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Model helicopter powered by miniature combustion engine - has cable operated linkage controlling lift blade angles of incidence

机译:由微型内燃机驱动的直升机模型-具有缆索操纵的连杆机构,用于控制提升叶片的入射角

摘要

The fuselage is made from reinforced plastic and fitted with landing gear and fuel tanks (1, 3). The power unit (5) is mounted in the central section with its output shaft vertical. The blade (17) hub fits directly onto the motor shaft and the blades have rods (14) linking their roots (16) to a disc (15) fitting around, and sliding on, the motor shaft. The blades are spring biased (18), giving a rest position under no load conditions. A lever (8) mounted on the engine brackets (7, 9) is cable (10) operated and raises a fixed disc (13) by means of two linking rods (11). This disc pushes up the spring biased disc to alter each blade angle of incidence.
机译:机身由增强塑料制成,并装有起落架和燃油箱(1、3)。动力单元(5)的输出轴垂直安装在中央部分。叶片(17)轮毂直接安装在电机轴上,叶片具有杆(14),这些杆(14)将其根部(16)连接到围绕并在电机轴上滑动的圆盘(15)。叶片受弹簧偏压(18),在空载条件下处于静止位置。电缆(10)操纵安装在发动机支架(7、9)上的杠杆(8),并通过两个连杆(11)升高固定盘(13)。该圆盘向上推弹簧偏置的圆盘以改变每个叶片的入射角。

著录项

  • 公开/公告号FR2269986B1

    专利类型

  • 公开/公告日1977-06-24

    原文格式PDF

  • 申请/专利权人 NITTI ITALO;

    申请/专利号FR19740016516

  • 发明设计人

    申请日1974-05-07

  • 分类号A63H27/12;

  • 国家 FR

  • 入库时间 2022-08-22 23:51:48

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