Abstract: A wireless charging system for charging a chargeable electrical energy source of a heating device for aerosol-gene rating articles comprises: —a charging device (3) comprising a planar flat transmitter coil (30), configured to supply an alternating current (I) to the planar flat transmitter coil (30); —a wirelessly chargeable electrical energy source (4) of a heating device (2) for aerosol-generating articles, comprising an electrical energy storage (41) and a tubular receiver coil (40) connected to the electrical energy storage (41), wherein the tubular receiver coil (40) has a longitudinal axis (42) and is adapted to be arranged in a charging position relative to the planar flat transmitter coil (30), wherein in the charging position the longitudinal axis (42) of the tubular receiver coil (40) extends in a plane parallel to the planar flat transmitter coil (30) and in radial direction relative to the planar flat transmitter coil (30), and wherein the tubular receiver coil (40) is arranged to overlap at leas

Abstract: This disclosure describes at least embodiments of an aircraft monitoring system for an electric or hybrid airplane. The aircraft monitoring system can be constructed to enable the electric or hybrid aircraft to pass certification requirements relating to a safety risk analysis. The aircraft monitoring system can have different subsystems for monitoring and alerting of failures of a component, such as a battery pack, a motor controller, and/or a motors. The failures that pose a greater safety risk may be monitored and indicated by one or more subsystems without use of programmable components.

Abstract: This disclosure describes at least embodiments of an aircraft monitoring system for an electric or hybrid airplane. The aircraft monitoring system can be constructed to enable the electric or hybrid aircraft to pass certification requirements relating to a safety risk analysis. The aircraft monitoring system can have different subsystems for monitoring and alerting of failures of a component, such as a battery pack, a motor controller, and/or a motors. The failures that pose a greater safety risk may be monitored and indicated by one or more subsystems without use of programmable components.

Abstract: This disclosure describes at least embodiments of an aircraft monitoring system for an electric or hybrid airplane. The aircraft monitoring system can be constructed to enable the electric or hybrid aircraft to pass certification requirements relating to a safety risk analysis. The aircraft monitoring system can have different subsystems for monitoring and alerting of failures of components, such as a power source for powering an electric motor, of the electric or hybrid aircraft. The failures that pose a greater safety risk may be monitored and indicated by one or more subsystems without use of programmable components.

Abstract: This disclosure describes at least embodiments of an aircraft monitoring system for an electric or hybrid airplane. The aircraft monitoring system can be constructed to enable the electric or hybrid aircraft to pass certification requirements relating to a safety risk analysis. The aircraft monitoring system can have different subsystems for monitoring and alerting of failures of components, such as a power source for powering an electric motor, of the electric or hybrid aircraft. The failures that pose a greater safety risk may be monitored and indicated by one or more subsystems without use of programmable components.

Abstract: This disclosure describes at least embodiments of an aircraft monitoring system for an electric or hybrid airplane. The aircraft monitoring system can be constructed to enable the electric or hybrid aircraft to pass certification requirements relating to a safety risk analysis. The aircraft monitoring system can have different subsystems for monitoring and alerting of failures of components, such as a power source for powering an electric motor, of the electric or hybrid aircraft. The failures that pose a greater safety risk may be monitored and indicated by one or more subsystems without use of programmable components.

Abstract: This disclosure describes at least embodiments of an aircraft monitoring system for an electric or hybrid airplane. The aircraft monitoring system can be constructed to enable the electric or hybrid aircraft to pass certification requirements relating to a safety risk analysis. The aircraft monitoring system can have different subsystems for monitoring and alerting of failures of components, such as a power source for powering an electric motor, of the electric or hybrid aircraft. The failures that pose a greater safety risk may be monitored and indicated by one or more subsystems without use of programmable components.

Abstract: A wireless charging system for charging a chargeable electrical energy source of a heating device for aerosol-gene rating articles comprises: —a charging device (3) comprising a planar flat transmitter coil (30), configured to supply an alternating current (I) to the planar flat transmitter coil (30); —a wirelessly chargeable electrical energy source (4) of a heating device (2) for aerosol-generating articles, comprising an electrical energy storage (41) and a tubular receiver coil (40) connected to the electrical energy storage (41), wherein the tubular receiver coil (40) has a longitudinal axis (42) and is adapted to be arranged in a charging position relative to the planar flat transmitter coil (30), wherein in the charging position the longitudinal axis (42) of the tubular receiver coil (40) extends in a plane parallel to the planar flat transmitter coil (30) and in radial direction relative to the planar flat transmitter coil (30), and wherein the tubular receiver coil (40) is arranged to overlap at leas

Abstract: This disclosure describes at least embodiments of an aircraft monitoring system for an electric or hybrid airplane. The aircraft monitoring system can be constructed to enable the electric or hybrid aircraft to pass certification requirements relating to a safety risk analysis. The aircraft monitoring system can have different subsystems for monitoring and alerting of failures of components, such as a power source for powering an electric motor, of the electric or hybrid aircraft. The failures that pose a greater safety risk may be monitored and indicated by one or more subsystems without use of programmable components.