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John75142
Joined: 05 Dec 2007 Posts: 56 Location: Kaufman, TX
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Posted: Thu Dec 20, 2007 2:34 pm Post subject: 601 and wing failiers |
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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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_________________ John Short |
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bryanmmartin
Joined: 10 Jan 2006 Posts: 1018
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Posted: Thu Dec 20, 2007 3:01 pm Post subject: 601 and wing failiers |
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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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_________________ --
Bryan Martin
N61BM, CH 601 XL, Stratus Subaru.
do not archive. |
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ronlee
Joined: 25 Dec 2006 Posts: 141
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Posted: Thu Dec 20, 2007 3:50 pm Post subject: Re: 601 and wing failiers |
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The Titan has a foam filled D-Cell.
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_________________ Ron Lee
Tucson, Arizona |
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ifly4fun2(at)sbcglobal.ne Guest
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Posted: Thu Dec 20, 2007 6:32 pm Post subject: 601 and wing failiers |
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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
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Gig Giacona
Joined: 10 Jan 2006 Posts: 1416 Location: El Dorado Arkansas USA
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Posted: Fri Dec 21, 2007 7:18 am Post subject: Re: 601 and wing failiers |
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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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_________________ W.R. "Gig" Giacona
601XL Under Construction
See my progress at www.peoamerica.net/N601WR |
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shilcom
Joined: 28 Sep 2007 Posts: 63
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Posted: Fri Dec 21, 2007 7:44 am Post subject: 601 and wing failiers |
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>>I'd have to guess
Quote: | > the wing is considerable stronger without the wing locker>>
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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
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Posted: Fri Dec 21, 2007 7:54 am Post subject: 601 and wing failiers |
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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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_________________ Alberto Martin
601 XL - Jabiru 3300
http://www.iberplanes.es
Igualada - Barcelona - Spain |
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John75142
Joined: 05 Dec 2007 Posts: 56 Location: Kaufman, TX
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Posted: Fri Dec 21, 2007 10:20 am Post subject: 601 and wing failiers |
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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
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Posted: Fri Dec 21, 2007 11:40 am Post subject: Re: 601 and wing failiers |
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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 Guest
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Posted: Fri Dec 21, 2007 1:11 pm Post subject: 601 and wing failiers |
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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. Guest
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Posted: Fri Dec 21, 2007 4:57 pm Post subject: 601 and wing failiers |
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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
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Posted: Sat Dec 22, 2007 5:56 am Post subject: Re: 601 and wing failiers |
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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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