Kevin
My system is a tri gear arrangement and therefore it retracts between the
spars and the pivot is 71mm up from the bottom of the main spar and 22mm in
from the end of the main centre spar.
Regards
Dene Collett
South Africa
KR2SRT builder
mailto: dene.coll...@telkomsa.net
www.whisperaircraft.co.za
----- Original Message -----
From: Golden, Kevin <kevin.gol...@churchdwight.com>
To: 'KRnet' <kr...@mylist.net>
Sent: Monday, April 25, 2005 15:24
Subject: RE: KR> wing ridgidity


> Is anyone building a KR landing gear to be more like the Wittman gear?  I
> would like to build the gear to come off of the motor mount like the RV's,
> Tailwind, T18, etc, but with a bit of a mixture of gear like the Titan
> Tornado has.  In other words, with Wittman gear, but instead of tapered
> steel gear legs, they would be fiberglass rods.  This is for the KR1.  Now
> the load is on the firewall.
>
> Kevin.
>
>
>
> -----Original Message-----
> From: Martindale Family [mailto:johnja...@optusnet.com.au]
> Sent: Sunday, April 24, 2005 7:13 PM
> To: KRnet
> Subject: Re: KR> wing ridgidity
>
> Hi Dean
>
> That sounds like a neat way to do it.
>
> My question is how do you get the wheels to finish up forward of the main
> spar (assuming a tail dragger) after extension from wells located between
> the spars? Do you somehow have the main tube running at an angle between
the
> spars?
>
> Also, how far out is your pivot from the fuselage? I guess that having it
at
> the ends of the stubs would allow the longest gear legs but then more stub
> distance and leg length would promote more twist between the spars which
> seems to be your concern. I think some uni-directional or carbon fibre
> strap, especially across the bottom of the wing between the pivot brackets
> wouldn't be a bad thing but I've no engineering analysis to support that.
>
> >From vague memory, my TC has his gear legs hanging off an extension of
the
> tube you mention that goes through the centre of the main and stops in the
> wing nose. His gear then folds up into the leading edge wing root fillet
> which is enlarged to allow it, that is, his legs and wheels all tuck away
> forward of the spar.
>
> I prefer your arrangement Dean but it would mean no stub fuel tanks...hmmm
>
> John
>
> The Martindale Family
> 29 Jane Circuit
> TOORMINA NSW 2452
> AUSTRALIA
>
> phone: 61 2 66584767
> email: johnja...@optusnet.com.au
> ----- Original Message -----
> From: "Dene Collett (SA)" <dene.coll...@telkomsa.net>
> To: "KRnet" <kr...@mylist.net>
> Sent: Monday, April 25, 2005 6:27 AM
> Subject: KR> wing ridgidity
>
>
> > Since my retract gear is attached to a tube running between the front
and
> rear spars that locates in a self aligning bearing/bush at each end much
> like the head of a rod end bearing which is attached by the WAF bolts to
the
> spars, my question is: How ridgid is the wing with regard to the distance
> between the two spars once the skin is laid up (Mark L style skins)?
> > For those that have seen the lancair 360 gear, mine is very similar
where
> it attaches to the wing spars which means that if the spars move approx
1/2"
> further apart, the gear will become "unplugged". My stubs are not yet
> skinned and the rear spar is able to move forward and back with very
little
> effort. How much force would it take to cause the wing to "stretch" once
> skinned and attached to the outer wing?
> > I suppose I could put a wrap of uni-directional tape around the wing in
> the area of the WAF's??
> > Regards
> > Dene Collett
> > South Africa
> > KR2SRT builder
> > mailto: dene.coll...@telkomsa.net
> > www.whisperaircraft.co.za
> > _______________________________________
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>
>
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