AeroElectric-List Digest Archive

Mon 01/18/16


Total Messages Posted: 2



Today's Message Index:
----------------------
 
     1. 03:17 PM - Re: Schematic for twin PM alternators (user9253)
     2. 08:06 PM - Re: Re: Schematic for twin PM alternators (ashleysc@broadstripe.net)
 
 
 


Message 1


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    Time: 03:17:08 PM PST US
    Subject: Re: Schematic for twin PM alternators
    From: "user9253" <fransew@gmail.com>
    B & C permanent magnet alternator schematic: http://www.bandc.aero/pdfs/420-506_revb.pdf > Please allow a 75 year old from New England, the home of > sarcastic humor, to note: So many e-mails entitled; "Schematic > for Twin PM Alternators." So few schematics actually presented. OK, I have attached another version. Design considerations: Rectifiers/Regulators get hot. Connecting two alternators to one rectifier/regulator could overheat it (when under heavy load). If the output of two separate rectifier/regulators are connected together, will the load be shared equally or will one be overworked and self destruct? If there is an over-voltage condition, how will the faulty regulator be identified and shut off quickly (in less than one second)? If one charging system fails, will the other one then be overloaded and fail also? Hundreds of Rotax powered aircraft are flying with modern glass panels and LED lighting powered by one 20 amp permanent-magnet dynamo (usually loaded to no more than 80 percent). The Revmaster should be able to do the same using one alternator at a time. An outbound leg can use the left alternator and the inbound leg can use the right alternator. The pilot will know that both systems work and there will always be a backup. -------- Joe Gores Read this topic online here: http://forums.matronics.com/viewtopic.php?p=452091#452091 Attachments: http://forums.matronics.com//files/revmaster3_492.pdf


    Message 2


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    Time: 08:06:09 PM PST US
    From: ashleysc@broadstripe.net
    Subject: Re: Schematic for twin PM alternators
    Hi Joe; Being internally regulated, each alternator has it's own regulator. I think I will probably wire so that only one is in use at a time. Cheers! Stu. ----- Original Message ----- From: "user9253" <fransew@gmail.com> Sent: Monday, January 18, 2016 3:08:51 PM Subject: AeroElectric-List: Re: Schematic for twin PM alternators B & C permanent magnet alternator schematic: http://www.bandc.aero/pdfs/420-506_revb.pdf > Please allow a 75 year old from New England, the home of > sarcastic humor, to note: So many e-mails entitled; "Schematic > for Twin PM Alternators." So few schematics actually presented. OK, I have attached another version. Design considerations: Rectifiers/Regulators get hot. Connecting two alternators to one rectifier/regulator could overheat it (when under heavy load). If the output of two separate rectifier/regulators are connected together, will the load be shared equally or will one be overworked and self destruct? If there is an over-voltage condition, how will the faulty regulator be identified and shut off quickly (in less than one second)? If one charging system fails, will the other one then be overloaded and fail also? Hundreds of Rotax powered aircraft are flying with modern glass panels and LED lighting powered by one 20 amp permanent-magnet dynamo (usually loaded to no more than 80 percent). The Revmaster should be able to do the same using one alternator at a time. An outbound leg can use the left alternator and the inbound leg can use the right alternator. The pilot will know that both systems work and there will always be a backup. -------- Joe Gores Read this topic online here: http://forums.matronics.com/viewtopic.php?p=452091#452091 Attachments: http://forums.matronics.com//files/revmaster3_492.pdf




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