Mailing List flyrotary@lancaironline.net Message #58939
From: <hoursaway1@comcast.net>
Subject: Re: [FlyRotary] Re: FIRST FLIGHT N655HC
Date: Sun, 2 Sep 2012 15:17:40 +0000 (UTC)
To: Rotary motors in aircraft <flyrotary@lancaironline.net>
On the pusher/rear eng. aircraft the air leaking  " OUT " from around the spinner/cowl area sounds like it would not be an issue, one more area for cowl pressure to escape then just follow the spinner back away.  David 


From: "Ernest Christley" <echristley@att.net>
To: "Rotary motors in aircraft" <flyrotary@lancaironline.net>
Sent: Friday, August 31, 2012 1:15:37 PM
Subject: [FlyRotary] Re: FIRST FLIGHT N655HC

The area between the cowl and spinner on my plane is used for intake air.  I seal the cowl to PSRU mount plate with 2" wide silicone baffling that is slitted every 1" to be more flexible.  Each slit ends in a 1/8th inch hole I punched to stop it from tearing all the way through.  It is riveted to the cowl.



Bill Bradburry <bbradburry@bellsouth.net> wrote:

>I didn't see any input when I last asked this question, so I will try now
>that we are again talking about cooling.
>
>
>
>How are you sealing around the PSRU outlet on the cowl?  I am talking about
>the area behind the spinner.  This area allows air to enter behind the heat
>exchangers and it seems to me that it would adversely affect cooling.  This
>area is open on my plane because I haven't figured out how to seal it.  I am
>wondering what others have done?
>
>
>
>Bill B
>
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>
>  _____  
>
>From: Rotary motors in aircraft [mailto:flyrotary@lancaironline.net] On
>Behalf Of Ed Anderson
>Sent: Friday, August 31, 2012 11:56 AM
>To: Rotary motors in aircraft
>Subject: [FlyRotary] Re: FIRST FLIGHT N655HC
>
>
>
>Congratulations David,
>
>
>
>I would completely seal any leaks around the sides or anyplace else that
>could leak between duct inlet and radiator.  I read someplace that a
>1/2"square hole could cost you 20% of your cooling effectiveness.  
>
>
>
>A gent who once sold Subaru engine installations tried just sticking the
>radiator in back of the opening (no ducting) - did not cool.
>
>
>
>Yes, I find that getting the airflow up as soon as safely possible will help
>a great deal in keeping temps down and bring them back down quickly.  My
>magic airspeed after take off is 120 MPH IAS then a 140 IAS for climbout.
>
>
>
>Looking forward to more reports
>
>
>
>Ed
>
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>
>From: Ernest Chrisltey <mailto:echristley@att.net>  
>
>Sent: Friday, August 31, 2012 11:01 AM
>
>To: Rotary <mailto:flyrotary@lancaironline.net>  motors in aircraft
>
>Subject: [FlyRotary] Re: FIRST FLIGHT N655HC
>
>
>
>Congratulations, David.  I hope to be following you soon.
>
>Are you able to cool on the ground?  What did you do to improve the cooling
>between the two flights?
>
>
>On 08/30/2012 10:48 PM, hoursaway1@comcast.net wrote:
>
>Thanks Mark, it was kind of anti-climatic for the others on the ground
>because they already saw that last month, but for me seeing the temps coming
>down at about the same stage as Terry saw them still climbing was
>comforting.  I'm setting up a video camera to record the panel so I can
>focus on flying for now until I get more comfortable.  We have a 100 mile
>radius to work with & I asked for & was granted a crew member during the
>flights that computer tuning will be worked on.  Tryed to get a stewardess
>also but FAA said no.  ????    Yes I read Ed's procedure for takeoff & our
>sys. is very similar so will use for next flights.  Terry is a member of our
>EAA Chapter 55 here in Mason MI,  his dad just flew his 400 th Young Eagle.
>(  where is that stewardess with my Margarita )          David.
>
>
>  _____  
>
>
>From: "Mark Steitle"  <mailto:msteitle@gmail.com> <msteitle@gmail.com>
>To: "Rotary motors in aircraft"  <mailto:flyrotary@lancaironline.net>
><flyrotary@lancaironline.net>
>Sent: Thursday, August 30, 2012 7:44:53 PM
>Subject: [FlyRotary] Re: FIRST FLIGHT N655HC
>
>David,  
>
>
>
>Congrats!!!  Job well done.  Terry Lutz... WOW!  
>
>
>
>What was the OAT?  I start to get nervous when my coolant temp goes above
>200 F.  No reason to climb at WOT if not needed and OAT is high.  
>
>
>
>Mark S.  
>
>On Thu, Aug 30, 2012 at 6:07 PM, <hoursaway1@comcast.net> wrote:
>
>First flight for me anyhow not for the aircraft, Terry Lutz ( AKA;;  world
>renowned professional test pilot, flew in from France to do the First, First
>flight )
>Temps went;;   coolant 221 F  max,  oil 210 F  max,  on full throttle clime
>out up to 2000 ft., powered back from 6300 rpm to 5000 rpm/135 mph
>indicated, push the nose over to level off, pulled power back to 4500 rpm  (
>made no prop pitch changes at this time )   temps went down to;;   coolant
>195 F,  oil 190 F,  this is without therm. & bypass blocked, also would like
>comments about sealing around sides of both radiators, we saw the extra fins
>there so we allowed air to pass through that area, may install a temp seal &
>recheck data points next flight. Then possibly install venting openings in
>bottom of cowl to let more airflow out quicker.   David  R. Cook  RV6A
>Rotary.
>
>
>  _____  
>
>
>From: "Joseph Pirch" <pirch@sbcglobal.net>
>To: hoursaway1@comcast.net, "rv man2010" <rv.man2010@hotmail.com>
>Sent: Wednesday, August 29, 2012 8:40:58 PM
>
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>Sent from my iPad
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>No virus found in this message.
>Checked by AVG - www.avg.com
>Version: 2012.0.2197 / Virus Database: 2437/5237 - Release Date: 08/31/12
>
 
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