DIVERSE DEPLOYABLE TUYERE FOR ROCKET PROPELLER

摘要

P DEPLOYABLE DIVERGENT OF FUSED PROPELLER NOZZLE, INCLUDING A SET OF ELEMENTAL INDIVIDUAL REFRACTORY PANELS BETWEEN THEM AND RELATIVE TO A FIXED UPSTREAM OF THE DIVERGENT NEAR THE TUYERE NECK, WHICH IS CHARACTERIZED AS THE ARTICULATIONS , 3 INTENDED TO BE FOLDED ONE OVER THE OTHER WITH THEIR INTERNAL FACES21, 31 IN REGARD TO ONE OF THE OTHER INCLUDE EACH AT LEAST ONE HINGE7 WITH TWO AXES11, 12 INSERTED IN THE WALLS OF THE TWO ARTICULATED PANELS ONE TO THE OTHER, AND MAINTAINED AT A CONSTANT REMOTE FROM ONE ANOTHER BY A CHAIN13 PROVIDED WITHDRAWAL IN RELATION TO THE THICKNESS OF THE PANELS AND IN THAT TWO ADJACENT PANELS PRESENT IN THE NEIGHBORHOOD OF A HINGE TWO CYLINDRICAL SURFACES14, 15 CENTERED RESPECTIVELY ON EACH AXIS 11, 12 AND CAPABLE OF RUNNING WITHOUT SLIDING ON ONE ANOTHER. /P