公开(公告)号：US12054266B2

公开(公告)日：2024-08-06

申请号：US17571800

申请日：2022-01-10

申请人： Aurora Flight Sciences Corporation

发明人： Daniel Benjamin Cottrell ,  Mahmood Abdulrazzaq Mahmood Alwash ,  Garrett Steven Hennig

IPC分类号： B64D27/24 ,  H01M10/613 ,  H01M10/625 ,  H01M10/6552

CPC分类号： B64D27/24 ,  H01M10/613 ,  H01M10/625 ,  H01M10/6552 ,  H01M2220/20

摘要： The present disclosure relates to propulsion system for an aircraft. The propulsion system comprises a motor, a battery bank, a thermal management system, and a controller. The motor being configured to rotate a rotor via a rotor shaft and to drive the thermal management system. The thermal management system configured to urge fluid through a fluid pathway defined by the battery bank. The controller configured to drive the motor and/or control charge and discharge of the battery bank.

公开(公告)号：US20220306305A1

公开(公告)日：2022-09-29

申请号：US17571800

申请日：2022-01-10

申请人： Aurora Flight Sciences Corporation

发明人： Daniel Benjamin Cottrell ,  Mahmood Abdulrazzaq Mahmood Alwash ,  Garrett Steven Hennig

IPC分类号： B64D27/24 ,  H01M10/613 ,  H01M10/625 ,  H01M10/6552

摘要： The present disclosure relates to propulsion system for an aircraft. The propulsion system comprises a motor, a battery bank, a thermal management system, and a controller. The motor being configured to rotate a rotor via a rotor shaft and to drive the thermal management system. The thermal management system configured to urge fluid through a fluid pathway defined by the battery bank. The controller configured to drive the motor and/or control charge and discharge of the battery bank.