FIELD: mechanics; aircraft construction.
SUBSTANCE: invention is referred to bulkhead of aircraft body frame capable of carrying significant loads at light weight characteristics. The bulkhead of aircraft body frame contains a low bail, cross beam retaining decking element, lattice girder connecting the said low bail and cross beam. The bulkhead includes upper bulkhead element with fastening shoulders, which ensure connection with cross beam and low bail. The upper bulkhead element forms aircraft body bulkhead together with low bail.
EFFECT: designing of bulkhead having high response rate and height and low weight.
12 cl, 6 dwg
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