A hybrid permanent magnet-electromagnet flux device including a plurality of electromagnets and permanent magnets cooperatively arranged to provide a first magnetic array such that when the electromagnets are activated in a first state the first magnetic array of magnets implements a Halbach array generating an augmented magnetic field on a first side of the first magnetic array and a cancelling magnetic field on opposite facing second side of the first magnetic array, and when the electromagnets are activated in a second state a respective magnetic field orientation of each of the electromagnets is reversed from that of the first state.

A hybrid permanent magnet-electromagnet flux device including a plurality of electromagnets and permanent magnets cooperatively arranged to provide a first magnetic array such that when the electromagnets are activated in a first state the first magnetic array of magnets implements a Halbach array generating an augmented magnetic field on a first side of the first magnetic array and a cancelling magnetic field on opposite facing second side of the first magnetic array, and when the electromagnets are activated in a second state a respective magnetic field orientation of each of the electromagnets is reversed from that of the first state.

A propulsion system, comprising: a fan blade housing; a plurality of fan blades within the fan blade housing; one or more rows of permanent magnets, affixed to the outside of the fan blade housing; one or more fan blade bearings; one or more magnetic field generators affixed to the one or more fan blade bearings and corresponding to the one or more rows of permanent magnets, the magnetic field generators configured to cause the permanent magnets to be propelled forward in the same direction, thereby causing the fan blade housing to which they are attached, and the fan blades within, to spin.

A propulsion system, comprising: a fan blade housing; a plurality of fan blades within the fan blade housing; one or more rows of permanent magnets, affixed to the outside of the fan blade housing; one or more fan blade bearings; one or more magnetic field generators affixed to the one or more fan blade bearings and corresponding to the one or more rows of permanent magnets, the magnetic field generators configured to cause the permanent magnets to be propelled forward in the same direction, thereby causing the fan blade housing to which they are attached, and the fan blades within, to spin.

An active part of an electric machine, the part being designed as a rotor or a stator for the electric machine, including a main part and a plurality of permanent magnets secured on/in the main part. The active part has one or more securing devices made of sheet metal, each of which holds at least one of the permanent magnets and via which the permanent magnets are secured on/in the main part. A corresponding electric machine and a method for producing a pre-mounted assembly for securing at least one permanent magnet to the main part of an active part of an electric machine, and the use of such pre-mounted assemblies are also provided.

A motor includes a commutator, a brush, a first spring, a second spring, and a holder. The brush is configured to come into contact with the commutator to be electrically connected to the commutator. The first spring is configured to push the brush along the first direction toward the commutator. The second spring pushes the brush along a second direction intersecting the first direction. The holder is disposed such that the brush is located between the holder and the second spring in the second direction. The holder holds the brush between the holder and the second spring.

An information handling resource blank configured to populate a slot of an information handling system in lieu of an information handling resource may include a form factor having at least some features in common with that of the information handling resource and one or more false fans mechanically coupled to the form factor. Each of the one or more false fans may be configured to have a first airflow impedance when airflow through such false fan is below a threshold airflow and have a second airflow impedance when airflow through such false fan is above the threshold airflow.

An information handling resource blank configured to populate a slot of an information handling system in lieu of an information handling resource may include a form factor having at least some features in common with that of the information handling resource and one or more false fans mechanically coupled to the form factor. Each of the one or more false fans may be configured to have a first airflow impedance when airflow through such false fan is below a threshold airflow and have a second airflow impedance when airflow through such false fan is above the threshold airflow.

Systems and methods relate to a vertical takeoff and landing (VTOL) platform that can include a stator and a rotor magnetically levitated by the stator. The rotor and stator can be annular, such that the rotor rotates about a rotational axis. The stator can include magnets that provide guidance, levitation, and drive forces to drive the rotor, as well as to control operation of rotor blades of the rotor that can be independently rotated to specific pitch angles to control at least one of lift, pitch, roll, or yaw of the VTOL platform. Various controllers can be used to enable independent and redundant control of components of the VTOL platform.

Systems and methods relate to a vertical takeoff and landing (VTOL) platform that can include a stator and a rotor magnetically levitated by the stator. The rotor and stator can be annular, such that the rotor rotates about a rotational axis. The stator can include magnets that provide guidance, levitation, and drive forces to drive the rotor, as well as to control operation of rotor blades of the rotor that can be independently rotated to specific pitch angles to control at least one of lift, pitch, roll, or yaw of the VTOL platform. Various controllers can be used to enable independent and redundant control of components of the VTOL platform.