SYNTHETIC MATERIALS IN AIRCRAFT PRODUCTION
Document Type:
Collection:
Document Number (FOIA) /ESDN (CREST):
CIA-RDP62-00328A000100510009-1
Release Decision:
RIPPUB
Original Classification:
S
Document Page Count:
5
Document Creation Date:
December 9, 2016
Document Release Date:
February 13, 2001
Sequence Number:
9
Case Number:
Publication Date:
August 5, 1958
Content Type:
MF
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Approved For Releasits2001/03/02 : CIA-RDP62-00328A000100510009-1
? ? ?
(WITH UNCLASSIFZED ATTACHMENT)
EDIC/ID
Centro/ No. 487847
5 August 1958
MEMORANDUM FOR: Econsmi Defense Intelligence Committee
FROM : Executive Secretary, EDIC
SUBJECT : Synthetic Materials in Aircraft Production
REFERENCE EDIC/ID - 34, SECRET
The attached abridged translation of am article by Major Genciml.
(Engineering Services) A. Tumanov? entitled "Synthetic Materials in
Aircraft Pro2uction"? discusses in sone detail the use of "glass tex-
tolite"(glass fiber reinforced plastic sheeting) as a sdhatitute .for
nettals in certain pNasace of aircraft production. This article appeared
in the Russian mamasine SOVIETWAYA AVIATSIYA (Soviet Aviation) of
25 May 1958. The trarzlatica is submitted to EDIC methers as being
wertinont to EDIC/ID - 34, "The Glass Fiber Industry in the Siao-Soviet
11.1]zeutive Secretary
;11tachlr.ent:
Ss-utleJAie Materials in Aircraft P duction
25X1A9a
ribution:
Ct B (3-55
(All)
(3)
8, 10)
k.,,,:roiarril USA kriet.
Direlei:45r, Coordination
HITH UNCLASSIFIED ATTACHMENT)
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25X1A9a
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'1YERIPTIC &irlivRIALS ir kniCROT Ca'15TRUCTION
lyhjor-Geofzelo Ergancering Swettlump
A. T4.111MOV
AviatAyas 1958,, N-41 25.
". ?Nr cel.
,tairldiffea Tranal.atten
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q/eTekTIC MATERIALS IN AIRCRAFT wiz:Lump!
By Wor-General, Eneineering Service
A. Tunenor.
eovetskeya Aviateiya, 1958, May 25.
4.11..mowt.
&rid-led Trasalation
man.
=zealotry ploys a very isportant role in aircraft
eezetructicn. Peoduction of rodern aeroglanes is unthinkable with-
out ueing e. vest -variety of syntbetic materias wad plestics.
Evea during the second world ear & very high strength tier plaetic,
"de/tee-blame, 'gee usod for the in streaoed aent of Tighter
elm:aft. The propellor blades for light aircraft and helicopters
ere asobeina node or a timber plastic. Combined 'with otter ateetala
it io used for the interior of the new passenger planes fn-104,
S1-181 in-10 axd Tu-13J.
CPYRGFE In modera aircraft so-called foam plastics awe extensively nallap
;4ereinbt of ehich ia eremy tines nsaller thee even tho very light
mete/ nnemestma. Due to their good beat and souad insulation pro-
perties, they canto used as fillers for internal walls and panels.
Uhen making closed volume out of sheets, for instance control
Tunders, it is frequometly almost impossible to ensure adeqgate
riffidity and in this come self-Toaning ylastics axe very useful.
Intronuction or a certain en:entity of such plastics into a closed
volume end subseqgent 'denting ensures unifonn filling of the entire
voleee, a stroae bond of the foam layer with the metal and a high
eigidity of the desien.
By weaning foam layore with atiffenteg elements "araoared
fonee layere" are cbteined in wbich veneer elass-textolite and vari-
ous sheet retelo are used. Such reinfore4 foam layers are succeas-
fully used as fill.= in pane/o fee. eith veneer in the pact/anger
aircraft Te-104, Tu-114, ii-18; Ia additioa to increased rigidity
ma strength, these materials ensure a conaiderably reduced weight.
It is well know tent the problem of reducing the 'weight of
aircraft is one of the met acete in eviation engineering. Reduction
by even 0.02 g of the snecific weight per cubic centimetre of the
foam plestic laud in the above mentioned aircraft would enable the
Bevies of bundreds of kg of weight in very Large aircraft like the
Accor di to Soviet Civil Air Line data reauction of the
'might of a passmeger aireraft by only 1 ka produces an annual economy
in tile operation of the machines of about 2000 roubles. Consequently
the reduction in weight by 300 kg for 100 aircraft leads to an
aroma economy of about 60 million rouble
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CPYRGHT
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Plastics base. 011 east. fab:lle? glesse fibre and various
kesins of high#5,17etolf:7,?o strength 4-2.1ad 41 anther a other properties
ere exte-gLeively urea fin aviatiaa eAsineeeing. Ittuufactum of large
Ccfgat4flelittin fma cac;7s.lo-te=tolito by the mothei of shaping applylvt:g
rilyezte:r?bi1r,f7f,Errz4.!tr.., aistplItir and cheapem caesideratly the
ta-chnolet7iwal 'process, se coosper410. to nalwit'acturs a tate& componsats
f-m.m neot IgptILL In a tumitter 4?:r CSISUS CalTiidOr.able sexing ta
T7.6.,sitt ang in -the diffieulty ofnagernstite.3:e le obtained
emorzaant, atrAlgik? Fcr instemm, tIze manufnebrne ?
of: eaenteiners11.1497A.1jane nteCe fkon glass-tantolite ad used as
coft feel temkgin airlraIN; 1;,Teight retuction by almost
trre. t.1',1f131SASNU11.1.tiG for AZ ."&I.es of aerial cameras szt;')Ife,.,s
idfrailleticin of tessePoioz the rf:A7..%irgof*lob does .7?.?Aot
fag a. r.agazit taVEA.ratILAV:1 arro tte seafficiead of 11E,imear
4.-nT.4:r,frarliem of '7-ktia cad of .Y.-atc- 0.9103-taRrtelite housin
In.,,rier to each other. FLIrthensole7 substitutioner Cap
zntel by Glaos-tortolit!t EirataTeCtV. e. weight mimetic= of 44he body by
P,:fg to P5%:.
Tfy7:1*-ifentoY5tes: Arie% ..agc? 7abia-vec. ragiG cv.a-gzaLc-Ang
cazbink.11::en. 11-..LEke. layerz or h..-4.araendo
Pitaterie,..a trel cortcAn tes.-4-3ikansture wage
tIlny 1?1,ociplueralitle flarin2: radio Lo*.L1;ion ontef-,?.m.,pe. By
cz.:....i1fsir4n.fj ',Amen fith al:tif.7eie1 rosins 716117 tpilealkc?ty staiike
Aftlitill iStit str.ch ALVICIAS parte, '4: aircraft instrl-
rr:?.:r; corpaaenti. ox:' sedaced. 7.:LyiJloressi.,
Pe2v,p2rit is usee. gand.ovm?
pmperties., s ppeciAc 4,,ravity eart., poraits producing
offe.-zip.c000ts of ok,y e.a?ltiourAsties. Rad it is ate13..I.11 to the effects
of atmospheric! eflYtditions. A die,,sdvantege of thl..s material is its
consit.17114.. to 3t/VOS Calleek:Oateti011. devcaopea&
jt"ti-g).=?=4;91. o-::" the persp,6r. ,lraving it at at
t!?.o. softeritug point of :e.7'...ass enabled obtaining
q2.ata:14..,e.tively Tema material, without atty 0.%:!!,I.7.3.10,..a in, chemical
itectich free of the above 7.Am-timed defect. Systbatie
end glues sm availSble ?7"1.1.:1 have a strong
to 141Y-tte:.:.teht .1.726*.V fat,21,141 c.1.! he most reliable
4:::ZTZLY,tii0:7nIy pra.Itteable st.frehod of joining non.-
Fsatcr:?iale slf-kth, attain eeikergeneo of ouch aue= hag
Tor the :31.7.,..317, 1,,rtall the 11114i? of 711110 for jokaing aetL
G171n.:7, n':Its.1 cosporiens elirolnatestL4tiisadvantmeea
fa-;.ent by rivetting, weldiug and ana, thorefo2s,
1:setb4 1 -Luling used on a???1 cale la aviation and
bri,Arelesri
Eeciy,:ritly? (glues ha-ro akly) Neczit,?-z?-,, 14-Tide
With fricttca discs for
cTi.7,c2.1 a:L.4o far g1us!,41--ceed gluoil-livetted joints
Aft aM w.,elf?-?fopters.
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CPYRGHT
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Application of glued joimts in the manufacture of helicopthr
blades enabled ialaroving the quality ant increasing their lifetime
to doUble and even mowe.
Local stress concentrations whieh occur around rivets, weld
spots, etc., distribute uniformly throughout the surface of tha
joint in the CE30 of glued joints and thereby enables sipplitiection
of the design end ensures a surface ?lash is smoother than that of
rivetted, welded or soldered joints.
New types of synthetic resins, particularly epoxide resins,
permit using more economic systcas of doping aircraft,. the coatiag
(gm be ea:plied directly to the metallic sheathing eittaut using
2ny priwnr (oil varnish ow glyptal zinc chromate primer). Use of
such doping systems In modern aviation permits saving of hundreds
of tons of prineri, and dogeas of to of vegotsble oils required
for manufacturing then.
It-is not possible to enummmte uithin bort article the
gl:eat variety of synthatic,mnteriels used for aircraft construction
but the few exaTemlas show clearly the impprtance of plastics and
otber synthetic ws9tria1s la aviation emIntering.
The successful fnlfillnent of the decree of the Central
Allmiunist Party on accaerating the development of the chemical
ilastry and wartioularly of the manufacture Gf synthetic materials
ke of great national importance ie. the Soviet Union.
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