Archangel_article.pdf

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February, 1950
L.
AEROMODELLER
8t
GAB RI ELS'
23 years old . . . . press toolmaker
by trade . . . . startid modelling 11
years ago,but due to study and ser-
vice in R.A.F. had little time until
'48 . . . . Press Sec. to Oldham
and District M.A.C. . . . . usos oM
lathe for engine making .. . . firet
interest sailplanes, secoud power
., . . other hobby photography,
used mainly with models.
to stand up to
nESIGNED
hard knocks and the windy
ff
weather of l.he North-Westerir
Area, the original is now 18
months old and still flying.
As
a result of one of itd two flv-
arvays, the model spent l.l winter
'Ihe
weeks on open moorland.
only damag-e suffered was a few
tears in the tissue and a waroed
tailplane. Archangel can be built
on a 30 in. drawins board.
The flight timeJ average over
4 minutes, and consistency is the
hallmark of the model's p6rform-
11ce-. It has been well placed regularly in Contests, always in
the first half dozen.
Construction.
Sta.rt by cutting out the formers and write your name and
address on F3, so that it can be seen inside the cabin.
Now mark out the two sides by piercing the outline on the
plan on to l/32nci in. sheet balsa using a pin. Cement the four
side longerons in place on the sides and add vertical spacers.
Mark the former positions on the sides and cement the
formers in place, setting them squarely. The cement having
dried, join the rear ends and clamp. Check for alignment.
Cut cross-braces in pairs and fit between side lonserons.
Now add paper tubes and hooks, and then sand fuselafe.
After shleei-covering, fix nose-biock ancl cover fusela{e with
rag tissue. Two coats of clear dope finely sanded, the addition
of the windscreen and colour dope complete the fuselase,
The door of the dethermalizer'chrlte comiartment shouldie
separated with a sharp blade and hinged with nylon.
Make up the mainspars, building in the outboard dihedral.
Cut out {our ply root ribs and face with l,z8th in. sheet balsa.
Clamp these togcther, yibs No. 2 being l/lDth in. higher than
ribs No. I and drill the dorvel holes.
Cement paper tubes at right angles to ribs No. l. Thread
ribs No. 2 loosely onto the tubes and insert mainspars. Support
these at the correct dihedral anqle on a level surface, insert
I in. dowcls in the tubes and adj-ust distance between ribs to
make dowels parallel with level surface. The whole set of ribs
is now cemented in place. Now
add trailing edge and wing-tips
and, alter sanding to cnsure a
a flat seating ior the leading
edge, cement this member in
place. Add appropriate sheet-
ing, sand and cover. Balance
wings bcfore and after covering.
Construction of tailplaneand fi n
is straightforward, the only point
to be watched being the fixing of
the auto-rudder.
If the locking-
pin should fail to pull out, th1
results will be disastrous, so en-
sure that the wire rinss are a
loose fit and lined up correctly.
I Toilplane fixing, outo-rudder and
I Pin attochment are shown, left,
'chute stowed in
I dethermolizer
I
bortment with the door oben.
locking-
ond the
its com-
rieht.
For the same reason, the rudder spring must not be too strong.
The prototype was covered with Jap tissue, which was found
to be the strongest available. Grain should, of course run
from root to tip on wings and tailplane.
Two coats of thinned hear,y waterproof dope were applied
first, followed by two coats mixed wit}a 5o/o of castor oil.
Experiment
may be necessary as to the best quantity of
castor oil to add with a particular brand of dope, The proper
percentage will prevent over-shrinking
and consequently,
warps, and make a completely waterproof job.
The dethermalizer has been used in all weathers, and there
have been only two flyaways as a result. In both cases the cause
was faulty fuses; the use of parachute nylon, with its crease-
resisting qualities, makes the'chute 100 per cent. foolproof.
Thc 'chute is 14 ins, square and has four shroud lines.
attached one at each cornei, these being 14 ins. long. In the
centre of the 'chute, a 3 in. diam. hole is cut. A11edges should
be hemmed or doped to avoid fraying.
The 'chute is attached
to a hook on the fuselage under the tailplane and an eiastic
band draws it out of its comDartment when the door is released.
Trimming.
First, check all surfaces for warps and if any are present,
remove.
It is bad policy to endeavour to cancel out warps
with the rudder : in level flight the results mav be fair, but on
the line, towing difficulty rnay be experienced
When the
C.G. has been adjusted to the position shown, limit all
trimming to the tailplane.
I
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