发明名称 PROPELLER BLADE RETENTION DEVICE
摘要 A propeller blade retention system and method of manufacture are disclosed. Because of the design, a truly integral hub is able to house a set of variable pitch blades. Each hub socket establishes a substantially cylindrical interface with its respective blade, making the blade slidably receivable for installation. Each blade is allowed axial rotation, and held inside the socket by a set of angular contact bearings. A snap ring locks the blade against coming back out of the socket. An O-ring is provided in the interface to create a fluid seal. The hub alone accomplishes all of the required load-bearing and weather-seal functions.
申请公布号 WO2009142792(A2) 申请公布日期 2009.11.26
申请号 WO2009US35513 申请日期 2009.02.27
申请人 CESSNA AIRCRAFT COMPANY;BALL, DANNY;PFEIFFER, KEVIN 发明人 BALL, DANNY;PFEIFFER, KEVIN
分类号 B64C11/30;B64C11/06;B64C27/473;B64C27/54 主分类号 B64C11/30
代理机构 代理人
主权项
地址