| 发明名称 | Alignment system and methodology to account for variation in a gas turbine engine | ||
| 摘要 | A gas turbine engine includes a bushing that is non-round in cross-section, the bushing receivable within an aperture. A fastener passes through the bushing to retain a second component to a third component with respect to the first component. | ||
| 申请公布号 | US9470151(B2) | 申请公布日期 | 2016.10.18 |
| 申请号 | US201213725312 | 申请日期 | 2012.12.21 |
| 申请人 | United Technologies Corporation | 发明人 | Ruberte Sanchez Jose E.;Wong Joey;Ricciardo Mark J.;Hanson Russell B. |
| 分类号 | F02C7/20;F02K1/80;F02K3/10;F16B35/04;F01D25/16;F16B33/00;F16B43/00 | 主分类号 | F02C7/20 |
| 代理机构 | O'Shea Getz P.C. | 代理人 | O'Shea Getz P.C. |
| 主权项 | 1. A gas turbine engine comprising: a first component with an aperture; a bushing that is non-round in cross-section, said bushing receivable within said aperture; and a fastener which passes through the bushing to retain a second component to a third component with respect to said first component, said third component with an elongated aperture greater in size than said aperture, said elongated aperture located within a recess, wherein said bushing includes a set of tabs and said fastener includes a head receivable between said set of tabs, and wherein said fastener includes a rectilinear interface section that corresponds with a rectilinear bushing aperture through said bushing. | ||
| 地址 | Farmington CT US | ||