X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Received: from omta2.toronto.rmgopenwave.com ([4.59.182.100] verified) by logan.com (CommuniGate Pro SMTP 5.3.9) with ESMTP id 4501876 for flyrotary@lancaironline.net; Mon, 11 Oct 2010 15:04:16 -0400 Received-SPF: pass receiver=logan.com; client-ip=4.59.182.100; envelope-from=lacombr@nbnet.nb.ca Received: from torspm02.toronto.rmgopenwave.com ([142.167.191.1]) by tormtz02.toronto.rmgopenwave.com (InterMail vM.8.00.01.00 201-2244-105-20090324) with ESMTP id <20101011190341.YKWG13337.tormtz02.toronto.rmgopenwave.com@torspm02.toronto.rmgopenwave.com> for ; Mon, 11 Oct 2010 15:03:41 -0400 Received: from PCdeRita ([142.167.191.1]) by torspm02.toronto.rmgopenwave.com with SMTP id <20101011190341.POUR12644.torspm02.toronto.rmgopenwave.com@PCdeRita> for ; Mon, 11 Oct 2010 15:03:41 -0400 Message-ID: From: "Rino" To: "Rotary motors in aircraft" References: In-Reply-To: Subject: Re: [FlyRotary] Re: Propeller design. Date: Mon, 11 Oct 2010 16:03:30 -0300 MIME-Version: 1.0 Content-Type: multipart/alternative; boundary="----=_NextPart_000_0030_01CB695D.D8F5BF10" X-Priority: 3 X-MSMail-Priority: Normal X-Mailer: Microsoft Windows Mail 6.0.6002.18197 X-MimeOLE: Produced By Microsoft MimeOLE V6.0.6002.18263 X-Opwv-CommTouchExtSvcRefID: str=0001.0A020207.4CB35F8D.01C0,ss=1,fgs=0 This is a multi-part message in MIME format. ------=_NextPart_000_0030_01CB695D.D8F5BF10 Content-Type: text/plain; charset="iso-8859-1" Content-Transfer-Encoding: quoted-printable I should be more precise. Full horsepower is about 165 at about 6300 = rpm and 15.5 usgph. Rino ----- Original Message -----=20 From: Rino=20 To: Rotary motors in aircraft=20 Sent: Monday, October 11, 2010 1:09 PM Subject: [FlyRotary] Re: Propeller design. One emergency water landing and one planned water landing. Good = takeoff at about 1700 lbs., gross weight is 1800 lbs. I had more work to = do on the plane and the pilot before getting to the Water landings and = takeoffs. It is next on the list, this fall. Engine temps is no problem here at this time of the year. I can do = full power, full time and engine temps stay below 200 deg. F. I = normally climb at 100 mph. I can climb at 80 mph with better vertical = speed but it is harder to keep the engine temp under control at that = speed. The upper wing incidence is an illusion because of the winglets. I = built the winglets for the fuel tank vents, it raises the vents a bit. = I do not remember the wing incidence but the two are very close if not = identical. Rino ----- Original Message -----=20 From: Bill Bradburry=20 To: Rotary motors in aircraft=20 Sent: Monday, October 11, 2010 11:00 AM Subject: [FlyRotary] Re: Propeller design. Congrats! Rino! =20 Have you tried a take off and landing on water yet? You were = getting a pretty steady climb rate of 1000 ft/min. I couldn't read the = temps and rpm on the EM-2 in the video. What were you getting? The two wings seemed to have very different angles of incidence. = What is up with that? =20 Bill B =20 -------------------------------------------------------------------------= --- From: Rotary motors in aircraft [mailto:flyrotary@lancaironline.net] = On Behalf Of Rino Sent: Sunday, October 10, 2010 8:52 PM To: Rotary motors in aircraft Subject: [FlyRotary] Re: Propeller design. =20 Anyone interested in seeing a takeoff and landing in a Renesis = powered Glass Goose go to the following YouTube site. =20 http://www.youtube.com/watch?v=3DR2xPPWD2-bE =20 Rino Lacombe Renesis powered Glass Goose =20 Search YouTube for Glass Goose for more videos. ------=_NextPart_000_0030_01CB695D.D8F5BF10 Content-Type: text/html; charset="iso-8859-1" Content-Transfer-Encoding: quoted-printable
I should be more precise.  Full = horsepower is=20 about 165 at about 6300 rpm and 15.5 usgph.
 
Rino
----- Original Message -----
From:=20 Rino
Sent: Monday, October 11, 2010 = 1:09=20 PM
Subject: [FlyRotary] Re: = Propeller=20 design.

One emergency water landing and one = planned water=20 landing.  Good takeoff at about 1700 lbs., gross weight is 1800 = lbs. I=20 had more work to do on the plane and the pilot before getting to the = Water=20 landings and takeoffs.  It is next on the list, this=20 fall.
 
Engine temps is no problem here at = this time of=20 the year. I can do full power, full time and engine temps stay below = 200 deg.=20 F.  I normally climb at 100 mph.  I can climb at 80 mph with = better=20 vertical speed but it is harder to keep the engine temp under control = at that=20 speed.
 
The upper wing incidence is an = illusion because=20 of the winglets.  I built the winglets for the fuel tank vents, = it raises=20 the vents a bit.  I do not remember the wing incidence but the = two are=20 very close if not identical.
 
Rino
----- Original Message -----
From:=20 Bill Bradburry
To: Rotary motors in = aircraft=20
Sent: Monday, October 11, = 2010 11:00=20 AM
Subject: [FlyRotary] Re: = Propeller=20 design.

Congrats! = Rino!

 

Have you = tried a=20 take off and landing on water yet?  You were getting a pretty = steady=20 climb rate of 1000 ft/min.  I couldn=92t read the temps and rpm = on the=20 EM-2 in the video.  What were you = getting?

The two = wings=20 seemed to have very different angles of incidence.  What is up = with=20 that?

 

Bill=20 B

 

From:=20 Rotary motors in = aircraft=20 [mailto:flyrotary@lancaironline.net] On=20 Behalf Of Rino
Sent: Sunday, October 10, = 2010 8:52=20 PM
To: = Rotary motors in aircraft
Subject: [FlyRotary] Re: = Propeller=20 design.

 

Anyone interested in = seeing a=20 takeoff and landing in a Renesis powered Glass Goose go to the = following=20 YouTube site.

 

http://www.youtube.= com/watch?v=3DR2xPPWD2-bE

 

Rino=20 Lacombe

Renesis powered Glass=20 Goose

 

Search YouTube for = Glass Goose=20 for more=20 videos.

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