Return-Path: Received: from smtp809.mail.sc5.yahoo.com ([66.163.168.188] verified) by logan.com (CommuniGate Pro SMTP 4.1.8) with SMTP id 3067980 for flyrotary@lancaironline.net; Sun, 07 Mar 2004 16:31:24 -0500 Received: from unknown (HELO Davidscmptr) (dcarter11@sbcglobal.net@64.219.118.170 with login) by smtp809.mail.sc5.yahoo.com with SMTP; 7 Mar 2004 21:31:15 -0000 Message-ID: <056001c4048b$7505dbe0$6401a8c0@Davidscmptr> Reply-To: "David Carter" From: "David Carter" To: "Rotary motors in aircraft" References: Subject: Re: [FlyRotary] Re: Ideal Cooling System Plumbing (wasRe:[FlyRotary]Re:overflow Date: Sun, 7 Mar 2004 15:30:47 -0600 MIME-Version: 1.0 Content-Type: text/plain; charset="iso-8859-1" Content-Transfer-Encoding: 7bit X-Priority: 3 X-MSMail-Priority: Normal X-Mailer: Microsoft Outlook Express 6.00.2800.1158 X-MimeOLE: Produced By Microsoft MimeOLE V6.00.2800.1165 I have a feeling that we are talking about two different "coolant level sensors". The one I'm talking about is in the "pressurized coolant/expansion/header tank" like a late 90's Ford Taurus. The point that must be noted to discuss this "logically" is that the coolant level in this tank ("FULL - HOT") is ABOVE the top of the high spot for coolant in the engine. And, there is air space above the FULL- HOT level. There is not other expansion tank. Coolant doesn't go "somewhere else". That is as high as the level gets (unless there is blowby which is discussed last below.) But, to discuss LEAKS, not BLOWBY/STEAM: This being the case, if the coolant level in this tank goes down and the "low" sensor activates, there is still coolant in the engine block (unless the coolant tank is very deep, where bottom is WAY below the top of engine - not the case on the Ford). If this is so, then how could the "coolant low" light NOT be a good indicator that you have a leak? - None of the coolant is being "expanded" into an unpressurized "expansion tank". That unpressurized tank is REPLACED by this "pressurized coolant/expansion/header tank". Coolant does not "expand" "OUT" of this tank. It is THE expansion tank. - I think we are mixing the two systems in this discussion. This "pressurized coolant/exp/hdr tank" is part of the CLOSED system - it is not "external" to the cooling system. It is PART OF THE SYSTEM - and if its level goes down, then the entire closed system is losing coolant - the SYSTEM has a leak. - When the sensor in this tank turns on the "low" or "check coolant" light, then you have a leak - and you know it immediately upon losing about 1/2 or 1 qt (whatever is in this tank between "Full - Hot" and the "low sensor". Yes we should know the pressure indications of problems - but I don't think we have anyone flying with a tank with a fluid level indication system. Thus, there will be no "real stories" to validate this proposed Ideal Cooling System. (ref someone else's post asking for "proof"). And, yes, if there is blowby as mentioned earlier (compression/combustion gasses leaking by bad seals into the cooling passages and forcing HIGH pressure into the coolant galleys) then, because this high pressure is greater than the cap's release pressure, this blowby WILL force liquid past the cap and out wherever you have it plumbed to go. - I would simply route the rubber line from that "cap pressure release overflow fitting" to go up and spray up beside the windscreen where I could see it - to warn me that I was either suffering compression blowby - either from bad seals or from overheating and steaming. In either case, I'd have instant warning that I need to terminate the flight ASAP. - It would be an desireable increase in parts count and would MASK the problem to vent the "pressure cap blowby" into some other "expansion tank" that you couldn't see or might not immediately notice. In summary, in the absence of "high pressure above cap release pressure" in this CLOSED system, a fluid level indicator system should give you an early, positive, and adequate warning that you have a leak, whether you notice the pressure "clues" or not. David ----- Original Message ----- From: "Tracy Crook" To: "Rotary motors in aircraft" Sent: Sunday, March 07, 2004 10:33 AM Subject: [FlyRotary] Re: Ideal Cooling System Plumbing (wasRe:[FlyRotary]Re:overflow > FIRST the pressure drops precipitously, and THEN the coolant level > starts to go down ... FINALLY the temps start to rise (provided the > temp sender is submerged in what water remains). Just a brief comment on this part. Coolant level sensors are of almost no use in this application. It is commonly assumed that the temp gauge reads low as soon as the sensor is no longer submerged. Not true. It only drops after the coolant is all boiled away because steam will heat the sensor. If you haven't caught the problem long before this, it's too late anyway. Tracy