| 发明名称 | Flexible seal system for a gas turbine engine | ||
| 摘要 | A flexible seal system for a gas turbine engine includes an annular mounting bracket, an annular support bracket, an annular flexible seal and a plurality of mounting spacers. The flexible seal extends axially between a first mounting segment and a second mounting segment. The first mounting segment is connected axially between the mounting bracket and the support bracket, and includes a plurality of mounting apertures that extend axially through the first mounting segment. Each of the mounting spacers is arranged within a respective one of the mounting apertures, and extends axially between the mounting bracket and the support bracket. | ||
| 申请公布号 | US9284889(B2) | 申请公布日期 | 2016.03.15 |
| 申请号 | US201113297458 | 申请日期 | 2011.11.16 |
| 申请人 | United Technologies Corporation | 发明人 | Damgaard Jocelyn C.;Roberts Steven D.;Dale Timothy |
| 分类号 | F02C7/28;F02K1/80 | 主分类号 | F02C7/28 |
| 代理机构 | O'Shea Getz P.C. | 代理人 | O'Shea Getz P.C. |
| 主权项 | 1. A flexible seal system for a gas turbine engine, comprising: an annular mounting bracket; an annular support bracket; an annular flexible seal extending axially between a first mounting segment and a second mounting segment, wherein the first mounting segment is connected axially between the mounting bracket and the support bracket, and comprises a plurality of mounting apertures that extend axially through the first mounting segment; and a plurality of mounting spacers, each arranged within a respective one of the mounting apertures, and extending axially between the mounting bracket and the support bracket; wherein the flexible seal is constructed from an elastomer composite that comprises a plurality of fibers, and wherein a quantity of the fibers are laid oblique to an axially extending contour line of the flexible seal. | ||
| 地址 | Hartford CT US | ||