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Aviation History
1919
1919 - 0597.PDF
account the special requirements of the aircraft which are extensively employed in aircraft construe - industry, which are in some cases somewhat different tion for various fittings, the importance of maximum to those obtaining in other branches of engineering, strength for minimum weight calls for somewhat Thus, in the case of mild-steel plates, for instance, smaller tolerances than are generally considered FLIGHT s 1* ! s •«* J Mi ; t : > Bill ""I 2 1 WEICHT or STEEL TUBES /A /AS «* fl»r /R&rr,- ,„. WklQHT 1/1 LBS P£R CUBIC I1CH - • 299 (flcciES 4 POLLOCK) ..... FOOT- 699-6 BMMOMNI orWuus m SW( 10 It IX /3 fr fS /<, 17 ft 19 20 21 2% OUTSIDE DlflMETER IN INCHES f •J4.2 •324 •307 •29% •1ST '231 •2/3 */** •169 •ILf •126 •lilt •103 -k */9 493 %SI %ai •367 •3 it, •300 •Z7Z •234. 'Zoif •m. •1*9 •/60 *r r •(.97 •C4Z •395 •533 •iTfl. '422 •3g>$ •34P '299 •259 -2/9 •20I •177 •F74 •too •740 •6S9 •3Fi. •317 '47/ •VLS J64 •31$ •265 •243 'W -Z- /•OS/ •959 •Wit- •7PS •696 •t/2 SSI •301 •42P •370 •31/ •293 •251 / /•229 liip 1-0 2 S> •9/0 •tot, •707 •64.3 •57F •4.93 •4-2(. •35T •32V •2rr it Wot, 1-277 /•/72 1-036 •9/& •tos '729 •as •5SF •4tz. '4*4 •370 32S /i 1*4.9 1-436 /•3/7 /•/C.2 /•02S •F9F •9/5 '731 •623 •S3 7 •ISO *» •362. /# 1723 1-59 4. /•4b/ 1-297 /•/35 •993 •90/ •TOP •tse •570 •515 •4*9 '403 fit 1996 /7S3 11.05 I-4J3 1-24.3 /•Off •9t7 •FF5 •747 •624 f t 204.9 /•?/2 1-749 1-539 /-35S I/F4 /•073 •962. •tot •477 •3bi [-64.4 1 •492,'\-*44 •4+0 •477 ft 2-239 2-07/ 1-996 1U4 1-463 1-279 I-IS9 /-03? •F72 •720 •659 •597 •5/5 <r 2409 2-Z30 2-039 1-790 I-S76 1-375 /•24S *//S •956 •794. •701 If 50 •S52 Z 2-397 2-399 2-192 l-9/h f-trs I-Jf70 /•33I /•/9Z /•OOO •137 •75* •6 72. •399 2t z* • t*-2p zk 29 2* 1 1 • Fig. 33. ' ; 1 1 l| - , . r i I: 1 > 3 a* & :S " :* •< I1! l! to to to r 1 ' i > >z ,"* : 2 1 1 WEIGHT or 3/e/iss TUBUS in ias SMMMB in SMS 10 II 12 /3 IU /S /6 (/7 IS 19 20 11 Zl i mm, ' PER FOOT *UH ^/<VT m LBf ^ e m .„, c rr 3iy OUTSIDE D/Aficren iff /ITCHES f •3U1 3L,ZI •324-Z •2979 •2174 •244- •IIS •206 •I7t5 1563 •133 -I2Z4- •/0F7 ± fir* •5/0 •471. •4.30 •3t7S •344 •3161 •2P7/ •247 •2/53 •if/i •1679 •/47S1 * •736 •6773 •62P •363 •302S •44* •4oi4 •3675 • 3139 •2734. •2313 •2/ZZ •1969 •923 S45 •m •696 •619 •54-i •4-97 •U97 •3943 •3323 •2?0 •23U •226 9 III /•Oil •934 ez9 •733 •446 •399 •5Z9 •45Z •3906 •32fS 30OP 21,51 1 1299 l-lf I0f4- •96/3 •951 •74X. •679 •C/ot •5205 •4*o •379 •3463 •3041 ft 1-493 1349 1-239 /-093 •169 •su? •77 •69Z •Jff 509 •4265 •3905 •343 ft 1-634 1-515 1390 1-229 1 072 •969 261 •773 •iSF •367 •4755 •^34 •3923 ft 1920 I-69Z f-MZ I-3S9 1199 I04S •951 •fSL. •7263 •6015 •56+ •495 •62 6 fir 2005 1 932 lk9S 1'492 /•3I4 1-14-9 1 04 •93S •799 •659 •5963 •5195 •4663 / 9 2/94 2-02 /•94b l-iZS 1-63 1-25 1 132 1-015 •954 •y/5 •690 •575 •504 fi 2-36/ 2-IE-4- Z-o /•737 1-547 1-35 1221 1-097 •92/ •7UI •695 •(,20 •54-4 ft 2*42 2-335 2 ISO 1-991 1-66/ t-451 1-314 1-111 •999 i29 •746 •ass •5929 2 2-733 2-5ZZ 2 303 2-011 1-179 I-55Z I-40S I-Z60 1056 •Sf4- •7975 •7099 •4 2.2. zt I Zf 2i H if H • 1 ! : Fig. 34. 597 H 2
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