View source for 20240018967. SHAFTLESS ELECTRIC FLUID-FLOW DEVICE simplified abstract (Unknown Organization)

=SHAFTLESS ELECTRIC FLUID-FLOW DEVICE=


==Organization Name==

[[:Category:Unknown Organization|Unknown Organization]]


[[Category:Unknown Organization]]

==Inventor(s)==

[[:Category:Gregory M. Waugh of Roseburg OR (US)|Gregory M. Waugh of Roseburg OR (US)]][[Category:Gregory M. Waugh of Roseburg OR (US)]]

==SHAFTLESS ELECTRIC FLUID-FLOW DEVICE - A simplified explanation of the abstract==


This abstract first appeared for US patent application 20240018967 titled 'SHAFTLESS ELECTRIC FLUID-FLOW DEVICE

==Simplified Explanation==

The abstract describes an aircraft that has a fuselage and wings, with a shaftless electric fluid-flow device connected to either the fuselage or one of the wings. The device consists of a housing and a shaftless hub that can rotate within the housing around a central axis. It also includes a fan blade assembly that co-rotates with the shaftless hub and has multiple fan blades.

* The aircraft has a fuselage and wings, with a shaftless electric fluid-flow device attached to either the fuselage or one of the wings.
* The shaftless electric fluid-flow device consists of a housing and a shaftless hub.
* The shaftless hub can rotate within the housing around a central axis.
* The shaftless electric fluid-flow device also includes a fan blade assembly.
* The fan blade assembly is coupled to the shaftless hub and co-rotates with it.
* The fan blade assembly has multiple fan blades.

Potential Applications:
* This technology can be used in aircraft propulsion systems to provide efficient fluid flow and generate thrust.
* It can be applied in both commercial and military aircraft to improve performance and fuel efficiency.

Problems Solved:
* The shaftless electric fluid-flow device eliminates the need for a traditional shaft, reducing weight and complexity.
* The design allows for improved aerodynamics and efficiency compared to conventional propulsion systems.

Benefits:
* The shaftless electric fluid-flow device offers a more compact and lightweight solution for aircraft propulsion.
* It provides improved aerodynamic performance, resulting in increased fuel efficiency and reduced emissions.
* The technology can potentially enhance the overall performance and maneuverability of the aircraft.


==Original Abstract Submitted==

an aircraft that includes a fuselage and wings fixed to the fuselage. the aircraft further includes a shaftless electric fluid-flow device that is coupled to the at least one of the fuselage or a corresponding one of the wings. the shaftless electric fluid-flow device includes a housing and a shaftless hub, which is rotatable within the housing, about a central axis, and defines an open central channel that is open along the central axis. the shaftless electric fluid-flow device also includes a fan blade assembly that is coupled to the shaftless hub, such that the fan blade assembly co-rotates with the shaftless hub. the fan blade assembly includes a plurality of fan blades.



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