X-Virus-Scanned: clean according to Sophos on Logan.com From: "Jeff Whaley" Received: from hub026-NJ-5.exch026.serverdata.net ([206.225.166.168] verified) by logan.com (CommuniGate Pro SMTP 6.0.9e) with ESMTPS id 6983590 for flyrotary@lancaironline.net; Thu, 17 Jul 2014 16:05:56 -0400 Received-SPF: none receiver=logan.com; client-ip=206.225.166.168; envelope-from=jwhaley@datacast.com Received: from MBX026-E1-NJ-2.exch026.domain.local ([10.240.14.52]) by HUB026-NJ-5.exch026.domain.local ([10.240.14.42]) with mapi id 14.03.0174.001; Thu, 17 Jul 2014 13:05:20 -0700 To: Rotary motors in aircraft Subject: RE: [FlyRotary] power circuit design, was: actual current use by a rotary? Thread-Topic: RE: [FlyRotary] power circuit design, was: actual current use by a rotary? Thread-Index: Ac+h+m6LnXAlEaV+RomYOnimlB+V0Q== Date: Thu, 17 Jul 2014 20:05:19 +0000 Message-ID: <234B758DE9A64449BEB6BB5D1345CA7A361ABD9F@mbx026-e1-nj-2.exch026.domain.local> Accept-Language: en-CA, en-US Content-Language: en-US X-MS-Has-Attach: yes X-MS-TNEF-Correlator: x-originating-ip: [209.87.232.162] Content-Type: multipart/related; boundary="_004_234B758DE9A64449BEB6BB5D1345CA7A361ABD9Fmbx026e1nj2exch_"; type="multipart/alternative" MIME-Version: 1.0 --_004_234B758DE9A64449BEB6BB5D1345CA7A361ABD9Fmbx026e1nj2exch_ Content-Type: multipart/alternative; boundary="_000_234B758DE9A64449BEB6BB5D1345CA7A361ABD9Fmbx026e1nj2exch_" --_000_234B758DE9A64449BEB6BB5D1345CA7A361ABD9Fmbx026e1nj2exch_ Content-Type: text/plain; charset="us-ascii" Content-Transfer-Encoding: quoted-printable I did similar to Steve, used 2 switchable fuses (5A) for the Injectors (1 P= RI and 2 SEC) with a separate cold-start switch as it was already there ...= I wanted/have to control it manually. I also used 2 separate switchable fuses (10A) for the ignition coils (1 ROT= 1 and 2 ROT2) ... my schematic of ignition and Main Electrical is below. Jeff [Ignition_13B] From: Rotary motors in aircraft on behalf of = Charlie England Sent: Thursday, July 17, 2014 12:14 PM To: Rotary motors in aircraft Subject: [FlyRotary] power circuit design, was: actual current use by a rot= ary? Charlie, I chose to install switch type circuit breakers, one for the primary inject= ors and one for the secondary injectors. I did this because if one injecto= r fails, the backup function requires the corresponding injector of the oth= er rotor to be shut off and then the cold function to be activated. If the= re were a power draw that tripped the breaker, the result would already tak= e care of that first step. The down side is that the cold switch needs to = be used for the backup function instead of being taken care of by the secon= d pole of the recommended DPDT injector switch. This required no additiona= l space on the panel. I did the same thing for the leading and trailing coils but for testing pur= poses rather than risk mitigation. Steve Boese RV6A, 1986 13B NA, RD1A, EC2 Well, time for some followup. My 1st draft for circuit protection looked a lot like what Steve describes = (thanks, Steve), with individual fuses for virtually everything, including = an individual fuse for each injector and each ignition coil. After ruminati= ng over the actual loads for the injectors & coils, I'm having second thoug= hts. The GM coil harness I have in hand has a single DC power wire for all = four coils that it feeds (obviously isn't a part intended for flight, but i= ncluded in Tracy's installation manual). The obvious concern is whether an individual coil or injector failure has a= statistically significant risk of taking out the power supply that's fused= for the total load. If there's no statistically significant danger, weight= & complexity could be reduced by feeding the coils and injectors as groups= . So, is there any consensus on how to handle injector & coil wiring? IIRC, t= here have been some coil failures in flight; were those planes wired with a= single fuse/breaker protecting all the coils, or with individual fuses/bre= akers for each coil? What about the injectors? Any failure modes I'm missing? (other than a dead short on a supply wire, o= f course) Thanks, Charlie This message, and the documents attached hereto, is intended only for the a= ddressee and may contain privileged or confidential information. Any unauth= orized disclosure is strictly prohibited. If you have received this message= in error, please notify us immediately so that we may correct our internal= records. Please then delete the original message. Thank you. --_000_234B758DE9A64449BEB6BB5D1345CA7A361ABD9Fmbx026e1nj2exch_ Content-Type: text/html; charset="us-ascii" Content-Transfer-Encoding: quoted-printable

I did similar to Steve, used 2 switchable fuses (5A)= for the Injectors (1 PRI and 2 SEC) with a separate cold-start switch as i= t was already there … I wanted/have to control it manually.

I also used 2 separate switchable fuses (10A) for th= e ignition coils (1 ROT1 and 2 ROT2) … my schematic of ignition and M= ain Electrical is below.

Jeff

 

3D"Ignition_13B"<= /o:p>

 

From: Rotary motors in aircraft <flyrotary@lancaironli= ne.net> on behalf of Charlie England <flyrotary@lancaironline.net>=
Sent: Thursday, July 17, 2014 12:14 PM
To: Rotary motors in aircraft
Subject: [FlyRotary] power circuit design, was: actual current use b= y a rotary?

 Charlie,

 

I chose to install switch type circu= it breakers, one for the primary injectors and one for the secondary inject= ors.  I did this because if one injector fails, the backup function requires the corresponding injector of the other rotor to be= shut off and then the cold function to be activated.  If there w= ere a power draw that tripped the breaker, the result would already take ca= re of that first step.  The down side is that the cold switch needs to be used for the backup function instead of being= taken care of by the second pole of the recommended DPDT injector switch.&= nbsp; This required no additional space on the panel.

 

I did the same thing for the leading= and trailing coils but for testing purposes rather than risk mitigation.

Steve Boese

RV6A, 1986 13B NA, RD1A, EC2<= /span>

 

 

 

Well, time for some followup.

My 1st draft for circuit protection looked a lot like what Steve describes = (thanks, Steve), with individual fuses for virtually everything, including = an individual fuse for each injector and each ignition coil. After ruminati= ng over the actual loads for the injectors & coils, I'm having second thoughts. The GM coil harness I h= ave in hand has a single DC power wire for all four coils that it feeds (ob= viously isn't a part intended for flight, but included in Tracy's installat= ion manual).

The obvious concern is whether an individual coil or injector failure has a= statistically significant risk of taking out the power supply that's fused= for the total load. If there's no statistically significant danger, weight= & complexity could be reduced by feeding the coils and injectors as groups.

So, is there any consensus on how to handle injector & coil wiring? IIR= C, there have been some coil failures in flight; were those planes wired wi= th a single fuse/breaker protecting all the coils, or with individual fuses= /breakers for each coil? What about the injectors?

Any failure modes I'm missing? (other than a dead short on a supply wire, o= f course)

Thanks,

Charlie

 

This message, and the documents attached hereto, is intended only for the a= ddressee and may contain privileged or confidential information. Any unauth= orized disclosure is strictly prohibited. If you have received this message= in error, please notify us immediately so that we may correct our internal records. Please then delete the origin= al message. Thank you. --_000_234B758DE9A64449BEB6BB5D1345CA7A361ABD9Fmbx026e1nj2exch_-- --_004_234B758DE9A64449BEB6BB5D1345CA7A361ABD9Fmbx026e1nj2exch_ Content-Type: image/png; name="image001.png" Content-Description: image001.png Content-Disposition: inline; filename="image001.png"; size=7384; creation-date="Thu, 17 Jul 2014 20:05:19 GMT"; modification-date="Thu, 17 Jul 2014 20:05:19 GMT" Content-ID: Content-Transfer-Encoding: base64 iVBORw0KGgoAAAANSUhEUgAAAeYAAAJ+CAMAAABRkFNOAAAAAXNSR0ICQMB9xQAAADxQTFRFAAAA AAAACggJBwYHBwYGTU1NfHx8aGhompqajIyMp6ensrKyvb292dnZx8fH0NDQ6enp8PDw4eHh//// 8P8R1wAAAAF0Uk5TAEDm2GYAAAAJcEhZcwAADsQAAA7EAZUrDhsAAAAZdEVYdFNvZnR3YXJlAE1p Y3Jvc29mdCBPZmZpY2V/7TVxAAAcA0lEQVR42u3dh2KjOrcFYK3z38ROMpl4wvu/63WhSEKAKmyJ xTmZOE4x5mOrF6V48ODBgwcPHjx4SDwA7aH2xePr8R/t8/wLHhUoa2SYfW9JlMy1Kb/CWRPF+CzG n5iee/6L58f0mId45Wc898CDOMZ/RvXhOfsLGtfA/DwGKy2ap6c1WWghDj3sfV7IeE3tAdxnpYYT GNMaHokRjQlYKTOQrQBW89D2QnCVAGB/w0pjhozDfSv0d6jzoOlSoOleryCbR/OQqKPPk1Uf9j7K 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