DE315694C - - Google Patents

Info

Publication number

DE315694C

DE315694C DENDAT315694D DE315694DA DE315694C DE 315694 C DE315694 C DE 315694C DE NDAT315694 D DENDAT315694 D DE NDAT315694D DE 315694D A DE315694D A DE 315694DA DE 315694 C DE315694 C DE 315694C

Authority

DE

Germany

Prior art keywords

wings

rigid

wing

aircraft

frame

Prior art date

Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)

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• 238000010276 construction Methods 0.000 description 2
• 210000000056 organ Anatomy 0.000 description 2
• XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 2
• PCTMTFRHKVHKIS-BMFZQQSSSA-N (1s,3r,4e,6e,8e,10e,12e,14e,16e,18s,19r,20r,21s,25r,27r,30r,31r,33s,35r,37s,38r)-3-[(2r,3s,4s,5s,6r)-4-amino-3,5-dihydroxy-6-methyloxan-2-yl]oxy-19,25,27,30,31,33,35,37-octahydroxy-18,20,21-trimethyl-23-oxo-22,39-dioxabicyclo[33.3.1]nonatriaconta-4,6,8,10 Chemical compound C1C=C2C[C@@H](OS(O)(=O)=O)CC[C@]2(C)[C@@H]2[C@@H]1[C@@H]1CC[C@H]([C@H](C)CCCC(C)C)[C@@]1(C)CC2.O[C@H]1[C@@H](N)[C@H](O)[C@@H](C)O[C@H]1O[C@H]1/C=C/C=C/C=C/C=C/C=C/C=C/C=C/[C@H](C)[C@@H](O)[C@@H](C)[C@H](C)OC(=O)C[C@H](O)C[C@H](O)CC[C@@H](O)[C@H](O)C[C@H](O)C[C@](O)(C[C@H](O)[C@H]2C(O)=O)O[C@H]2C1 PCTMTFRHKVHKIS-BMFZQQSSSA-N 0.000 description 1
• 230000015572 biosynthetic process Effects 0.000 description 1
• 238000005253 cladding Methods 0.000 description 1
• 230000010006 flight Effects 0.000 description 1
• 238000004519 manufacturing process Methods 0.000 description 1
• 230000003068 static effect Effects 0.000 description 1
• 239000003351 stiffener Substances 0.000 description 1