X-Junk-Score: 0 [] X-Cloudmark-Score: 0 [] X-Cloudmark-Analysis: v=2.3 cv=PNVxBsiC c=1 sm=1 tr=0 a=nMnKDt7L5N/liDxpcIebAQ==:117 a=b79/JNUwnjdyXvH342spcg==:17 a=jpOVt7BSZ2e4Z31A5e1TngXxSK0=:19 a=IkcTkHD0fZMA:10 a=x7bEGLp0ZPQA:10 a=CKeqCrOqW6IA:10 a=0o9FgrsRnhwA:10 a=UKPAHat8AAAA:8 a=Ia-xEzejAAAA:8 a=3oc9M9_CAAAA:8 a=pGLkceISAAAA:8 a=7g1VtSJxAAAA:8 a=ycAuczkubwpwn96dlrcA:9 a=QEXdDO2ut3YA:10 a=Qa1je4BO31QA:10 a=gvSQh4r-fQ0A:10 a=Fc6xXSS-RxGHxrvp76Qp:22 a=Urk15JJjZg1Xo0ryW_k8:22 a=grOzbf7U_OpcSX4AJOnl:22 From: "Stephen Izett stephen.izett@gmail.com" Received: from mail-pg1-f171.google.com ([209.85.215.171] verified) by logan.com (CommuniGate Pro SMTP 6.2.13) with ESMTPS id 12738496 for flyrotary@lancaironline.net; Fri, 05 Jul 2019 19:16:50 -0400 Received-SPF: pass receiver=logan.com; client-ip=209.85.215.171; envelope-from=stephen.izett@gmail.com Received: by mail-pg1-f171.google.com with SMTP id s27so4883875pgl.2 for ; Fri, 05 Jul 2019 16:16:51 -0700 (PDT) DKIM-Signature: v=1; a=rsa-sha256; c=relaxed/relaxed; d=gmail.com; s=20161025; h=from:content-transfer-encoding:mime-version:subject:date:references :to:in-reply-to:message-id; bh=8HgXBBj5eZoLknFQ1r1gIog74myz6T22naojn6P5EqQ=; b=nOXNFHbi3CA4RGB3fZyX7Y4e6PudkLOVMpKL4DZ8fQBJLaMP/dmdOTq/tiMzsRm11F eDNgdM4F88U+8JYLnbHZdFDzLXfke8XP9FJ7PHm+1OnokZidVOy9z+JWviFgGSznW5ME 6Dd+MZhyK6//kcogfLA+hVWuLXP850jIMMFLj/dvQjFRnBsWPpHhHdEM/OEg8FUAEscn myrroSQ7Gq1dfOJOTWD6AuR8oMJdKpxZCmSbZLrI3X4szHsFtB+YIQxgn3zYlgcIYsP/ FUt9MhRiFuW13yGz5b3dpNEQ0TBuTBK5ukrc8xUmY53vkL6pQdTYjGH0orDgywlaTIOk xooA== X-Google-DKIM-Signature: v=1; a=rsa-sha256; c=relaxed/relaxed; d=1e100.net; s=20161025; h=x-gm-message-state:from:content-transfer-encoding:mime-version :subject:date:references:to:in-reply-to:message-id; bh=8HgXBBj5eZoLknFQ1r1gIog74myz6T22naojn6P5EqQ=; b=Fs1mbADNP6+2k0M/9YpZzAfdt22bSQldFek33Mit3LJQqA3LwgvpMJUTaMWXkiBmz1 CpL43JQ+zgv++pffo7RJSGH7+46rx8AfeBFCaw5bALbmsFkFlyTyYG3wDf0uaHzNVD1Y JpBHXU2rVtOf4xll1OHP+YdxQu9Q/K41YaAJySe0pxoWRqJUkp5J4Bm0Is6BDYIWamt+ +B0aUDVj+BueFFkuhNnrRzPvG3l2jz+NlRKIh4JCdVxHcA+EMHY4xv3FFt+n2/bbO6zN zALKBatd0KulJAOiDPVZz2hbus7fgwCptrlObLGm/n2m9HnVJVF5xBv6d/o7MrcufiqN aG+Q== X-Gm-Message-State: APjAAAWNLqhpuJgn/XB7EZOjPzHseXELd1hwxivUUjrJSPghfiTfIGyX nD9rFSXLohwBkJH5yX5jedRCzUc2 X-Google-Smtp-Source: APXvYqxrbBOqZOLlit5D6TFc6u1h0MXOREiLpsNq/t+x4Y60FP2ECEr7Q1icmLwJ7Ts8TE+2vvZzTg== X-Received: by 2002:a63:6143:: with SMTP id v64mr7885878pgb.407.1562368593063; Fri, 05 Jul 2019 16:16:33 -0700 (PDT) Return-Path: Received: from steves-mbp.lan ([118.209.173.119]) by smtp.gmail.com with ESMTPSA id y8sm11973504pfn.52.2019.07.05.16.16.31 for (version=TLS1_2 cipher=ECDHE-RSA-AES128-GCM-SHA256 bits=128/128); Fri, 05 Jul 2019 16:16:32 -0700 (PDT) Content-Type: text/plain; charset=utf-8 Content-Transfer-Encoding: quoted-printable Mime-Version: 1.0 (Mac OS X Mail 12.2 \(3445.102.3\)) Subject: Re: [FlyRotary] Re: timing on renesis engines Date: Sat, 6 Jul 2019 07:16:27 +0800 References: To: Rotary motors in aircraft In-Reply-To: Message-Id: <9F0B24DE-0E6D-4317-BAD0-19B7B92DB92E@gmail.com> X-Mailer: Apple Mail (2.3445.102.3) Thanks Bobby and Lyn. According to Tracy=E2=80=99s code - 2.6 mSec RX8, 3.5 mSec RX7, 4.0 = mSec LS2, 4.3 mSec LS1. I also wondered about the timing difference between the various coils = trigger circuit actually firing. Now I suppose that difference might be a few uSec and insignificant, but = if its 100uSec=20 then the timing difference between various coil types might become = significant. @ 7000 RPM=20 1 rev takes 8.6mSec So each degree of EShaft rotation is 24uSec. Thanks again for the help. Steve > On 6 Jul 2019, at 2:52 am, Bobby J. Hughes bhughes@qnsi.net = wrote: >=20 > Lynn, >=20 > Default is what ever Tracy set it to. The CAS location is not = adjustable so default is set in his code.=20 >=20 > Bobby >=20 > Sent from my iPhone >=20 > On Jul 5, 2019, at 12:43 PM, lehanover lehanover@aol.com = wrote: >=20 >> What is the "Default" advance? Is that checked with a timing light? = Easy starting can be up to 15 degrees of advance. For full power use up = to 27 degrees of advance is good up to 10,500 RPM. Boosted engines = require less advance as boost increases. Because the effective = compression ratio as well as charge temperature is going up. Very high = boost my have advance closer to zero. Advance is used to allow full = combustion >> of the charge before the exhaust port opens. At higher pressure and = temps the flame front speeds are increasing. So, less time is needed. = Thus less advance is needed. Lowering intake air temps with an = inter-cooler and adding water spray can allow higher boost. >>=20 >> Boosting to maintain sea level performance would probably not shorten = engine life. Boosting for additional performance does shorten engine = life. The kids get over 600 HP with boosted drag racing engines. This is = fine if you only need the engine for 9 seconds. You have to know what = the actual advance is to make any decision. Mark the flex plate or = flywheel teeth with paint so you can check actual advance during any = RPM. >>=20 >>=20 >> It is difficult to detonate an NA engine. It is not difficult = detonate a boosted engine. >>=20 >> Lynn E. Hanover >>=20 >>=20 >> In a message dated 7/5/2019 10:22:44 AM Eastern Standard Time, = flyrotary@lancaironline.net writes: >>=20 >> Steve, >> I=E2=80=99m running default timing or maybe 1 degree advanced. Early = on I experimented with 1-2 degrees advance for many flight hours and did = not detect any noticeable change in engine performance. I did push the = engine to what I believe was detonation during a ground tuning session. = I was tuning under boost (44=E2=80=9D MP) , 7000 rpm with a wideband O2 = on each runner and adjusting Mode 9 and Mode 4. With F/A balanced = between each rotor and EGT=E2=80=99s under 1600F I was trying to see if = increasing timing would lower EGT=E2=80=99s. F/A was in the 11=E2=80=99s. = This was at the end of the session and the engine and supercharger were = already hot. I think I had added 4-5 degrees advance with no noticeable = EGT decrease when I encountered a mild bang or misfire. This condition = was well above my 38=E2=80=9D MP limit I sometimes use for takeoff. >>=20 >> I=E2=80=99m curious about the dwell time setting difference between = LS1 and LS2 coils. I switched to LS2 coils sometime back with no = failures to date. I remember seeing an option setting in some of the = code you or Finn posted. Internet research indicates LS2 coils require = less dwell time than LS1. Possibly 0.5-1 ms less. >>=20 >> Bobby >>=20 >> Sent from my iPad >>=20 >> > On Jul 5, 2019, at 12:58 AM, Stephen Izett stephen.izett@gmail.com = wrote: >> > >> > Hi there Guys >> > >> > Of the guys with Renesis engines using EC2/3 can you comment on = your timing settings. >> > I=E2=80=99ve to date left the timing at the default setting = figuring its set by the location of the CAS. >> > Not sure if the various coil options have different trigger timing = latency. >> > >> > Thanks >> > >> > Steve Izett >> > >> > >> > >> > >> > -- >> > Homepage: http://www.flyrotary.com/ >> > Archive and UnSub: = http://mail.lancaironline.net:81/lists/flyrotary/List.html >>=20 >> -- >> Homepage: http://www.flyrotary.com/ >> Archive and UnSub: = http://mail.lancaironline.net:81/lists/flyrotary/List.html