Construction and operation of electric or hybrid aircraft
First Claim
1. An aircraft monitoring system for an electric or hybrid airplane, the aircraft monitoring system being constructed to enable the electric or hybrid aircraft to pass certification requirements relating to a safety risk analysis, the aircraft monitoring system having different subsystems for monitoring and alerting of failures of components of the electric or hybrid aircraft, the failures that pose a greater safety risk being monitored and indicated by one or more subsystems without use of programmable components, the aircraft monitoring system comprising:
- a first subsystem configured to be supported by a housing and consisting of non-programmable components, the housing being configured to fly and be propelled by an electric motor,wherein the non-programmable components are configured to;
monitor a power source supported by the housing, the power source being configured to power the electric motor, andoutput a first alert to notify of a first condition associated with the power source, the first condition being likely to imminently cause a fatality or a destruction of the housing; and
a second subsystem configured to be supported by the housing and comprising a processor and a communication bus,wherein the processor is configured to;
monitor the power source from communications on the communication bus, andoutput a second alert to notify of a second condition associated with the power source.
1 Assignment
0 Petitions
Accused Products
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.
85 Citations
30 Claims
-
1. An aircraft monitoring system for an electric or hybrid airplane, the aircraft monitoring system being constructed to enable the electric or hybrid aircraft to pass certification requirements relating to a safety risk analysis, the aircraft monitoring system having different subsystems for monitoring and alerting of failures of components of the electric or hybrid aircraft, the failures that pose a greater safety risk being monitored and indicated by one or more subsystems without use of programmable components, the aircraft monitoring system comprising:
-
a first subsystem configured to be supported by a housing and consisting of non-programmable components, the housing being configured to fly and be propelled by an electric motor, wherein the non-programmable components are configured to; monitor a power source supported by the housing, the power source being configured to power the electric motor, and output a first alert to notify of a first condition associated with the power source, the first condition being likely to imminently cause a fatality or a destruction of the housing; and a second subsystem configured to be supported by the housing and comprising a processor and a communication bus, wherein the processor is configured to; monitor the power source from communications on the communication bus, and output a second alert to notify of a second condition associated with the power source. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14, 15, 16, 17, 18, 19, 20, 21, 22, 23, 24, 25, 26)
-
-
27. A method of operating an aircraft monitoring system of an electric or hybrid airplane, the aircraft monitoring system being constructed to enable the electric or hybrid aircraft to pass certification requirements relating to a safety risk analysis, the method comprising:
-
supporting a first subsystem and a second subsystem with a housing, the first subsystem consisting of non-programmable components, the second subsystem comprising a processor and a communication bus, the housing being configured to fly and be propelled by an electric motor; powering, by a power source supported by the housing, the electric motor; monitoring, by the non-programmable components, the power source; outputting, by the non-programmable components, a first alert to notify of a first condition associated with the power source, the first condition being likely to imminently cause a fatality or a destruction of the housing; monitoring, by the processor, the power source from communications on the communication bus; and outputting, by the processor, a second alert to notify of a second condition associated with the power source. - View Dependent Claims (28, 29, 30)
-
Specification