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HELICOPTER TAIL ROTOR BLADES AND BLADE ASSEMBLIES

机译:直升机尾桨叶片和叶片组件

摘要

A tail rotor blade for a helicopter includes a blade body defining a longitudinally extending spar cavity, a leading edge forward of the spar cavity, and a trailing edge aft of the spar cavity. Upper and lower airfoil surfaces extend from the leading edge to the trailing edge on opposite sides of the spar cavity. The upper and lower airfoil surfaces define between one another a constant airfoil segment and transition airfoil segments disposed longitudinally adjacent to the constant airfoil segment on inboard and outboard sides of the constant airfoil segment.
机译:用于直升机的尾旋翼桨叶包括桨叶主体,该桨叶主体限定了纵向延伸的翼梁腔,翼梁腔前方的前缘以及翼梁腔的后缘。翼型的上,下表面在翼梁腔的相对两侧从前缘延伸到后缘。上翼面表面和下翼面表面在彼此之间限定恒定翼型片段和在恒定翼型片段的内侧和外侧上在纵向上邻近于恒定翼型片段布置的过渡翼型片段。

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