X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Received: from relais.videotron.ca ([24.201.245.36] verified) by logan.com (CommuniGate Pro SMTP 5.2.0) with ESMTP id 2784137 for flyrotary@lancaironline.net; Sun, 09 Mar 2008 11:39:38 -0400 Received-SPF: pass receiver=logan.com; client-ip=24.201.245.36; envelope-from=jrmjoseph@videotron.ca MIME-version: 1.0 Content-type: multipart/alternative; boundary="Boundary_(ID_LKEqSREqX7RzQNSuNaQSnA)" Received: from vl-mo-mpf01.ip.videotron.ca ([10.23.37.50]) by VL-MO-MR003.ip.videotron.ca (Sun Java(tm) System Messaging Server 6.3-4.01 (built Aug 3 2007; 32bit)) with ESMTP id <0JXG00E7NZGZPWF0@VL-MO-MR003.ip.videotron.ca> for flyrotary@lancaironline.net; Sun, 09 Mar 2008 11:38:59 -0400 (EDT) Received: from videotron.ca (unknown [10.23.32.115]) by vl-mo-mpf01.ip.videotron.ca (Postfix) with ESMTP id 0748E294078 for ; Sun, 09 Mar 2008 11:38:59 -0400 (EDT) Received: from [10.23.32.85] (Forwarded-For: [10.23.32.85]) by VL-MO-MS011.ip.videotron.ca (mshttpd); Sun, 09 Mar 2008 15:38:59 +0000 (GMT) From: jrmjoseph@videotron.ca To: Rotary motors in aircraft Message-id: Date: Sun, 09 Mar 2008 15:38:59 +0000 (GMT) X-Mailer: Sun Java(tm) System Messenger Express 6.2-5.02 (built Dec 1 2005) Content-language: fr Subject: Re : [FlyRotary] Re: Anyone have an RD-1C for sale? X-Accept-Language: fr Priority: normal In-reply-to: References: This is a multi-part message in MIME format. --Boundary_(ID_LKEqSREqX7RzQNSuNaQSnA) Content-type: text/plain; charset=iso-8859-1 Content-transfer-encoding: quoted-printable Content-disposition: inline Yes a two rotor direct drive with hp between 80 and 120=2E For a CH701 = or another stol aircraft=2E This is the engine I=27m looking for=2E I = know of one person (cant remember his name) who built one using a 12A=2E= Marc J=2E ----- Message d=27origine ----- De=3A Tracy Crook =3Ctracy=40rotaryaviation=2Ecom=3E Date=3A Dimanche=2C Mars 9=2C 2008 11=3A30 am Objet=3A =5BFlyRotary=5D Re=3A Anyone have an RD-1C for sale=3F =C0=3A Rotary motors in aircraft =3Cflyrotary=40lancaironline=2Enet=3E =3E Damn Rusty=2C I=27d give anything for your organizational skills and= = =3E work habits =3E but darned if I can figure out your masochistic (sp=3F) = =3E tendencies on this =3E plane =3A=3E) One Rotor=3F=3F=3F=3F =3E = =3E Sure=2C that can work but why not something completely = =3E different=3F I want =3E to see someone do a direct drive 2 rotor (maybe even turboed) in = =3E the right =3E application and the RV-3 comes close=2E That would be Kool! =3E = =3E I know=2C everyone has their own idea of what=27s cool=2E Kick ass o= n = =3E whateveryou decide to do Rusty=2E =3E = =3E Tracy (making carbon fiber parts) =3E = =3E = =3E = =3E On Sun=2C Mar 9=2C 2008 at 1=3A04 AM=2C Russell Duffy = =3E wrote=3A =3E = =3E =3E Good one mate=2C I knew you couldn=27t let it go=2E =3E =3E =3E =3E Hi George=2C =3E =3E =3E =3E Well that certainly IS the problem=2E I was all set to bolt a = =3E Lycoming=3E on the RV-3=2C but I realize that what I need is a = =3E project=2C not a plane=2E =3E =3E Since there=27s no doubt a single will work for an RV-3=2C there= =27s = =3E really no =3E =3E reason not to do it=2E =3E =3E =3E =3E While it may seem wishy washy to go back to the RD-1C=2C the = =3E damper on the =3E =3E Autoflight drive didn=27t magically fix the resonance problem=2C= = =3E and the RV-3 =3E =3E has changed the power requirements=2E For previous aircraft=2C I= = =3E was only =3E =3E planning to have about 80 HP=2C and that would fall within the = =3E 6000 rpm limit =3E =3E of the Autoflight drive=2E Now that I can use as much power as = =3E I can make=2C I =3E =3E need more RPM=2E =3E =3E =3E =3E The offset thrust line of the Autoflight drive would have = =3E worked well for =3E =3E the previous aircraft I was considering=2C but not so well for = =3E the RV cowl=2E =3E =3E The mount plate on Tracy=27s drive is also really handy for moun= ting =3E =3E coolers for the RV cowl inlets=2E =3E =3E =3E =3E The Autoflight drive is about 12 lbs lighter IIRC=2C but I have = =3E the opposite =3E =3E problem with weight now=2E A single made from stock housings is = way =3E =3E overweight compared to 912S=2C but compared to an O-200 or O- =3E 235=2C it=27s just =3E =3E fine=2E Using stock housings will just limit you to aircraft = =3E that were =3E =3E designed for 100-125 HP LyConts=2E =3E =3E =3E =3E Finally=2C I really like the carbon fiber ground adjustable prop= that =3E =3E Sensenich makes=2C and the RD-1C rotates the proper direction to= = =3E use it=2E =3E =3E =3E =3E I should probably be more concerned with building the plane = =3E for now=2C but I =3E =3E can=27t help but think of engine stuff=2E I=27ve got a partial = =3E mount on order =3E =3E from the guys who make Van=27s mounts=2E I don=27t know if I=27l= l try = =3E to make a =3E =3E beam style mount=2C or use a sandwich plate similar to the old = =3E CCI mount=2E =3E =3E Either way=2C I=27ll size it to fit either the single rotor=2C o= r a = =3E two rotor as a =3E =3E fall back plan=2E =3E =3E =3E =3E Enough babbling for now=2E =3E =3E =3E =3E Rusty (watching the salt magically melt snow) =3E =3E =3E =3E =3E =3E =3E =3E =3E --Boundary_(ID_LKEqSREqX7RzQNSuNaQSnA) Content-type: text/html; charset=iso-8859-1 Content-transfer-encoding: quoted-printable Content-disposition: inline =3CDIV=3EYes a two rotor direct drive with hp between 80 and 120=2E=26nb= sp=3B For a CH701 or another stol aircraft=2E=26nbsp=3B This is the engi= ne I=27m looking for=2E=26nbsp=3B I know of one person (cant remember hi= s name) who built one using a 12A=2E=3C/DIV=3E =3CDIV=3E=26nbsp=3B=3C/DIV=3E =3CDIV=3EMarc J=2E=3CBR=3E=3CBR=3E----- Message d=27origine -----=3CBR=3E= De=3A Tracy Crook =26lt=3Btracy=40rotaryaviation=2Ecom=26gt=3B=3CBR=3EDa= te=3A Dimanche=2C Mars 9=2C 2008 11=3A30 am=3CBR=3EObjet=3A =5BFlyRotary= =5D Re=3A Anyone have an RD-1C for sale=3F=3CBR=3E=C0=3A Rotary motors i= n aircraft =26lt=3Bflyrotary=40lancaironline=2Enet=26gt=3B=3CBR=3E=3CBR=3E= =26gt=3B Damn Rusty=2C I=27d give anything for your organizational skill= s and =3CBR=3E=26gt=3B work habits=3CBR=3E=26gt=3B but darned if I can f= igure out your masochistic (sp=3F) =3CBR=3E=26gt=3B tendencies on this=3C= BR=3E=26gt=3B plane =3A=26gt=3B) One Rotor=3F=3F=3F=3F=3CBR=3E=26gt=3B =3C= BR=3E=26gt=3B Sure=2C that can work but why not something completely =3C= BR=3E=26gt=3B different=3F I want=3CBR=3E=26gt=3B to see someone do a di= rect drive 2 rotor (maybe even turboed) in =3CBR=3E=26gt=3B the right=3C= BR=3E=26gt=3B application and the RV-3 comes close=2E That would be Kool= !=3CBR=3E=26gt=3B =3CBR=3E=26gt=3B I know=2C everyone has their own idea= of what=27s cool=2E Kick ass on =3CBR=3E=26gt=3B whateveryou decide to = do Rusty=2E=3CBR=3E=26gt=3B =3CBR=3E=26gt=3B Tracy (making carbon fiber = parts)=3CBR=3E=26gt=3B =3CBR=3E=26gt=3B =3CBR=3E=26gt=3B =3CBR=3E=26gt=3B= On Sun=2C Mar 9=2C 2008 at 1=3A04 AM=2C Russell Duffy =3CBR=3E=26gt=3B = =3CRUSTY=40RADROTARY=2ECOM=3Ewrote=3A=3CBR=3E=26gt=3B =3CBR=3E=26gt=3B =26= gt=3B Good one mate=2C I knew you couldn=27t let it go=2E=3CBR=3E=26gt=3B= =26gt=3B=3CBR=3E=26gt=3B =26gt=3B Hi George=2C=3CBR=3E=26gt=3B =26gt=3B= =3CBR=3E=26gt=3B =26gt=3B Well that certainly IS the problem=2E I was al= l set to bolt a =3CBR=3E=26gt=3B Lycoming=26gt=3B on the RV-3=2C but I r= ealize that what I need is a =3CBR=3E=26gt=3B project=2C not a plane=2E=3C= BR=3E=26gt=3B =26gt=3B Since there=27s no doubt a single will work for a= n RV-3=2C there=27s =3CBR=3E=26gt=3B really no=3CBR=3E=26gt=3B =26gt=3B = reason not to do it=2E=3CBR=3E=26gt=3B =26gt=3B=3CBR=3E=26gt=3B =26gt=3B= While it may seem wishy washy to go back to the RD-1C=2C the =3CBR=3E=26= gt=3B damper on the=3CBR=3E=26gt=3B =26gt=3B Autoflight drive didn=27t m= agically fix the resonance problem=2C =3CBR=3E=26gt=3B and the RV-3=3CBR= =3E=26gt=3B =26gt=3B has changed the power requirements=2E For previous = aircraft=2C I =3CBR=3E=26gt=3B was only=3CBR=3E=26gt=3B =26gt=3B plannin= g to have about 80 HP=2C and that would fall within the =3CBR=3E=26gt=3B= 6000 rpm limit=3CBR=3E=26gt=3B =26gt=3B of the Autoflight drive=2E Now = that I can use as much power as =3CBR=3E=26gt=3B I can make=2C I=3CBR=3E= =26gt=3B =26gt=3B need more RPM=2E=3CBR=3E=26gt=3B =26gt=3B=3CBR=3E=26gt= =3B =26gt=3B The offset thrust line of the Autoflight drive would have =3C= BR=3E=26gt=3B worked well for=3CBR=3E=26gt=3B =26gt=3B the previous airc= raft I was considering=2C but not so well for =3CBR=3E=26gt=3B the RV co= wl=2E=3CBR=3E=26gt=3B =26gt=3B The mount plate on Tracy=27s drive is als= o really handy for mounting=3CBR=3E=26gt=3B =26gt=3B coolers for the RV = cowl inlets=2E=3CBR=3E=26gt=3B =26gt=3B=3CBR=3E=26gt=3B =26gt=3B The Aut= oflight drive is about 12 lbs lighter IIRC=2C but I have =3CBR=3E=26gt=3B= the opposite=3CBR=3E=26gt=3B =26gt=3B problem with weight now=2E A sing= le made from stock housings is way=3CBR=3E=26gt=3B =26gt=3B overweight c= ompared to 912S=2C but compared to an O-200 or O-=3CBR=3E=26gt=3B 235=2C= it=27s just=3CBR=3E=26gt=3B =26gt=3B fine=2E Using stock housings will = just limit you to aircraft =3CBR=3E=26gt=3B that were=3CBR=3E=26gt=3B =26= gt=3B designed for 100-125 HP LyConts=2E=3CBR=3E=26gt=3B =26gt=3B=3CBR=3E= =26gt=3B =26gt=3B Finally=2C I really like the carbon fiber ground adjus= table prop that=3CBR=3E=26gt=3B =26gt=3B Sensenich makes=2C and the RD-1= C rotates the proper direction to =3CBR=3E=26gt=3B use it=2E=3CBR=3E=26g= t=3B =26gt=3B=3CBR=3E=26gt=3B =26gt=3B I should probably be more concern= ed with building the plane =3CBR=3E=26gt=3B for now=2C but I=3CBR=3E=26g= t=3B =26gt=3B can=27t help but think of engine stuff=2E I=27ve got a par= tial =3CBR=3E=26gt=3B mount on order=3CBR=3E=26gt=3B =26gt=3B from the g= uys who make Van=27s mounts=2E I don=27t know if I=27ll try =3CBR=3E=26g= t=3B to make a=3CBR=3E=26gt=3B =26gt=3B beam style mount=2C or use a san= dwich plate similar to the old =3CBR=3E=26gt=3B CCI mount=2E=3CBR=3E=26g= t=3B =26gt=3B Either way=2C I=27ll size it to fit either the single roto= r=2C or a =3CBR=3E=26gt=3B two rotor as a=3CBR=3E=26gt=3B =26gt=3B fall = back plan=2E=3CBR=3E=26gt=3B =26gt=3B=3CBR=3E=26gt=3B =26gt=3B Enough ba= bbling for now=2E=3CBR=3E=26gt=3B =26gt=3B=3CBR=3E=26gt=3B =26gt=3B Rust= y (watching the salt magically melt snow)=3CBR=3E=26gt=3B =26gt=3B=3CBR=3E= =26gt=3B =26gt=3B=3CBR=3E=26gt=3B =26gt=3B=3CBR=3E=26gt=3B =26gt=3B=3CBR= =3E=26gt=3B =3C/DIV=3E --Boundary_(ID_LKEqSREqX7RzQNSuNaQSnA)--