X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Received: from cdptpa-omtalb.mail.rr.com ([75.180.132.121] verified) by logan.com (CommuniGate Pro SMTP 5.2c4) with ESMTP id 2635256 for flyrotary@lancaironline.net; Mon, 07 Jan 2008 19:12:51 -0500 Received-SPF: pass receiver=logan.com; client-ip=75.180.132.121; envelope-from=eanderson@carolina.rr.com Received: from edward2 ([24.74.103.61]) by cdptpa-omta04.mail.rr.com with SMTP id <20080108001210.TENN29372.cdptpa-omta04.mail.rr.com@edward2> for ; Tue, 8 Jan 2008 00:12:10 +0000 Message-ID: <001801c8518b$21680bb0$2402a8c0@edward2> From: "Ed Anderson" To: "Rotary motors in aircraft" References: Subject: Re: [FlyRotary] 60 Hour Inspecton Date: Mon, 7 Jan 2008 19:12:17 -0500 MIME-Version: 1.0 Content-Type: multipart/alternative; boundary="----=_NextPart_000_0015_01C85161.3851C660" X-Priority: 3 X-MSMail-Priority: Normal X-Mailer: Microsoft Outlook Express 6.00.2900.3138 X-MimeOLE: Produced By Microsoft MimeOLE V6.00.2900.3138 This is a multi-part message in MIME format. ------=_NextPart_000_0015_01C85161.3851C660 Content-Type: text/plain; charset="iso-8859-1" Content-Transfer-Encoding: quoted-printable Hey! Way to go! Dennis.=20 Sounds to me you have had a good 60 hours to prove the air worthiness of = your installation. Since the Hushmaster has been good for 40 hours on = my old turbo block 13B with the strongest exhaust pulses, I suspect it = will last a good long time on your Renesis. Great looking airframe and paint job as well. Hope you make it to Sun & = Fun! Ed=20 ----- Original Message -----=20 From: Dennis Haverlah=20 To: Rotary motors in aircraft=20 Sent: Monday, January 07, 2008 6:33 PM Subject: [FlyRotary] 60 Hour Inspecton 60 Hour Inspection : RV-7A, RX-8 Renesis engine, James Rotary Cowl, = Radiators under engine As of January 08 I've flown my Renesis powered RV-7A about 60 hours. = At the 60 hour mark I did a detailed inspection of the intake and = exhaust systems as well as everything else under the cowl.=20 I found no cracks or other problems with the exhaust system!! The = heat shield between the muffler and the left cowl had lost one = attachment screw- no big deal. Attached are pictures of the exhaust. I = use a stock RX-8 exhaust manifold - a 4 in dia. X approx. 6 inch long = swirl pipe(see third picture) to redirect the exhaust from the front to = the rear of the plane and a Flowmaster Hushpower Resonator (PN - = 12512400) as the exhaust muffler. Everyone who hears the airplane fly = comments on how quiet the engine is - neighbors call it the Stealth = Rotary RV! It is super quiet compared to my neighbors 180 Lycom. RV-7A. = I don't know if the Flowmaster muffler will withstand the exhaust = pulses from the RX-7 engine rotors but I feel confident the muffler will = work with the Renesis. Mark Steitle with his 20 B engine and Flowmaster = resonator will have first hand knowledge soon! I had previously found that one EGT probe extension wire melted - it = was about 8 inches from the exhaust system. The probe wires leads were = not damaged but the extension thermocouple wire from A/S had insulation = that melted from the exhaust heat. I have rerouted the extension wire = to keep it away from the exhaust.=20 There were no problems with the intake system. It is fabricated using = part of the RX-8 manifold and a home-made intake plenum. I used the = stock injectors, fuel rails and injector locations. The fuel pulse = damper was removed! (Pictures in next E-Mail) I did find several very small oil leaks in the casting of the PSRU. = I'll confer with Tracy as to how to address these.=20 I used the James Rotary Cowl - same one as the Power Sport rotary used = - mounted my oil and water radiators underneath the engine, bought an = engine from a wrecked RX-8 with less than 10,000 miles on it. The = engine was not disassembled. I also used (with some modifications) the = exhaust, intake, fuel injection parts, spark plugs, plug wires, coils, = 100 amp alternator, oil injecton with Richards adaptor, water pump and = water outlet system with the thermostat removed. (See attached pictures) I will be adding a cowl flap to keep the oil and water temps. cooler = in the hottest summer and warmer in the coldest winter temperatures. My prop is a Catto 76 in. dia X 88 in. pitch and my max. cruise rpm is = only 6200. I am over- propped for the HP currently being produced. = This does allow me to cruise at rpms around 5400 when I want to go = fairly fast and keep fuel flow down.=20 My intake and muffler systems could be improved to raise HP. I've = been flying side-by-side with my neighbors RV-7A with a Lyco. 180 HP = engine and a metal fixed pitch prop. At the same take-off weight we = climb about the same rate and in cruise we are about the same speed. I = believe I will be slightly faster above 8000 feet alt. in cruise. My success so far is in large part due to the contributions others = have made to my project by posting - their successes and failures, = thoughts, knowledge, suggestions and references to other sources - to = this list!!! A Special "Thank You" to Ed Anderson, Lynn Hanover, Al Gietzen and all = the other contributors for all the great knowledge they bring to the = rotary group! Dennis Haverlah -------------------------------------------------------------------------= ----- -------------------------------------------------------------------------= ----- -------------------------------------------------------------------------= ----- -------------------------------------------------------------------------= ----- -- Homepage: http://www.flyrotary.com/ Archive and UnSub: = http://mail.lancaironline.net:81/lists/flyrotary/List.html ------=_NextPart_000_0015_01C85161.3851C660 Content-Type: text/html; charset="iso-8859-1" Content-Transfer-Encoding: quoted-printable
Hey! Way to go! Dennis.
 
Sounds to me you have had a good 60 hours to = prove the air=20 worthiness of your installation.   Since the Hushmaster has = been good=20 for 40 hours on my old turbo block 13B with the strongest exhaust = pulses, I=20 suspect it will last a good long time on your Renesis.
 
Great looking airframe and paint job as = well.  Hope=20 you make it to Sun & Fun!
 
Ed 
----- Original Message -----
From:=20 Dennis Haverlah
Sent: Monday, January 07, 2008 = 6:33=20 PM
Subject: [FlyRotary] 60 Hour=20 Inspecton



60 Hour Inspection : RV-7A, RX-8 Renesis = engine, James=20 Rotary Cowl, Radiators under engine

As of January 08 I've flown = my=20 Renesis powered RV-7A about 60 hours.  At the 60 hour mark I did = a=20 detailed inspection of the intake and exhaust systems as well as = everything=20 else under the cowl.
I found no cracks or other problems with the = exhaust=20 system!!  The heat shield between the muffler and the left cowl = had lost=20 one attachment screw- no big deal.  Attached are pictures of the=20 exhaust.  I use a stock RX-8 exhaust manifold - a 4 in dia. X = approx. 6=20 inch long swirl pipe(see third picture) to redirect the exhaust from = the front=20 to the rear of the  plane and a Flowmaster Hushpower Resonator = (PN -=20 12512400) as the exhaust muffler.  Everyone who hears the = airplane fly=20 comments on how quiet the engine is - neighbors call it the Stealth = Rotary=20 RV!  It is super quiet compared to my neighbors 180 Lycom.=20 RV-7A.   I don't know if the Flowmaster muffler will = withstand the=20 exhaust pulses from the RX-7 engine rotors but I feel confident the = muffler=20 will work with the Renesis.  Mark Steitle with his 20 B engine = and=20 Flowmaster resonator will have first hand knowledge soon!

I had = previously found that one EGT probe extension wire melted - it was = about 8=20 inches from the exhaust system.  The probe wires leads = were not=20 damaged but the extension thermocouple wire from A/S had = insulation=20 that melted from the exhaust heat.  I have rerouted the extension = wire to=20 keep it away from the exhaust.

There were no problems with the = intake=20 system. It is fabricated  using part of the RX-8 manifold  = and a=20 home-made intake plenum.  I used the stock injectors, fuel rails = and=20 injector locations.  The fuel pulse damper was removed! (Pictures = in next=20 E-Mail)

I did find several very small oil leaks in the casting = of the=20 PSRU.  I'll confer with Tracy as to how to address these. =

I used=20 the James Rotary Cowl - same one as the Power Sport rotary used - = mounted my=20 oil and water radiators underneath the engine, bought an engine = from a=20 wrecked RX-8  with less than 10,000 miles on it.  The engine = was not=20 disassembled.   I also used (with some modifications) the = exhaust,=20 intake, fuel injection parts, spark plugs, plug wires, coils, 100 amp=20 alternator, oil injecton with Richards adaptor,  water pump and = water=20 outlet system with the thermostat removed. (See attached = pictures)

I=20 will be adding a cowl flap to keep the oil and water temps. cooler in = the=20 hottest summer and warmer in the coldest winter = temperatures.

My prop=20 is a Catto 76 in. dia X 88 in. pitch and my max. cruise rpm is only=20 6200.  I am over- propped for the HP currently being = produced.  This=20 does allow me to cruise at rpms around 5400 when I want to go fairly = fast and=20 keep fuel flow down.

My intake and muffler systems = could be=20 improved to raise HP.  I've been flying side-by-side with my = neighbors=20 RV-7A with a Lyco. 180 HP engine and a metal fixed pitch prop.  = At the=20 same take-off weight we climb about the same rate and in cruise we are = about=20 the same speed.  I believe I will be slightly faster above 8000 = feet alt.=20 in cruise.

My success so far is in large part due to the = contributions others have made to my project by posting - their = successes and=20 failures, thoughts, knowledge, suggestions  and references to = other=20 sources - to this list!!!

A Special "Thank You" to Ed Anderson, = Lynn=20 Hanover, Al Gietzen and all the other contributors  for all the = great=20 knowledge they bring to the rotary group!

Dennis Haverlah





--
Homepage:  http://www.flyrotary.com/
Archive and=20 UnSub:  =20 = http://mail.lancaironline.net:81/lists/flyrotary/List.html
------=_NextPart_000_0015_01C85161.3851C660--