X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Received: from eastrmmtao102.cox.net ([68.230.240.8] verified) by logan.com (CommuniGate Pro SMTP 5.2.10) with ESMTP id 3331319 for flyrotary@lancaironline.net; Thu, 04 Dec 2008 17:16:19 -0500 Received-SPF: none receiver=logan.com; client-ip=68.230.240.8; envelope-from=taspilot@cox.net Received: from eastrmimpo01.cox.net ([68.1.16.119]) by eastrmmtao102.cox.net (InterMail vM.7.08.02.01 201-2186-121-102-20070209) with ESMTP id <20081204221544.TLAY19141.eastrmmtao102.cox.net@eastrmimpo01.cox.net>; Thu, 4 Dec 2008 17:15:44 -0500 Received: from eastrmwml43 ([172.18.18.217]) by eastrmimpo01.cox.net with bizsmtp id nAFj1a00P4h0NJL02AFj9F; Thu, 04 Dec 2008 17:15:43 -0500 X-Authority-Analysis: v=1.0 c=1 a=0uUEV_YqwagA:10 a=Hrs9-Pl8cFEA:10 a=xY3j4B6z203P4gJ+umuYrw==:17 a=arxwEM4EAAAA:8 a=kviXuzpPAAAA:8 a=QdXCYpuVAAAA:8 a=lAp0fRAZlJpma_j6y3AA:9 a=-1JgxnegfGz2F3fKnNUA:7 a=T0I93TJNb5fBnTqZLv8xAYuBm7gA:4 a=4vB-4DCPJfMA:10 a=U8Ie8EnqySEA:10 a=at0Q5_2dr5wA:10 a=EzXvWhQp4_cA:10 a=ndTQkonOMSIA:10 X-CM-Score: 0.00 Received: from 72.213.42.202 by webmail.central.cox.net; Thu, 4 Dec 2008 17:15:43 -0500 Message-ID: <20081204171543.WLGIL.409042.imail@eastrmwml43> Date: Thu, 4 Dec 2008 17:15:43 -0500 From: To: Rotary motors in aircraft Subject: Re: [FlyRotary] Re: Hose and Expansion Tank ... was Hose Cc: wrjjrs@aol.com In-Reply-To: MIME-Version: 1.0 Content-Type: text/plain; charset=utf-8 Content-Transfer-Encoding: quoted-printable X-Priority: 3 (Normal) Sensitivity: Normal Bill Please remove me from your mailing lists. taspilot@cox.net ---- wrjjrs@aol.com wrote:=20 Jeff, Many systems with restricted height run a bleed hose from the highest point= in the system to the bottom of the expansion tank. Usually a restrictor is= used, about .030-.060 inches. any bypass isn't sagnifigant, but air will l= eave the system that way.=C2=A0 Bill Jepson=C2=A0 -----Original Message----- From: Jeff Whaley To: Rotary motors in aircraft Sent: Tue, 2 Dec 2008 12:16 pm Subject: [FlyRotary] Re: Hose and Expansion Tank ... was Hose If there is any doubt about the hose I=E2=80=99ll remove it =E2=80=A6 I wou= ld never have guessed how that expansion tank is working with this setup. Originally I wanted the tank to be the highest point in the system and be c= onnected to the inlet side of the pump where pressures are lower and it wou= ld make an ideal filling point for entire system; however, there isn=E2=80= =99t enough height under the cowl to mount it above the water pump outlet. During first flight the pressure got pegged to >20 psi > cap pressure =E2= =80=A6 I removed that cap and put back the old one at 16 psi =E2=80=A6 now = if the system is pressurized through the snifter valve it is regulated at 1= 6 psi by the cap, as I would expect. So I relieved the pressure to 10 psi a= nd ground-operated the engine; it pressurized and regulated itself back to = 16 psi from 130F water temp all the way up to 200F water temp =E2=80=A6 but= what is startling is that the tank is actually cool to the touch =E2=80=A6= the water pump is hot, radiator and its hoses are hot =E2=80=A6 hot pressurized air is exiting th= e engine through that hose and 1 cup of coolant but having very little temp= erature effect on either =E2=80=A6 I love it =E2=80=A6 I believe the system= is working perfectly and don=E2=80=99t see any reason to operate at pressu= re above 16 psi. Jeff (Just waiting for the weekend and flight #2) =C2=A0 From: Rotary motors in aircraft [mailto:flyrotary@lancaironline.net] On Beh= alf Of Ed Anderson Sent: Tuesday, December 02, 2008 2:41 PM To: Rotary motors in aircraft Subject: [FlyRotary] Hose was Re: First Flight, short and hot =C2=A0 Jeff, you might check with Tracy Crook.=C2=A0 Way back when, he attempted t= o use some clear plastic/nylon cored reinforced hose for his coolant system= for the same reason (I think) =E2=80=93 so you could see what was going on= .=C2=A0 As best I recall, it was not up to the task due to heat and pressur= e =E2=80=93 but these were the main line hoses and not just to the header t= ank.=C2=A0=20 =C2=A0 I can not recall the type =E2=80=93 but think he got them at the local hard= ware store. =C2=A0 Ed =C2=A0 Ed Anderson Rv-6A N494BW Rotary Powered Matthews, NC eanderson@carolina.rr.com http://www.andersonee.com http://members.cox.net/rogersda/rotary/configs.htm#N494BW http://www.dmack.net/mazda/index.html From: Rotary motors in aircraft [mailto:flyrotary@lancaironline.net] On Beh= alf Of Jeff Whaley Sent: Tuesday, December 02, 2008 2:03 PM To: Rotary motors in aircraft Subject: [FlyRotary] Re: First=20 Flight, short and hot =C2=A0 Thanks Kelly, I copied (Bill Eslick=E2=80=99s) installation (seen at Round-= up) and the see-through aspect of that hose was a major selling point; it= =E2=80=99s easy to see whether there=E2=80=99s air or fluid in the line, wh= ich is very helpful =E2=80=A6 ideally there should be fluid in the line and= about 1 cup in the expansion tank; I suppose removing the cap would provid= e same information =E2=80=A6 but the tank has to be de-pressurized, cap rem= oved and re-pressurized before flight. Bill any comments on durability of that hose? Jeff=20 =C2=A0 From: Rotary motors in aircraft [mailto:flyrotary@lancaironline.net] On Beh= alf Of Kelly Troyer Sent: Tuesday, December 02, 2008 12:24 PM To: Rotary motors in aircraft Subject: [FlyRotary] First Flight, short and hot =C2=A0 =C2=A0=C2=A0 Jeff, =C2=A0=C2=A0=C2=A0 You might keep an eye on the plastic hose goinng to the = bottom of your expansion tank..........This particular hose is not durable and under the h= igh heat under the cowl (perhaps not during your Canadian winter) might have a short service life..........Project looks great and am looking forward to= all further flight test info.......... -- Kelly Troyer=20 "Dyke Delta"_13B ROTARY Engine=20 "RWS"_RD1C/EC2/EM2=20 "Mistral"_Backplate/Oil Manifold=20 =C2=A0 -------------- Original message from Jeff Whaley : --= ------------=20 Thanks to you all for the congratulatory comments =E2=80=A6 attached is a p= icture of expansion tank and preflig ht roll-out =E2=80=A6 the orange line is fuel return; the brass is pressure= gauge pickup and snifter valve installation. After reading Eds=E2=80=99 email I now know why the water temperature was s= o high. =C2=A0I installed a thermostat with the onset of cold weather, but = I couldn=E2=80=99t use the original Mazda thermostat because my temperature= bulb protrudes across the bypass hole. =C2=A0Originally the bypass hole wa= s plugged and there was no thermostat; however, I removed the bypass plug a= nd used a non-Mazda thermostat !! =E2=80=A6 so that=E2=80=99s why the under= side of the Mazda thermostat is so long! Thanks Ed for setting me straight = and based on your comment about 20% loss of efficiency, I could possibly se= e 230F x 0.8 or as low as 184F on next flight =E2=80=A6 that would be great= ! For now the thermostat is gone and bypass is re-plugged. Closer examination of the belt and rubber deposits on underside of top cowl= ing suggests the belt got jammed in the pulley and cut by friction. I tried again last night to remove the alternator pulley nut =E2=80=A6 what= =E2=80=99s the secret? Left-hand thread? Loctite or what? It=E2=80=99s so t= ight I=E2=80=99m afraid of damaging something trying to get it off. Jeff =C2=A0 =C2=A0