F03D15/00

Method and device for managing the offtake of power produced by an auxiliary power unit of an aircraft and aircraft equipped with said power offtake management device

A method for managing the offtake of power produced by an auxiliary power unit of an aircraft. The method comprises a step of calculating a maximum capacity for offtake of mechanical power that the auxiliary power unit can provide to the aircraft, a step of determining an actual offtake of mechanical power taken off by a first mechanical power offtake system of the auxiliary power unit, a step of comparing the maximum capacity for offtake of mechanical power and the actual offtake of mechanical power, a step of optimizing the offtake of mechanical power which step, based on the comparison of the maximum capacity for offtake of mechanical power and the actual offtake of mechanical power, determines at least one corrective action. A device for managing the offtake of power produced by an auxiliary power unit of an aircraft and an aircraft including such a device are provided.

Method and device for managing the offtake of power produced by an auxiliary power unit of an aircraft and aircraft equipped with said power offtake management device

A method for managing the offtake of power produced by an auxiliary power unit of an aircraft. The method comprises a step of calculating a maximum capacity for offtake of mechanical power that the auxiliary power unit can provide to the aircraft, a step of determining an actual offtake of mechanical power taken off by a first mechanical power offtake system of the auxiliary power unit, a step of comparing the maximum capacity for offtake of mechanical power and the actual offtake of mechanical power, a step of optimizing the offtake of mechanical power which step, based on the comparison of the maximum capacity for offtake of mechanical power and the actual offtake of mechanical power, determines at least one corrective action. A device for managing the offtake of power produced by an auxiliary power unit of an aircraft and an aircraft including such a device are provided.

DRIVE SYSTEM FOR INTERIOR WIND TURBINES OF GREAT HEIGHTS AND PERFORMANCE
20230044349 · 2023-02-09 · ·

The invention relates to a drive system for interior wind turbines, consisting of a rotatable tower (5) with a rotor mounted at hub height, the generator (16) being located at the foot of the tower (5) on a drive/generator platform (13) and the rotor torque being transferred from above downwards to the generator (16). Particular requirements are placed on such a drive system as the height of the interior wind turbine increases. A steel-wire-cable-reinforced flat belt (18) is used as a transfer element, the ends of which are joined in a particular way to form an endless belt the pretensioning of which is regulated dependent on the properties of the wind, and automatic monitoring is provided which executes an immediate controlled shut-down of the drive system if damage occurs.

DRIVE SYSTEM FOR INTERIOR WIND TURBINES OF GREAT HEIGHTS AND PERFORMANCE
20230044349 · 2023-02-09 · ·

The invention relates to a drive system for interior wind turbines, consisting of a rotatable tower (5) with a rotor mounted at hub height, the generator (16) being located at the foot of the tower (5) on a drive/generator platform (13) and the rotor torque being transferred from above downwards to the generator (16). Particular requirements are placed on such a drive system as the height of the interior wind turbine increases. A steel-wire-cable-reinforced flat belt (18) is used as a transfer element, the ends of which are joined in a particular way to form an endless belt the pretensioning of which is regulated dependent on the properties of the wind, and automatic monitoring is provided which executes an immediate controlled shut-down of the drive system if damage occurs.

COMPACT GEARED REDUCTION UNIT FOR APPLICATION WITH TRANSMISSION SHAFT SUBJECTED TO RADIAL LOADS
20230012263 · 2023-01-12 ·

A compact geared reduction unit for application with transmission shaft subjected to radial loads, comprising a box-like body inside which a gear system is accommodated for the transmission of rotary motion from a driving shaft to a transmission shaft, which is provided with an output reduction stage of the epicyclic type; the output reduction stage comprises a driving sun gear which rotates about a main axis and a ring gear which is integrally associated with the box-like body, between which multiple planet gears are engaged which are supported in rotation about respective longitudinal axes which are parallel to the main axis by a transmission planet carrier, which in turn rotates about the main axis and is associated so as to be integral in rotation with the transmission shaft at a connection region. The reduction unit furthermore provides for rolling means adapted to support radial loads associated with the transmission shaft.

COMPACT GEARED REDUCTION UNIT FOR APPLICATION WITH TRANSMISSION SHAFT SUBJECTED TO RADIAL LOADS
20230012263 · 2023-01-12 ·

A compact geared reduction unit for application with transmission shaft subjected to radial loads, comprising a box-like body inside which a gear system is accommodated for the transmission of rotary motion from a driving shaft to a transmission shaft, which is provided with an output reduction stage of the epicyclic type; the output reduction stage comprises a driving sun gear which rotates about a main axis and a ring gear which is integrally associated with the box-like body, between which multiple planet gears are engaged which are supported in rotation about respective longitudinal axes which are parallel to the main axis by a transmission planet carrier, which in turn rotates about the main axis and is associated so as to be integral in rotation with the transmission shaft at a connection region. The reduction unit furthermore provides for rolling means adapted to support radial loads associated with the transmission shaft.

Renewable power generation system
11592002 · 2023-02-28 ·

Disclosed embodiments provide a renewable power generation apparatus. In embodiments, the renewable power generation apparatus is driven by wind. In other embodiments, the renewable power generation apparatus is driven by water. Disclosed embodiments utilize two cylindrical turbines placed adjacent to each other. A diverter directs wind towards both turbines, causing them to rotate about their respective longitudinal axis. The turbines are coupled to a driveshaft that drives a generator to generate power. Embodiments utilize an airfoil adjacent to each turbine. The airfoil causes air to move faster over the airfoil surface to create low pressure which increases the performance of the turbines. The renewable power generation apparatus of disclosed embodiments is relatively compact compared to a traditional wind turbine. This allows disclosed embodiments to have more flexibility in where they are installed, facilitating local power generation, off-grid applications, and other important environmental applications.

Renewable power generation system
11592002 · 2023-02-28 ·

Disclosed embodiments provide a renewable power generation apparatus. In embodiments, the renewable power generation apparatus is driven by wind. In other embodiments, the renewable power generation apparatus is driven by water. Disclosed embodiments utilize two cylindrical turbines placed adjacent to each other. A diverter directs wind towards both turbines, causing them to rotate about their respective longitudinal axis. The turbines are coupled to a driveshaft that drives a generator to generate power. Embodiments utilize an airfoil adjacent to each turbine. The airfoil causes air to move faster over the airfoil surface to create low pressure which increases the performance of the turbines. The renewable power generation apparatus of disclosed embodiments is relatively compact compared to a traditional wind turbine. This allows disclosed embodiments to have more flexibility in where they are installed, facilitating local power generation, off-grid applications, and other important environmental applications.

POWER TRANSMISSION DEVICE
20180006544 · 2018-01-04 ·

A power transmission device includes: a high speed magnet rotor which includes a magnet array which is magnetized in a radial direction; a low speed magnet rotor which includes a magnet array which is magnetized in a circumferential direction; and an inductor rotor which allows magnetic fluxes from the magnet array of the high speed magnet rotor to pass, and the high speed magnet rotor, the low speed magnet rotor and the inductor rotor are concentrically arranged and the magnet array of the low speed magnet rotor is formed such that homopolar surfaces of neighboring magnets face each other in the circumferential direction.

POWER TRANSMISSION DEVICE
20180006544 · 2018-01-04 ·

A power transmission device includes: a high speed magnet rotor which includes a magnet array which is magnetized in a radial direction; a low speed magnet rotor which includes a magnet array which is magnetized in a circumferential direction; and an inductor rotor which allows magnetic fluxes from the magnet array of the high speed magnet rotor to pass, and the high speed magnet rotor, the low speed magnet rotor and the inductor rotor are concentrically arranged and the magnet array of the low speed magnet rotor is formed such that homopolar surfaces of neighboring magnets face each other in the circumferential direction.