A control system for a rescue hoist attached to an aircraft is disclosed. In various embodiments, the control system includes a first bus extending between a control module of the rescue hoist and a control input device; and a second bus extending between the control module of the rescue hoist and the control input device. The first bus is configured to transmit a first signal from the control input device to the control module and the second bus is configured to transmit a second signal from the control input device to the control module, both the first signal and the second signal being generated by the control input device in response to a manipulation of the control input device.
DUAL BUS ARCHITECTURE FOR HIGH RELIABILITY CONTROL OF HELICOPTER HOIST
10.12.2020
Patent
Elektronische Ressource
Englisch
DUAL BUS ARCHITECTURE FOR HIGH RELIABILITY CONTROL OF HELICOPTER HOIST
Europäisches Patentamt | 2024
|DUAL BUS ARCHITECTURE FOR HIGH RELIABILITY CONTROL OF HELICOPTER HOIST
Europäisches Patentamt | 2020
|Dual bus architecture for high reliability control of helicopter hoist
Europäisches Patentamt | 2022
|DUAL BUS AND HARDWIRE ARCHITECTURE FOR HIGH RELIABILITY CONTROL OF HELICOPTER HOIST
Europäisches Patentamt | 2025
|DUAL BUS AND HARDWIRE ARCHITECTURE FOR HIGH RELIABILITY CONTROL OF HELICOPTER HOIST
Europäisches Patentamt | 2020
|