Abstract: A cascade for a thrust reverser device intended to be mounted on a turbomachine of an aircraft, the cascade including first partitions extending in a first direction, seconds partitions extending in a second direction orthogonal to the first direction, the second partitions extending in a third direction secant to a plane comprising first and second directions between a first and a second end. Each second partition forms, with reference planes parallel to the second direction and to the third direction, a plurality of different angles at positions distinct from the height of the second partitions separating the first end from the second end of the second partitions, each angle being formed between a reference plane and the tangent to the second partition taken at the intersection between said corresponding reference plane and the second partition at the position of the height of the corresponding second partition.

Abstract: Various embodiments of the present disclosure provide environmental modeling techniques for generating and presenting diverse sets of geographic insights for a geographic region. The geographic insights include landcover insights derived from hyperspectral data using machine learning techniques. The landcover insights include landcover predictions that correspond to geographic polygons and the machine learning techniques leverage models that are trained using hyperspectral image frames that correspond to labeled geographic polygons. The geographic insights include carbon stock insights derived from multiple static and dynamic rasters for a geographic region. The rasters include carbon zone, a landcover, a burned area, a soil carbon stock rasters, and the like, that may be aggregated according to a prediction scheme to generate time-dependent insights tailored to a particular point in time. These insights and others may be presented through specially designed overlays for a user interface.

Abstract: Various embodiments of the present disclosure provide environmental modeling techniques for generating and presenting diverse sets of geographic insights for a geographic region. The geographic insights include landcover insights derived from hyperspectral data using machine learning techniques. The landcover insights include landcover predictions that correspond to geographic polygons and the machine learning techniques leverage models that are trained using hyperspectral image frames that correspond to labeled geographic polygons. The geographic insights include carbon stock insights derived from multiple static and dynamic rasters for a geographic region. The rasters include carbon zone, a landcover, a burned area, a soil carbon stock rasters, and the like, that may be aggregated according to a prediction scheme to generate time-dependent insights tailored to a particular point in time. These insights and others may be presented through specially designed overlays for a user interface.

Abstract: A closing cap for containers with a threaded neck portion, includes a lower ring coupled to the neck of the container and an upper cap provided internally with a thread to be coupled to the outer threaded neck portion, the upper cap and the lower ring are joined to rotate together. The connection between the upper cap and the lower ring is made by two flexible extensions diametrically opposed to each other, which are formed by a thickening present in the lower ring that includes a grooved portion. The lower edge of the body of the upper cap has a step defining a recessed portion where the extensions are located. In a closed condition, the two extensions are arranged above and parallel to the body of the lower ring. In an open position, the upper end of the extensions acts as a hinge region allowing the upper cap to rotate.

Abstract: The present invention relates to a closing cap for containers that have a neck provided with a threaded portion, comprising a lower ring that can be coupled to the neck of the container and an upper cap (2) having a thread configured to be coupled to the outer threaded portion of the neck, the upper cap (2) and the lower ring (1) being integrally joined together. The upper cap (2) and the lower ring (1) are joined by means of two flexible extensions (3) diametrically opposed to each other, each one formed by a thickening in the lower ring that includes a grooved portion (7), such that the two extensions have the same outer diameter as the outer diameter of the thickening, the lower edge of the body of the upper cap having a step where the extensions are located, such that in a closed condition both extensions (3) are arranged above and parallel to the body of the lower ring (1).

Abstract: The invention relates to acoustic management, on an aircraft turbomachine or on a nacelle, via a panel (30,32). On a support (38) is reserved a recess (34), recessed with respect to a surrounding general surface (36) for contact with moving air. The recess (34) is adapted to receive the panel, as another so-called surface for contact with moving air. The support (38) and/or the panel comprise removable connecting elements for, in the recess, mounting the panel removably with respect to the support, the panel being an acoustic panel (30) or a non-acoustic panel (32).

Abstract: A heating element for heating air or liquid may include an electrically conductive heating conductor equipped for heating at least one of air and liquid, a converter unit configured to convert a high DC voltage into a high AC voltage, and a transformer. The transformer may include a primary winding and a secondary winding. The secondary winding may have a lower winding number than the primary winding such that the high AC voltage, which is fed to the primary winding by the converter unit, is transformed into a low AC voltage in the secondary winding. The heating conductor may at least partially form the secondary winding and may be flowed through by a secondary current heating the heating conductor. An amperage of the secondary current may materialise as a function of an ohmic resistance of the heating conductor and of the low AC voltage.

Abstract: The present invention relates to novel differentially methylated genetic elements associated with cutaneous Spitzoid tumors. The invention also relates to improved methods for classifying said tumors.

Abstract: An electrical monitoring device for a high-voltage electrical power supply may include a high-voltage electrical connection unit, a microcontroller, and an electrical connection. The electrical connection unit may include a plug, a plug receptacle, a high-voltage connection electrically connectable to a voltage source, an electrical signal input connection, and an electrical signal output connection. The electrical signal input connection and the electrical signal output connection may be electrically connected when the plug is accommodated in the plug receptacle, and may be electrically separated when the plug is not accommodated in the plug receptacle. The microcontroller may include (i) an electrical signal output electrically connected via a first signal processing unit to the electrical signal input connection and (ii) a signal input electrically connected to the electrical signal output connection.

Abstract: A closing cap for containers with a threaded neck portion, includes a lower ring coupled to the neck of the container and an upper cap provided internally with a thread to be coupled to the outer threaded neck portion, the upper cap and the lower ring are joined to rotate together. The connection between the upper cap and the lower ring is made by two flexible extensions diametrically opposed to each other, which are formed by a thickening present in the lower ring that includes a grooved portion. The lower edge of the body of the upper cap has a step defining a recessed portion where the extensions are located. In a closed condition, the two extensions are arranged above and parallel to the body of the lower ring. In an open position, the upper end of the extensions acts as a hinge region allowing the upper cap to rotate.

Abstract: A cascade type thrust reverser device for a turbomachine of an aircraft, comprising a cascade including first partitions, second partitions intersecting the first partitions, and cavities, and a casing including a housing into which the cascade can be inserted in a first direction, the casing and the cascade being in relative translation with respect to one another in the first direction. The casing comprises a perforated wall intended to be in contact with an air flow and including orifices and wall strips with no orifices and intended to face the first walls of the cascade when the device is in a first position in which the cascade is entirely positioned in the housing.

Abstract: The disclosure is directed to improved methods for preparing substituted quinolinylcyclohexylpropanamide compounds.

Abstract: A cascade type thrust reverser device for a turbomachine of an aircraft, comprising a thrust reverser cascade and a casing, the cascade including first cavities, and the casing comprising an opening defining a housing wherein said cascade can be inserted in a first direction, and the casing and said cascade being in relative translation with respect to one another in the first direction between a first position of the device in which the cascade is entirely positioned in the housing and a second position of the device in which said cascade is at least partially outside said housing. The casing comprises an acoustic treatment panel including second cavities extending in a second plane parallel to the first plane, each first cavity facing a second cavity when the device is in the first position to form an acoustic treatment cell.

Abstract: A cascade for a thrust reversal device intended to be mounted on a turbomachine of an aircraft, the cascade including first partitions extending in a first direction, second fixed partitions extending in a second direction orthogonal to the first direction, and a frame inside which the first and second partitions extend, the frame including at least two fixed walls extending according to the first direction, and at least one part of each first partition extending between two second partitions. At least one first partition is mobile according to the second direction between a first position wherein the first partition is distant, in the second direction, from the fixed walls to form a plurality of resonating cavities with the first partitions and/or the fixed walls, and a second position wherein the one first partition is in contact with a fixed wall or another first partition.

Abstract: A method of reducing noise includes: driving a first propulsor using one or more of the first electrical motor and the first thermal engine, and driving a second propulsor of the second hybrid power plant using one or more of the second electrical motor and the second thermal engine; receiving a signal indicative of an initial combined noise signature; determining, from the signal, that an initial amplitude variation of a periodically fluctuating amplitude of the initial combined noise signature is greater than an amplitude variation threshold; modulating a thrust produced by the second hybrid power plant, by changing a power output of the second thermal engine or the second electrical motor, to produce a modulated combined noise signature having a modulated amplitude variation less than the initial amplitude variation; and compensating for a difference in thrusts generated by the first hybrid power plant and the second hybrid power plant.

Abstract: The invention relates to a closing cap for containers, particularly intended for containers that have an opening in a neck provided with an outer threaded portion, comprising a lower ring intended for being coupled to the neck of the container and an upper cap having an inner threaded region configured for being coupled to the outer threaded portion of a container neck, the upper cap and the lower ring being articulated to each other by means of a hinged portion, such that the lower ring is formed by an annular-shaped body. Said lower ring has a section with a diameter larger than the remaining section of the annular-shaped body, wherein the hinged portion is located in the section with the larger diameter.

Abstract: The present disclosure concerns a mounting device for semiconductor packages, and a heat dissipation assembly with such a mounting device. The mounting device includes a bottom side comprising one or more cavities to house semiconductor packages, and a top side comprising a plurality of holes extending from the bottom side to the top side for accommodating contact pins of the semiconductor packages. A fixation mechanism fixes the mounting device to a heat dissipation structure.

Abstract: The invention relates to acoustic management, on an aircraft turbomachine (3,12) or on a nacelle (1,10), via a panel (30,32). On a support (38) is reserved a recess (34), recessed with respect to a surrounding general surface (36) for contact with moving air. The recess (34) is adapted to receive the panel, as another so-called surface for contact with moving air. The support (38) and/or the panel comprise removable connecting elements for, in the recess (34), mounting it removably with respect to the support, the panel being an acoustic panel or a non-acoustic panel.

Abstract: An acoustic panel for an aircraft propulsion unit, comprises a core and an entry layer in contact with the core, the entry layer comprising lower elements and upper elements, each comprising an inner face, an outer face and at least one through-hole, the inner faces of the lower elements and upper elements being in contact with each other and forming a channel defining a baffle and opening into a cell of the core.