X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Received: from rv-out-0506.google.com ([209.85.198.225] verified) by logan.com (CommuniGate Pro SMTP 5.2.12) with ESMTP id 3497645 for flyrotary@lancaironline.net; Tue, 17 Feb 2009 15:26:14 -0500 Received-SPF: pass receiver=logan.com; client-ip=209.85.198.225; envelope-from=wdleonard@gmail.com Received: by rv-out-0506.google.com with SMTP id b25so2420755rvf.7 for ; Tue, 17 Feb 2009 12:25:39 -0800 (PST) DKIM-Signature: v=1; a=rsa-sha256; c=relaxed/relaxed; d=gmail.com; s=gamma; h=domainkey-signature:mime-version:received:in-reply-to:references :date:message-id:subject:from:to:content-type; bh=9R5EUBWkc7L9OYQLQcoG/HJjhfGVw5OeE4QaLmJRWQc=; b=fNU+CWb5Kjd4Kjc8qBiu19WLpz61QAdVD5TqF1x115ncIUANRrygxpFKzQmNa049JL SBbPACfxQ9TvxrewjZVaqJ1ALWloDiNNccWb4auBLqX2LlIOm/7DBTlEeCIxAgxLQ0Tu WdnzukVWTJbRMHr4tvt106o7q77GOJimT3S5w= DomainKey-Signature: a=rsa-sha1; c=nofws; d=gmail.com; s=gamma; h=mime-version:in-reply-to:references:date:message-id:subject:from:to :content-type; b=txThDTJ/Mi8yI/CxtTOUQMOhxuFNTBf4BG+gryvA55r7GCHY+n9ba0izT+mh46DwvW i9s/qpUpZFtd/jIoqe4illv05OJIgHij4uchhDD5vdjsJ7mDRommYepusi/Nfg3tWUtj ZgsaK0LjTzsBXnXs2WsnX96tab3RxTV+/6o+4= MIME-Version: 1.0 Received: by 10.140.136.5 with SMTP id j5mr1006708rvd.167.1234902339533; Tue, 17 Feb 2009 12:25:39 -0800 (PST) In-Reply-To: References: Date: Tue, 17 Feb 2009 12:25:39 -0800 Message-ID: <1c23473f0902171225k52657cd8i7518b8c55b2f9560@mail.gmail.com> Subject: Re: [FlyRotary] Successful flight at last From: David Leonard To: Rotary motors in aircraft Content-Type: multipart/alternative; boundary=000e0cd2900e47ba800463231b2d --000e0cd2900e47ba800463231b2d Content-Type: text/plain; charset=windows-1252 Content-Transfer-Encoding: quoted-printable Hey Jeff, Many congrats! Sure must feel good to have a successful flight. Well done= ! --=20 David Leonard Turbo Rotary RV-6 N4VY http://N4VY.RotaryRoster.net http://RotaryRoster.net On Tue, Feb 17, 2009 at 10:01 AM, Jeff Whaley wrote: > On Saturday we made the first "successful" test flight of the rotary > engine installation. Previous flights had too high water temps and/or too > high oil temps and a low coolant pressure that sent us earthward early. T= he > OAT was 10F on this test flight; oil got a maximum of 190F and water neve= r > exceeded 170F. The coolant system was pre-pressurized to 16 LBs and prett= y > much stayed there. We circled the field on the upwind side for about 20 > minutes doing figure-8s. The oil was cycling between 180F and 190F; the > water was pegged at 160F. We decided to temperature-cycle the engine a fe= w > times to see what happened, so we did 2 touch and goes. Everything was go= od > =85 water would cool to about 130F and oil to about 160F on approach, as = we > climbed out the temperatures returned to W:160F and O:190F =85 I will mak= e a > few more refinements to the oil cooler inlet diffusers as 190F is still a > bit high. > > > > On another note I got in the left set finally for some taxi training =85 = not > too good =85 my big feet and the configuration of rudders/toe-brakes made= it > almost impossible to stay off the brakes when applying rudder =85 I'm goi= ng to > weld a tube at the rudder/brake lower pivot-point to ensure that first > contact is with rudder and some effort will be required to activate the > brakes. > > Jeff > > (happy, happy) > --000e0cd2900e47ba800463231b2d Content-Type: text/html; charset=windows-1252 Content-Transfer-Encoding: quoted-printable
Hey Jeff,
 
Many congrats!  Sure must feel good to have a successful flight.&= nbsp; Well done!
 
--
David Leonard

Turbo Rotary RV-6 N4VY
http://N4VY.RotaryRoster.net
http://RotaryRoster.net


On Tue, Feb 17, 2009 at 10:01 AM, Jeff Whaley <jwhaley@datacas= t.com> wrote:

On Saturday we made the first "successful" test flight of the rotary eng= ine installation. Previous flights had too high water temps and/or too high= oil temps and a low coolant pressure that sent us earthward early. The OAT= was 10F on this test flight; oil got a maximum of 190F and water never exc= eeded 170F. The coolant system was pre-pressurized to 16 LBs and pretty muc= h stayed there. We circled the field on the upwind side for about 20 minute= s doing figure-8s. The oil was cycling between 180F and 190F; the water was= pegged at 160F. We decided to temperature-cycle the engine a few times to = see what happened, so we did 2 touch and goes. Everything was good =85 wate= r would cool to about 130F and oil to about 160F on approach, as we climbed= out the temperatures returned to W:160F and O:190F =85 I will make a few m= ore refinements to the oil cooler inlet diffusers as 190F is still a bit hi= gh.

 

On another note I got in the left set finally for some taxi training =85= not too good =85 my big feet and the configuration of rudders/toe-brakes m= ade it almost impossible to stay off the brakes when applying rudder =85 I'= m going to weld a tube at the rudder/brake lower pivot-point to ensure that= first contact is with rudder and some effort will be required to activate = the brakes.

Jeff

(happy, happy)



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