COMPOSITE BLADING MEMBER AND METHOD FOR MAKING
14 ABSTRACR COMPOSITE BLADTNG MEMBER AND METHOD FOR MAKING A COMPOSITE BLADING MEMBER (10) INCLUDES AN AIRFOIL (12) AND A BASE (20) OF COMPOSITE MATERIAL LAYERS (40) AND A PLATFORM (38) OF COMPOSITE MATERIAL LAYERS (40) INTERFUSED WITH THE AIRFOIL (12) AND BASE (20). THE PLATFORM (38) COMPRISES A PL...
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Main Authors | , |
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Format | Patent |
Language | English |
Published |
31.01.2011
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Subjects | |
Online Access | Get full text |
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Summary: | 14 ABSTRACR COMPOSITE BLADTNG MEMBER AND METHOD FOR MAKING A COMPOSITE BLADING MEMBER (10) INCLUDES AN AIRFOIL (12) AND A BASE (20) OF COMPOSITE MATERIAL LAYERS (40) AND A PLATFORM (38) OF COMPOSITE MATERIAL LAYERS (40) INTERFUSED WITH THE AIRFOIL (12) AND BASE (20). THE PLATFORM (38) COMPRISES A PLATFORM SHELF (42) AND A PLURALITY OF SPACED-APART PLATFORM SUPPORTS (44,46) INTEGRAL WITH THE PLATFORM SHELF (42) AND INTERFUSED WITH SURFACES (26,28) OF THE BASE. SUCH BLADING MEMBER (10) WAS MADE BY PROVIDING A PARTIALLY CURED AIRFOIL-BASE PREFORM (36) AND A PLATFORM PERFORM (38), INCLUDING AN AIRFOIL SHAPED OPENING (43) THERETHROUGH AND 10 PREFORMS OF THE PLATFORM SUPPORTS (44,46). THE AIRFOIL-BASE PREFORM (36) WAS INSERTED THROUGH THE AIRFOIL SHAPED OPENING (43) WHEREBY COOPERATING SURFACES OF THE PLATFORM PERFORM (38) AND AIRFOIL-BASED PREFORM (36) WERE IN JUXTAPOSITION. THE PERFORMS (36,38) WERE HEATED TO PARTIALLY CURE THEM TOGETHER. THEN THEY WERE INTERFUSED WITH A BINDER COMPATIBLE WITH MATERIAL OF THE PREFORMS (36,38) UNDER CONDITIONS TO 15 SUBSTANTIALLY FULLY CURE THE STRUCTURES. |
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Bibliography: | Application Number: MY2006PI04730 |