发明名称 Aircraft propeller blade - is twisted about radial axis and is constructed from segments enclosed in elastic envelope
摘要 The propeller blade can be twisted about an axis at right angles to the axis of propeller rotation. The propeller blade is constructed from segments enclosed in an envelope of thin elastic material. Each segment (4-6) consists of two parts, a front part and a rear part (8,10,12). Each front part (7,9) is mounted on a bush (13) which is free to rotate on a shaft (1) which extends from the propeller blade root to the blade tip. The outermost front part (11) is secured to the shaft by a pin (21) to prevent relative rotation. Each rear part is attached to its corresp. front part by a bolt (16,17,18) which permits the rear part to rotate relative to the front part. The bolts are connected by a flat strip (20) which is rigid in the plane of the drawing but flexible in the plane at right angles to the drawing plane. USE - Propellers for aircraft and wind machines.
申请公布号 DE3943075(A1) 申请公布日期 1991.07.04
申请号 DE19893943075 申请日期 1989.12.27
申请人 LUTZ, FERDINAND, DR., 6148 HEPPENHEIM, DE 发明人 LUTZ, FERDINAND, DR., 6148 HEPPENHEIM, DE
分类号 B64C11/30;B64C27/46;F03D1/06 主分类号 B64C11/30
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