Multifunctional pod for an aircraft |
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| 申请号 | US15082219 | 申请日 | 2016-03-28 | 公开(公告)号 | US10086941B2 | 公开(公告)日 | 2018-10-02 |
| 申请人 | Airbus Defence and Space GmbH; | 发明人 | Horst Christof; | ||||
| 摘要 | A multifunctional pod for an aircraft has at least two separate regions. At least one first region of the pod is provided for receiving fuel. A second region of the pod includes at least one receiving device for releasably attaching at least one additional load. The additional load can be releasably attached to the receiving device via a loading opening on the side of the pod facing away from the aircraft. | ||||||
| 权利要求 | |||||||
| 说明书全文 | |||||||
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