Return-Path: Received: from snoopy.pacific.net.au ([61.8.0.36] verified) by logan.com (CommuniGate Pro SMTP 4.1.5) with ESMTP id 2641549 for flyrotary@lancaironline.net; Sat, 18 Oct 2003 06:41:46 -0400 Received: from mongrel.pacific.net.au (mongrel.pacific.net.au [61.8.0.107]) by snoopy.pacific.net.au (8.12.3/8.12.3/Debian-6.6) with ESMTP id h9IAfeUC023951 for ; Sat, 18 Oct 2003 20:41:40 +1000 Received: from imanic (ppp3.dyn1.pacific.net.au [61.8.1.3]) by mongrel.pacific.net.au (8.12.3/8.12.3/Debian-6.6) with ESMTP id h9IAbVsv025518 for ; Sat, 18 Oct 2003 20:37:35 +1000 From: peon@pacific.net.au To: "Rotary motors in aircraft" Date: Sat, 18 Oct 2003 20:35:36 +1000 MIME-Version: 1.0 Content-type: text/plain; charset=US-ASCII Content-transfer-encoding: 7BIT Subject: EWP Series vs PARALLEL pumps & flowmeter Reply-to: leon@aerota.com Message-ID: <3F91A418.19800.1CF143C@localhost> Priority: normal In-reply-to: X-mailer: Pegasus Mail for Win32 (v3.12c) Hi Guys, Maybe I'm having a "Senior Moment" as Jim Sower would say, but I feel I've just gotta butt in here. Been reading all the to and fro of this dual EWP thingy. As you can imagine, I have devoted much thought to redundancy of EWPs in an aircraft situation since I first spoke about EWPs on that "other" place (where HIM ran the numbers and said they wouldn't work).. My idea is that the most efficient use of a dual (redundant) EWP set-up is that they should be run in PARALLEL with two simple non return valves. Yep, sure it's a bit more complicated to engineer, but I believe it is worth the extra effort. That way, you will get nearly double increase in flow (weeeellll ,,, maybe 70 - 80%?? depending on the actual flow capacity of the system ) with both pumps running when you need it - for take-off and climb-out or go-around - once in cruise mode, you can turn one of them off to reduce current draw. As an aside, similarly, when running dual EFI fuel pumps, they are always (well in race cars at least) run in parallel with non return valves. What we need is extra FLOW, not pressure. In aircraft use, I plan to run two fuel pumps in parallel feeding from a common sump or header tank, and have both on for take-off and climbout and landing (in case of go-around), but be able to switch one of them off for cruise to reduce curent draw. Same applies with the EWPs. With EWPs, a switching mechanism can be arranged so that the second pump will come on and off automatically whenever the water temp goes over or under pre-set limits. An ordinary thermoswitch of the type used for auto radiator fans - especially the auxillary air cond fan(s) are pretty reliable. Obviously, you have a manual over-ride switch and a nice big coolant temp warning light in case the thermoswitch decided to go awol. When you run pumps in SERIES, you will increase the PRESSURE considerably, but not the flow by much. The reason you only get a 25% increase in flow when both are going is that the second pump and the first pump is seeing a bit LESS 'head" as the outlet is on the "suck" side of the second pump). But it's still pumping through the same size orifice! My concern is that if they are run in series, just when you need flow most, (as in one pump failing - which is the purpose of redundancy - you will get 20% LESS flow than one pump on its own as per Todd's tests). See, . runing just one pump in series with the other freewheeling, the other impellor will cause resistance to the flow as it tries to spin up the impellor, and make the electric motor try to act as a sort of dynamo. By the same token, the MAX flow capacity has to do with the minimum diameter of the inlet and / or outlet the size of the hoses, and the total internal resistance of the centrifual housing.as well as any restrictions elsewhere in the cooling system. So my personal opinion is that EWPs should be the same as fuel pumps - run in parallel. (But now I'm repeating myself - I'd better get out of your way now!) Comments and criticism welcome. Cheers, Leon