I'm building a Lancair Legacy (all carbon fiber) and am planning to put
copper foil strips on the belly to serve as a ground plane for the
belly-mounted com antenna. I'm going to use 1/4" wide copper foil with an
adhesive back, attached to the outside of the fuselage and covered with a
thin layer of fiberglass (not carbon fiber) to protect the foil. I'll
solder it together at the center and attach it somehow to the outside of the
BNC connector.
I'm planning to make four radials, each 22" long, connected at the center of
the antenna and oriented at 90° to each other.
I'm using narrow 1/4" copper foil for two reasons: 1) I already own it,
left over from my wife's stained glass hobby, and 2) since I'll be sticking
it on the outside, the narrow strips are more likely to stay attached to the
fuselage when covered with the fiberglass. I think a wider strip is more
likely to separate from the fuselage and create a bubble that would be
objectionable.
Here are my questions:
1. I'm planning to make each of the four radials from three 1/4" wide
strips run side-by-side, with 1/8" space between the strips. I hope that
this will provide epoxy bonding areas between the strips but still make the
antenna think that each radial is a single piece 1" wide. Any idea how the
performance of this might compare with a solid 1" wide strip?
2. Is there any benefit to soldering a foil strip across the ends of the
three individual strips making up each radial to bond them together at the
end opposite the center?
3. I'm assuming that 1" wide radials are significantly better than1/4" wide
radials; is that true? Maybe I'd be just as well off to make each radial
out of a single 1/4" wide strip?
4. The Com antenna is a Comant 122, which has a streamlined metal base a
couple of inches in diameter. Should the length of the ground plane radials
be 22" from the BNC connector at the center of the base or should it have
22" of length extending beyond the base?
Thanks for your help,
Dennis Johnson
pine...@volcano.net
> Hi,
>
> I'm building a Lancair Legacy (all carbon fiber) and am planning to put
> copper foil strips on the belly to serve as a ground plane for the
> belly-mounted com antenna. I'm going to use 1/4" wide copper foil with an
> adhesive back, attached to the outside of the fuselage and covered with a
> thin layer of fiberglass (not carbon fiber) to protect the foil. I'll
> solder it together at the center and attach it somehow to the outside of the
> BNC connector.
Why not attach it to the INSIDE of the fuselage? That's where all of the
grounding takes place -- and -- you don't have to cover it up!
I would use the 4 strips of the 1/4" tape, at 45 deg from each other and
a piece of thin copper sheet about 1" dia, soldered to the center,
joining all the radials.
1/4" wide is plenty wide for the frequency band you are using -- just
make sure that each radial is about the same or greater length as the
antenna.
Thanks for the reply!
I have heard that carbon fiber does not allow radio signals to pass through
it, so that for a ground plane to be effective, it would have to be outside
the carbon barrier. As a practical matter, I'm sure some radio signals get
through, but if it were a significant amount, I'd put the antenna inside!
Another benefit of putting the foil on the outside is that I have clear
space to put the foil. Inside the fuselage, there isn't 22" of clear space
around the antenna, because the antenna is near the aft spar.
Some Legacy builders have installed short ground plane radials inside the
fuselage, some have put them outside, others have painted the belly with
special metal paint, and others have done nothing about ground planes. So
far as I know, every method tried that uses an external antenna seems to
work, so I'm likely worrying over nothing anyway. But the search for an
answer is, by itself, a pretty interesting process!
Thanks again,
Dennis Johnson
Hi and thanks for the reply.
I looked at Jim Weir's site and didn't see an answer to my specific
question, but I'll take another look.
Thanks,
Dennis Johnson
Hi,
Thanks for the reply. I may be wrong, but the foil that I remember using
for a burglar alarm was much thinner than the copper foil my wife uses for
stained glass, which I plan to use. I "stress tested" it and it seems quite
durable. Since copper is such a ductile material, it should tolerate the
expansion/contraction cycles it will encounter.
Thanks,
Dennis Johnson
First you are right, carbon is conductive to a degree, if you get a meter
and measure the resistance between two points in the structure (you need to
touch fibers with the probes for best results) you will get a resistance
which indicates that it is a conductor albeit not that good. I don't
remember exact numbers but I think 50-100 milli ohm over a few feet of
length (but don't shoot me if I got those numbers wrong). I can get the
exact numbers if you are interested. So placing the ground plane on the
inside is probably not going to work. It is this conductivity that allows
many carbon aircraft to be certificated for lightning strike with no copper
mesh in the laminate. The carbon conducts the lightning current away from
the strike and disipates the current within the laminate itself.
If carbon fiber is conductive then the obvious question is "what is its
performance as a ground plane". We have searched the literature and there is
little if any data out there. Consequently we tested two large panels one
with copper mesh (Exmet expanded copper foil) bonded in place with a film
adhesive and another panel with just carbon fibre. The performance of the
carbon only panel was good enough that we chose not to install copper mesh.
I do need to caution you though; the panels had an aluminium honeycomb core
and the effect of this compared to the carbon is not clear but the core was
not earthed to the antenna base where as the carbon was.
There are several things coming out of this.
First the testing we did was recommended by an antenna design specialist
because she didn't know what the effects of carbon, aluminium core etc were
and could not predict what would happen. Neither could the OEM of the
antenna. So I suggest you test your installation, possibly without the foil
tape at all to start with - just to see what happens. Testing is the only
sure way to know. A rudimentary test can be done on the cheap.
Second instead of the foil tape you are proposing to use, bond in some of
the expanded copper mesh from Exmet or Astrostrike .. this is what the
aerospace industry does when they have this sort of a problem. This stuff is
cheap and for what you need you may even get a free sample if you play the
game right.
Third ... I don't know about the Legacy but the Lancair IV already has
copper mesh in some parts of the airframe for lightning protection. Is there
any in the area where you are proposing to mount the antenna ?? If not could
you relocate the antenna to an area where there is some ???
Fourth ... you are not the first person to mount a comm's antenna on a
Legacy .. just take the lead from the others. If I works why bother. All
this stuff is black magic and even those who are supposed to know are
usually only guessing !!!
"Dennis Mountains" <pine...@volcano.net> wrote in message
news:10isfe1...@corp.supernews.com...
Why not put foil on the inside of the fuselage as a ground plane?
That's what Diamond did on my Star. The entire 'scuppers' of the
fuselage is lined with metal (but not copper) foil, as a ground plane
for the Com 2, DME, Marker, and Transponder antennas. Although not
entirely made of carbon fiber, the Star has a lot of it in that area
(spar carry through structure). I can e-mail some pics to you if you
are interested.
Com 1 and GPS antennas on the 'roof' have metal plate ground planes,
also located inside.
Steve
Hi and thanks for the lengthy reply! Your experience with supersonic
aircraft sounds pretty interesting. I'll check into Exmet and Astrostrike,
but since I already have the copper foil...
As far as I know, the Legacy doesn't have any copper mesh in the layups.
As I said in a previous post, I just talked to a Legacy flyer who didn't do
anything for a ground plane, other than thoroughly sanding the carbon fiber
under the antenna mount so that the antenna base would be in direct contact
with the carbon. He reports that people hear him fine. But I'm always
reluctant to put too much faith in anecdotal stories.
I have a friend who may be able to help me rig up some kind of test; thanks
for the idea.
Thanks again,
Dennis Johnson
I have seen a similar metallic strip along the bottom of the fuselage in
other composite aircraft that all the antenna earth to.
The use of mesh in lieu of foil just makes it easier to bond in place (and
more reliable) because the adhesive impregnates the mesh. The mesh is cheap
at a few dollars / sq ft. They also make aluminium and possibly monel mesh -
although I won't use aluminium on a carbon structure because they are widely
separated on the galvanic scale. Both Exmet and Astroseal (Astrostrike) can
be found on the web.
"Steve Chalfin" <cha...@uthscsa.edu> wrote in message
news:da9d550a.04082...@posting.google.com...
Didn't the carbon/aluminum honeycomb have some major corrosion issues?
That is why you NEVER use a lead pencil on aluminum.
Whoa! You are using the foil for a ground plane not an antenna. It is
perfectly OK for your foil to be inside the carbon because it is your antenna,
sticking outside, that does all of the radiating. Your foil will capacitively
couple to the carbon and the two should combine to make should should be a great
ground plane. Depending on the conductivity of your plane's skin, length of the
foil may not be critical. If possible, dummy everything together, borrow an SWR
meter and a radio, and make sure that everything is OK while you can still
change things without a major hassle.
Vaughn
> Whoa! You are using the foil for a ground plane not an antenna. It
is
> perfectly OK for your foil to be inside the carbon because it is your
antenna,
> sticking outside, that does all of the radiating. .
>
> Vaughn
>
Whoa! This is going to be fun, when Jim W. gets back with some replies.
--
Jim in NC
They separate the alumnium honeycomb from the carbon via a film adhesive
which has a fiberglass scrim in it. Corrosion is not normally a problem.
You are right though ... carbon is at +0.1 Volt and alumnium at something
like -0.75 Volt on the galvanic series so you have a battery !! Normally
you would not want any more than 0.3 Volt difference.
"Orval Fairbairn" <orfairbairn...@earthjunk.net> wrote in message
news:orfairbairn_spam_sucks...@news03.east.earthlink.net.
..
Lancair and RV are the only ones who told us to go pound sand. So be it.
You've paid tens of thousands of dollars for their designs and their parts and
those cheap bastards won't even give you the plans for an antenna design?
Please, sir, don't come on these newsgroups pleading poormouth and how-to-do-it.
Write or call Lancair and ask them why they don't understand how to do INTERNAL
antennas in carbon fiber. There are ways. They are too lazy or too cheap to
investigate them or too proud to ask us how to do them. According to Rutan, you
save between a knot and a knot-point-five per 100 knots of airspeed for each
COM/NAV antenna you get off the outside of the airframe.
Don't believe me? Go look at an F-117 Stealth Fighter. How many external
antennas do you see on that carbon composite airframe? Zero in my picture.
Got the idea?
Don't come back here asking for professional help. Go ask your
designer/supplier.
Jim
"Dennis Mountains" <pine...@volcano.net>
shared these priceless pearls of wisdom:
->Hi,
->
->I'm building a Lancair Legacy
Jim Weir (A&P/IA, CFI, & other good alphabet soup)
VP Eng RST Pres. Cyberchapter EAA Tech. Counselor
http://www.rst-engr.com j...@rst-engr.com
"Jim Weir" <j...@rst-engr.com> wrote in message
news:qqdti0t9a2k1apnf8...@4ax.com...
My thoughts exactly! For me, part of the fun of building my own airplane is
the opportunity to learn new skills as well as the intellectual challenge of
understanding new concepts. I would like to thank all of those on this
group who have helped me, on this thread as well as so many other threads.
Thanks,
Dennis Johnson
Or am I wrong? Somebody want to make me a sheet of glued-up material? That's
how this whole thing started, you know. Bellanca wanted inside-the-wing
antennas and they crated up a whole WING and sent it out to me to destroy. That
is how we got the data in the first place.
Any takers?
Jim
"smjmitchell" <smjmi...@yahoo.com>
shared these priceless pearls of wisdom:
->It is sad that Jim reacted the way he did .. I was hoping to learn
->something. Just a pity he took his frustrations out on a builder who is
->unaware of what transpired between Lancair and Jim ...........
Any differences will be immaterial.
The width of an individual ground-plane 'radiator element' is not particularly
significant. Lots of amateur radio stuff uses simple _wire_ for the radials.
Works just fine.
The only real concern, using 'foil' radials, is to ensure you've got enough
cross-sectional area in the radials for the transmitter power level.
>2. Is there any benefit to soldering a foil strip across the ends of the
>three individual strips making up each radial to bond them together at the
>end opposite the center?
NO. There may, in fact, be a _slight_ disadvantage to doing so. At your
proposed 1/8" gap, it is, however, _VERY _UNLIKELY_ you'd see any measurable
degradation.
>3. I'm assuming that 1" wide radials are significantly better than1/4" wide
>radials; is that true?
'Better?', yes.
'Significantly', no.
Using more narrow strips, with the resulting smaller angle between them, is
better than a few wide strips.
> Maybe I'd be just as well off to make each radial
>out of a single 1/4" wide strip?
If you're going to run additional strips, run them as separate radials.
12 strips at 15 degree intervals will provide a closer imitation to a
true ground _plane_ than 4 somewhat wider strips will. With any 'non-solid'
ground-plane there will be some 'bias' favoring the direction
of each radial, vs. 'between the radials'.
>
>4. The Com antenna is a Comant 122, which has a streamlined metal base a
>couple of inches in diameter. Should the length of the ground plane radials
>be 22" from the BNC connector at the center of the base or should it have
>22" of length extending beyond the base?
the 'outside edges' of the radials should be the nominal 22" from the center
of the base-plate. Obviously, you can run them just from the outside edge
of the base-plate out to the required distance.
->>
->>Here are my questions:
->>
->>1. I'm planning to make each of the four radials from three 1/4" wide
->>strips run side-by-side, with 1/8" space between the strips. I hope that
->>this will provide epoxy bonding areas between the strips but still make the
->>antenna think that each radial is a single piece 1" wide. Any idea how the
->>performance of this might compare with a solid 1" wide strip?
->
->Any differences will be immaterial.
That doesn't happen to be true. See next comment
->
->The width of an individual ground-plane 'radiator element' is not particularly
->significant. Lots of amateur radio stuff uses simple _wire_ for the radials.
->Works just fine.
That's because amateur radio stuff doesn't have to cover an instantaneous 15%
bandwidth ... 2 meters, for example, is just under 3% wide, and thin wire will
work just fine.
Having said that, and not having done the experiment, my GUT feeling is that
1/4" wide tape will be sufficient in and of itself, without going to the
3-strips-bonded-together trick for width. However, as in ALL fields, not doing
the experiment before welding the sucker together is cause for concern.
->
->The only real concern, using 'foil' radials, is to ensure you've got enough
->cross-sectional area in the radials for the transmitter power level.
Has not a WHIT of difference as to power level. You melt a one-mil thick
quarter-inch wide copper strip and you are running a flame thrower, not an
aircraft band transceiver limited by law to twenty-five watts.
->
->12 strips at 15 degree intervals will provide a closer imitation to a
->true ground _plane_ than 4 somewhat wider strips will. With any 'non-solid'
->ground-plane there will be some 'bias' favoring the direction
->of each radial, vs. 'between the radials'.
Not enough to measure. Try modeling it in EZNEC and see what you get.
Before you weld this sucker together, are you willing to temporarily tack-glue a
dipole INSIDE the fuselage and give it a try ... reporting your results to the
rest of us so that we can learn from your experiments? You *may* be able to get
away without making your pretty airplane look like a porcupine in heat.
I'll supply the materials for nuthin' if you will make the measurements I
outline to you.
Jim
Thanks for your very thorough and thoughtful reply to my questions. You've
given me some good ideas to chew on.
Thanks,
Dennis Johnson