A vectored thrust control module for an aircraft that includes a servo system that couples to the aircraft structure at an output shaft connection point. A thrust motor assembly is fully supported by the servo system and rotates a bladed component to provide thrust to the aircraft. Further, the thrust motor assembly is rigidly connected with the servo system to rotate together about a longitudinal axis thrust line with respect to the aircraft structure. The bladed component and the thrust motor assembly generate a line of thrust that extends through the connection point of the servo system to the aircraft structure.
Gimbaled thruster configuration for use with unmanned aerial vehicle
26.12.2023
Patent
Elektronische Ressource
Englisch
GIMBALED THRUSTER CONFIGURATION FOR USE WITH UNMANNED AERIAL VEHICLE
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|Gimbaled thruster configuration for use with unmanned aerial vehicle
Europäisches Patentamt | 2020
|GIMBALED THRUSTER CONFIGURATION FOR USE WITH UNMANNED AERIAL VEHICLE
Europäisches Patentamt | 2017
|Gimbaled thruster configuration for use with unmanned aerial vehicle
Europäisches Patentamt | 2020
|GIMBALED THRUSTER CONFIGURATION FOR USE WITH UNMANNED AERIAL VEHICLE
Europäisches Patentamt | 2017
|