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rbjjr
Joined: 18 Mar 2007 Posts: 36
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Posted: Mon Mar 19, 2007 5:11 pm Post subject: Zenith Rudder Design |
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I am building the 701 and having fun and learning a lot. It's a design that perfectly fits my mission.
Although I know the "all flying" rudder is a Zenith trademark, it strikes me as really the only potential question in the overall design. I am saying this as a layman, not being a designer or engineer, however.
The concentration of the hinges so low on the rudder seems to place much more stress on them than if the hinges were evenly spaced from top to bottom like many aircraft. The forces acting on the rudder while turning are concentrated all at one end and only on two hinges a few inches apart on a relatively large surface.
Anyone ever heard of issues with this rudder design? Anyone considered adding a third, middle hinge to provide some additional strength? This is not meant as a criticism, just a question from someone new to homebuilding.
Thanks
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bryanmmartin
Joined: 10 Jan 2006 Posts: 1018
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Posted: Mon Mar 19, 2007 5:26 pm Post subject: Zenith Rudder Design |
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There's nothing wrong with concentrating the load in a small area as
long as the structure is strong enough to handle it. I've never heard
any occurrences of rudders on Zodiacs falling off in flight and they
are very easy to check out during pre-flight.
On Mar 19, 2007, at 9:11 PM, rbjjr wrote:
Quote: | Although I know the "all flying" rudder is a Zenith trademark, it
strikes me as really the only potential question in the overall
design. I am saying this as a layman, not being a designer or
engineer, however.
The concentration of the hinges so low on the rudder seems to place
much more stress on them than if the hinges were evenly spaced from
top to bottom like many aircraft. The forces acting on the rudder
while turning are concentrated all at one end and only on two
hinges a few inches apart on a relatively large surface.
Anyone ever heard of issues with this rudder design? Anyone
considered adding a third, middle hinge to provide some additional
strength? This is not meant as a criticism, just a question from
someone new to homebuilding.
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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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dougsnash(at)yahoo.com Guest
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Posted: Tue Mar 20, 2007 3:00 am Post subject: Zenith Rudder Design |
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I am also building a CH-701. I am by no means an
aeronautical engineer but I have the rudder built and
the fuselage sitting on the gear.
I think you might be overthinking the rudder situation
a little bit. The attachment points are pretty stout
on this design. The upper and lower hinge points feed
into the upper and lower longerons so a third hinge
point would add little addtional strength since it
wouldn't have anything of substance to attach to on
the fuselage.
Another thing that I've noticed is that with the nose
rib extending ahead of the hinge point, there will be
a certain amount of aerodynamic balance to the rudder
that should reduce any stresses significantly.
This is not a new design by any means. The CH-701 has
been around for over twenty years. I am far from an
expert on this but I have never heard of a failure of
the rudder hinge mechanism. Although it does seem a
little odd at first, it is designed that way.
According to the designer (Chris Heintz), the whole
plane was designed with a good dose of safety margin
in mind. Since the top speed is only just over 100
mph, the stresses on the tail are fairly low.
Good luck with your build. I know I am looking
forward to getting mine into the sky.
Doug MacDonald
NW Ontario, Canada
CH-701 Scratch Builder
working on controls
do not archive
--- rbjjr <burkeandsusan(at)verizon.net> wrote:
Quote: | Although I know the "all flying" rudder is a Zenith
trademark, it strikes me as really the only
potential question in the overall design. I am
saying this as a layman, not being a designer or
engineer, however.
The concentration of the hinges so low on the rudder
seems to place much more stress on them than if the
hinges were evenly spaced from top to bottom like
many aircraft. The forces acting on the rudder
while turning are concentrated all at one end and
only on two hinges a few inches apart on a
relatively large surface.
Anyone ever heard of issues with this rudder design?
Anyone considered adding a third, middle hinge to
provide some additional strength? This is not meant
as a criticism, just a question from someone new to
homebuilding.
Thanks
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bill_dom(at)yahoo.com Guest
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Posted: Tue Mar 20, 2007 4:28 am Post subject: Zenith Rudder Design |
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This picture will give you an idea about the strenght of the rudder attachment:
http://www.ch601.org/stories.htm
This is a 601 but the rudder attachment is the same for both 601 and 701.
William Dominguez
Zodiac 601XL Plans
Miami, Florida
rbjjr <burkeandsusan(at)verizon.net> wrote:[quote] --> Zenith-List message posted by: "rbjjr"
I am building the 701 and having fun and learning a lot. It's a design that perfectly fits my mission.
Although I know the "all flying" rudder is a Zenith trademark, it strikes me as really the only potential question in the overall design. I am saying this as a layman, not being a designer or engineer, however.
The concentration of the [quote][b]
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zodierocket(at)hsfx.ca Guest
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Posted: Tue Mar 20, 2007 4:54 am Post subject: Zenith Rudder Design |
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Dam, I took that picture. You think I would have thought of it ! Thanks William. That plane sat inverted for 6 months, through thunderstorms and wind, bashing the rudder every day almost. No One would touch it due to fear of law suit. But after 6 months the airline had it removed stating that it caused undue distress to it’s customers boarding their plane! I was told some of the comments by the pilots, non aviation people are pretty imaginative. By that way that picture is still posted as a reminder that polypropylene rope is not an acceptable tie down material. Best I have found by far is hemp rope for tie down. ( No, I’m not a hemp hippie, it was proven to me at a show once and I did testing on my own and for strength and UV exposure, the hemp material outlasted everything else)
Mark Townsend Alma, Ontario
Zodiac 601XL C-GOXL, CH701 just started
www.ch601.org / www.ch701.com/ www.Osprey2.com
do not archive
--
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dredmoody(at)cox.net Guest
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Posted: Tue Mar 20, 2007 5:07 am Post subject: Zenith Rudder Design |
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The rudder surface that is ahead of the hinge axis reduces the cable and rudder pedal pressure needed for a given amount of rudder deflection but does nothing to reduce the lateral load on the rudder during that deflection. That being said I agree that the hinge attachments are sufficiently strong as proven by no reports of incidents. It ain't broke so no need to fix it IMHO.
Dred
---- MacDonald Doug <dougsnash(at)yahoo.com> wrote:
Quote: |
I am also building a CH-701. I am by no means an
aeronautical engineer but I have the rudder built and
the fuselage sitting on the gear.
I think you might be overthinking the rudder situation
a little bit. The attachment points are pretty stout
on this design. The upper and lower hinge points feed
into the upper and lower longerons so a third hinge
point would add little addtional strength since it
wouldn't have anything of substance to attach to on
the fuselage.
Another thing that I've noticed is that with the nose
rib extending ahead of the hinge point, there will be
a certain amount of aerodynamic balance to the rudder
that should reduce any stresses significantly.
This is not a new design by any means. The CH-701 has
been around for over twenty years. I am far from an
expert on this but I have never heard of a failure of
the rudder hinge mechanism. Although it does seem a
little odd at first, it is designed that way.
According to the designer (Chris Heintz), the whole
plane was designed with a good dose of safety margin
in mind. Since the top speed is only just over 100
mph, the stresses on the tail are fairly low.
|
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amyvega2005(at)earthlink. Guest
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Posted: Tue Mar 20, 2007 5:35 am Post subject: Zenith Rudder Design |
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if you go back a few years, to the 1970s, this rudder design for the ecception of size, has been on every zenith aircraft, back to the Cricket. refer to the zenith journals to 1984. that is well over 3000 aircraft. If it ain't broke..........
Juan
--
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pchapman(at)ionsys.com Guest
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Posted: Tue Mar 20, 2007 8:48 am Post subject: Zenith Rudder Design |
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Although nice things are being said about the integrity of the Zenith
rudder design, with its two closely spaced hinges, I recall Chris
Heintz writing in the Zenith newsletter some years ago about the 601
(pre-XL series) and mild aerobatics. It was something about how
although the aircraft spins fine, it hasn't officially been approved
for spins, and besides, one wouldn't want to be doing them all the
time given the closely spaced rudder hinges.
Unfortunately I don't have a source for the quote to confirm this. So
the hinges may be fine for the job, but not exactly overbuilt for
things the aircraft wasn't designed for.
Peter Chapman
Toronto, ON 601 HDS / 912 / C-GZDC
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rbjjr
Joined: 18 Mar 2007 Posts: 36
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Posted: Tue Mar 20, 2007 2:57 pm Post subject: Re: Zenith Rudder Design |
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Thanks all for the thoughtful responses and the picture is worth a thousand (more) words.
Rgds
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cgbrt(at)mondenet.com Guest
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Posted: Fri Mar 23, 2007 8:27 pm Post subject: Zenith Rudder Design |
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I do not have a problem with the rudder design and the comments made. I do
however pay special attention to the attachments since the loss of the
rudder would most likely render the 701 uncontrolable.
Of all the bolts on the controls, the only one I have changed in 450 hrs is
the top hinge on the rudder. It was noticeably worn after 300 hrs.
Happy STOLing,
Carl
701, 912, amphibs
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ashontz

Joined: 27 Dec 2006 Posts: 723
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Posted: Tue Mar 27, 2007 5:54 am Post subject: Re: Zenith Rudder Design |
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I was just talking about this with Geoff Heap on Sunday (I was over his place and he had his plane out and the tail feathers on, looks good!). We both figured it wouldn't hurt to put a doubler plate in the lower and of the rudder spar that spans the distance between the hinge points. As it is those hinge brackets just rivet directly to the spar web. Considering the picture of the flipped over airplane, it's strong as it is. Add a double/stiffener plate (say .032) and you should be golden.
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