| 发明名称 | Systems and methods for heat shield assemblies | ||
| 摘要 | Systems and methods disclosed herein may be useful for aircraft heat shield assemblies. In this regard, a heat shield assembly is provided comprising a heat shield having an aperture, the aperture comprising an end portion and an insertion portion, the insertion portion having a width larger than the end portion, a spacer comprising an upper portion, an undermount flange and a gap between the upper portion and the undermount flange, wherein a surface of the gap is engaged with the heat shield, and wherein the undermount flange has a width less than the insertion portion of the aperture and greater than the width of the end portion. | ||
| 申请公布号 | US9103393(B2) | 申请公布日期 | 2015.08.11 |
| 申请号 | US201213552334 | 申请日期 | 2012.07.18 |
| 申请人 | Goodrich Corporation | 发明人 | Houser Joshua Craig;King Katrina Lynn |
| 分类号 | F16D65/78;F16D55/36;F16D65/84 | 主分类号 | F16D65/78 |
| 代理机构 | Snell & Wilmer LLP | 代理人 | Snell & Wilmer LLP |
| 主权项 | 1. A heat shield assembly comprising: a heat shield having an aperture, the aperture comprising an end portion and an insertion portion, the insertion portion having a width larger than the end portion; and a spacer comprising an upper portion, an undermount flange and a gap between the upper portion and the undermount flange, wherein a surface of the gap is engaged with the heat shield, and wherein the undermount flange has a width less than the insertion portion of the aperture and greater than the width of the end portion. | ||
| 地址 | Charlotte NC US | ||