KR> Canopy hinge

2015-05-11 Thread Mark Langford
Paul Visk wrote:

 >> I'm trying to decide on which way to hinge my canopy. I know the 
currant trend is to mount it from the front.  But I can't get over the 
inability to open the canopy in flight if you need to jump out.
Is anyone putting with a side hinge in or is everyone hinging from the 
front?<<

Are you going to wear a parachute every time you fly?  I doubt it.  I 
couldn't wear a parachute in N891JF if my life depended on it (and I 
don't think it does).  Keep in mind that inflight structural or control 
failures in these planes are VERY rare.  You'd do far better to 
concentrate on how to get the plane on the ground safely, or at least 
under control, rather than trying to bail out.

Consider that if you take off with one latch disconnected (or even both) 
the forward hinging canopy will almost close itself...it'll hover maybe 
an inch over the longeron at the rear, but it will be in equilibrium and 
stay more or less closed.  if you take off with a side hinged canopy 
unlatched, it will likely slam open, killing lift on the right wing, and 
stall, if on takeoff.  This is basically  what happened to Allen Buzza 
in Australia.  Fortunately he survived and went on the rebuild the 
plane, and is working to finish another.

I almost lost the side-hinged canopy on N891JF the first time I started 
the engine and didn't have it latched.  That's when I decided to make it 
front hinged.

Just some food for thought.  I could go on, but it's past my bedtime...

Mark Langford
ML at N56ML.com
http://www.n56ml.com




KR> Canopy hinge

2015-05-11 Thread Mark Jones
Paul,
Here is my version :
http://flykr2s.com/gullwing.html
http://flykr2s.com/gullwingdoor.html
http://flykr2s.com/doorspring.html


Mark Jones (N886MJ)
Stevens Point, WI
E-mail: flykr2s at charter.net
Web: www.flykr2s.com



-Original Message- 
From: Paul Visk via KRnet
Sent: Monday, May 11, 2015 9:44 PM
To: KR EMAIL BOARD
Cc: Paul Visk
Subject: KR> Canopy hinge

I'm trying to decide on which way to hinge my canopy. I know the currant 
trend is to mont it from the front.  But I can't get over the inability to 
open the canopy in flight if you need to jump out.
Is anyone putting with a side hinge in or is everyone hinging from the 
front?

Paul Visk
Belleville Il.
618-406-4705
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KR> Canopy hinge

2015-05-11 Thread Paul Visk
I'm trying to decide on which way to hinge my canopy. I know the currant trend 
is to mont it from the front. ?But I can't get over the inability to open the 
canopy in flight if you need to jump out.
Is anyone putting with a side hinge in or is everyone hinging from the front?

Paul Visk
Belleville Il.
618-406-4705


KR> Ballast weight installation

2015-05-11 Thread Jeff Scott
Sid brings up a good point here, especially for builders that are early on in 
their projects.  I think sometimes we forget that the original KR design tended 
to be a tail heavy design that was balanced by a large header tank in the nose. 
 That didn't work out so great as it left the pilot landing in an aft CG 
configuration when low on fuel.  20 years ago, there were lots of stories about 
guys taking a friend for a ride and experiencing an exciting landing with low 
fuel and an aft CG at the end of the flight.

With the advent of the -2S design nearly 20 years ago, many of those lessons 
have been forgotten.  But as Sid points out, the wings were essentially moved 
forward in the -2S to help balance the plane.  Additionally, most builders are 
putting their fuel in the wings to avoid the large CG shift, as well as for 
other safety reasons.  

My KR has the extended tail, but was not stretched in the nose (started before 
the release of the -2S plans).  I knew when I was building it that this plane 
wanted to be tail heavy, so made a concerted effort throughout the build 
process to move weight forward.  I used the Rand Robinson designed O-200 motor 
mount and a C-85, then eventually an O-200 with the heavy accessories to help 
keep that weight forward.  I also mounted my battery on the front of the 
firewall.  When completed, my CG came out where I wanted it without the need to 
move more things around or the need for ballast.  However, as I said, I made an 
effort through out the build to move weight forward.  

As for Sid's checklist of modifications to move the CD forward, I did them all 
to get the plane right:
1) Move the engine forward (used a longer mount than what was normally used).
2) Hung Battery on the firewall.
3) Installed a heavier engine.

That's what it took to get a nicely balanced plane with the shorter KR-2 
firewall placement.

-Jeff Scott
Los Alamos, NM


>
> John,
> If I knew the actual answer to why so tail heavy, I would have fixed that 
> long ago and would not be having all this discussion.  The only plausible 
> explanation I have is: The designer, Stu Robinson, set the RAF-48 wing 
> 2-inches farther forward in the stock plans than it should have been.  That 
> is a moot point with the advent of the KR-2S.
> I know there are hundreds of KR-2 aircraft flying.  It seems they either 
> have moved the engine forward, hung batteries on the the firewalls, 
> installed heavier engines and/or fly them onto the runway at 70+ knots and 
> never ever stall them.  That or the builders are not around to tell about 
> their last flight.
> 
> Sid Wood
> Tri-gear KR-2 N6242 N6242
> Mechanicsville, MD, USA
> -



KR> Ballast weight installation

2015-05-11 Thread Ken
The counter balance for the elevator could be adding to the problem with 
Sid's KR-2.  That is addition weight aft of CG that isn't in the plans 
that I have.
Kr-2 builder C-FKRN
Ken Nathan

On 5/11/2015 3:02 PM, Jeff Scott via KRnet wrote:
> Sid brings up a good point here, especially for builders that are early on in 
> their projects.  I think sometimes we forget that the original KR design 
> tended to be a tail heavy design that was balanced by a large header tank in 
> the nose.  That didn't work out so great as it left the pilot landing in an 
> aft CG configuration when low on fuel.  20 years ago, there were lots of 
> stories about guys taking a friend for a ride and experiencing an exciting 
> landing with low fuel and an aft CG at the end of the flight.
>
> With the advent of the -2S design nearly 20 years ago, many of those lessons 
> have been forgotten.  But as Sid points out, the wings were essentially moved 
> forward in the -2S to help balance the plane.  Additionally, most builders 
> are putting their fuel in the wings to avoid the large CG shift, as well as 
> for other safety reasons.
>
> My KR has the extended tail, but was not stretched in the nose (started 
> before the release of the -2S plans).  I knew when I was building it that 
> this plane wanted to be tail heavy, so made a concerted effort throughout the 
> build process to move weight forward.  I used the Rand Robinson designed 
> O-200 motor mount and a C-85, then eventually an O-200 with the heavy 
> accessories to help keep that weight forward.  I also mounted my battery on 
> the front of the firewall.  When completed, my CG came out where I wanted it 
> without the need to move more things around or the need for ballast.  
> However, as I said, I made an effort through out the build to move weight 
> forward.
>
> As for Sid's checklist of modifications to move the CD forward, I did them 
> all to get the plane right:
> 1) Move the engine forward (used a longer mount than what was normally used).
> 2) Hung Battery on the firewall.
> 3) Installed a heavier engine.
>
> That's what it took to get a nicely balanced plane with the shorter KR-2 
> firewall placement.
>
> -Jeff Scott
> Los Alamos, NM
>
>
>> John,
>> If I knew the actual answer to why so tail heavy, I would have fixed that
>> long ago and would not be having all this discussion.  The only plausible
>> explanation I have is: The designer, Stu Robinson, set the RAF-48 wing
>> 2-inches farther forward in the stock plans than it should have been.  That
>> is a moot point with the advent of the KR-2S.
>> I know there are hundreds of KR-2 aircraft flying.  It seems they either
>> have moved the engine forward, hung batteries on the the firewalls,
>> installed heavier engines and/or fly them onto the runway at 70+ knots and
>> never ever stall them.  That or the builders are not around to tell about
>> their last flight.
>>
>> Sid Wood
>> Tri-gear KR-2 N6242 N6242
>> Mechanicsville, MD, USA
>> -
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KR> 5 bladed prop

2015-05-11 Thread CraigW
Just got of the phone with Darryl @ Warp Drive.  I initially used their online
quote form to get a price on a 5 bladed prop.  Because if your building a
Seafury you gotta have a 5 bladed prop. RIGHT?  Anyway, the response from
HoverHawk Corp that sells the props was that its too heavy and they quoted me a
3 bladed prop for an O-235.  After calling the factory I am excited to say I am
still good to use a 5 bladed prop.  The Sensenich used was 24 lbs and the 5
blades with hub will be about 20 lbs.   SO the plan is  to start with 60 inch
blades and cut them down from there as I experiment with the performance.  I
suspect I can go as small as 52-55 inches if need be.  It will not be my daily
flyer but when going to an airshow the 5 blades are the choice for sure.

Excited Builder Craig


KR> Ballast weight installation

2015-05-11 Thread Sid Wood
John,
If I knew the actual answer to why so tail heavy, I would have fixed that 
long ago and would not be having all this discussion.  The only plausible 
explanation I have is: The designer, Stu Robinson, set the RAF-48 wing 
2-inches farther forward in the stock plans than it should have been.  That 
is a moot point with the advent of the KR-2S.
I know there are hundreds of KR-2 aircraft flying.  It seems they either 
have moved the engine forward, hung batteries on the the firewalls, 
installed heavier engines and/or fly them onto the runway at 70+ knots and 
never ever stall them.  That or the builders are not around to tell about 
their last flight.

Sid Wood
Tri-gear KR-2 N6242 N6242
Mechanicsville, MD, USA
-

Agreed, a new mount seems to be the preferred solution and if it has to be
so be it but.why is this particular girl so tail heavy to start
with? How is it built so differently from the KR2 design plans to require
such a change?


John Martindale
29 Jane Circuit
Toormina NSW 2452
Australia









KR> Ballast weight installation

2015-05-11 Thread John Martindale
Agreed, a new mount seems to be the preferred solution and if it has to be
so be it but.why is this particular girl so tail heavy to start
with? How is it built so differently from the KR2 design plans to require
such a change?


John Martindale
29 Jane Circuit
Toormina NSW 2452
Australia

ph:61 2 6658 4767
m:0403 432179
email:john_martindale at bigpond.com
web site: 
-Original Message-
From: KRnet [mailto:krnet-bounces at list.krnet.org] On Behalf Of Dan Heath via
KRnet
Sent: Monday, 11 May 2015 7:56 AM
To: 'KRnet'
Cc: Dan Heath
Subject: Re: KR> Ballast weight installation

2" not a problem.  But, yes, if you can do the mount over, that would be
ideal.snip




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KR> Ballast weight installation

2015-05-11 Thread Tony King
There'd have to be a limit to how far you can move the engine forward using
spacers.  I'd expect even at 2" spacers would be starting to be prone to a
bit of movement due to torsional forces and the like.  I'd be looking to
redo the engine mount if I needed to move the engine forward by more than
an inch or so.  Of course I say that having not yet experienced the joy of
fabricating an engine mount, so I could be completely misguided.

Cheers,

Tony

On 11 May 2015 at 06:22, jon kimmel via KRnet  wrote:

> Spacers work well.  If you still want to hang weights and you are opposed
> to lead, consider tungsten.  It is quite a bit denser than lead and doesn't
> have the environmental concerns.  A tungsten alloy that is available is
> called fansteel.
>
> https://sites.google.com/site/mykr2stretch/
> https://sites.google.com/site/mykr2stretch/parts-for-sale
> ___
> Search the KRnet Archives at http://tugantek.com/archmailv2-kr/search.
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>