X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Received: from [216.211.128.10] (HELO mail-in03.adhost.com) by logan.com (CommuniGate Pro SMTP 5.1c.2) with ESMTP id 1302116 for flyrotary@lancaironline.net; Sat, 05 Aug 2006 11:01:23 -0400 Received-SPF: none receiver=logan.com; client-ip=216.211.128.10; envelope-from=joeh@pilgrimtech.com Received: from Pilgrim10 (c-67-183-14-47.hsd1.wa.comcast.net [67.183.14.47]) by mail-in03.adhost.com (Postfix) with ESMTP id 606F42AA231 for ; Sat, 5 Aug 2006 08:01:06 -0700 (PDT) (envelope-from joeh@pilgrimtech.com) From: "Joe Hull" To: "'Rotary motors in aircraft'" Subject: RE: ***SPAM*** [FlyRotary] It's officially an airplane Date: Sat, 5 Aug 2006 07:59:21 -0700 Message-ID: <007d01c6b89f$c7d53f30$bb02a8c0@redmond.corp.microsoft.com> MIME-Version: 1.0 Content-Type: multipart/alternative; boundary="----=_NextPart_000_007E_01C6B865.1B766730" X-Mailer: Microsoft Office Outlook 11 X-MimeOLE: Produced By Microsoft MimeOLE V6.00.2900.2869 Thread-Index: Aca4nc3fva0JyBYoRFiXADbmmJH24AAAXSyA In-Reply-To: This is a multi-part message in MIME format. ------=_NextPart_000_007E_01C6B865.1B766730 Content-Type: text/plain; charset="us-ascii" Content-Transfer-Encoding: 7bit Hey Al, CONGRATULATIONS! That's a MAJOR milestone in the development of N755V. On the oil cooling - you've probably checked this - but after my experience - make sure you have oil flowing through the cooler (i.e. thermostat working properly, Input on the lowest hole, output on the highest hole). I don't want you to repeat my folly! Keep us posted! Joe Hull Cozy Mk-IV N31CZ (65 hrs - Rotary 13B NA) Redmond (Seattle), Washington _____ From: Rotary motors in aircraft [mailto:flyrotary@lancaironline.net] On Behalf Of Al Gietzen Sent: Saturday, August 05, 2006 7:45 AM To: Rotary motors in aircraft Subject: ***SPAM*** [FlyRotary] It's officially an airplane A high speed nose lift; a high speed crow hop; and finally off and away around the pattern; the 20B powered Velocity, N755V maid its maiden flight yesterday, 8/04/06. What an exciting milestone - even though in this case I was watching from the ground as the test pilot did his thing. The engine performed well, and the pilot reported that all handling characteristics were good. The flight was short, however; because the oil temp was 10-15F higher than the limit I had set, and the pilot did the right thing in abbreviating the flight so that can be evaluated and changes made as necessary. All in all, with that as the only issue of note at this point; it was a good day. It's such a common thing, isn't it - these cooling issues. The oil temp (downstream from the cooler) peaked at 230F, somewhat after the end of the climb (OAT about 80F); I guess it takes a little while for the hot oil to get to the bottom of the 8 qt sump and back through the cooler. The main concern was that the temp didn't drop more that 3-4 degrees as he went around the pattern, and after landing and rolling out it was still 225F. Coolant temps peaked about 190F. I had a video camera mounted reading the engine monitor display which is great for review later. Unfortunately, even though I have all sorts of instrumentation for doing diagnostics, in his focusing on flight characteristics, and the concern about the high oil temp the pilot forgot to push the 'page up' button; so the only data I have is page 1. Regardless of further data, it seems clear that there is insufficient air flow through the wing root oil cooler - a condition that was not entirely unexpected. Another major step in an on-going process. Al ------=_NextPart_000_007E_01C6B865.1B766730 Content-Type: text/html; charset="us-ascii" Content-Transfer-Encoding: quoted-printable

Hey Al, CONGRATULATIONS! = That’s a MAJOR milestone in the development of = N755V.

 

On the oil cooling – = you’ve probably checked this – but after my experience – make sure = you have oil flowing through the cooler (i.e. thermostat working properly, = Input on the lowest hole, output on the highest hole). I don’t want you to = repeat my folly!

 

Keep us = posted!

 

Joe = Hull

Cozy Mk-IV N31CZ (65 hrs - Rotary = 13B NA)

Redmond (Seattle), Washington

 


From: = Rotary motors in aircraft = [mailto:flyrotary@lancaironline.net] On Behalf Of Al = Gietzen
Sent: Saturday, August = 05, 2006 7:45 AM
To: Rotary motors in aircraft
Subject: ***SPAM*** = [FlyRotary] It's officially an airplane

 

A high speed nose lift; a high speed crow hop; and = finally off and away around the pattern; the 20B powered Velocity, N755V maid = its maiden flight yesterday, 8/04/06.  What an exciting milestone = – even though in this case I was watching from the ground as the test pilot did = his thing.

 

The engine performed well, and the pilot reported = that all handling characteristics were good.  The flight was short, however; because the oil temp was 10-15F higher than the limit I had set, and the = pilot did the right thing in abbreviating the flight so that can be evaluated and = changes made as necessary.  All in all, with that as the only issue of note = at this point; it was a good day.

 

It’s such a common thing, isn’t it = – these cooling issues.  The oil temp (downstream from the cooler) = peaked at 230F, somewhat after the end of the climb (OAT about 80F); I guess it = takes a little while for the hot oil to get to the bottom of the 8 qt sump and = back through the cooler.  The main concern was that the temp = didn’t drop more that 3-4 degrees as he went around the pattern, and after landing = and rolling out it was still 225F.  Coolant temps peaked about = 190F.

 

I had a video camera mounted reading the engine = monitor display which is great for review later.  Unfortunately, even = though I have all sorts of instrumentation for doing diagnostics, in his focusing = on flight characteristics, and the concern about the high oil temp the = pilot forgot to push the ‘page up’ button; so the only data I have = is page 1.  Regardless of further data, it seems clear that there is insufficient air flow through the wing root oil cooler – a = condition that was not entirely unexpected.

 

Another major step in an on-going = process.

 

Al

 

 

 

 

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