AeroElectric-List Digest Archive

Sat 03/31/12


Total Messages Posted: 11



Today's Message Index:
----------------------
 
     1. 07:10 AM - St Patrick's Day (RV7ASask)
     2. 09:05 AM - Re: Uneven dipole elements (Noel Loveys)
     3. 11:30 AM - motorcycle coolant sensor question (Sheldon Olesen)
     4. 12:10 PM - Re: motorcycle coolant sensor question (Robert L. Nuckolls, III)
     5. 12:21 PM - Re: St Patrick's Day (Robert L. Nuckolls, III)
     6. 12:23 PM - Re: Uneven dipole elements (Robert L. Nuckolls, III)
     7. 01:00 PM - Re: motorcycle coolant sensor question (rayj)
     8. 06:31 PM - Re: motorcycle coolant sensor question (Robert L. Nuckolls, III)
     9. 06:34 PM - Re: LED WigWag with B&C SSF-1 (Robert L. Nuckolls, III)
    10. 08:13 PM - Re: motorcycle coolant sensor question (rayj)
    11. 08:52 PM - Re: LED WigWag with B&C SSF-1 (B Tomm)
 
 
 


Message 1


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    Time: 07:10:59 AM PST US
    Subject: St Patrick's Day
    From: "RV7ASask" <rv7alamb@sasktel.net>
    I would like to thank Bob for sharing his knowledge, for his patience, guidance and the Aeroelectric course I took in North Carolina about four years ago. Also, thanks to all the other forum contributors from whom I have gleaned so much. On St Patricks Day, 17 March 2012, in Tisdale, Saskatchewan, with sunny skies, light wind and 8 degrees C, RV7A, C-FLAM flew for the first time. It was nine years in construction and worth every moment. The aircraft flew exactly as I hoped it would. It has an Aero Sport IO-360 with dual Light Speeds and dual alternators. The electrical architecture is Bobs Z12 and I am very happy with the final results. On the panel there is a Dynon Skyview and four Garmins, a GDU370, SL30, GTX327 and GMA340. An iPad 2 is mounted with a Ram mount and has checklists, charts, POH and more. My grandson says he will be able to play Angry Birds on the long hauls. Thanks again to everyone. Warmest regards David Lamb Read this topic online here: http://forums.matronics.com/viewtopic.php?p=369684#369684


    Message 2


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    Time: 09:05:23 AM PST US
    From: "Noel Loveys" <noelloveys@yahoo.ca>
    Subject: Uneven dipole elements
    Bob: Thanks for explaining the shortened shield on the coax. Sa soon as I saw your diagram I immediately wondered why only 14". Noel From: owner-aeroelectric-list-server@matronics.com [mailto:owner-aeroelectric-list-server@matronics.com] On Behalf Of Robert L. Nuckolls, III Sent: March 31, 2012 2:06 AM Subject: RE: AeroElectric-List: Uneven dipole elements At 06:46 PM 3/30/2012, you wrote: I'm wondering if it is now operating like a modified Windom antenna (not straight at centre and different length elements). I also would like to know if it is vertical or horizontal This would be a vertically polarized antenna and appears to be 1/2 wavelength. Is there enough 'bulk' at the coax end to house a small toroid transformer? There's another 1/2-wave kid on the block which is actually a center-fed dipole with the feedline running up the middle of the lower half of the dipole. It's marketed as the Air Whip at http://miracleantenna.com/shop-products/aviation/42 <http://miracleantenna.com/shop-products/aviation/42> Emacs! The black box houses the common-mode choke which de-couples the feed line from the high-voltage end of the dipole thusly. http://tinyurl.com/78ph8nz http://tinyurl.com/6ul4o6f Waaayyy back when, there was a brief brush with tiny toroids to match coax feedlines to center fed dipoles the cores they used were very low power handling . . . hence good for receive only. The Antenna Dynamics product has the look and 'smell' of a similar product. By the way, the reason it's not 44" (half wave in free space) long is because the lower 1/4 wave is in coax which is shortened to about 14" by the coax velocity factor. Miracle Antenna is a newer kid on the block and gets very good reviews from their whole customer base which includes amateur radio and SWL applications. Dave, is there any chance you can get the remnants of the old antenna out? Putting one of these in it's place would be a prudent move. If that's not practical/possible, then splicing an extension on the upper end to replace the cut off length would be helpful . . . even if it lays off at right angles to the antenna. This would serve as an extension moving back toward 1/4 wave for the upper element and/or 'capacity' hat to load the shortened antenna thus making it look electrically like a quarter wave. Your antenna guy will know all about this and will be able to help you with the patch. Bob . . .


    Message 3


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    Time: 11:30:51 AM PST US
    Subject: motorcycle coolant sensor question
    From: Sheldon Olesen <saolesen@sirentel.net>
    Can a single coolant temperature sensor be used to send temp data to two different units, an engine control unit and display unit? My son is building a self designed racing bike and I have been placed in charge the electrical system. Sheldon Olesen N475PV RV-10 Sent from my iPad


    Message 4


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    Time: 12:10:29 PM PST US
    From: "Robert L. Nuckolls, III" <nuckolls.bob@aeroelectric.com>
    Subject: Re: motorcycle coolant sensor question
    At 01:25 PM 3/31/2012, you wrote: ><saolesen@sirentel.net> > >Can a single coolant temperature sensor be used to send temp data to >two different units, an engine control unit and display unit? My >son is building a self designed racing bike and I have been placed >in charge the electrical system. It depends. To find the answer you need to know what the characteristics are for the sensor -AND- the circuitry that watches it. Legacy temperature sensors are thermistors . . . a resistor that changes value in a predictable and repeatable way depending on surrounding temperature. A newer device is an integrated circuit which generally offers more user friendly, linear signals. How are these two temperature inputs to be used? Is the 'sensor' already part of the suite of components for one of the data users . . . and you have a second user that wants to eavesdrop on the data? Sensing temperature in a meaningful way is really easy. It might be better that each system have its own sensor tailored to its technology. Have you crafted a power/data distribution diagram? Suggest you start with emulating one of the z-figures and do a pen-to-paper actualization of your design goals. Then do a similar drawing that speaks to control and signal lines while identifying the systems and parts KNOWN to be compatible with their function. At Beech this was called a system interface document. It was a drawing of wire bundles PLUS a table of inputs and outputs from each device along with gains, offsets, and scale factors for signals expected and offered. If you had such a set of documents to share, I and others here on the List can be more specific in our advice. Bur right now, there's not enough data in your question to give a reliable answer. Bob . . .


    Message 5


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    Time: 12:21:35 PM PST US
    From: "Robert L. Nuckolls, III" <nuckolls.bob@aeroelectric.com>
    Subject: Re: St Patrick's Day
    At 09:09 AM 3/31/2012, you wrote: > >I would like to thank Bob for sharing his >knowledge, for his patience, guidance and the >Aeroelectric course I took in North Carolina >about four years ago. Also, thanks to all the >other forum contributors from whom I have gleaned so much. > >On St Patricks Day, 17 March 2012, in >Tisdale, Saskatchewan, with sunny skies, light >wind and 8 degrees C, RV7A, C-FLAM flew for the >first time. It was nine years in construction >and worth every moment. The aircraft flew >exactly as I hoped it would. It has an Aero >Sport IO-360 with dual Light Speeds and dual >alternators. The electrical architecture is >Bobs Z12 and I am very happy with the final results. > > On the panel there is a Dynon Skyview and four > Garmins, a GDU370, SL30, GTX327 and GMA340. An > iPad 2 is mounted with a Ram mount and has > checklists, charts, POH and more. My grandson > says he will be able to play Angry Birds on the long hauls. That seminar was in Winterville, NC in the spring of 2007. You've come a long way my friend. How about a picture of your airplane . . . preferably with yourself included? For that matter, it would be interesting to add a page to aeroelectric.com for pictures of List Member's airplanes. Email to me directly along with basic particulars including date of first flight. Congratulations! Bob . . .


    Message 6


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    Time: 12:23:41 PM PST US
    From: "Robert L. Nuckolls, III" <nuckolls.bob@aeroelectric.com>
    Subject: Re: Uneven dipole elements
    At 01:33 AM 3/31/2012, you wrote: >We found a diagram of what we think the antenna >looks like. I'll post of a picture of it next >week at the latest. It's a slanted-N shape similar to an Archer. > >Earlier I described equal-length parallel >elements. Turns out they're carbon >reinforcements that aren't part of the >antenna. I'll show them in the picture when I post it. How much of the structure/skin around this antenna is carbon? Buried antennas in carbon aircraft typically don't do real well. Fiberglas/epoxy is okay but the carbon is both conductive as well as dissipative . . . in other words it turns a portion of your signal into heat. Bob . . .


    Message 7


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    Time: 01:00:59 PM PST US
    From: rayj <raymondj@frontiernet.net>
    Subject: Re: motorcycle coolant sensor question
    Greetings Bob, Could you point to a simple example of the document you recommend? To provide some idea how others have done it. do not archive Thanks, Raymond Julian Kettle River, MN "And you know that I could have me a million more friends, and all I'd have to lose is my point of view." - John Prine On 03/31/2012 02:05 PM, Robert L. Nuckolls, III wrote: > <nuckolls.bob@aeroelectric.com> > > At 01:25 PM 3/31/2012, you wrote: >> <saolesen@sirentel.net> snip > > At Beech this was called a system interface document. > It was a drawing of wire bundles PLUS a table of inputs > and outputs from each device along with gains, offsets, > and scale factors for signals expected and offered. > snip


    Message 8


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    Time: 06:31:12 PM PST US
    From: "Robert L. Nuckolls, III" <nuckolls.bob@aeroelectric.com>
    Subject: Re: motorcycle coolant sensor question
    At 02:57 PM 3/31/2012, you wrote: > >Greetings Bob, > >Could you point to a simple example of the document you >recommend? To provide some idea how others have done it. > >do not archive Sure, check the Z-figures . . . in particular one that uses a PM alternator. Z-16 is probably good http://tinyurl.com/7vp9g4e You wont need an e-bus but if you have electronic ignition, then you'll need to accommodate that. The system interface document is simply a schematic of all the black boxes, sensors and how they connect to each other. But in particular, you need to KNOW the nature of the sensor data and whether or not two different client systems can listen to the same sensor. That will take some detective work on your part. Do you have installation diagrams for the proposed clients? Bob . . .


    Message 9


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    Time: 06:34:02 PM PST US
    From: "Robert L. Nuckolls, III" <nuckolls.bob@aeroelectric.com>
    Subject: Re: LED WigWag with B&C SSF-1
    At 06:19 PM 3/30/2012, you wrote: > >Bob, can I wire two LED landing and taxi lights per Page 3.0 (Ref DE >12/15/11) but using a single switch (already installed and labeled >in unflown RV-6) as shown on Page 3.0 from 2003? Thank you Give me a few days on this. It occurs to me that I've been twisting what WAS a good system for incandescent lamps into a pretzel in search of the elegant solution for LED lamps. I'm going to do a clean-piece-of-paper study of some alternatives to the automotive flasher. Given the very low current draw and insignificant inrush for the LED lamps, some sort of all solid state approach is called for. I think some others here on the List have mentioned their own adventures in this arena. Perhaps they'll share. In any case, there's a cleaner way to go about it and so the answer is "Yes, we can use the single switch configuration you've already installed." Bob . . .


    Message 10


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    Time: 08:13:23 PM PST US
    From: rayj <raymondj@frontiernet.net>
    Subject: Re: motorcycle coolant sensor question
    A little mix up perhaps. I was just asking for an example of an interface document for my own information. Sometimes organizing the info. is half the battle. I like to see how others have solved a problem. I guess I was expecting something with:"a table of inputs and outputs from each device along with gains, offsets, and scale factors for signals expected and offered." Sorry about the mix up. do not archive Raymond Julian Kettle River, MN "And you know that I could have me a million more friends, and all I'd have to lose is my point of view." - John Prine On 03/31/2012 08:29 PM, Robert L. Nuckolls, III wrote: > <nuckolls.bob@aeroelectric.com> > > At 02:57 PM 3/31/2012, you wrote: >> <raymondj@frontiernet.net> >> >> Greetings Bob, >> >> Could you point to a simple example of the document you recommend? >> To provide some idea how others have done it. >> >> do not archive > > Sure, check the Z-figures . . . in particular one that uses a PM > alternator. Z-16 is probably good > > http://tinyurl.com/7vp9g4e > > You wont need an e-bus but if you have electronic ignition, then > you'll need to accommodate that. > > The system interface document is simply a schematic of all the black > boxes, sensors and how they connect to each other. But in particular, > you need to KNOW the nature of the sensor data and whether or not two > different client systems can listen to the same sensor. That will > take some detective work on your part. > > Do you have installation diagrams for the proposed clients? > > > Bob . . . > > http://www.matronics.com/contribution > >


    Message 11


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    Time: 08:52:32 PM PST US
    From: "B Tomm" <fvalarm@rapidnet.net>
    Subject: LED WigWag with B&C SSF-1
    I used a ETHFSS-SP with my HID landing lights as other on VAF have suggested. I can have them both on or flashing mode. Should work with LED's I would think see... http://www.bestwarninglights.com/m7/ETHFSS-SP--sound-off-signal-select-a-pat tern-headlight-flasher-positive-switching.html $48 so not cheap but solid state and good for up to 55W per side. Bevan -----Original Message----- From: owner-aeroelectric-list-server@matronics.com [mailto:owner-aeroelectric-list-server@matronics.com] On Behalf Of Robert L. Nuckolls, III Sent: Saturday, March 31, 2012 6:33 PM Subject: Re: AeroElectric-List: LED WigWag with B&C SSF-1 --> <nuckolls.bob@aeroelectric.com> At 06:19 PM 3/30/2012, you wrote: >--> <ashuramj@hotmail.com> > >Bob, can I wire two LED landing and taxi lights per Page 3.0 (Ref DE >12/15/11) but using a single switch (already installed and labeled in >unflown RV-6) as shown on Page 3.0 from 2003? Thank you Give me a few days on this. It occurs to me that I've been twisting what WAS a good system for incandescent lamps into a pretzel in search of the elegant solution for LED lamps. I'm going to do a clean-piece-of-paper study of some alternatives to the automotive flasher. Given the very low current draw and insignificant inrush for the LED lamps, some sort of all solid state approach is called for. I think some others here on the List have mentioned their own adventures in this arena. Perhaps they'll share. In any case, there's a cleaner way to go about it and so the answer is "Yes, we can use the single switch configuration you've already installed." Bob . . .




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