X-Junk-Score: 0 [] X-Cloudmark-Score: 0 [] X-Cloudmark-Analysis: v=2.3 cv=RZTu9Glv c=1 sm=1 tr=0 a=fDytfHDwyAaJ+kdFvMuM1Q==:117 a=23p7aaL3ge7Dbi2M5fw6HQ==:17 a=IkcTkHD0fZMA:10 a=x7bEGLp0ZPQA:10 a=CKeqCrOqW6IA:10 a=nTHF0DUjJn0A:10 a=pGLkceISAAAA:8 a=Ia-xEzejAAAA:8 a=6KCspYaHAAAA:8 a=on22okXAAAAA:8 a=7g1VtSJxAAAA:8 a=Azj7rWc3o7Huyt9OjF8A:9 a=QEXdDO2ut3YA:10 a=Qa1je4BO31QA:10 a=gvSQh4r-fQ0A:10 a=Urk15JJjZg1Xo0ryW_k8:22 a=CnniZz1SSAwyvaD4Xt4M:22 a=NPqpj5bUEVj9vR1HIonK:22 a=grOzbf7U_OpcSX4AJOnl:22 From: "Stephen Izett stephen.izett@gmail.com" Received: from mail-pg1-f177.google.com ([209.85.215.177] verified) by logan.com (CommuniGate Pro SMTP 6.2.14) with ESMTPS id 394260 for flyrotary@lancaironline.net; Sat, 20 Jun 2020 02:46:07 -0400 Received-SPF: pass receiver=logan.com; client-ip=209.85.215.177; envelope-from=stephen.izett@gmail.com Received: by mail-pg1-f177.google.com with SMTP id d4so5544503pgk.4 for ; Fri, 19 Jun 2020 23:46:09 -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=dR53yXjntf+X8Frtm7cLyhRSRqHfl9X9/SYc24E0SrE=; b=TOUIYk3qfGnpdOJx2/reWbjScjv0zS+DrrRrQy3128xeKmRlBT2lwhLR//39pvfzxe 4Hu/7c9xlRzRvtsccCEgyV4KuhiTfyWtSUai+c5M371KtKbjVA96NvuBWQVgD8K4pA+9 3aFb95eBr5ha473wKFogP+LlXr5Nt+i06VlYjJNmXr2yeBeYnR5JKF1hfFe6e4AelLvO kiveZLxc7Ak04mjXAouSvedYf1lqhvRo750enA4B1hLjaBowQ3WD+SCGsqnyykgZzTP5 DsvYmEO1IcfBxLdU4QnhZaMEJ08WLq8f8SH/sZ0vCTH+0cNrTk/75FgiiAYYbs2mlqDW 21/g== 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=dR53yXjntf+X8Frtm7cLyhRSRqHfl9X9/SYc24E0SrE=; b=sX12r/l4M3SzCst2r2039vH+3akE5dDinredD2lnIMfjLoAfEFuVC4m2S5Aver+Qxv eotZ87hVlKzKd9k8C1KQR+Le4R6rlsJNXodxx4rEZk3jdgHKZ/76QAH+62z7rm/mcICJ 90lmJaKwVrbm8zCxtOs95TPLyf8/qsu/rrZLvus3jJ1H1Eq90J2UMSqc1QBxfHodA8b8 35ckiK7yZjJQi1AgOM6HO2VTXf+nAEGCmjfp5hYzhECsLIj83mUQwz5oh3pjhC5YM/73 T3xaiXdbrrP1aZ8JT+mwEFbnZYeD55HYWpzleuUP9PE5xo/LQy1HMUC2D0FkriTHqzvN Up4w== X-Gm-Message-State: AOAM533/DuysHAtaqmg3vw+eW99TC9RSho+PYjmnX4Dp/2JtJ+78IZ0v SRMZC2bdtjOfLHP9QRVIM+HeE10j6bk= X-Google-Smtp-Source: ABdhPJy7G8PfEueDUA4+Je6SqZyn4wq/cGw8hKbxuesc2b3jgqJaTMUT7liCkNyNBDn0lLw8CoVldA== X-Received: by 2002:a63:464c:: with SMTP id v12mr5753228pgk.275.1592635550404; Fri, 19 Jun 2020 23:45:50 -0700 (PDT) Return-Path: Received: from [192.168.0.59] (pa49-196-29-68.pa.vic.optusnet.com.au. [49.196.29.68]) by smtp.gmail.com with ESMTPSA id w190sm7504308pfw.35.2020.06.19.23.45.48 for (version=TLS1_2 cipher=ECDHE-ECDSA-AES128-GCM-SHA256 bits=128/128); Fri, 19 Jun 2020 23:45:49 -0700 (PDT) Content-Type: text/plain; charset=utf-8 Content-Transfer-Encoding: quoted-printable Mime-Version: 1.0 (Mac OS X Mail 12.4 \(3445.104.11\)) Subject: Re: [FlyRotary] Re: Modifying the EC2 Staging point Date: Sat, 20 Jun 2020 14:45:45 +0800 References: To: Rotary motors in aircraft In-Reply-To: Message-Id: <03535EEE-3520-40F3-A334-EC53EEA17331@gmail.com> X-Mailer: Apple Mail (2.3445.104.11) Hi there Le Roux. I thought the BSFC would more realistically be around 0.55 for best = power in the Renesis with 10:1 compression. We burn PULP 95 unleaded. So calculated might be in the ball park of - hp =3D 16.4 x 6.2 / 0.55 =3D = 185hp at 6800 static As the rpm rises on takeoff I would expect the hp to rise with rpm until = the torque curve dives faster than the RPM rise. What numbers are others seeing and how do they compare with Lycoming = powered RV=E2=80=99s etc. These are the numbers I got of the web for fuel weight (so not = confirmed). AU PULP 6.26 lb.gal Premium 95 Unleaded here in Western Aust AU ULP 6.13 Standard 92 Unleaded here in = Western Aust AU Avgas 5.84 US Avgas 6.01=20 Cheers Steve Izett > On 20 Jun 2020, at 2:01 pm, Le Roux Breytenbach = breytenbachleroux@gmail.com wrote: >=20 > =EF=BB=BF > Steve: =46rom what i have read, you could use this formula to = calculate horsepower ( or more or less) >=20 > = https://performancedevelopments.com/fuel-flow-calculations-for-horsepower/= >=20 > HP =3D (GPH) x 5.92 / 0.44 (BSFC) >=20 > 16,4 (GPH) x 5.92 ( weight of 1 pound of fuel )=20 > devide by > 0,44 Brake Specific Fuel Consumption BSFC.=20 >=20 > =3D 220 Hp >=20 > I could be wrong >=20 > Sent from my iPhone > Le Roux Breytenbach=20 >=20 >=20 >=20 > Sent from my iPhone > Le Roux Breytenbach=20 >> On 20 Jun 2020, at 04:49, Stephen Izett stephen.izett@gmail.com = wrote: >>=20 >> =EF=BB=BFThanks Jeff and all >>=20 >> Last flight (after playing around with Mode #1 tuning on the ground) = the Primaries (4 port Red) were saturating at various times, indicated = as Steve Boese reminded me, by the loss of RPM readouts (EM3 & Dynon = Skyview) sensed from the Primary Injector line. >> Do others with small Primaries have this issue or is it a Tuning = issue? >> ie. Getting modes # 3,6,2 right will spread the load between the Pri = and Secondaries so the primaries don=E2=80=99t saturate? >> I do have another set of the larger (Blue) secondary injectors that = could replace the small red Primaries giving us 4 equal injectors, if = this was helpful. >> Do injectors have a sweet spot or better spray pattern at a = particular band of duty cycle? >>=20 >> We have an electric inflight adjustable prop which may make a = difference from those with experience with FP props. >>=20 >> On another note, I rechecked max fuel flow at static ~6800 rpm and = 0.92 Lambda which I think is best power. Fuel Flow peeks at 16.4 Gal/hr. >> It's a Renesis 4 Port with the stock exhaust header and resonator and = a modified stock intake manifold which is basically shortened from = 23.6=E2=80=9D to 18.1=E2=80=9D.=20 >> I had noted down that Tracy recommended 16=E2=80=9D and Paul L 20=E2=80= =9D for the intake length. >> What kind of hp do you think this might be producing and what are = others seeing? >>=20 >> How could we determine peak power/rpm? Could we use the airframe as a = dyno in some way? >> What about at WOT clean air and level, and adjust prop pitch/rpm for = maximum airspeed. >> I suppose is we kept the mixture constant we could look for highest = fuel flow. >> I=E2=80=99m trying ti ascertain the best rpm for takeoff. >> At the moment I=E2=80=99m leaving the prop set fine and rpm is = peaking at ~7500 on climb out. >>=20 >> Your expertise and insights would be greatly appreciated. >>=20 >> Steve Izett >>=20 >>=20 >>=20 >>=20 >>=20 >>=20 >>=20 >>> On 19 Jun 2020, at 9:37 pm, Jeff Whaley jwhaley@datacast.com = wrote: >>>=20 >>> I don't think you're missing anything Steve - my EC2 is the same : = fixed at 20" ... >>> It was originally 15.5" and could be set anywhere ... but after sent = back to Tracy it is now 20" and cannot be changed. >>> Jeff=20 >>>=20 >>> Hi people. >>>=20 >>> I did some tuning this morning. >>> But I couldn't get the staging point to change. >>>=20 >>> I reset all modes to default. >>> The built in default Stage Point on my EC2 seems to be ~20" >>>=20 >>> Ran engine at the desired MAP, selected Mode #7 (I was aiming at = 15.5") and pressed the Store Button. >>> I also tried holding it for a few seconds. >>> Staging Point stayed at ~20". >>> What am I missing here? >>>=20 >>> Steve Izett >>>=20 >>> -- >>> Homepage: http://www.flyrotary.com/ >>> Archive and UnSub: = http://mail.lancaironline.net:81/lists/flyrotary/List.html >>=20 >>=20 >> -- >> Homepage: http://www.flyrotary.com/ >> Archive and UnSub: = http://mail.lancaironline.net:81/lists/flyrotary/List.html