Wing Q & A
Revised: February 04, 1999
From Danrihn@aol.com
The rear spar will require you to first set the wing in the fuselage to see where the rear
spar will lay. You may have to add plywood doublers to get it to line up or
offset jog) the steel spar plates to get the line up you want.
- Plan to start working on the welding, meanwhile I'll start
the wing. Anyone want to comment on the pros and cons of going spruce or douglas fir on
the spar?Re:Fired Up-Spruce or Doug Fir?
- From: SKYBOLT55@aol.com
- Spruce spars are great but hard to come by! Most people are building fir spars
....it's easier to get I'm building spruce spars but the 2 ...18ft boards were on order
for 4 months.
- As far as I know either wood works very well. Don't be affraid either way.
- I read somewhere that there was going to be some form or
fashion of a wing tank option in the plans of the 1D. That would be great for any cross
country flights ie: Lakeland or Oshkosh. I did not see it on the plans. Has anyone built
any form of a wing tanks? Will the wings accomadate a wing tank?
- From: SKYBOLT55@aol.com
- The only wing tank at this time is a small smoke tank that goes in the left rib bay
between nose rib at WS12 and nose rib at WS24.I don't know of any plans for a fuel tank in
the wing.
- Looking at drawing 1-202 (Wing Spanwise Members), part -19
(Trailing Edge Closure) and it's associated Section A-A; -19 is described as 1/2" x
2" x 21 1/2". Section A-A shows it being tapered from 1/2" down to
1/16" Obviously it gets cut in two and fitted between the trailing edge ribs. My
question, or confusion, is that I don't see how this piece constitutes a closure of the
inboard trailing edge. I seems to me that it needs to be notched and fit fully against
it's adjacent ribs so that it will move aft to mate with the trailing edge line. I see how
it serves to stiffen the trailing edge, but I don't quite see how this closes the trailing
edge. Am I missing something? Looking at sheet 1-310 (Aileron Assembly); the aileron
trailing edge (part -7) is constructed quite differently. Looks to me that a similar
arrangement for the inboard trailing edge be nicer.
- From: SKYBOLT55@aol.com
- You sure make it sound confusing with your section this and section that...basicly
the rib thickness at the trailing edge of the long ribs are wrong on the plans. You should
make the the same thickness as the aileron ribs at the trailing edge, to achieve the thick
trailing edge that has proved superior in aerobatic performance. Boy that sounds good. In
laymans terms make part A fit part B. The wing should have the same width trailing edge
all along the wing.Don't forget the thickness of the plywood covering when calculating the
thickness of the trailing edge. I've built my wing and it works great....press on.
- As far as wing weights go, how about the finishing / cover
methods? Epoxy tends to be fairly heavy because nothing much evaporates off as it cures, I
hear most people are covering with a thin layer of glass as well as coating the inside of
the wing! This must add a lot of weight too. What is really needed and what is
"Extra" in this kind of construction? I would have thought that the inside would
not need much protection, and glass on the outside would just add extra weight. I am
interested in hearing what others have done and think about this.
- From: ACRO240Y@aol.com
- In reference to the epoxy used on the inside of the wing it does not weigh any more
than a couple of good coats of varnish. IT IS VERY IMPORTANT TO PROTECT THE WOOD ON THE
INSIDE OF THE WING FROM MOISTURE VAPOR. This another reason to use the epoxy instead of
varnish,it is much better at keeping out moisture vapor. As for the glass on the outside
of the wing , 1.4oz.to as light as
- 3/4oz. per square yard should be used this will be the lightest way to finish the
wood. DO NOT USE DACRON ON THE WINGS. The dacron fabric STITS, CECONITE, etc, are a
slippery material like nylon and glues do not bond to them very well. There was a lot of
problems in earlier times with the Stephens Akro type airplanes with fabric separating
from the wood. If you want to use dope as a finish on the wing you should use good old
fashion cotton.Imagine what would happen if a one or two foot section of the fabric
decided to ballon at high speeds. I have seen the results, it was fatel.
- From: Wilyum yum@aol.com
- Inside of wing on bare wood. 3 coats of epoxy varnish should be applied until surface
is shiny.
- All wood aircraft I have had any experience with have had some sort of cloth cover on
the exterior of the wings. very light glass or dacron. Don't forget to put an extra strip
on the leading edge to provide wear resistance. Bugs Rain crap in the air etc.
- If you don"t you will wish you had in a few years.
- The blueprints call for the ailerons to be weighted 10 %
nose heavy. What the heck does that mean ? Does it mean you should bring the cg of the
aileron forward 10% of the distance between the hinge line and the nose of the aileron ?
- From: RIHNAIRCO@aol.com
- After the aileron is completed including all covering and paint and definitely before
flight put weight in the aileron nose board channel until the aileron balances. Measure
that weight by removing it from the aileron. Add ten per cent to that amount and that is
the amount you want to put in permanently. Most people are using lead shot in west systems
epoxy.
- Anyone got an idea what wall square tube they had in mind
for the aileron bell cranks ? I spent a few hours cutting and milling the slots on some
1x1x.049 and think I will switch to some heavier mat'l .
- From: Outlaw 406@aol.com
- I agree that Doug Dodge has nice components as I have been to his shop but I am a
welder and fabricator myself , since posting the question on the bell cranks I have
finished them using 1x1 .065 just thought I would ask in case someone had experienced the
same problem.
- From: PMorgan001@aol.com
- What exactly was the problem you had using the 1 x 1 x .049 that the plans call for,
was it
- not strong enough ?
- From: Outlaw 406@aol.com
- I just thought after milling the slots out that there was not enough materiel in the
049 tube strictly my opinion as I am a dreamer not an engineer so I went to 065 wall and I
am satisfied now with the end results.
- I have completed plywood skinning of my wing and ailerons.
The next step is surface finishing. I need details on application of West Systems
epoxy/fiberglass cloth to get a light-weight smooth surface finish that won't peel off and
will provide a satisfactory surface for paint adherence. Any experiences favorable or
unfavorable are helpful.
- From: PMorgan001@aol.com
- The best way I have found for getting a fast smooth finish is a bit messy but works
Great!
- What you do is lay up your glass, paying extra attention to edges, etc, (remember
glass is hard to sand when fully cured). squeegy it down well to remove the excess epoxy.
When you have a layup that looks good, while the expoxy is still wet but starting to gel a
bit, pour glass bubbles over your layup. (wear a good mask). this is a bit messy but the
results are worth it. Brush the excess glass bubbles back into a plastic bag, they can be
reused on your next layup. When the layup is half cured 4 - 5 hours, trim trailing edges,
ect with a sharp blade. this will save Hours of work. When your layup is fully cured, you
will find a light sanding with only little more filling is required for a great base to
work with.
- I noticed in the newsletter that someone used fir using the
spruce design ribs for a super strong spar, (at some increase in weight) what do you think
of this Dan ?, I am sure that you don't think it is required, but do you think it is
reasonable, will it be to stiff ?, etc
- From: RIHNAIRCO@aol.com
- There is no reason to burden the aircraft with the extra weight. I have seen the
prototype pull 10 G s with a 235 lb pilot plus parachute etc. There was no problem and the
aircraft has flown hundreds of hard aerobatic hours on it since with heavy pilots. Stick
to the plans it is safer, and cheaper in the long run.That occurred because the builder
had planned on spruce and completed his ribs when he switched to fir. He was willing to
take on the extra weight rather than build new ribs. He didn't do this to create greater
strength. This is a rather stiff wing as it is and is plenty strong. Remember adding
weight to an aerobatic airplane is more serious than standard aircraft. Every pound added
is going to be like 10 pounds at 10G.
-
- Anybody know what is accpetable moisture content is for
Douglas fir for wing spars
- From: DanRihn@aol.com
- Aircraft quality lumber usually has a moisture content of 12%. It should not be less
than 8%, this would make the wood too brittle. Good reading on wood and wood building
techniques-
- EAA Aircraft Building Techniques WOOD; available from the EAA. This is the best book
I have seen. I highly recomend it for every One Design builder.
- Government issue books-
- CAM-18
- AC 43.13-1 A&2 good general guides, this is a modern version of CAM-18
- Airframe and Powerplant Mechanics Handbooks- Airframe, and General
- These last two were published by the Forest Products Laboratory. The data in these
books were used for the design of the One Design wing. Copies of thiese books are hard to
get. They contain mostly test and engineering data.
- ANC-19 Wood Aircraft Inspection and Fabrication
- ANC-18 Design of Wood Aircraft Structures
- Remeber to monitor the humididty of your work place while building your wing. An
inexpensive humidifier works great when conditions get too dry. A good rule is to keep
your humidity at about 75% (or higher) during the construction process, especially during
skinning of the wing.
- Just ordered my scratch build kits, and I am wondering what
everyone has used hold their gussets to the rib while the epoxy dries. A friend used a
large sheet of aluminum with wax paper on the bottom, and a 50 lb weight on top. Is this
sufficient, or should some type of removeable staple be used?
- From: ddavila546@aol.com
- Wing ribs--use staples or nails to hold gussets in place, otherwise they slide
around. air powered nailers are under $75 and you can tell your wife its for her new
kitchen cabinets(someday)
- From tfabian@netrix.com
Answer to C - Raka Fiberglass carries .75 oz cloth. They have a web page at www.raka.com.
- From Danrihn@aol.com
The lightest I have found is 1.4 oz/sq. yd. 1.45 Deck cloth is fine. The lighter
cloth is very hard to find these days.
From: billd3@indy.net
I am a builder/flyer of giant scale R/C aircraft. One of my favorite's is a 40% DR107 One
Design. I also have a 55% Giles 202 in progress. I have been building giants exclusively
for 14 years or so & although I'm not an A&P by education or license, I can help
your builder with the .75oz fibreglass question.
First of all, I'm a little suprised to see the use of such a light weave in full scale
aircraft. I typically use 1.0 oz obtained from Nick ZIROLI's Plans to cover wings
& fuse assemblies.
Anyway, you can get the 3/4 oz cloth from any number of modeling suppliers. I suggest you
go to a book store and purchase RCM (R/C Modeler)Magazine & look through the ads.
Here's a brief list:
1.) Aerospace Composites - www.acp-composites.com
2.) CST Composites - www.cstsales.com
3.) Fibre Glast Composites- www.fibreglast.com
4.) Lone Star Balsa- www.dcinet.com/lonestar/
5.) SIG Models- www.sigmfg.com
6.) Nick Ziroli ( 1oz.) ph:(516)-467-4765
Note: I have used .5oz & .75oz both and my
favorite is the Nick Ziroli 1 oz. cloth. It seems to fill better,using less resin, and I
believe giving me a overall lighter overall finish.
PS: I also don't know if you require a special weave or not
- What
should be the setup on the wing mounting? Maybe: Nut, Washer, Front of saddle, shim
(0.020?), 062 in. facing plywood (bonded to spar), wing spar (fir, 3 inch nom.), 0.5
in. ply spacer (bonded to spar), 0.062 in. facing plywood (bonded to spar), shim?,
back of saddle, washer, nut
From: Danrihn@aol.com
The wing attach set up you describe sounds good
RIB DRAWING
From: SKYBOLT55@aol.com
In order to make the first 3 long ribs match the aileron you need to make them a total of
5/8 wide at the trailing edge. Including the 3 mill ply wing skin. It runs in a straight
line from the back of the rear spar. This was pointed out to me by Doug Dodge. He built
the prototype. The plans are wrong.
- Aileron Hinges
- Date: 95-01-19 20:01:02 EST
- From: SKYBOLT55@aol.com
- I have spent several days with Doug Dodge at Acro Specialties. He has a better
aileron hinge and belcrank assembly for the 1D. The plans belcrank makes it nec. to
enlarge the lightning holes in the ribs for the ail. push-pull tube. This design
eliminates the problem.
- Todd W. Ashcraft
- I can't afford a good fine wire staple gun, so I clamped each rib (to glue on the
capstrips/gusstes/etc.) in my wing. A person can quickly go broke buying enough spring
clamps for this, and spring-loaded clothespins are too weak and don't open wide enough. I
found a company (ACCO) who makes what they call "BINDER CLIPS" in various sizes.
The large size, which come about 6 per box, work well for the thicknesses of these parts.
Made from black painted spring steel (or Iconel?), they are strong enough to get a good
hold, but don't squeeze out all of the West Epoxy. They can be found at any office supply
store, and are far cheaper than the made-for-woodworking clamps. Try them.
- Also, using these clamps, a long/slim work table(closet door) covered in plastic
sheet, and the 1/2" acid brushes plumbers use for pipe cement, you can work in
assembly-line fashion and crank out all the ribs in about two sessions.
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