FIELD: aerospace engineering. SUBSTANCE: three-layer fuselage fairing is secured to case by means of adapter members located at definite pitch and made in form of nonmetallic brackets from organotextolite, for example; one end of fuselage fairing is rigidly secured to brackets longitudinally; other points of attachment are movable in this direction; in transversal direction, one side of fuselage fairing is secured rigidly and other side is mounted for motion in transversal direction. EFFECT: enhanced reliability and avoidance of damage to functional members. 2 cl, 3 dwg
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Authors
Dates
1997-02-10—Published
1993-06-30—Filed