基本信息:
- 专利标题： SHOCK ABSORBER CONFIGURED WITH A DEFORMABLE ENERGY ABSORBING MEMBER
- 申请号：PCT/US2019/013929 申请日：2019-01-17
- 公开(公告)号：WO2019143764A1 公开(公告)日：2019-07-25
- 发明人： YADOLLAHI, Morteza , MANARA, Alan
- 申请人： ADAMS RITE AEROSPACE INC.
- 申请人地址： 4141 N. Palm Street Fullerton, California 92835 US
- 专利权人： ADAMS RITE AEROSPACE INC.
- 当前专利权人： ADAMS RITE AEROSPACE INC.
- 当前专利权人地址： 4141 N. Palm Street Fullerton, California 92835 US
- 代理机构： HILTEN, John S. et al.
- 优先权： US62/618,546 20180117
- 主分类号： B64C1/14
- IPC分类号： B64C1/14 ; E05F3/00 ; F16F7/12 ; F16F9/00 ; F16F9/16 ; F16F9/48 ; F16F9/58
摘要：
A shock absorber includes a first end configured to be mechanically fastened to a first component, a second end configured to be mechanically fastened to a second component, a main body, a main shaft, and a primary piston. The primary piston configured to move within the main body and further configured to provide a first damping force by movement of a fluid through the primary piston while the main shaft moves a first distance. The shock absorber also includes a deformable solid material arranged in the main body. The primary piston configured to further move within the main body and further configured to provide a second damping force by deforming the deformable solid material after the main shaft moves the first distance.
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 |
| --------B64C1/14 | .窗；门；舱盖或通道壁板；外层框架结构；座舱盖；风挡 |