
基本信息:
- 专利标题: Modular counter rotating propeller system
- 专利标题(中):模块化反向旋转的螺旋桨系统
- 申请号:EP12179560.3 申请日:2012-08-07
- 公开(公告)号:EP2557033A3 公开(公告)日:2015-11-11
- 发明人: Perkinson, Robert H.
- 申请人: Hamilton Sundstrand Corporation
- 申请人地址: One Hamilton Road Windsor Locks, CT 06096-1010 US
- 专利权人: Hamilton Sundstrand Corporation
- 当前专利权人: HAMILTON SUNDSTRAND CORPORATION
- 当前专利权人地址: HAMILTON SUNDSTRAND CORPORATION
- 代理机构: Hull, James Edward
- 优先权: US201113208648 20110812
- 主分类号: B64C11/48
- IPC分类号: B64C11/48 ; B64C11/30
摘要:
A self-contained counter rotating turbo prop system (14) is driven by a gas turbine engine (10) through a reduction gearbox (12). A gear train housed separate from the reduction gearbox (12) provides the counter-rotation of a first and second pluralities of propeller blades (18,20). The entire counter-rotating propeller system (14) is disposed within cowlings (16A,16B) and is separate from the gas turbine engine (10) and reduction gearbox (12). The counter rotating propeller system (14) includes a collective blade angle actuation system (55) that provides for adjustment of blade angle of both the first and second plurality of propeller blades (18,20) with a single actuator.
公开/授权文献:
- EP2557033B1 Modular counter rotating propeller system 公开/授权日:2019-10-02
IPC结构图谱:
B | 作业;运输 |
--B64 | 飞行器;航空;宇宙航行 |
----B64C | 飞机;直升飞机 |
------B64C11/00 | 螺旋桨,例如管道型的;螺旋桨和旋翼机旋翼共有的特征 |
--------B64C11/02 | .桨毂结构 |
----------B64C11/48 | ..两个或多个同轴螺旋桨的装置 |