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公开(公告)号:US11804138B2
公开(公告)日:2023-10-31
申请号:US17528597
申请日:2021-11-17
申请人: BETA AIR, LLC
发明人: Steven J. Foland , Lochie Ferrier , Nick Warren , John Palombini
CPC分类号: G08G5/0008 , B64C29/00 , G08G5/0039
摘要: In an aspect of the present disclosure is a system of automated fleet management for aerial vehicles, including a first aerial vehicle, the aerial vehicle comprising: a first sensor configured to measure an external metric and generate external datum based on the external metric; and a second sensor configured to measure an aircraft metric and generate aircraft datum based on the aircraft metric; and a computing device operating on the first aerial vehicle, the computing device communicatively connected to a network including at least a second aerial vehicle, the computing device configured to: receive the external datum from the first sensor of the first aerial vehicle and the aircraft datum from the second sensor of the first aerial vehicle; and transmit at least a flight plan update element to the network based on the external datum and the aircraft datum.
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公开(公告)号:US12080176B2
公开(公告)日:2024-09-03
申请号:US18083974
申请日:2022-12-19
申请人: BETA AIR, LLC
发明人: Steven J. Foland , Lochie Ferrier , Nick Warren , John Palombini
CPC分类号: G08G5/0039 , B60L58/24 , B64C29/0091 , B64C39/024 , G08G5/0069 , G08G5/0091 , B60L2200/10 , B60L2260/56 , B64U50/19
摘要: In an aspect of the present disclosure is a system for in-flight re-routing of an electric aircraft including a battery pack configured to provide electrical power to the electric aircraft; a sensor configured to detect at least a temperature metric of the battery pack and generate a temperature datum based on the at least a temperature metric; a controller communicatively connected to the sensor, the controller configured to: receive the temperature datum from the sensor; and re-route the electric aircraft based on the temperature datum.
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公开(公告)号:US20230154340A1
公开(公告)日:2023-05-18
申请号:US18083974
申请日:2022-12-19
申请人: BETA AIR, LLC
发明人: Steven J. Foland , Lochie Ferrier , Nick Warren , John Palombini
CPC分类号: G08G5/0039 , B64C29/0091 , G08G5/0069 , B64C39/024 , G08G5/0091 , B60L58/24 , B64U50/19
摘要: In an aspect of the present disclosure is a system for in-flight re-routing of an electric aircraft including a battery pack configured to provide electrical power to the electric aircraft; a sensor configured to detect at least a temperature metric of the battery pack and generate a temperature datum based on the at least a temperature metric; a controller communicatively connected to the sensor, the controller configured to: receive the temperature datum from the sensor; and re-route the electric aircraft based on the temperature datum.
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公开(公告)号:US20230154337A1
公开(公告)日:2023-05-18
申请号:US17528597
申请日:2021-11-17
申请人: BETA AIR, LLC
发明人: Steven J. Foland , Lochie Ferrier , Nick Warren , John Palombini
CPC分类号: G08G5/0008 , G08G5/0039 , B64C29/00
摘要: In an aspect of the present disclosure is a system of automated fleet management for aerial vehicles, including a first aerial vehicle, the aerial vehicle comprising: a first sensor configured to measure an external metric and generate external datum based on the external metric; and a second sensor configured to measure an aircraft metric and generate aircraft datum based on the aircraft metric; and a computing device operating on the first aerial vehicle, the computing device communicatively connected to a network including at least a second aerial vehicle, the computing device configured to: receive the external datum from the first sensor of the first aerial vehicle and the aircraft datum from the second sensor of the first aerial vehicle; and transmit at least a flight plan update element to the network based on the external datum and the aircraft datum.
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公开(公告)号:US11562653B1
公开(公告)日:2023-01-24
申请号:US17528673
申请日:2021-11-17
申请人: BETA AIR, LLC
发明人: Steven J. Foland , Lochie Ferrier , Nick Warren , John Palombini
摘要: In an aspect of the present disclosure is a system for in-flight re-routing of an electric aircraft including a battery pack configured to provide electrical power to the electric aircraft; a sensor configured to detect at least a temperature metric of the battery pack and generate a temperature datum based on the at least a temperature metric; a controller communicatively connected to the sensor, the controller configured to: receive the temperature datum from the sensor; and re-route the electric aircraft based on the temperature datum.
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