公开(公告)号：US11999509B2

公开(公告)日：2024-06-04

申请号：US17322739

申请日：2021-05-17

申请人： Pratt & Whitney Canada Corp.

发明人： Daniel Mackay

IPC分类号： B64F5/40 ,  B60L9/00 ,  B60L50/50 ,  B60L53/16 ,  B64D27/24 ,  B64F1/36

CPC分类号： B64F5/40 ,  B60L9/00 ,  B60L50/50 ,  B60L53/16 ,  B64D27/24 ,  B64F1/364 ,  B60L2200/10

摘要： A system for an aircraft includes an electric energy module and a connector module operatively connected to the electric energy module. The connector module is: structured to attach the electric energy module to the aircraft when the connector module is in an engaged mode while in use, and operable between the engaged mode and a disengaged mode. The connector module in the disengaged mode while in use disengages the electric energy module from the aircraft.

公开(公告)号：US20220363412A1

公开(公告)日：2022-11-17

申请号：US17322739

申请日：2021-05-17

申请人： Pratt & Whitney Canada Corp.

发明人： Daniel Mackay

IPC分类号： B64F5/40 ,  B64D27/24 ,  B60L9/00 ,  B60L50/50 ,  B60L53/16 ,  B64F1/36

摘要： A system for an aircraft, comprises an electric energy module; and a connector module operatively connected to the electric energy module. The connector module is: structured to attach the electric energy module to the aircraft when the connector module in an engaged mode while in use, and operable between the engaged mode and a disengaged mode, the connector module in the disengaged mode while in use disengaging the electric energy module from the aircraft.