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601 and wing failiers
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John75142



Joined: 05 Dec 2007
Posts: 56
Location: Kaufman, TX

PostPosted: Thu Dec 20, 2007 2:34 pm    Post subject: 601 and wing failiers Reply with quote

Just a thought and it probably ain't a good one but what about filling
certain cavities with a low expansion foam.
---


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bryanmmartin



Joined: 10 Jan 2006
Posts: 1018

PostPosted: Thu Dec 20, 2007 3:01 pm    Post subject: 601 and wing failiers Reply with quote

It had better be an open cell foam or it will expand with altitude and
bulge the skin outward. In any case it will add some weight. It will
add even more weight and will promote corrosion if it absorbs water.

On Dec 20, 2007, at 5:32 PM, John Short wrote:

Quote:

>

Just a thought and it probably ain't a good one but what about
filling certain cavities with a low expansion foam.


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Bryan Martin
N61BM, CH 601 XL,
RAM Subaru, Stratus redrive.
do not archive.


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ronlee



Joined: 25 Dec 2006
Posts: 141

PostPosted: Thu Dec 20, 2007 3:50 pm    Post subject: Re: 601 and wing failiers Reply with quote

The Titan has a foam filled D-Cell.

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ifly4fun2(at)sbcglobal.ne
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PostPosted: Thu Dec 20, 2007 6:32 pm    Post subject: 601 and wing failiers Reply with quote

You guys have it all wrong you need to fill the wings with helium...

Art
do not archive
--- John Short <creativesigns(at)embarqmail.com> wrote:

[quote]

Just a thought and it probably ain't a good one but what about filling
certain cavities with a low expansion foam.


---


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kmccune



Joined: 22 Sep 2007
Posts: 577
Location: Wisconsin, USA

PostPosted: Thu Dec 20, 2007 7:02 pm    Post subject: Re: 601 and wing failiers Reply with quote

Anyone ever wish that they had never asked a question? Laughing

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Gig Giacona



Joined: 10 Jan 2006
Posts: 1416
Location: El Dorado Arkansas USA

PostPosted: Fri Dec 21, 2007 7:18 am    Post subject: Re: 601 and wing failiers Reply with quote

Probably a bad idea. Other than the obvious weight penalty you would have to do a complete engineering test to see how the weight out in the wings would effect g-loading.
John75142 wrote:
Just a thought and it probably ain't a good one but what about filling
certain cavities with a low expansion foam.
---


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shilcom



Joined: 28 Sep 2007
Posts: 63

PostPosted: Fri Dec 21, 2007 7:44 am    Post subject: 601 and wing failiers Reply with quote

>>I'd have to guess
Quote:
> the wing is considerable stronger without the wing locker>>

I wouldn't worry about the wing locker area, as I'm sure heinz has put adequate doublers in the wing locker area. Highest stress in positive G mode for the top area should be nearer the fuselage. Bob U.
[quote] ---


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Iberplanes



Joined: 10 Dec 2007
Posts: 174
Location: Igualada - Barcelona - Spain

PostPosted: Fri Dec 21, 2007 7:54 am    Post subject: 601 and wing failiers Reply with quote

Hi list,

That is a BAD idea. Today a friend of mime just told me a about a well known
Zephyr pilot that crash and was dead for that reason. His hangar was next to
ours.. It would change the way the wing is supposed to act and move "between
limits".

Take care,

---


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John75142



Joined: 05 Dec 2007
Posts: 56
Location: Kaufman, TX

PostPosted: Fri Dec 21, 2007 10:20 am    Post subject: 601 and wing failiers Reply with quote

Sounds reasonable it would probably stiffen the structure to much.

Well I said it is was just a thought and probably a bad one but for a second
it kind of made sense.
Merry Christmas to all.

---


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PatrickW



Joined: 27 Oct 2006
Posts: 380
Location: Fort Worth, Texas

PostPosted: Fri Dec 21, 2007 11:40 am    Post subject: Re: 601 and wing failiers Reply with quote

daveaustin2(at)primus.ca wrote:
Can I suggest changing all 6061T6 to 2024T3 for greater strength and making everything twice as thick?


Could call it a "601 RV".

Patrick
XL/Corvair


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rsteele(at)rjsit.com
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PostPosted: Fri Dec 21, 2007 1:11 pm    Post subject: 601 and wing failiers Reply with quote

I'm no aeronautical engineer and I've certainly never analyzed this
wing, but I do have an engineering degree and you sort of get a feel for
these things. In a positive G load, the upper skin probably carries no
(structural - like the spar) load at all - it would be in compression
and I'm pretty certain it's compressive strength is going to be
considered zero for this purpose. It should actually have some amount
of tension in from the lift generating forces.

In negative G loads which are smaller than the positive, the upper skin
would certainly be in tension, and carrying a small part of the load,
but at the point where the lockers are located, the load won't be close
to the maximum, which is at the wing root.

Really, the issue is stiffness, which can be affected also. The big
question is, do the added bits that make up the locker, along with the
hole in the skin, increase or decrease the stiffness of that area of the
wing. Ideally neither, and I'm betting, because I'm getting wing
lockers, that this is the very close to the case. Don't forget that
there are fasteners all the way around the cover which should make the
cover act as a shear plate, so there likely very little lose of strength
from the hole at all.

Ron

PS when I went on the demo ride, the plane was probably close to max
gross due to my size, there was a gusty 25 knot wind blowing and we were
doing max cruise. It was rough as all get-out. The plane was just as
solid as you could possible want, and very stable. It just plain felt
solid and in control. Much better an any Cessna I've been in in rough
air. I don't have much experience in light planes and I was frankly
surprised.

------


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amyvega2005(at)earthlink.
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PostPosted: Fri Dec 21, 2007 4:57 pm    Post subject: 601 and wing failiers Reply with quote

If you dont mind a 601 able only to cary one pasenger and 20 gallons of fuel.

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Dave Nixon



Joined: 20 Sep 2007
Posts: 25

PostPosted: Sat Dec 22, 2007 5:56 am    Post subject: Re: 601 and wing failiers Reply with quote

Personally, I think all this talk about wing lockers causing or will cause a failure is a lot of garbage. As stated previously, when the wing locker is cut in, it is truly beefed up with a very rigid rear locker panel (6-WLO-1(2). That coupled with good construction practices (which should be employed during the whole process) will insure that every reasonable doubt should be erased.
I, also, would like to see some empirical data that shows that the wing locker has caused a structural failure. From what I have been able to determine on the NTSB reports, other than Stupid Pilot Tricks, the CH601XL is very reliable aircraft. Unfortunately Paralysis By Analysis is a trait that we all endure at one time or another. It is builder thing.
But don't let your imaginations find things that aren't there. Should you be concerned? Absolutely! So overcome it with good construction practices and some good old Common Sense. There is long way to go and many more decisions are going to be made before your beauty flies. And some of these seem pretty extreme at the time but for the life of me, without looking at my notes, I can't even remember them anymore. That's how insignificant they are now in the total build scheme of things.
Let's enjoy the process and be safe out there. Common Sense should prevail.
Dave Nixon
CH601XL Jabiru 3300
93% Done 75% To Go


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