FW: KR> KR2 ARTICLE-KITPLANES NOV 2010

2010-10-03 Thread Patrick and Robin Russo
Geez, it comes down to this; does one single bolt and spacer weigh less than 
two?!!

> 



FW: KR> KR2 ARTICLE-KITPLANES NOV 2010

2010-10-03 Thread James Ferris
Where is all this stuff coming from? I got plans for a KR-1 in the mid 
seventies 
and have never herd of a wing failer on a KR>
Jim



- Original Message 
From: Glenn Martin <rep...@martekmississippi.com>
To: KRnet <kr...@mylist.net>
Sent: Sat, October 2, 2010 9:49:57 PM
Subject: Re: FW: KR> KR2 ARTICLE-KITPLANES NOV 2010

John Martindale wrote:
> A long time ago before "experimental" came along (like in the 1980s), the
> Australian authorities did mandate a change to the bolt arrangement that
> specified a spacer tube between each pair of WAFs and a longer single
> through bolt instead of two short independent bolts.
>
> I think this reflects a better engineering solution with respect to shear
> forces
I can see how a thicker bolt could improve shear strength, or a bolt of 
a greater rating, but unless I am missing something, I see no way that a 
longer bolt of the same type and size could improve its shear strength 
at the wing attach fitting junction through an increase in its length. 
Did I miss somthing in physics class?

-- 
Glenn Martin (N5PQ)
Martek Mississippi Electronic Repair
13238 Hudson-Krohn Rd.
Biloxi, MS, 39532
rep...@martekmississippi.com


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FW: KR> KR2 ARTICLE-KITPLANES NOV 2010

2010-10-02 Thread John Martindale
Hi Glenn

Yeh. I think you did but I don't just what :-)

I'm pretty sure a bolt in double shear apparently is proportionately
stronger than two single ones in single shear of the same dia. I presume the
Australian authorities knew what they were on about when they insisted on
thisbut then again I'm known for my dislike of the buggers.

John Martindale
29 Jane Circuit
Toormina NSW 2452
AUSTRALIA
ph: 61 2 6658 4767
mobile: 0403 432179
email: john_martind...@bigpond.com

snipDid I miss somthing in physics class?

-- 
Glenn Martin (N5PQ)
Martek Mississippi Electronic Repair
13238 Hudson-Krohn Rd.
Biloxi, MS, 39532
rep...@martekmississippi.com


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FW: KR> KR2 ARTICLE-KITPLANES NOV 2010

2010-10-02 Thread Glenn Martin
Pete wrote:
>It's the addition of the tube spacer that adds the strength not the
> length of the bolt. What it effectively does is take an area that has
> two potential failure modes and replaces it with one.
> Cheers.
>
O k..but that is not SHEAR STRENGTH we're talking about, and I cant see 
any improvement in the Tensile Strength either.  Common sense seems to 
indicate that if one bolt fails in a single bolt structure, the results 
would likely be more catastrophic than if one bolt fails in a two bolt 
system. It does not make sense to me. That being said,  what are these 
"Failure Modes"you are referring to?

-- 
Glenn Martin (N5PQ)
Martek Mississippi Electronic Repair
13238 Hudson-Krohn Rd.
Biloxi, MS, 39532
rep...@martekmississippi.com



FW: KR> KR2 ARTICLE-KITPLANES NOV 2010

2010-10-02 Thread Pete
  It's the addition of the tube spacer that adds the strength not the 
length of the bolt. What it effectively does is take an area that has 
two potential failure modes and replaces it with one.
Cheers.
Peter Bancks.
Ballina, Oz.


On 3/10/2010 12:49, Glenn Martin wrote:
> I can see how a thicker bolt could improve shear strength, or a bolt of
> a greater rating, but unless I am missing something, I see no way that a
> longer bolt of the same type and size could improve its shear strength
> at the wing attach fitting junction through an increase in its length.
> Did I miss somthing in physics class?





FW: KR> KR2 ARTICLE-KITPLANES NOV 2010

2010-10-02 Thread Glenn Martin
John Martindale wrote:
> A long time ago before "experimental" came along (like in the 1980s), the
> Australian authorities did mandate a change to the bolt arrangement that
> specified a spacer tube between each pair of WAFs and a longer single
> through bolt instead of two short independent bolts.
>
> I think this reflects a better engineering solution with respect to shear
> forces
I can see how a thicker bolt could improve shear strength, or a bolt of 
a greater rating, but unless I am missing something, I see no way that a 
longer bolt of the same type and size could improve its shear strength 
at the wing attach fitting junction through an increase in its length. 
Did I miss somthing in physics class?

-- 
Glenn Martin (N5PQ)
Martek Mississippi Electronic Repair
13238 Hudson-Krohn Rd.
Biloxi, MS, 39532
rep...@martekmississippi.com



FW: KR> KR2 ARTICLE-KITPLANES NOV 2010

2010-10-02 Thread John Martindale


Hi Mark

A long time ago before "experimental" came along (like in the 1980s), the
Australian authorities did mandate a change to the bolt arrangement that
specified a spacer tube between each pair of WAFs and a longer single
through bolt instead of two short independent bolts. 

I think this reflects a better engineering solution with respect to shear
forces but having said that there were no instances of any failures at the
time and I know of none since under the original RR arrangement.

The Aussie authorities mandated a number of things back then that are now
superceded by experience or supply (like glues and Dynon cloth) but several
remain valid, eg., flight in the rear 2" of CoG envelope.

John Martindale
29 Jane Circuit
Toormina NSW 2452
AUSTRALIA

ph: 61 2 6658 4767
mobile: 0403 432179
email: john_martind...@bigpond.com

-Original Message-
From: krnet-boun...@mylist.net [mailto:krnet-boun...@mylist.net] On Behalf
Of Mark Langford
Sent: Friday, 1 October 2010 3:54 AM
To: KRnet
Subject: Re: KR> KR2 ARTICLE-KITPLANES NOV 2010

I met Bob Grimstead while in Perth.  He's a nice guy, likes to write "flight

test" articles for Aussie and US magazines, but apparently he's not 
qualified to speak to the integrity of the KR wing attach system.  The 
Aussies have dictated a couple of changes to KRs built and flown there, but 
"improving" the WAFs isn't one of them, as far as I know.

..snip.