KR>elevator balance!

2008-10-12 Thread Ross Evans
HI guys thanks for the feed back! I have just asked the questions to get 
some oppions of other builders as I am no engineer and really want to fly 
and safely. I have been told by different fellows that elevator balancing is 
needed and have emphasised the need with more power but yes flutter can 
happen at any speed and I have seen some kr's that are flying with no 
balancing I am putting in a more powerful engine and have been told that 
flutter could be a problem at higher speeds that is why I have asked about 
the subject as I want to fly for a long time not a short stint. My plane had 
been built straight to the plans and was going to have an 0200 but they are 
quite a dear engine to get and overhaul so I looked around and got a little 
more power but I was told to by the previous builder balance that elevator 
before u fly it! I am going to balance it for piece of mind! I am going to 
use a piece of chromolly on each side of the elevator and attach it to the 
elevator. How have other's done it that are flying I am looking to have mine 
looking like marty roberts plane how did he do it. I don't have his email 
address and would love to talk to him about how he did his!
cheers
Ross

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KR>elevator balance!

2008-10-12 Thread larry flesner
 How have other's done it that are flying I am looking to have mine 
>looking like marty roberts plane how did he do it. I don't have his email 
>address and would love to talk to him about how he did his!
>cheers
>Ross
+++

Marty Roberts would be very hard to get in touch with but I'd give you
ten to one odds that Dan Diehl would know and you could reach
him almost any time at Diehl Aeronautical.  

Larry Flesner




KR>Elevator balance

2008-10-12 Thread JW
How critical is it to make sure both ends of an elevator is balanced evenly. 
Mean one side of the balance being heavier than the other but still 100% 
balanced elevator.

Justin


KR>Elevator balance

2008-10-12 Thread Ron Freiberger
That means your elevator will fall off if you go fast.

Ron Freiberger
mailto: rfreiber...@swfla.rr.com

-Original Message-
From: krnet-boun...@mylist.net [mailto:krnet-boun...@mylist.net]On Behalf Of
JW
Sent: Saturday, March 20, 2004 8:03 PM
To: KRnet
Subject: KR>Elevator balance

How critical is it to make sure both ends of an elevator is balanced evenly.
Mean one side of the balance being heavier than the other but still 100%
balanced elevator.

Justin
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KR> Elevator balance

2008-10-12 Thread larry flesner
At 07:02 PM 3/20/04 -0600, you wrote:
>How critical is it to make sure both ends of an elevator is balanced
evenly. Mean one side of the balance being heavier than the other but still
100% balanced elevator.
>Justin


Justin,

What are we talking here, ounces?  If it's close there probably would
not be a problem.  Ounces would probably not be enough to induce
any twisting into the control surface under air loads.  

Try giving a bit more detail and maybe one of the engineer types
will venture an answer.

Larry Flesner





KR> Elevator balance

2008-10-12 Thread joe
Larry,
  I am going to be intentionally vague.
The spiral slipstream of the prop is adjusted for statically by angling the
engine and later dynamically by rudder control. Design adjustments can be
made to reduce this
effect when designing the vertical stabilizer.
 There are similar adjustments that can be made during
the design and test stage of the elevator thru GVT
ground vibration testing. Thats why we follow the plans
on this one.  Joe

I can hear it now!


- Original Message - 
From: "larry flesner" 
To: "KRnet" 
Sent: Sunday, March 21, 2004 5:36 AM
Subject: KR> Elevator balance


> At 07:02 PM 3/20/04 -0600, you wrote:
> >How critical is it to make sure both ends of an elevator is balanced
> evenly. Mean one side of the balance being heavier than the other but
still
> 100% balanced elevator.
> >Justin
> 
>
> Justin,
>
> What are we talking here, ounces?  If it's close there probably would
> not be a problem.  Ounces would probably not be enough to induce
> any twisting into the control surface under air loads.
>
> Try giving a bit more detail and maybe one of the engineer types
> will venture an answer.
>
> Larry Flesner
>
>
>
> ___
> to UNsubscribe from KRnet, send a message to krnet-le...@mylist.net
> please see other KRnet info at http://www.krnet.org/info.html




KR> Elevator balance?

2008-10-12 Thread larry flesner
>Larry,
>  I am going to be intentionally vague.
>The spiral slipstream of the prop is adjusted for statically by angling the
>engine and later dynamically by rudder control. Design adjustments can be
>made to reduce this
>effect when designing the vertical stabilizer.
> There are similar adjustments that can be made during
>the design and test stage of the elevator thru GVT
>ground vibration testing. Thats why we follow the plans
>on this one.  Joe
>I can hear it now!


Joe,

You maybe ment this for Justin?  He was asking the question about
elevator balance being distributed evenly across the span.  Please
enlighten as to how your answer relates.

As to propeller spirial slipstream,  I built my KR with "zero - zero"
thrust alignment and the vertical and horizontal stabs both set
to "zero" alignment and it flys just fine.  

The greatest effect I've ever noted on propeller spirial slipstream
is that one side of the airplane gets dirtier than the other on
a grass strip. :-)

Larry Flesner







KR> Elevator balance?

2008-10-12 Thread joe
Sorry about the mixup

I'm going to add the grass strip comment to my  best
comment book.
 Thanks Joe

Ps. Do you have a taildragger?
- Original Message - 
From: "larry flesner" 
To: "KRnet" 
Sent: Sunday, March 21, 2004 12:29 PM
Subject: KR> Elevator balance?


> >Larry,
> >  I am going to be intentionally vague.
> >The spiral slipstream of the prop is adjusted for statically by angling
the
> >engine and later dynamically by rudder control. Design adjustments can be
> >made to reduce this
> >effect when designing the vertical stabilizer.
> > There are similar adjustments that can be made during
> >the design and test stage of the elevator thru GVT
> >ground vibration testing. Thats why we follow the plans
> >on this one.  Joe
> >I can hear it now!
> 
>
> Joe,
>
> You maybe ment this for Justin?  He was asking the question about
> elevator balance being distributed evenly across the span.  Please
> enlighten as to how your answer relates.
>
> As to propeller spirial slipstream,  I built my KR with "zero - zero"
> thrust alignment and the vertical and horizontal stabs both set
> to "zero" alignment and it flys just fine.
>
> The greatest effect I've ever noted on propeller spirial slipstream
> is that one side of the airplane gets dirtier than the other on
> a grass strip. :-)
>
> Larry Flesner
>
>
>
>
>
> ___
> to UNsubscribe from KRnet, send a message to krnet-le...@mylist.net
> please see other KRnet info at http://www.krnet.org/info.html




KR>Elevator balance amount

2008-10-12 Thread Steve and Lori McGee
  I did the elevator counter balance today with the elevator being the "Horn " 
style ( Richard Mole design ) with the naca 63009 airfoil.
With the weight in the horns it took a total of 28 ounces of lead in 4 peices 
of conduit.  Maybe 29 OZ in all.  Anyone else know the weight required for 
their counter balance?  I was wondering where I sat  for weight comparison.  
Also this  HS is almost 8 feet wide. 
   Now with the weight in the horns there is no worry of a bracket breaking 
under G loads.  The horns are well wrapped with carbon and I plan on wraping 
some light deck cloth around the wood rib on the outside as there is room.  
This will also make up for the extra weight of paint on the larger rear side of 
the elevator.  

Steve McGee
Endeavor Wi. USA
Building a KR2S widened.
lmc...@maqs.net 




KR>Elevator balance amount

2008-10-12 Thread Kenneth L Wiltrout
I did not counterbalance my elevator as per the plans. These airplanes
are usually tail heavy as opposed to nose heavy with today's over weight
pilots. That being saidputting almost 2 lbs of lead that far
to the rear will have a more dramatic effect on the cg than you may
think. Use caution. If you are hanging a corvair upfront then I wouldn't
worry about it.




On Sat, 13 Mar 2004 18:05:44 -0600 "Steve and Lori McGee"
 writes:
>   I did the elevator counter balance today with the elevator being 
> the "Horn " style ( Richard Mole design ) with the naca 63009 
> airfoil.
> With the weight in the horns it took a total of 28 ounces of lead in 
> 4 peices of conduit.  Maybe 29 OZ in all.  Anyone else know the 
> weight required for their counter balance?  I was wondering where I 
> sat  for weight comparison.  Also this  HS is almost 8 feet wide. 
>Now with the weight in the horns there is no worry of a bracket 
> breaking under G loads.  The horns are well wrapped with carbon and 
> I plan on wraping some light deck cloth around the wood rib on the 
> outside as there is room.  This will also make up for the extra 
> weight of paint on the larger rear side of the elevator.  
> 
> Steve McGee
> Endeavor Wi. USA
> Building a KR2S widened.
> lmc...@maqs.net 
> 
> 
> 
> ___
> to UNsubscribe from KRnet, send a message to krnet-le...@mylist.net
> please see other KRnet info at http://www.krnet.org/info.html
> 
> 


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