METHOD OF ASSEMBLY OF FLYING VEHICLE STRUCTURAL MEMBERS

FIELD: aviation; methods of assembly of wing outer panels. SUBSTANCE: simultaneously at pressing off the upper skin by means of pressing-off devices 4, members of longitudinal framework 6 secured on this skin and sealed up at joint area are pressed off. EFFECT: reduction of time required for assembl...

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Bibliographische Detailangaben
Hauptverfasser:	Tsvetkov E.A, Sedov A.D, Mishin V.I
Format:	Patent
Sprache:	eng ; rus
Schlagworte:	AIRCRAFT AVIATION COSMONAUTICS DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR PERFORMING OPERATIONS TRANSPORTING
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Beschreibung
Zusammenfassung:	FIELD: aviation; methods of assembly of wing outer panels. SUBSTANCE: simultaneously at pressing off the upper skin by means of pressing-off devices 4, members of longitudinal framework 6 secured on this skin and sealed up at joint area are pressed off. EFFECT: reduction of time required for assembly; facilitated procedure and improved quality of coupling jobs. 1 dwg Изобретение относится к области авиации, а более конкретно к способам сборки консольных частей крыла летательного аппарата. Цель изобретения - сокращение времени, повышение технологичности и качества стыковочных работ. Для этого одновременно с отжатием верхней обшивки с помощью отжимных приспособлений 4 осуществляют отжатие элементов прикрепленного продольного набора 6, закрепленных и загерметизированных на ней в зоне стыка. 1 ил.