X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Received: from fed1rmfepo101.cox.net ([68.230.241.143] verified) by logan.com (CommuniGate Pro SMTP 5.4c2) with ESMTP id 4905474 for flyrotary@lancaironline.net; Mon, 14 Mar 2011 02:25:50 -0400 Received-SPF: none receiver=logan.com; client-ip=68.230.241.143; envelope-from=alventures@cox.net Received: from fed1rmimpo03.cox.net ([70.169.32.75]) by fed1rmfepo101.cox.net (InterMail vM.8.01.04.00 201-2260-137-20101110) with ESMTP id <20110314062513.KCFU17030.fed1rmfepo101.cox.net@fed1rmimpo03.cox.net> for ; Mon, 14 Mar 2011 02:25:13 -0400 Received: from BigAl ([72.199.216.14]) by fed1rmimpo03.cox.net with bizsmtp id JuRD1g0080KDB3c04uRD6p; Mon, 14 Mar 2011 02:25:13 -0400 X-VR-Score: -100.00 X-Authority-Analysis: v=1.1 cv=+7g07FftAVK5SzfBDSzY8IJIWiAWL38p2qa3Op/8zMo= c=1 sm=1 a=X9gsYuSiZwkA:10 a=TPvrVRyicAsl4VeEYn0L5g==:17 a=Ia-xEzejAAAA:8 a=aqbCFVM2AAAA:8 a=RMaiJEGVAAAA:8 a=iksI56yM9MmthiV4A4IA:9 a=1q-Dx6sfbIfWnsm_z8UA:7 a=Ydg4XpxlTBoSysat2Jw-3mP6UK4A:4 a=CjuIK1q_8ugA:10 a=dw6XmgibHwQA:10 a=tXcarIeGnVYA:10 a=E0nWgSthiVIA:10 a=FeQN90nXSYAA:10 a=EzXvWhQp4_cA:10 a=c9EzqnwR0tUA:10 a=FGINFF-h6CuWHrWI:21 a=5din_Fh2gsz1XGQs:21 a=KxuMX9wriy7cr_ggqZIA:9 a=7Kth1rNKrJLkzmxsB-wA:7 a=6YBQKiAjiLjaZl6E0a7fLorvS1QA:4 a=jHEDC6EaesKvcm2UKUMA:9 a=FhoxTsrB6iqwc-YyRmEfBay3tOwA:4 a=1Vq_FK4TplAA:10 a=2UObvGdkA9g9R0zms_4A:9 a=TPvrVRyicAsl4VeEYn0L5g==:117 X-CM-Score: 0.00 Authentication-Results: cox.net; none From: "Al Gietzen" To: "'Rotary motors in aircraft'" Subject: RE: [FlyRotary] Re: Marcotte PSRU vs 550HP Turbo/20B Date: Sun, 13 Mar 2011 23:24:52 -0800 Message-ID: MIME-Version: 1.0 Content-Type: multipart/related; boundary="----=_NextPart_000_0020_01CBE1D5.DAF034D0" X-Priority: 3 (Normal) X-MSMail-Priority: Normal X-Mailer: Microsoft Outlook, Build 10.0.6863 In-Reply-To: Importance: Normal Thread-Index: Acvh4xSfYa4v1aPNRseHhh1ltLgy8wAMzRsg X-MimeOLE: Produced By Microsoft MimeOLE V6.00.2900.5994 This is a multi-part message in MIME format. ------=_NextPart_000_0020_01CBE1D5.DAF034D0 Content-Type: multipart/alternative; boundary="----=_NextPart_001_0021_01CBE1D5.DAF034D0" ------=_NextPart_001_0021_01CBE1D5.DAF034D0 Content-Type: text/plain; charset="us-ascii" Content-Transfer-Encoding: quoted-printable . However on my application it is actually a plus. How much HP do you estimate on your Velocity?=20 Tom Mine is ormally aspirated with the 9:1 rotors. Before break-in, the = dyno runs gave WOT power (corrected to sea level, standard day) shown below. = Max prop rpm is 3000 (6500 engine); so 'rated' power is 275 hp. But then of course we never fly at sea level. Takeoff WOT climb is typically less = than 250 hp; cruise power at altitude more like 150 hp. That gets me lean = cruise of 170 KTAS at 10 gph. Quite satisfactory. On Mar 13, 2011, at 9:41 PM, Al Gietzen wrote: Tom; =20 I have no comment about the quality/capacity of the Marcotte; but I = think the 2.4 ratio is a good one. I had considered the Marcotte for that = reason, but liked the in-line drive of the planetary, and had more confidence in Tracy's overall design and coupling design. =20 Al (Velocity 20B; 210 hours and counting) =20 -----Original Message----- From: Rotary motors in aircraft [mailto:flyrotary@lancaironline.net] On Behalf Of Thomas Giddings Sent: Sunday, March 13, 2011 11:37 AM To: Rotary motors in aircraft Subject: [FlyRotary] Re: Marcotte PSRU vs 550HP Turbo/20B =20 Thanks Kelly for the reply...Guy Marcotte claims 600HP is not a = problem....I would really like to hear from others with first hand knowledge...I just read of his PSRU being used on a Glassair /Suburu project. They had = broken the gear ,but it was from a prop strike...I am gathering up what I need = to mock this up in the Airframe and need to make a decision on it fairly soon...Honestly I had made my mind up it was the best choice for my application . Tom Giddings VP Avionics Sales MIDWEST AVIONICS 200 Hardy Roberts Dr PO Box 219 West Paducah,KY 42086 877-904 9966 Cell; 727 858-1772 FAX:270 744 3466 tom@midwestaviation.net Online Store www.midwest-avionics.com =20 On Mar 13, 2011, at 3:15 PM, Kelly Troyer wrote: =20 Thomas, What HP rating is Marcotte claiming for his PSRU ?...............From the experience of a few users on this group and others using product have reported it seems to have a checkered operational and maintenance history..............John of this group (13B/Marcotte in Tailwind) reported a problem he had to resolve not long ago..............John jump in here and give Thomas = your experience and if you think this PSRU will stand up to a Turbo/20B of about 550+ = HP..................I personally would have severe reservations about the Marcotte at that power level..............FWIW =20 =20 Kelly Troyer "DYKE DELTA JD2" (Eventually) "13B ROTARY"_ Engine "RWS"_RD1C/EC2/EM2 "MISTRAL"_Backplate/Oil Manifold "TURBONETICS"_TO4E50 Turbo =20 =20 _____ =20 From: Thomas Giddings To: Rotary motors in aircraft Sent: Sun, March 13, 2011 1:37:10 PM Subject: [FlyRotary] Re: Crankcase ventilation Does anyone have any experience using a 2.40 gear reduction on the 20B? = I am going to use the Marcotte PSRU only because he has a much higher HP = Rating and it is only offered in the 2.40 ratio in the configuration I am = using. However I notice everyone uses the 2.85 more commonly. Is there a = specific reason why this would be better for the 20B?. I would appreciate any = input any of you might have to offer. =20 Kind Regards Tom=20 =20 =20 =20 ------=_NextPart_001_0021_01CBE1D5.DAF034D0 Content-Type: text/html; charset="us-ascii" Content-Transfer-Encoding: quoted-printable

. However on my application it is actually a = plus. How much HP do you estimate on your Velocity? 

Tom

Mine is ormally aspirated with the 9:1 rotors.  Before break-in, the = dyno runs gave WOT power (corrected to sea level, standard day) shown below.  Max = prop rpm is 3000 (6500 engine); so ‘rated’ power is 275 hp.  = But then of course we never fly at sea level. Takeoff WOT climb is typically = less than 250 hp; cruise power at altitude more like 150 hp. That gets me = lean cruise of 170 KTAS at 10 gph. Quite satisfactory.

On Mar 13, 2011, at 9:41 PM, Al = Gietzen wrote:



Tom;

 

I have no comment about the quality/capacity of the Marcotte; but I think = the 2.4 ratio is a good one. I had considered the Marcotte for that reason, but = liked the in-line drive of the planetary, and had more confidence in Tracy’s overall design and coupling = design.

 

Al (Velocity 20B; 210 hours = and counting)

 

-----Original = Message-----
From: Rotary motors in aircraft [mailto:flyrotary@lancaironline.net] On Behalf Of Thomas Giddings
Sent: 
Sunday, March 13, 2011 11:37 = AM
To: Rotary motors in aircraft
Subject: [FlyRotary] Re: Marcotte PSRU = vs 550HP Turbo/20B

 

Thanks Kelly for the reply...Guy Marcotte = claims 600HP is not a problem....I would really like to hear from others with first = hand knowledge...I just read of his PSRU being used on a Glassair /Suburu = project. They had broken the gear ,but it was from a prop strike...I am gathering = up what I need to mock this up in the Airframe and need to make a decision = on it fairly soon...Honestly I had made my mind up it was the best choice for = my application .

Tom Gid= dings
VP Avionics Sales

MIDWEST AVIONICS
200 Hardy
Roberts = Dr
PO Box 219
West = Paducah,KY 42086=
877-904 9966
Cell; 727 858-1772
FAX:270 744 3466
tom@midwestaviation.net


<image001.jpg>

 

On Mar 13, 2011, at 3:15 PM, = Kelly Troyer wrote:

 

Thomas,

    &nbs= p;   What HP rating is Marcotte claiming for his PSRU ?...............From the experience of a few = users

on this group and = others using product have reported it seems to have a checkered = operational and

maintenance history..............John of this group (13B/Marcotte in Tailwind) = reported a problem he had

to resolve not long ago..............John jump in here and give Thomas your experience and = if you think

this PSRU will stand up to = a Turbo/20B of about 550+ HP..................I personally would have = severe

reservations about the = Marcotte at that power level..............FWIW

 
 

Kelly Troyer
"DYKE DELTA = JD2" (Eventually)

"13B ROTARY"_ Engine
"RWS"_RD1C/EC2/EM2
"MISTRAL"_Backplate/Oil Manifold

"TURBONETICS"_TO4E50 = Turbo

 

 

 

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