Return-Path: Received: from smtp810.mail.sc5.yahoo.com ([66.163.170.80] verified) by logan.com (CommuniGate Pro SMTP 4.2.5) with SMTP id 559568 for flyrotary@lancaironline.net; Tue, 07 Dec 2004 17:59:56 -0500 Received-SPF: none receiver=logan.com; client-ip=66.163.170.80; envelope-from=dcarter@datarecall.net Received: from unknown (HELO Davidscmptr) (dcarter11@sbcglobal.net@69.148.208.164 with login) by smtp810.mail.sc5.yahoo.com with SMTP; 7 Dec 2004 22:59:28 -0000 Message-ID: <03f201c4dcb0$65683720$6501a8c0@Davidscmptr> Reply-To: "David Carter" From: "David Carter" To: "Rotary motors in aircraft" Cc: "Ned Thomas" <923te@cox.net> References: Subject: Re: [FlyRotary] Re: gear drive for distributor and oil metering pump Date: Tue, 7 Dec 2004 16:59:23 -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 6.00.2800.1437 X-MIMEOLE: Produced By Microsoft MimeOLE V6.00.2800.1441 Output Alternator Alternator . . . Regulator . . . . Regulator Amps . . . . P/N . . . . wt & cost . . . . P/N. . . . . . . . . .wt & cost . . . Total cost & wt . . 20 . . AM877557 . 1.81#, $145.49 . AM101406 . . 0.2# $66.56 . . $212.05 & 2.01# The above info is an extract from 1st line of a spreadsheet about John Deere PM alternators. On 2 Apr 2003, Ned Thomas reported: "I went to the local John Deere dealer and bought the 20 amp PM alternator. I then bought a 14 amp PM alternator that is used on the 3 cylinder diesel Kubota engines. It is 2 lbs lighter than the 20 amp and I think is adequate for a backup alternator. Fell free to give me a call to discuss further. . . . Ned Thomas, 405-360-4298, Norman, OK, RV9A" I just called Ned and we figure he meant 0.2 pounds difference. He's going out to his shop and recheck his notes or re-weigh the alternator. So, looks like we need to address the "design factors" for getting a PM alternator to fit in the distributor (or oil metering pump) hole securely with the Mazda gear on the end: . . . 1) Length of shaft of stock Mazda device vs the alternator shaft - cut down if too long; extend with shaft extension with Woodruff key and/or shrink fit or press fit. Long term durability of such a 'joint' is biggest need if have to extend the shaft. . . . 2) Diameter of shaft of stock Mazda device vs the alternator shaft - if shaft is too large, can turn it down for proper fit into Mazda gear; if too small, maybe can machine a spacer (collar?) for "press" or "shrink" fit over end of alternator shaft, that will provide an OD to give an appropriately tight fit into the Mazda gear. . . . 3) Mount for alternator, so it fits centered in hole for distributor or CAS and secured so it won't slide out, for example (not sure how the oil pump drive gear & shaft are). I don't have an engine so can't address this part of the physical install. . . . 4) Clearance of mounted alternator - any interference with engine or any other installed parts? Ned, when you get this, will you measure the OD of the PM alternators (Deere & Kubota) and send it to us on this list so we will have an idea if interference is going to be a problem? Also, Ned (or anyone else on this rotary list), did you get any size and wt info from B&C on the SD-8 (8 amp PM alternator)? I'm not sure 8 amps is enough to run 1 EFI pump and ignition & fuel inj systems if lose main alternator in flight. If 8 amps was enough, then we ought to get size data and run that alternative through the "design factors" above. - My "electrical loads" spreadsheet has a "6 amp" entry for each of the two efi pumps. Didn't document brand name of pump and who gave the info. Ken Powell says, "It takes a minimum of 13 amps to drive the fuel injection and ignition system." - Is that running both pumps for landing or just 1 pump "enroute"? - I've never noticed anyone say what the current draw is for Tracy's EC-2 and the 4 njectors it drives during cruise and at full power (in case of go around during landing after alternator failure). If only 2 injectors are in use at normal cruise and only 1 pump is on, will the B&C SD-8 PM alternator produce enough current at 1/2 of "engine cruise rpm of, say, 5400 rpm", i.e., at 2700 shaft rpm of SD-8? - If the SD-8 was OK for cruise but not "landing", it would be OK to let extra current needs be met by battery for the few minutes of approach and landing - SD-8 doesn't have to be big enough for "all possible" loads all the time. David Carter 409-722-7259 ----- Original Message ----- From: "Jim Sower" To: "Rotary motors in aircraft" Sent: Monday, December 06, 2004 11:30 PM Subject: [FlyRotary] Re: gear drive for distributor and oil metering pump > What about those little PM alternators that John Deere has on lots of stuff? > > > Ernest Christley wrote: > > > David Carter wrote: > > > >> Wonder if "we" could come up with an alternator to drop into that hole - > >> some back-up "juice" for our "electrically dependent engines". > >> > >> David > >> > > > > That is exactly what I've been thinking, David. Steve stopped by to > > look at my project last week, and we were discussing it. Thanks to Mr. > > Leonard over there, I now know what to look for. > > > > I need to find a 2/3HP or 500W or 30Amp generator/DC PM motor. It'll > > be 3" or 4" in diameter, with a couple inches of shaft sticking out. > > I'm thinking it would be easy enough to key the shaft to fit as a > > direct replacement for the metering pump. > > > > I don't have the numbers with me, but I was doodling with them a while > > back. I figured something like a couple of in.lb. of torque on the > > worm gear to produce 500W at 6000RPM. I now know the gear would turn > > at half that, so it is still less that 5in.lb. on the gear. The > > upshot is that 3000RPM motors are much more abundant that 6000RPM motors. > > > > I'm trying to source a part. I'm also thinking that a standard > > alternator can be made to fit by cutting down the housing. > > > > > >> Homepage: http://www.flyrotary.com/ > >> Archive: http://lancaironline.net/lists/flyrotary/List.html >