X-Junk-Score: 0 [] X-Cloudmark-Score: 0 [] X-Cloudmark-Analysis: v=2.2 cv=cojZqBwi c=1 sm=1 tr=0 a=TAJ2QmXZTKeFX/9C59XSww==:117 a=b0WXXb1TpCRXX/ruI2YXbQ==:17 a=IkcTkHD0fZMA:10 a=x7bEGLp0ZPQA:10 a=CKeqCrOqW6IA:10 a=ocR9PWop10UA:10 a=3oc9M9_CAAAA:8 a=Ia-xEzejAAAA:8 a=L634gqZl23BDorns8cAA:9 a=V5v9xZirLe58u7eY:21 a=tSb5bwfJzLGHmFSL:21 a=QEXdDO2ut3YA:10 a=Urk15JJjZg1Xo0ryW_k8:22 From: "Stephen Izett stephen.izett@gmail.com" Received: from mail-pl0-f49.google.com ([209.85.160.49] verified) by logan.com (CommuniGate Pro SMTP 6.2.0) with ESMTPS id 10483463 for flyrotary@lancaironline.net; Thu, 28 Dec 2017 17:14:29 -0500 Received-SPF: pass receiver=logan.com; client-ip=209.85.160.49; envelope-from=stephen.izett@gmail.com Received: by mail-pl0-f49.google.com with SMTP id bd8so21849323plb.9 for ; Thu, 28 Dec 2017 14:14:29 -0800 (PST) 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=vk2AXaMZdNKozMtTYI57wHh8aAjxMVo4mVXR/vnHuG4=; b=FsxeIWRbW0CYAmZ5+IMr7phSwAsYAaH3zAd5p9XRzSxYNNyxttEdLm7tqEY+c3Hqdv cq57VzamFdAMgZ2/Bn4YcLSTgfZhBRGaCxNVrtFsmeb9A2TmT0jFaiyiG6CMicwHyFuT rXH6KZXMeSa/b8/Xw6gNd55Mp55kG2QHDTqmUCm1CsYP+s6nMy/qlM3g8pOz2RUc69NY DwzBTyelPA57xN1UkMo5bWNymKTQErKfoeg7Jm69zqysycS2VfdZeZGIArihApuHqg3X 4eSH3gpXw4f6gFT6Ot6nxvxhW/W5j6qub4R3E4gaRRjyrBatJ3ZU5bjLcjXofQhl/aRL AtTA== 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=vk2AXaMZdNKozMtTYI57wHh8aAjxMVo4mVXR/vnHuG4=; b=ohTJhBAK6fUYoM6PPeQ0qCY9NnKq0ODvdtaAf5n4H0UjAF1Bf4OHglcZs2Vf5obY7W FoBlCdouKma0l5AUXPha607Yevez+4UuosSWwIm9Fa6rX/KPuYkEZhXcRYE0bbH+cZ9l HfrEzW2IAfToL8OAqgl/vQ3teNKwIhPOccRKBfDdaWl4Vw05XG+YNiyWoFeV+XhmV0dv Nwg9ZXtKIeFbnX6GbldfoFlKf4U+4hCEhsLPgyDEMeVQCQAGbxtssLusYUtdPUyXYrq1 A3ukuf0WD4fo3WQfDC+SiBvPENl91kkvAwnImMWcw5OoAF2CkWyGWRHJMLo1xShFQD2f rSHQ== X-Gm-Message-State: AKGB3mKzSiXN6fmbMqaWKCVuiprvGz9rKSeNfETHmylvrJjJ9EeLs8Ma VUQoLnAmEq3t6LeP4wViLYtYmMQj X-Google-Smtp-Source: ACJfBouFJuJV3268CZDRB5y8dnE6Do+R/RBhrhCLklSDq/mVdCrR7p8PmhI2mhXilUY4W3slJqItxQ== X-Received: by 10.159.198.76 with SMTP id y12mr1748506plt.257.1514499251606; Thu, 28 Dec 2017 14:14:11 -0800 (PST) Return-Path: Received: from [10.1.1.29] (220-253-221-100.dyn.iinet.net.au. [220.253.221.100]) by smtp.gmail.com with ESMTPSA id a23sm67138718pfa.177.2017.12.28.14.14.09 for (version=TLS1_2 cipher=ECDHE-RSA-AES128-GCM-SHA256 bits=128/128); Thu, 28 Dec 2017 14:14:11 -0800 (PST) Content-Type: text/plain; charset=utf-8 Content-Transfer-Encoding: quoted-printable Mime-Version: 1.0 (Mac OS X Mail 10.3 \(3273\)) Subject: Re: [FlyRotary] Cooling problems. Date: Fri, 29 Dec 2017 06:14:03 +0800 References: To: Rotary motors in aircraft In-Reply-To: Message-Id: <7E7A57A6-8443-4573-B178-42DC05C2CD0D@gmail.com> X-Mailer: Apple Mail (2.3273) Hi Lynn I really appreciate your input and would appreciate seeing a picture of = your cooling circuit. I should have mentioned, I have temp senders on the in and out of both = oil and water, In the test yesterday after 20 minutes of running the oil cooler (Rx7 = turbo - not sure which model) drops the temps by about 12F while the = water Rad is only about 6F. I=E2=80=99ve seen this as high as 18F oil and 9F water previously. Apart from the cooling system, what else can cause overheating? If I pressurise the system it holds that pressure for some time for over = 30 mins. Cheers Steve I > On 29 Dec 2017, at 1:32 am, Subscriber Lehanover@aol.com = wrote: >=20 > I started racing rotary powered cars in 1980. An RX-2 with a junk yard = engine. Had to pour motor oil and hot coffee into it in order to start = it. No compression. People gathered around just to watch me do it. Ran = well, never a reliability problem. No overheating problems. Oil cooler = was an air conditioning core from a large GM car. Cheap and available. > =20 > I copied the cooling system from the stock RX-2. It had a coolant = recovery tank made of plastic. The pressure cap was on this tank. The = radiator cap was just to seal the system. Those engines had the giant = monkey motion thermostat that closed a hole in the water pump body after = a quick warm up.( Pollution control). Stock radiator. Bigger oil cooler. = No problems. > =20 > Then I started building bridgeported engines. Big problems. I = installed a big aluminum radiator. A double pass top to bottom. This put = both inlet and outlet on the same end. Very handy. No problems for a = while. Then an occasional overheat after an engine change. I could not = get all of the air out of the engine after a rebuild. I lifted an idea = from the Cosworth installation manual and installed a swirl pot. The top = of the swirl pot plumbed to the bottom of the stock RX-2 recovery tank. = So as the engine warms up any air removed by the swirl pot enters the = bottom of the recovery bottle. The bottle is kept half full of coolant, = so the air pops to the top of the bottle. On cooldown or off throttle = situations only coolant can return to the engine. After several sessions = of refilling the bottle to one half full, the engine has removed all of = the air and full RPM shifting is available. For us that was shifting at = 9,600 RPM. Coolant temps 180. Oil 160. At low RPM the air will not come = out of its hiding places. My idle was 2,200 RPM. Timing is checked at = 4,000 RPM. Clear out the bubbles at least at 4,000 RPM. > =20 > On cool days (below 65 dgrees) we would install a thermostat that had = two 5/16 holes drilled through the flange. > And tape over half of the radiator. > =20 > Some items are not obvious. > =20 > The best coolant pump location is at the very bottom of the coolant = loop. The rotary pump is at the top of the coolant loop. The pump will = gleefully stop pumping if a dose of air enters the suction side. Very = bad MOJO. The center irons on 12-A engines at first had a temp sender = hole. Great place to let air out of the coolant before start up. Then = the hole was filled in but the machined flat was still there as well as = two tapped holes. I drilled and tapped for 1/4 pipe and installed a = radiator bleed fitting. Got out lots of air before even running the = engine. > =20 > The recovery bottle need not be mounted high in the circuit. That = bottle in the racer is mounted on the passenger floor. Also the top of = the swirl pot need not be mounted high in the coolant circuit. Does not = matter.=20 > =20 > I found a Stant pressure cap for the RX-2 bottle rated at 28 pounds. I = installed a Shrader valve in the swirl pot and pressurized the whole = system to 28 pounds before start up. This also tests the pressure cap. > =20 > My coolant is 10% prestone antifreeze. 1 bottle of RedLIine Water = Wetter, or 1/2 teaspoon of Dawn dishwashing soap. The rest is distilled = water. And 28 pounds of pressure. > =20 > The racer is gone now but the last iteration of the coolant system is = as above. The oil cooling had to be improved as HP went up. (Store = bought engines). Daryl Drummond 250 HP 12-As. So the last oil system was = a full dry sump with one 44 row setrab in the pressure loop. And two 44 = row setrabs in the scavenge loop. We ran 100 pounds of oil pressure with = 40 weight RedLine racing synthetic. No oil related failures > since 1980. The modern "Square" Peterson pumps tend to split open the = pressure section. I changed to the older round body Peterson, no = problems. > =20 > Lynn E. Hanover > =20 > I will draw the coolant loop if you like. It was published many times = but died several computers ago.