RE: Hartzell Composite Three blade RPM Test


Subject:    RE: Hartzell Composite Three blade RPM Test
From:    Rene Felker (rene@felker.com)
Date:    Wed Sep 03 - 4:05 PM
Boy, I really feel slow now......

12,500
12.2 GPH Rich of peak
2480 RPM
161 knots (TAS from GRT)

My speed test at 8000 feet and 75% power showed about 171......but I have
not seen speeds like that in cruise at 12500.


Rene' Felker
RV-10 N423CF Flying
801-721-6080

-----Original Message-----
From: owner-rv10-list-server@matronics.com
[mailto:owner-rv10-list-server@matronics.com] On Behalf Of Rob Kermanj
Sent: Wednesday, September 03, 2008 4:28 PM
To: rv10-list@matronics.com
Subject: Re: Hartzell Composite Three blade RPM Test


I have been reporting best speeds at 2250 RPM.  Perhaps with your  
theory I can do better.  I am curious and will test it and report back.

I consistently get 172 kts at 12,500 with 10 gal/hr burn.  Perhaps I  
really mean best speed/fuel economy combination and don't realize it.

I do know that being in absolute smooth air and giving the plane a  
chance to accelerate for a few long minutes makes a big difference.   
The speed goes all over the place with the slightest turbulence.

It will be a while before I can do the test but I WILL report back.  I  
also need to qualify that I do not have three blades so, who knows!

Thank for making me think.


On Sep 3, 2008, at 1:40 PM, William Curtis wrote:

>
> This is one of the reasons I shake my head when some report the best  
> speeds at some low ~2200-2400 RPM.  I discovered when I was breaking  
> in a new engine on the Cardinal that my best power and speeds was at  
> 2700 RPM.  Anything less than 2700 would produce a slower speed.   
> Now I primarily use two settings for my prop--2700 for takeoff, 2500  
> for climb and cruise with occasional reduction during letdown.
>
> All things being equal, you will achieve the best power and speed  
> from a prop at 2700 RPM.  At 2700 RPM, and 50 degree ambient  
> temperature, an 84" prop will have a tip speed of Mach 0.895. To  
> produce maximum thrust at full power your tip speed should fall  
> between .88 and .92 mach.  The primary benefit of reducing RPM is  
> for increased passenger comfort (less noise) and reduced engine wear  
> an tear.
>
> What is the diameter of the Hartzell Composite Three blade?
>
> William
> http://nerv10.com/wcurtis/
>
> -------- Original Message --------
>> X-Rcpt-To: <wcurtis@nerv10.com>
>>
>> On my trip to Moses Lake and back over the weekend I tried different
>> propeller RPM's for speed.  I was level at 8500 Ft and full  
>> throttle.   I started at
>> 2600 RPM and then tried 2500, 2400, 2300, and 2200;  for every  100  
>> RPM drop I
>> would see a couple of knots drop in airspeed.
>>
>> Rob Hickman
>> N402RH  RV-10
>>
>>
>>
>> **************It's only a deal if it's where you want to go. Find  
>> your travel
>> deal here.
>> (http://information.travel.aol.com/deals?ncid=aoltrv00050000000047)
>
>




Other Matronics Email List Services

  • Post A New Message
  •   RV10-List@matronics.com
  • UN/SUBSCRIBE
  •   http://www.matronics.com/subscription
  • List FAQ
  •   http://www.matronics.com/FAQ/RV10-List.htm
  • Full Archive Search Engine
  •   http://www.matronics.com/search
  • 7-Day List Browsing
  •   http://www.matronics.com/browse
  • Browse the List Digests
  •   http://www.matronics.com/digest
  • Live Online Chat!
  •   http://www.matronics.com/chat
  • Archive Downloading
  •   http://www.matronics.com/archives
  • Photo Share
  •   http://www.matronics.com/photoshare
  • Other Email Lists
  •   http://www.matronics.com/emaillists
  • Contributions
  •   http://www.matronics.com/contributions

    These Email List Services are sponsored solely by Matronics and through the generous contributions of its members.

    -- Please support this service by making your Contribution today! --