X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Received: from nm8.access.bullet.mail.sp2.yahoo.com ([98.139.44.135] verified) by logan.com (CommuniGate Pro SMTP 5.4c3j) with SMTP id 4952706 for flyrotary@lancaironline.net; Wed, 20 Apr 2011 20:17:57 -0400 Received-SPF: none receiver=logan.com; client-ip=98.139.44.135; envelope-from=keltro@att.net Received: from [98.139.44.99] by nm8.access.bullet.mail.sp2.yahoo.com with NNFMP; 21 Apr 2011 00:17:23 -0000 Received: from [98.139.44.67] by tm4.access.bullet.mail.sp2.yahoo.com with NNFMP; 21 Apr 2011 00:17:23 -0000 Received: from [127.0.0.1] by omp1004.access.mail.sp2.yahoo.com with NNFMP; 21 Apr 2011 00:17:23 -0000 X-Yahoo-Newman-Property: ymail-3 X-Yahoo-Newman-Id: 186113.93142.bm@omp1004.access.mail.sp2.yahoo.com Received: (qmail 45962 invoked by uid 60001); 21 Apr 2011 00:17:23 -0000 DKIM-Signature: v=1; a=rsa-sha256; c=relaxed/relaxed; d=att.net; s=s1024; t=1303345043; bh=YnUPsgVBfWjrRHy2Y6S09oholgHJ6XemIPVaxTRSReU=; h=Message-ID:X-YMail-OSG:Received:X-Mailer:References:Date:From:Subject:To:In-Reply-To:MIME-Version:Content-Type; b=tIJt6sy5o/3yuIJnAZ6Pa0QCsVdEVBvjkbrf5mjDc12UMgPPlr/pN6usF0CLNzT9Zj2wxjV71Hkq9qXMCXb5TirzpVCTkxP6Ru0EckvVyPrBwQL1c3386JhBnIjnEVDidjHD/MDRN16HLPYfhyFLXu0F8NRCekE8LUid701LoRU= DomainKey-Signature:a=rsa-sha1; q=dns; c=nofws; s=s1024; d=att.net; h=Message-ID:X-YMail-OSG:Received:X-Mailer:References:Date:From:Subject:To:In-Reply-To:MIME-Version:Content-Type; b=oQq11jqWJfUCtRIcf7vYBqFGsuSp9ImnoA2hXAe7aFGQyJIOY5o9fkHtwdtFiNe7E2ZQAMmiBCzDiPnJEqnt1y/d03VmQ72HR+icUx9zC4JFVn/GH7hA2GK6REXcs+Dgo5ECwMXt1SCqLgE5SJnDPps3qMLxYIPHmAU3ugZbcbk=; Message-ID: <11427.32688.qm@web83904.mail.sp1.yahoo.com> X-YMail-OSG: vjmBAW8VM1myd2mHBkvL_IEaeVJKZ_HU0kOC0cY2D0ZSW_3 NEUyyC_3hCDZxs49Zs.PGn8pe9BfewdPiCEKPKRD0fgZgR7i43Hsx2UsGUfE HiIfFspYKMDSFGaWt_cenZLoubwfscnH3vl_MrqYjR7JogU9IKNj6AqLeeU. bI5V_sJtX.QGzqmun42paHscXyDI4OrKbX5fydL3ZwztRc8YhLgC_kCPCqDg MbhqR_2ZOeUnd9TOUinAy_hGcqbqv6Pzt3RnntJ_mSBuTOOP3qq1ufOJ4958 ddiw5TlxTkIJB2zC_8aEb15ZLtJazNWh6NDzg3DJ6q15pwD6Ndqv0y5aKADd v6p4cscvAQa_gzkpF Received: from [208.114.35.116] by web83904.mail.sp1.yahoo.com via HTTP; Wed, 20 Apr 2011 17:17:22 PDT X-Mailer: YahooMailRC/559 YahooMailWebService/0.8.109.295617 References: Date: Wed, 20 Apr 2011 17:17:22 -0700 (PDT) From: Kelly Troyer Subject: Re: [FlyRotary] 13B Rotary Timing & Leaning Procedure To: Rotary motors in aircraft In-Reply-To: MIME-Version: 1.0 Content-Type: multipart/mixed; boundary="0-898324051-1303345042=:32688" --0-898324051-1303345042=:32688 Content-Type: multipart/alternative; boundary="0-2027664775-1303345042=:32688" --0-2027664775-1303345042=:32688 Content-Type: text/plain; charset=iso-8859-1 Content-Transfer-Encoding: quoted-printable This will make it easier to print off a copy and save as a "ODT" (Open Offi= ce =0AText) document..........=0A=0AKelly Troyer=0A"DYKE DELTA JD2" (Eventu= ally)=0A"13B ROTARY"_ Engine=0A"RWS"_RD1C/EC2/EM2=0A"MISTRAL"_Backplate/Oil= Manifold=0A"TURBONETICS"_TO4E50 Turbo=0A=0A=0A=0A=0A______________________= __________=0AFrom: Kelly Troyer =0ATo: Rotary motors in air= craft =0ASent: Wed, April 20, 2011 6:45:49 PM= =0ASubject: [FlyRotary] 13B Rotary Timing & Leaning Procedure=0A=0A=0ARotor= heads we all need to "Copy , Save and or Memorize"=A0the post below from = =0ALynn...............IMHO=0A=A0=0AKelly Troyer=0A"DYKE DELTA JD2" (Eventua= lly)=0A"13B ROTARY"_ Engine=0A"RWS"_RD1C/EC2/EM2=0A"MISTRAL"_Backplate/Oil = Manifold=0A"TURBONETICS"_TO4E50 Turbo=0A=0A=0A=0A=0A_______________________= _________=0AFrom: "Lehanover@aol.com" =0ATo: Rotary moto= rs in aircraft =0ASent: Wed, April 20, 2011 5:= 42:11 PM=0ASubject: [FlyRotary] Re: My Mistral Engine Status=0A=0AYour "Fee= ble" mind is right on.=0A=A0=0APeak EGTs can get to near 2,000 degrees. Onl= y ceramic apex seals come back from =0Athat after more than a few seconds. = All of my comments apply to 12 A normally =0Aaspirated engines, but in gene= ral the data can be applied to other rotaries.=0A=0AThe object of lighting = the fuel in the confined space is to have the cylinder =0Apressure to =0A= =0Apeak at about 50 degrees after After Top Dead Center (ATDC). Think big p= iston, =0Ashort stroke. So it likes high revs to make power. =0A=0A=0AFrom = too rich to run to too lean to run is a bigger range than a piston engine. = =0A=A0The ideal power producing fire happens when the EGTs are just rich of= peak. =0APeak EGT is different on each engine, and is all over the map as = you tune the =0Aburn with timing changes, fuel type and octane and so-on. S= o you have to think =0Aabout what happens with each possible change you can= make. First, the EGT probes =0Aare in the outside of any bends, 3" from th= e port face. So the supersonic flow =0Apasses over the probes, and delivers= accurate combustion data. You may find =0Asubsonic flow returning to the p= ort=A0=0Aalong the short side radius, thus the need for the probe on the bo= ttom of the =0Apipe or outside of the turn. =0A=0A=A0=0AOnce at speed chang= ing the timing for a specific set of conditions, changes the =0Alocation of= peak pressure. In general you will be moving away from ideal, and =0Awatch= ing the revs with a fixed load will tell you this. More revs is better. So,= =0Asince an airplane is just a big expensive Dyno, you can dial up best re= vs with =0Atiming variations,=A0 =0A=0Aand then with that setting recorded,= you move mixture up and down until you get =0Abest revs again. Then go bac= k to timing and tune again. You are looking for the =0Abest combination of = settings not just a collection of best settings unrelated to =0Aeach other.= =0A=A0=0AThe low EGTs suggested are for maximum power while staying well ri= ch of peak. =0ASo for take off and fast climb you will be=A0producing close= to max power while =0Afuel cooling the engine and apex seals. It uses more= fuel and less engine life. =0ATo save fuel=0Ayou can lean quickly past pea= k EGT to well lean of peak for low fuel consumption =0Acruise. Again tune f= or this set of conditions. Since the fuel bits are further =0Aapart (Lean) = they tend to burn slower, so a bit more ignition advance can be =0Aused. Ke= ep leaning to lean miss, then back up rich a bit then add more advance =0Aa= nd lean again.=0A=A0=0AA monster ignition system can get you further into l= ean. Notice the low EGTs =0Aindicate low fuel consumption (and lower power)= .=0A=0ARemember the object is peak pressure at 50 degrees ATDC. =0A=0AEvery= thing affects everything.=A0The OAT, the pressure, humidity. And so-on. =0A= =A0=0AI can trick factory controllers and so can you. Measure the resistanc= e values of =0Athe sensors that the controller uses to determine fuel deliv= ery. Then get some =0ARadio Shack pots that cover that range top and bottom= . Install two DPDT switches =0Awith the controllers wires on the center lug= s, the sensor wires on one end and =0Athe pot wires on the other end. Now i= n one switch position the system is as =0Astock. In the other position=0Ath= e sensor is replaced with the pot, and you can change the value to tune the= =0Aengine.=0ANow if you should loose a sensor you have a backup. Once you = have this working, =0Areplace the Chinese crap with American pieces.=0A=A0= =0AThis is not to suggest that people driving "Show Room Stock" racers woul= d ever =0Astoop this low just to go fast. I would never do this. But if you= did, you would =0Ahide the switch in the heater ducting (they never look i= n the ducting) and use a =0Amagnetic switch, and turn it off on exiting the= car=A0with that magnet in the toe =0Aof your driving shoe. The idiot light= goes out when the switch is off and all is =0Astock again. Like taking can= dy from a baby.=0A=A0=0ALynn E. Hanover=0A=A0=0A=0AIn a message dated 4/20/= 2011 4:33:35 P.M. Atlantic Daylight Time, =0Aceengland@bellsouth.net writes= :=0AI wouldn't claim to have any hands-on experience with running a rotary = =0A>(except in cars), but 'normal' internal combustion engine EGTs would go= =0A>up as you lean, to a point, but should then start dropping as you =0A>= continue to lean. If your 'lean' setting is too rich, that might explain = =0A>both high EGT & high fuel consumption relative to HP. In my rather =0A>= feeble mind (based on conventional a/c engine experience), I'd expect =0A>'= rich' to yield slightly lower than max EGT for full power operation, =0A>an= d 'lean' to yield significantly lower than max EGT for cruise power =0A>set= tings.=0A>=0A>Unfortunately, no constructive thoughts on how to remedy the = situation =0A>if you're running Mistral's controller....=0A>=0A>Charlie=0A>= =0A>=0A> --0-2027664775-1303345042=:32688 Content-Type: text/html; charset=iso-8859-1 Content-Transfer-Encoding: quoted-printable
=0A
This will make it easier to print off a copy and sa= ve as a "ODT" (Open Office Text) document..........
=0A
 =0A

Kelly Troyer
"DYKE DELTA JD2" (Eventually)

=0A

"13B ROTARY"_ Engine
"R= WS"_RD1C/EC2/EM2
"MISTRAL"_Backplate/Oil Manifold

=0A

"TURBONETICS"= _TO4E50 Turbo

=0A

=0A

=0A
=0A
=0AFrom: Kelly Troyer <keltro@att.net>
To: Rotary motors in aircraft <flyrotary@lancaironli= ne.net>
Sent: Wed, Ap= ril 20, 2011 6:45:49 PM
Subject: [FlyRotary] 13B Rotary Timing & Leaning Procedure
=0A
=0A
=0A
Rotorheads we all need to "Copy , Save and or Mem= orize" the post below from Lynn...............IMHO
 
=0A<= P>Kelly Troyer
"DYKE DELTA JD2" (Eventually)

=0A

"13B ROTARY"_ Engine
"RWS"_RD= 1C/EC2/EM2
"MISTRAL"_Backplate/Oil Manifold

=0A

"TURBONETICS"_TO4E5= 0 Turbo

=0A

=0A

=0A
=0A
=0AFrom: = "Lehanover@aol.com" <Lehanover@aol.com>
To: Rotary motors in aircraft <flyrotary@lancairon= line.net>
Sent: Wed, = April 20, 2011 5:42:11 PM
Subject:<= /SPAN> [FlyRotary] Re: My Mistral Engine Status

=0A
Your "Feeble= " mind is right on.
=0A
 
=0A
Peak EGTs can get to near 2,000 degree= s. Only ceramic apex seals come back from that after more than a few second= s. All of my comments apply to 12 A normally aspirated engines, but in gene= ral the data can be applied to other rotaries.
=0A
 =0A
The object of lighting the fuel in the confined = space is to have the cylinder pressure to
=0A
peak at about 50 degrees after After Top Dead Center (ATDC). Think big= piston, short stroke. So it likes high revs to make power.
= =0A
 
=0A
From too rich to run to too lean= to run is a bigger range than a piston engine.  The ideal power producing fire happens when the EGTs are just rich of peak= . Peak EGT is different on each engine, and is all over the map as you tune= the burn with timing changes, fuel type and octane and so-on. So you have = to think about what happens with each possible change you can make. First, = the EGT probes are in the outside of any bends, 3" from the port face. So t= he supersonic flow passes over the probes, and delivers accurate combustion= data. You may find subsonic flow returning to the port 
= =0A
along the short side radius, thus the need for the p= robe on the bottom of the pipe or outside of the turn.
=0A 
=0A
Once at speed cha= nging the timing for a specific set of conditions, changes the location of = peak pressure. In general you will be moving away from ideal, and watching = the revs with a fixed load will tell you this. More revs is better. So, sin= ce an airplane is just a big expensive Dyno, you can dial up best revs with= timing variations, 
=0A
and then with= that setting recorded, you move mixture up and down until you get best rev= s again. Then go back to timing and tune again. You are looking for the bes= t combination of settings not just a collection of best settings unrelated = to each other.
=0A
 
=0AThe low EGTs suggested are for maximum power while staying= well rich of peak.
=0A
So for take off and= fast climb you will be producing close to max power while fuel coolin= g the engine and apex seals. It uses more fuel and less engine life. To sav= e fuel
=0A
you can lean quickly past peak EG= T to well lean of peak for low fuel consumption cruise. Again tune for this= set of conditions. Since the fuel bits are further apart (Lean) they tend = to burn slower, so a bit more ignition advance can be used. Keep leaning to= lean miss, then back up rich a bit then add more advance and lean again.
=0A
 
=0A
A monster ignition system can get you further into lean. Notice the low EG= Ts indicate low fuel consumption (and lower power).
=0A
&nb= sp;
=0A
Remember the object is peak pressure at 50 = degrees ATDC.
=0A
 
=0A
Every= thing affects everything. The OAT, the pressure,= humidity. And so-on.
=0A
 =0A
I can trick factory controllers and so can you. Me= asure the resistance values of the sensors that the controller uses to dete= rmine fuel delivery. Then get some Radio Shack pots that cover that range t= op and bottom. Install two DPDT switches with the controllers wires on the = center lugs, the sensor wires on one end and the pot wires on the other end= . Now in one switch position the system is as stock. In the other position<= /FONT>
=0A
the sensor is replaced with the pot, and= you can change the value to tune the engine.
=0A
Now if you should loose a sensor you have a backup. Once you have thi= s working, replace the Chinese crap with American pieces.
=0A 
=0A
This is not to = suggest that people driving "Show Room Stock" racers would ever stoop this = low just to go fast. I would never do this. But if you did, you would hide = the switch in the heater ducting (they never look in the ducting) and use a= magnetic switch, and turn it off on exiting the car with that magnet = in the toe of your driving shoe. The idiot light goes out when the switch i= s off and all is stock again. Like taking candy from a baby.
= =0A
 
=0A
Lynn E. Ha= nover
=0A
 
=0A
 <= /DIV>=0A
=0A
In a message dated 4/20/2011 4:33:35 P.M. Atlantic Day= light Time, ceengland@bellsouth.net writes:
=0A
I = wouldn't claim to have any hands-on experience with running a rotary
(e= xcept in cars), but 'normal' internal combustion engine EGTs would go
u= p as you lean, to a point, but should then start dropping as you
contin= ue to lean. If your 'lean' setting is too rich, that might explain
both= high EGT & high fuel consumption relative to HP. In my rather
feeb= le mind (based on conventional a/c engine experience), I'd expect
'rich= ' to yield slightly lower than max EGT for full power operation,
and 'l= ean' to yield significantly lower than max EGT for cruise power
setting= s.

Unfortunately, no constructive thoughts on how to remedy the situ= ation
if you're running Mistral's controller....

Charlie


=
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