Back to results
US 2026/0242079 A1Published application
Industrial aerial robot systems and methods
OwnerThomas W. Melcherinventor
Life of this patent
Estimating the term…
Abstract
A propulsion system includes a first plurality of rotor blades configured to rotate about an engine longitudinal axis and a motor module. The motor module includes a plurality of electric motors for rotating the first plurality of rotor blades. The propulsion system can further include a dual power turbine including a first power turbine module and a second power turbine module.
Claims20
An aircraft comprising:
- a boom;
- a propulsion system coupled to a first end of the boom via a stanchion;
- and
- a first wing coupled to a second end of the boom;
- wherein the propulsion system comprises:
- a first plurality of rotor blades configured to rotate about an engine longitudinal axis;
- and
- a motor module comprising a first plurality of electric motors for rotating the first plurality of rotor blades.
5 more elements
A propulsion system comprising:
- a first plurality of rotor blades configured to rotate about an engine longitudinal axis;
- and
- a motor module comprising:
- a first plurality of electric motors for rotating the first plurality of rotor blades;
- and
- a harmonic damper comprising a plurality of posts, wherein each post extends into an output shaft of the first plurality of electric motors.
3 more elements
A propulsion system comprising:
- a first plurality of rotor blades configured to rotate about an engine longitudinal axis;
- and
- a motor module comprising:
- a first plurality of electric motors for rotating the first plurality of rotor blades;
- a first coolant reservoir configured to contain a coolant for providing cooling to the first plurality of electric motors;
- and
- a plurality of heat exchangers disposed circumferentially about the motor module and at least partially defining a core flow path through the propulsion system.
4 more elements
Dependencies are inferred from the claim text.