AeroElectric-List Digest Archive

Mon 03/16/09


Total Messages Posted: 10



Today's Message Index:
----------------------
 
     1. 06:05 AM - Re: Rotax w/ Perihelion OVM (Chris Stone)
     2. 07:39 AM - Re: Polyfuses (Radioflyer)
     3. 07:40 AM - Anyone with a KR22 Marker Beacon pinout? (Radioflyer)
     4. 07:48 AM - Re:  (Gilles Thesee)
     5. 08:03 AM - S-Tec 30 problem (galaxyone@juno.com)
     6. 08:20 AM - Re: AeroElectric-List Digest: (Jan de Jong)
     7. 08:41 AM - S-Tec 30 problem (David LLoyd)
     8. 08:46 AM - Question on Z-11, Main Buss Feed (Don Morrisey)
     9. 09:03 AM - Re: Re: Polyfuses ()
    10. 09:06 AM - Re: S-Tec 30 problem (Ralph E. Capen)
 
 
 


Message 1


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    Time: 06:05:40 AM PST US
    From: Chris Stone <rv8iator@earthlink.net>
    Subject: Re: Rotax w/ Perihelion OVM
    Thanks Bob... et al. This list is a wonderful resource. Saves me unknown hours researching! Chris do not archive -----Original Message----- >From: "Robert L. Nuckolls, III" <nuckolls.bob@aeroelectric.com> >Sent: Mar 15, 2009 4:19 PM >To: aeroelectric-list@matronics.com >Subject: Re: AeroElectric-List: Rotax w/ Perihelion OVM > > >>I purchased this to provide over voltage protection for the >>electrics powered by the built-in alternator on the Rotax. I am not >>entirely clear on the operation of the Rotax alternator nor is the >>Rotax manual. It contains only a schematic, no theory of >>operation. It has what appear to be two B leads. Per Bob's >>schematic breaking one B lead shuts down the alternator. Per Rotax >>the output is 20A@5,000 RPM. Thus a 20A relay would be suitable if >>each B lead produces 10A max. Since Rotax calls the voltage >>regulator a rectifier/regulator I am assuming each B lead is single >>phase AC but I am not clear as to how breaking one B lead would shut >>down the alternator. > > You have two wires coming out of a wall socket to > power some device, but the ON-OFF switch needs to > open or close only one leg of the wall-power to > control the device. Those are not "B" (battery) > leads coming off the engine. They are as you've > guessed, two leads with single phase, AC power on them. > > The B-leads are the "R" and "B+" wires that > come off the rectifier/regulator. > > Breaking one of the green ac power input leads > is the same as the single switch on your desk > lamp. The PM alternator continues to develop > voltage but it has no place to go. > > >>A couple of questions: Why both a fusable link and 5A CB in series >>on the master sw/OV disconnect relay? > > This is to accommodate some legacy design rules adopted > from certified aircraft . . . since the power to operate > the relay is so small, and since you've elimnated the > need for a pilot accessible circuit breaker, I'll suggest > you eliminate both the fusible link and the 5A breaker. > Power your alternator control circuit directly from a > 3A fuse on your main bus. > >> How does breaking one line from the 'dynamo' shut it down, or >> does it? Per this schematic power is required from the battery to >> close the OV disconnect relay and bring the 'dynamo' on-line. Thus >> with a dead battery there is no way to bring the 'dynamo' on-line? > > Right. But given what we know about the internals > of the rectifier regulator, it doesn't matter. It's > not self-exciting. I suspect we could do a "band-aid" > not unlike that which was developed for the SD-8 and > shown in the latest z-figures . . . but the proof-of- > concept study has not been accomplished for that > product. If you have a dead battery, the prudent > action is to recharge it from some ground based source > before you start the engine to go flying. > > Except for elimination of the fusible link and CB, > what you've proposed should work as advertised. > > > Bob . . . > > ----------------------------------------) > ( . . . a long habit of not thinking ) > ( a thing wrong, gives it a superficial ) > ( appearance of being right . . . ) > ( ) > ( -Thomas Paine 1776- ) > ---------------------------------------- >


    Message 2


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    Time: 07:39:02 AM PST US
    Subject: Re: Polyfuses
    From: "Radioflyer" <skyeyecorp@airpost.net>
    I'm late into this discussion, but have been wondering how to implement the polyfuses since I first read about them in Jim Weir's article and Blue Mountain's wiring guide. They are very attractive to me due to their compact size, inexpensiveness, and solid state reliability. Everyone agrees they perform as advertised. But, as others have stated, the packaging issue makes their use somewhat problematic, especially if you're interested in taking them offline, bypassing their auto-reset feature. What I would like to see is a polyfuse mounted into an ATC fuse shell, preferably one of those ATC types that have the LED already built in to indicate a fault. By so doing, you could use the readily available ATC fuse blocks, thereby retaining the option to simply pull the Polyfuse out when you need to. For my first attempt, I was going to try a little surgery on an ATC fuse package and epoxy a Polyfuse to it..., but I have not yet taken the chance to play with this. My guess is that it may be only a matter of time before some Taiwanese manufacturer starts putting polyfuses in the ATC fuse format. --Jose Read this topic online here: http://forums.matronics.com/viewtopic.php?p=234820#234820


    Message 3


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    Time: 07:40:44 AM PST US
    Subject: Anyone with a KR22 Marker Beacon pinout?
    From: "Radioflyer" <skyeyecorp@airpost.net>
    Can anyone point me to some KR-22 marker beacon receiver pinout info? I think I can figure out the antenna, power and audio out pins, but I would appreciate some confirmation before proceeding, just to make sure I get the grounds correct. --Jose Read this topic online here: http://forums.matronics.com/viewtopic.php?p=234821#234821


    Message 4


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    Time: 07:48:17 AM PST US
    From: Gilles Thesee <Gilles.Thesee@ac-grenoble.fr>
    Subject: Re: ectric-List:
    Robert L. Nuckolls, III a crit : > Some time back some fellows of your acquaintance were > exploring the thermal deficiencies in the stock Rotax/Ducati > rectifier regulator. > > Has that work evolved further than what's currently > described on your website? Hi Bob, That was some years ago, so part of the info may no longer be available : the researcher who helped me has changed assignment. I'll try to retrieve as much data as I can. Just give me a few days. Also, the parts we used may be lost. I'll see if someone has heard of them. Best regards, -- Gilles http://contrails.free.fr


    Message 5


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    Time: 08:03:15 AM PST US
    From: "galaxyone@juno.com" <galaxyone@juno.com>
    Subject: S-Tec 30 problem
    I have a Lancair with an S-Tec 30 auto pilot. It can be follow either a GNS 530 (with GPSS), or a SL 30. Initially it worked OK but has now deve loped a problem in the altitude hold mode. Most times it will drop out of altitude after 1-15 minutes and occasiona lly it will drop out as soon as it is engaged. It will not do this on th e ground, which makes it hard to diagnose what is wrong. I do not have a schematic for this unit, only the install manual. Two questions. Can some one point me to a site for the manual? Has anyone seen this kind of response from an S-Tec? ____________________________________________________________ Digital Photography - Click Now. http://thirdpartyoffers.juno.com/TGL2141/fc/BLSrjpTDvmQRLqGa6vHPLwyjHuJ3 82KmgG1ZiXKbI9qS8MJJFlHiX1YB9za/


    Message 6


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    Time: 08:20:38 AM PST US
    From: Jan de Jong <jan_de_jong@casema.nl>
    Subject: Re: AeroElectric-List Digest:
    Bob, Your question to Gilles regarding Rotax/Ducati regulator reminded me of something I mentioned on the Europa list last year. Maybe of use here, maybe not. ----- I think I found an interesting bit of forum: http://www.pilots24.com/pilots24/forum/viewtopic.php?t=7756&sid=542ce097cbdde3a5ceba2e5bd0d71c38 Scroll down to 40% of the page. Writer Arrow is convinced that he has found the problem with the 912/Ducati regulators, as follows. The regulating bridge has 4 elements: 2 power diodes MR2510 and 2 thyristors TP154E (obsolete) or 2N6504. One diode and one thyristor in series conduct part of one half sinus of the alternator output, the other diode and other thyristor in series conduct part of the other half sinus of the alternator output. The thyristors have TO220AB packaging and are mounted directly to the housing. The diodes have MICRODE BUTTON CASE 193 leadless packaging and Ducati designed a mounting technique: both diodes with their cathodes soldered to a small copper sheet, copper sheet mounted to the housing using silicone foil heat conducting isolation; wires to the PCB soldered to both anodes and the copper sheet. Everything potted with a potting compound. The problem is that heating/cooling cycles work the electrical connections to the diodes loose. The symptoms are as follows: charging ok after startup (13.8V), losing it after half an hour, but the warning light stays off. The writer has a diagnostic test using a battery and two 12V lamps to check continuity under heating. The writer has a solution: parallelling the diodes with an external pair. The writer has notified Rotax and asked them what they had done / were doing about the problem (January 2008). The correspondence can be followed at: http://www.pilots24.com/pilots24/forum/viewtopic.php?p=48297&highlight=#48297 Scroll 30% down. The upshot seems to be that Rotax knows there is a problem but it must be because units are operated above 80C. No redesign yet. ----- More translation from German if required... Regards, Jan de Jong


    Message 7


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    Time: 08:41:38 AM PST US
    From: "David LLoyd" <skywagon@charter.net>
    Subject: S-Tec 30 problem
    A couple of thoughts on your S-Tec A/P...... On your aircraft, I do not know where the pitch sensing static pressure ports are installed, however check them carefully for any kind of spider web, tiny wasp nest, etc. in the port hole. On Cessna's the pitch static ports (2) are aft on the fuselage sides. Check inside to make sure the plastic tubing to the ports are routed ok and not pinched or kinked. Cargo stuffed in the rear can shift and kink these lines or break them. You probably have 2 static sensing ports, one on each side for the pitch control computer. If your aircraft did a mild porpoise routine in pitch, I would mention to check control cable tensions, but, your model may not use cables. The pitch controller also uses clutches in the system, and maybe those have developed a problem. S-Tec at one time had a web link to their library of very good field notes mostly written by their own staff. I assume these are still linked to their web even though they were bought out by other firms. Their support staff was also quite good and would answer email. I am not familiar with the -30, however, I have heard it is a very nice A/P. I have used their -55 with GPSS for years and it is a winner. Holds altitude to better than 20 ft. If you have to have service performed, be sure to get references for a shop that "really" knows S-Tec products..... Let us know what you discover.... David ----- Original Message ----- From: galaxyone@juno.com To: aeroelectric-list@matronics.com Sent: Monday, March 16, 2009 7:57 AM Subject: AeroElectric-List: S-Tec 30 problem I have a Lancair with an S-Tec 30 auto pilot. It can be follow either a GNS 530 (with GPSS), or a SL 30. Initially it worked OK but has now developed a problem in the altitude hold mode. Most times it will drop out of altitude after 1-15 minutes and occasionally it will drop out as soon as it is engaged. It will not do this on the ground, which makes it hard to diagnose what is wrong. I do not have a schematic for this unit, only the install manual. Two questions. Can some one point me to a site for the manual? Has anyone seen this kind of response from an S-Tec? ____________________________________________________________ Digital Photography - Click Now.


    Message 8


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    Time: 08:46:13 AM PST US
    From: Don Morrisey <donmorrisey@hotmail.com>
    Subject: Question on Z-11, Main Buss Feed
    Howdy Listers=2C I am using Z-11 as the basis for my wiring architecture. My question is on the 6 AWG wire between the battery contactor and the main buss. In my ins tallation this wire will be running back through the firewall. Z-11 shows no protection for this wire but does show an ANL 60 current limiter between the starter contactor and the alternator. A similar VFR elec drawing on the B&C website shows the 6 AWG wire between the battery contactor and the main buss being protected with a ANL 60 curre nt limiter and also shows another ANL 60 current limiter between the starte r contactor and the alternator. So for this type of setup are two ANL 60's required or one??? Thanks. Don... www.donsbushcaddy.com _________________________________________________________________ Express your personality in color! Preview and select themes for Hotmail=AE . http://www.windowslive-hotmail.com/LearnMore/personalize.aspx?ocid=TXT_MS GTX_WL_HM_express_032009#colortheme


    Message 9


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    Time: 09:03:50 AM PST US
    Subject: Re: Polyfuses
    From: <longg@pjm.com>
    Jose, Would you bet your life on a floppy adaptation on your Lightspeed ignition? Perhaps yours is just cursory interest. I'm sure you can jam pennies in there if you like. There's no reason that would not work. Right now I am using Bob's proposed schematic which adds two in-line 30 amp fuses in front of two 5 amp breakers. He also considered two relays in place of the 30 amp ATC's. I guess my deal is how am I going to get at those 30 amp in-line fuses and still keep my eye on flying the airplane. I suppose if you blow two 30 amp fuses behind the two five amp breakers suggested by LSA, you're already in deep doo-doo. I wanted to ask Bob why the 30 amp fuse? Couldn't we get-a-way with something lighter, say 20 amp? Glenn -----Original Message----- From: owner-aeroelectric-list-server@matronics.com [mailto:owner-aeroelectric-list-server@matronics.com] On Behalf Of Radioflyer Sent: Monday, March 16, 2009 10:37 AM Subject: AeroElectric-List: Re: Polyfuses <skyeyecorp@airpost.net> I'm late into this discussion, but have been wondering how to implement the polyfuses since I first read about them in Jim Weir's article and Blue Mountain's wiring guide. They are very attractive to me due to their compact size, inexpensiveness, and solid state reliability. Everyone agrees they perform as advertised. But, as others have stated, the packaging issue makes their use somewhat problematic, especially if you're interested in taking them offline, bypassing their auto-reset feature. What I would like to see is a polyfuse mounted into an ATC fuse shell, preferably one of those ATC types that have the LED already built in to indicate a fault. By so doing, you could use the readily available ATC fuse blocks, thereby retaining the option to simply pull the Polyfuse out when you need to. For my first attempt, I was going to try a little surgery on an ATC fuse package and epoxy a Polyfuse to it..., but I have not yet taken the chance to play with this. My guess is that it may be only a matter of time before some Taiwanese manufacturer starts putting polyfuses in the ATC fuse format. --Jose Read this topic online here: http://forums.matronics.com/viewtopic.php?p=234820#234820


    Message 10


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    Time: 09:06:23 AM PST US
    From: "Ralph E. Capen" <recapen@earthlink.net>
    Subject: Re: S-Tec 30 problem
    I have a 'sorta-kinda' similar setup in my RV6A. The S-Tec 30 is connected to my GX60 through the S-Tec GPSS box which switches between the GX60 and my Century HSI. During my ground troubleshooting (I haven't tried it at altitude yet), I found a wire that had broken off right behind the solder connection - in the altitude control box. I'm not getting a clean signal from my HSI yet - that's the reasoning behind not trying it so far. How is your SL30 controlling the S-Tec 30? Is the autopilot dropping off-line or just the altitude hold part (blue-light)? If I recall correctly, the system holds altitude by sensing barometric pressure - this implies that if you go through a pressure change area, your altitude should be controlled to the original pressure altitude. I have the install manuals (scanned) and the charts (some scanned) that came with my system (two mergers ago). I don't know what part might help - but I'm willing to try. Ralph RV6A N822AR @ N06 5.9 hrs -----Original Message----- >From: "galaxyone@juno.com" <galaxyone@juno.com> >Sent: Mar 16, 2009 10:57 AM >To: aeroelectric-list@matronics.com >Subject: AeroElectric-List: S-Tec 30 problem > >I have a Lancair with an S-Tec 30 auto pilot. It can be follow either a GNS 530 (with GPSS), or a SL 30. Initially it worked OK but has now developed a problem in the altitude hold mode. >Most times it will drop out of altitude after 1-15 minutes and occasionally it will drop out as soon as it is engaged. It will not do this on the ground, which makes it hard to diagnose what is wrong. I do not have a schematic for this unit, only the install manual. >Two questions. >Can some one point me to a site for the manual? >Has anyone seen this kind of response from an S-Tec? >____________________________________________________________ >Digital Photography - Click Now. >http://thirdpartyoffers.juno.com/TGL2141/fc/BLSrjpTDvmQRLqGa6vHPLwyjHuJ382KmgG1ZiXKbI9qS8MJJFlHiX1YB9za/




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