| 发明名称 |
Max Phase Reinforced Polymer Matrix Composite Abradables with Enhanced Thermal Conductivity |
| 摘要 |
A turbine engine system comprising a turbine engine component, such as a fan includes a fan casing and a fan blade rotatable within the fan casing. An abradable seal coupled to the fan casing proximate the fan blade. The abradable seal comprising an abradable composite layer including a MAX phase solid and a polymer based abradable composition. |
| 申请公布号 |
US2016327059(A1) |
申请公布日期 |
2016.11.10 |
| 申请号 |
US201514709721 |
申请日期 |
2015.05.12 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
Amini Shahram;Strock Christopher W.;Guo Changsheng |
| 分类号 |
F04D29/52;F04D29/02;F04D29/16;F02K3/06;F04D19/00 |
主分类号 |
F04D29/52 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A turbine engine system comprising:
a turbine engine fan section; said fan section including a fan casing and a fan blade rotatable within said fan casing; an abradable seal coupled to said fan casing between said fan casing and said fan blade, said abradable seal comprising an abradable composite layer including MAX phase solids and a polymer based abradable composition. |
| 地址 |
HARTFORD CT US |
