Abstract:
A ducted fan air-vehicle capable of generating control moments. The ducted fan air-vehicle includes an air duct, a fan, a center body, a plurality of control vanes. The vanes are independently controlled and are deflected in the same direction but at different angles, thereby providing an increased control moments to the vehicle compared to the prior art. The increased pitching moment allows for additional control authority. Additional control authority is useful in forward flight and is especially desirable when the ducted fan air-vehicle is maneuvering in unsteady or turbulent winds or with various types of cargo that may effect the vehicle center of gravity location.
Abstract:
A ducted fan air-vehicle capable of generating control moments. The ducted fan air-vehicle includes an air duct, a fan, a center body, a plurality of control vanes. The vanes are independently controlled and are deflected in the same direction but at different angles, thereby providing an increased control moments to the vehicle compared to the prior art. The increased pitching moment allows for additional control authority. Additional control authority is useful in forward flight and is especially desirable when the ducted fan air-vehicle is maneuvering in unsteady or turbulent winds or with various types of cargo that may effect the vehicle center of gravity location.
Abstract:
Provided is a self-leveling support apparatus for use with a UAV or stationary device such as a table or ladder, the apparatus having multiple leg members, each associated with a hydraulic or pneumatic cylinder; a connection among the hydraulic or pheumatic cylinders such that they share a common reservoir of fluid; a locking mechanism that obstructs free flow of fluid among the cylinders and stabilizes the UAV or stationary device without the need for electronic sensors or control systems.
Abstract:
Provided is a self-leveling support apparatus for use with a UAV or stationary device such as a table or ladder, the apparatus having multiple leg members, each associated with a hydraulic or pneumatic cylinder; a connection among the hydraulic or pheumatic cylinders such that they share a common reservoir of fluid; a locking mechanism that obstructs free flow of fluid among the cylinders and stabilizes the UAV or stationary device without the need for electronic sensors or control systems.
Abstract:
A ducted fan air-vehicle having alternative methods of control is described. The ducted fan air-vehicle includes an air duct, a fan, a center body, a plurality of control vanes. Each control vanes includes a separate servo for independent control of each control vane, and is therefore able to operate the control vanes in a non-traditional manner to provide maximum control authority.
Abstract:
A ducted fan air-vehicle having alternative methods of control is described. The ducted fan air-vehicle includes an air duct, a fan, a center body, a plurality of control vanes. Each control vanes includes a separate servo for independent control of each control vane, and is therefore able to operate the control vanes in a non-traditional manner to provide maximum control authority.
Abstract:
An adjustable camshaft system for an automotive engine includes a camshaft having machined and fabricated axially-directed control passages combined with an oil-activated camshaft phaser. The fabricated oil control passages are formed within a portion of the camshaft having an outside diameter which is substantially equal to the outside diameter of other portions of the camshaft fitted within bearings carried within the engine's cylinder head.