| 发明名称 |
RECEPTACLE, PAYLOAD ASSEMBLY AND RELATED METHODS FOR AN AIRCRAFT |
| 摘要 |
An aircraft includes a support structure, an outer skin coupled to the support structure, and a port that defines a break in the support structure and extends through the outer skin. The aircraft also includes a receptacle coupled to portions of the support structure proximate the port, such that the receptacle routes at least a portion of the load borne by the support structure around the break defined by the port. The receptacle includes an opening defined therein. The aircraft further includes a removable payload assembly coupled within the receptacle opening, and a pressure ring configured to form a seal between an inner surface of the receptacle and an outer surface of the payload assembly. |
| 申请公布号 |
US2017050717(A1) |
申请公布日期 |
2017.02.23 |
| 申请号 |
US201615241894 |
申请日期 |
2016.08.19 |
| 申请人 |
Georgian Aerospace, LLC |
发明人 |
Scimone Michael J.;Vollmer Richard;Simansky Joel;Henke Jason |
| 分类号 |
B64C1/14;B64F5/00 |
主分类号 |
B64C1/14 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. An aircraft comprising:
a support structure; an outer skin coupled to the support structure; a port that defines a break in the support structure and extends through the outer skin; a receptacle attached to portions of the support structure proximate the port, such that the receptacle routes at least a portion of the load borne by the support structure around the break defined by the port, the receptacle comprising an opening defined therein; a removable payload assembly mounted within the receptacle opening; and a pressure ring forming a seal between an inner surface of the receptacle and an outer surface of the payload assembly. |
| 地址 |
Chesterfield MO US |
