17 Nov 2011 16:37:58 -0000 X-Yahoo-Newman-Property: ymail-3 X-Yahoo-Newman-Id: 391237.93154.bm@omp1017.mail.ne1.yahoo.com Received: (qmail 56570 invoked by uid 60001); 17 Nov 2011 16:37:58 -0000 DomainKey-Signature:a=rsa-sha1; q=dns; c=nofws; s=s1024; d=yahoo.com; h=X-YMail-OSG:Received:X-Mailer:References:Message-ID:Date:From:Reply-To:Subject:To:In-Reply-To:MIME-Version:Content-Type; b=BVxRqDiedw0JFLKUxyW3L8w0LmJ49VbFfj97N5MctgKn3mZ5wb40X2Lajx1LqgjMqzrRPftceSDicWMKf0YV3bZfawucrdclUvqVsbiaUVoItXa9bphsIj8FDSG2B5jHmeFdUFKffnYARTQgJ1l8uow4FyRLWdSNRiZVJl0n1BA=; X-YMail-OSG: b5F_NxoVM1m7nNovu2CFfgYs3_RpOr8Lp8L0iXujxgNQQOr Y7QwhxH1qBS3PpeNp1YUYqn0NAdH3_qCfuSpaGzuwfqyUyBVXOr7EKd9few3 n7iaOeNzrY7pgsPr7JdBGzmzd5NxI5vGtMhzW4hiwjY.YGh7w5pdZDwCq_3i fQay.FFSu1_rwyg5TbCs2sSTWDGV3CVQ3DxAgHY13Y62nc0bgtnnB5w1WFg8 vWojIQ3outE1fanToWGabrNRSrMBh8ARyiSdgUIHZ9r08lQOEkM74gWh1GVn 5GurEPABcZ9sf0sOYSy0tS_rXgwg4fzaflqPJNGVaSan42K2Wg4dZR4ToDvp 0x8F9T5pr7BMbLHaJ9mW9SLnGI7j.VY6fQayArqUg76R4nouyVpUMgP0Gzpk AmIpYRyvPa26byWSx_mXE2Zz45i0.OThnAONzBWQ- Received: from [97.122.154.57] by web125607.mail.ne1.yahoo.com via HTTP; Thu, 17 Nov 2011 08:37:58 PST X-Mailer: YahooMailWebService/0.8.115.325013 References: X-Original-Message-ID: <1321547878.56416.YahooMailNeo@web125607.mail.ne1.yahoo.com> X-Original-Date: Thu, 17 Nov 2011 08:37:58 -0800 (PST) From: Gary Casey Reply-To: Gary Casey Subject: Re: E-Mag/P-Mag X-Original-To: Lancair Mailing List In-Reply-To: MIME-Version: 1.0 Content-Type: multipart/alternative; boundary="1219445386-1343500212-1321547878=:56416" --1219445386-1343500212-1321547878=:56416 Content-Type: text/plain; charset=iso-8859-1 Content-Transfer-Encoding: quoted-printable It all depends on the spark advance schedule built into the units, and I do= n't know much about the p-mag. =A0I'm told that at high altitude cruise (lo= w manifold pressures) the Lightspeed will advance the spark by at least 7 d= egrees over the base timing. =A0That should (will) give a substantial perfo= rmance benefit at altitude. =A0Low-elevation takeoffs won't be any differen= t because there is no spark advance change over a standard mag. =A0All I ca= n tell is that my non-turbocharged ES will degrade significantly less than = a normal plane as the altitude goes up. =A0It is very happy above 12,000 fe= et and still has good performance at 17,000. =A0Some say 10 to 20 percent, = but I'm not sure I buy that. =A0"Up to 10 percent", as the ads say, is cert= ainly believable. =A0If you fly a lot above 12,000 feet having a system tha= t advances the timing is well worth it, in my opinion. =A0If you routinely = fly at 3,000 feet throttled back to less than 20 inches manifold pressure y= ou probably wouldn't be subscribed to the Lancair list :-)=0A=0AOn the other = hand, I wouldn't go to the trouble for a turbocharged engine, as the engine= will never - or rarely - operate at low manifold pressure for any length o= f time. =A0The only operational problem with a mag is potential cross-firin= g at high altitude, high boost conditions. =A0So for that reason you might = want a distributorless system(Lightspeed, e-mag, p-mag or whatever), I don'= t know.=0A=0AAgain, the important thing is not so much about how the spark = is formed, but WHEN it fires. =A0Regarding the question from Scott about ef= ficiency or performance - the engine always inhales the same amount of air = and fuel, so the spark advance just increases the power derived - which is = the same as efficiency. =A0More power on the same fuel. =A0The difference i= s greater as the engine is run leaner of peak as well as at high altitude. = =A0Both slow the burn rate, so more advance is welcome.=0A=0AThese comments= apply to any open-loop system. =A0Adaptive systems, such as the PRISM, are= a different story.=0AGary Casey=0A=0A=0A=0A=A0For those using the p-mag.= =A0 Is there any significant increase in fuel efficiency or=0Aincrease in p= erformance noticed?=0A=A0=0AThanks=0AScott Keighan --1219445386-1343500212-1321547878=:56416 Content-Type: text/html; charset=iso-8859-1 Content-Transfer-Encoding: quoted-printable
It all depends= on the spark advance schedule built into the units, and I don't know much = about the p-mag.  I'm told that at high altitude cruise (low manifold = pressures) the Lightspeed will advance the spark by at least 7 degrees over= the base timing.  That should (will) give a substantial performance b= enefit at altitude.  Low-elevation takeoffs won't be any different bec= ause there is no spark advance change over a standard mag.  All I can = tell is that my non-turbocharged ES will degrade significantly less than a = normal plane as the altitude goes up.  It is very happy above 12,000 f= eet and still has good performance at 17,000.  Some say 10 to 20 perce= nt, but I'm not sure I buy that.  "Up to 10 percent", as the ads say, = is certainly believable.  If you fly a lot above 12,000 feet having a system that advances the timing is well worth it, in my opinion. =  If you routinely fly at 3,000 feet throttled back to less than 20 inc= hes manifold pressure you probably wouldn't be subscribed to the Lancair li= st :-)

On the other hand, I wouldn't go to the tro= uble for a turbocharged engine, as the engine will never - or rarely - oper= ate at low manifold pressure for any length of time.  The only operati= onal problem with a mag is potential cross-firing at high altitude, high bo= ost conditions.  So for that reason you might want a distributorless s= ystem(Lightspeed, e-mag, p-mag or whatever), I don't know.

Again, the important thing is not so much about how the spark is f= ormed, but WHEN it fires.  Regarding the question from Scott about eff= iciency or performance - the engine always inhales the same amount of air a= nd fuel, so the spark advance just increases the power derived - which is the same as efficiency.  More power on the same fuel.  = The difference is greater as the engine is run leaner of peak as well as at= high altitude.  Both slow the burn rate, so more advance is welcome.<= /div>

These comments apply to any open-loop system. &nbs= p;Adaptive systems, such as the PRISM, are a different story.
Gar= y Casey


 For those using the p-mag.  Is there any significa= nt increase in fuel efficiency or
increase in performance noticed?
&n= bsp;
Thanks
Scott Keighan
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