FIELD: aircraft engineering.
SUBSTANCE: proposed device comprises insert, fasteners and detonating charge. Said insert has lugs to connect it to aircraft separating elements. Note that said insert is fitted with gaps between lug transverse faces and those of separating elements. Insert central part has through channels to accommodate elongated charges. Gaskets are fitted between insert lugs and jointed parts, their acoustic compliance exceeding that of insert and separating elements.
EFFECT: reduced impact loads on jointed elements, preset stiffness of joint.
2 cl, 5 dwg, 1 ex
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Authors
Dates
2010-05-20—Published
2008-10-07—Filed