
基本信息:
- 专利标题: 一种直升机专用减振装置
- 专利标题(英):Helicopter dedicated damping device
- 申请号:CN201410188504.0 申请日:2014-05-07
- 公开(公告)号:CN105083527A 公开(公告)日:2015-11-25
- 发明人: 高磊 , 孙秀文 , 张亚军 , 赵泽乾
- 申请人: 哈尔滨飞机工业集团有限责任公司
- 申请人地址: 黑龙江省哈尔滨市平房区友协大街15号
- 专利权人: 哈尔滨飞机工业集团有限责任公司
- 当前专利权人: 哈尔滨飞机工业集团有限责任公司
- 当前专利权人地址: 黑龙江省哈尔滨市平房区友协大街15号
- 代理机构: 中国航空专利中心
- 代理人: 郭平
- 主分类号: B64C1/38
- IPC分类号: B64C1/38
The invention belongs to the technical field of helicopter design, and especially relates to a helicopter dedicated damping device. The helicopter dedicated damping device is characterized by comprising a base plate (1), an upper edge strip (2), a lateral edge (3), a lower edge strip (4), and a vertical rib (5); the base plate (1) is in a trapezoid shape, the upper edge strip (2) is arranged on the upper bottom edge of the base plate (1), the lateral edge (3) is arranged on the lateral edge of the base plate (1), the lower edge strip is arranged on the lower bottom edge of the base plate (1), and the vertical rib (5) is parallel to the upper edge strip (2) and the lower edge strip (4) and is arranged on the median line of the base plate (1). The base plate (1) is connected to the fuselage vertical web (14) through rivets; the upper edge strip (2) is connected to the fuselage vertical beam upper edge strip (9) and floor (15) through rivets; the lower edge strip (4) is connected to the fuselage vertical beam lower strip (13) through rivets; and the lateral edge (3) is connected to the edge gasket (8), frame web (10), and beam edge strip (11) through bolts and rivets. The damping device has the advantages of simple structure and lightness, and is convenient to installed, and the connection rigidity is adjustable.
公开/授权文献:
- CN105083527B 一种直升机专用减振装置 公开/授权日:2017-04-19
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 |
------B64C1/00 | 机身;机身,机翼,稳定面或类似部件共同的结构特征 |
--------B64C1/38 | .适合于减少空气动力效应或其他外部加热效应的结构 |