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公开(公告)号:US20220402620A1
公开(公告)日:2022-12-22
申请号:US17751172
申请日:2022-05-23
Applicant: ROLLS-ROYCE plc
Inventor: Michael Adam ZAGRODNIK , Krishnamoorthi SIVALINGAM , Satyanarayana Reddy GAJJELA , Vidor VERES-SZEKELY , Daniel LORINCZ , István ÖRÖKÖS-TÓTH , Anand Prabhu MATHIVANAN
Abstract: An aircraft including a battery pack having a plurality of battery cells arranged to vent into a venting region of the battery pack. A path is defined between the venting region and an exterior of the aircraft, whereby thermal products vented by the cells can exit the aircraft via the path. In some embodiments, the venting region is or is in fluid communication with an air channel through which air flows from an aircraft air inlet to an aircraft air outlet. In other embodiments, the path joins the venting region and an opening in an external surface of the aircraft.
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公开(公告)号:US20220407135A1
公开(公告)日:2022-12-22
申请号:US17751113
申请日:2022-05-23
Applicant: ROLLS-ROYCE plc
Inventor: Michael Adam ZAGRODNIK , Krishnamoorthi SIVALINGAM , Satyanarayana Reddy GAJJELA , Vidor VERES-SZEKELY , Daniel LORINCZ , István ÖRÖKÖS-TÓTH , Anand Prabhu MATHIVANAN , Umesh MAHAJAN , Rakesh MURALI
IPC: H01M10/625 , H01M50/204 , H01M50/249 , H01M10/44 , H01M10/613 , H01M10/615 , H01M10/6565 , H01M10/6568 , H02J7/00 , B60L58/26
Abstract: Methods for thermally regulating batteries of aircraft are provided. The aircraft comprises: an air inlet; an air outlet; a battery pack comprising battery cells; and an air channel in fluid communication with the air inlet and the air outlet, a surface of the air channel being in thermal communication with the battery cells whereby air flowing through the air channel exchanges heat with the battery cells through the surface of the air channel. The methods comprise: connecting an external supply of air to the air inlet of the aircraft; and delivering a flow of air through the air channel using the external supply of air. A kit comprising the aircraft and the external supply of air is also provided.
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公开(公告)号:US20240283079A1
公开(公告)日:2024-08-22
申请号:US18442822
申请日:2024-02-15
Applicant: ROLLS-ROYCE PLC
Inventor: István ÖRÖKÖS-TÓTH , Daniel LORINCZ , Kolos HASZNOSI , Mark ANKA , Andras LUKACS , Matthew DOBSON , Stene CHARMER , Elliott READ , James MARCO
IPC: H01M50/293 , H01M50/213 , H01M50/249 , H01M50/35 , H01M50/375
CPC classification number: H01M50/293 , H01M50/213 , H01M50/35 , H01M50/375 , H01M50/249 , H01M2220/20
Abstract: A battery pack includes: a plurality of cylindrical battery cells, each one of the plurality of cells having a cylindrical outer cell wall that extends in a z-direction between opposed first and second ends of the cell; a carrier structure that locates the battery cells relative to one another and arranges them in an array in an x-y plane perpendicular to the z-direction; and a plurality of barriers for preventing propagation of thermal runaway between cells of the array, each one of the plurality of barriers forming a barrier wall that surrounds a group of one or more of the cells. A gap is defined between the barrier wall of each respective barrier and the outer cell wall of each of the respective one or more cells enclosed by the respective barrier.
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公开(公告)号:US20220402402A1
公开(公告)日:2022-12-22
申请号:US17751072
申请日:2022-05-23
Applicant: ROLLS-ROYCE plc
Inventor: Michael Adam ZAGRODNIK , Krishnamoorthi SIVALINGAM , Satyanarayana Reddy GAJJELA , Vidor VERES-SZÉKELY , Daniel LORINCZ , István ÖRÖKÖS-TÓTH , Anand Prabhu MATHIVANAN , Umesh MAHAJAN , Rakesh MURALI
Abstract: Aircraft with battery thermal regulation systems, including: an aircraft air inlet and an aircraft air outlet; a battery pack including battery cells; and a battery thermal regulation system including a first air channel, a surface of which is in thermal communication with the battery cells so that air flowing through the first air channel exchanges heat with the cells through the surface; and an airflow device for driving an airflow. The battery thermal regulation system has a first and a second mode operation. In the first mode, the first air channel is fluidly connected with the aircraft air inlet and the aircraft air outlet whereby, during flight of the aircraft, air can enter the aircraft through the air inlet, flow through the first air channel and exit the aircraft through the air outlet. In the second mode, the airflow device drives an airflow through the first air channel.
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