Abstract: Method for supervising an additive manufacturing process performed by an additive manufacturing device (1), comprising providing a set of data to a supervision system (6), said set of data comprising product geometry data, production data, production history data, and measurements (7) from said additive manufacturing device (1), and, at said supervision system (6): predicting the occurrence of a defect (S1) from said set of data, when an occurrence of a defect is predicted, determining a type of defect (S2), and deciding for stopping (8, 5) or not (S3) said additive manufacturing process according to said type of defect and of a seriousness level.

Abstract: A user device incorporates a user interface platform that combines user notifications and various operational settings as part of a common display region. The notifications and settings are separated from one another, and the user interface dynamically adjusts the arrangement of these features to make it convenient for a user to quickly see the information and to manage it. The setting information may incorporate user logins, network and communication data, display and audio information, as well as other settings. And the application-related notifications may include information about active applications such as an email account, audio or video calls, texting apps, social media platforms, calendars, music players, video players, and the like. In response to a new notification, the system may consolidate the operational settings into core settings information. The system may also auto collapse (or expand) the notification list when a new notification is received.

Abstract: A method for holding a part blank inside a holding assembly. The holding assembly includes a first holding portion. The first holding portion includes an inner cavity containing a fluid. The part blank and the first holding portion are at least partially manufactured by additive manufacturing. The holding method includes a heating of the holding assembly and the part blank to deform the first holding portion by fluid expansion in the inner cavity and to reduce a gap between the part blank and the holding assembly by expansion of the first holding portion in relation to the part blank.

Abstract: A method for manufacturing a part by additive manufacturing, the part to be manufactured including at least one portion to be held forming an angle of less than 45° with respect to a building direction of the part to be manufactured, the portion to be held having a first lateral surface and a second lateral surface opposite each other, the method comprising the steps of: providing a digital model of the part to be manufactured, adding to the digital model at least one holding element positioned on one side of the portion to be held, so as to be in contact with said first lateral surface or said second lateral surface.

Abstract: A heat exchanger module having at least two fluid circuits, of longitudinal axis including a stack of plates, defining at least two fluid circuits, at least a part of the plates each including fluid circulation channels, the channels of at least one of the two circuits, referred to as first circuit, having at least one fluid supply and distribution zone for supplying and distributing fluid from outside the stack, forming a fluid pre-header, in which zone the channels are delimited by studs distributed over the surface of the plate; an exchange zone continuous with the pre-header and wherein the channels are each delimited by a groove separated from one another by a rib and extending along the longitudinal axis.

Abstract: A dynamic seal for a turbomachine, including a fixed portion provided with at least one abradable wear part and a movable portion including at least one lip arranged to interact with the at least one wear part during the rotation of the movable portion. The wear part includes a structure forming cavities arranged in one or more series such that, in each series, the cavities of this series are superposed radially with respect to the central axis, the structure being configured to limit or prevent the circulation of gas between each pair of radially adjacent cavities. A method for the additive manufacture of the fixed portion of this dynamic seal is also described.

Abstract: An aircraft turbomachine blade includes an aerodynamic part manufactured in one piece by additive manufacturing, this aerodynamic part including a pressure-side wall, a suction-side wall and an internal fluid passage, this internal fluid passage being crossed by a plurality of disruptive elements that each connect the pressure-side wall to the suction-side wall, being irregularly spaced apart according to varied parameters in a chosen and optimized range, the junction of the disruptive elements with the pressure-side and suction-side walls not following a particular arrangement along the internal passage so as to form a disorderly arrangement.

Abstract: On a computing device, an overview mode is provided to present overview windows of all applications currently running on the computing device. When one or more applications are running in a windowed mode, a first overview window is generated for each of the one or more applications running in the windowed mode; when one or more applications are running in a full-screen mode, a second overview window is generated for each of the one or more applications running in the full-screen mode. The one or more first overview windows in the first space can be arranged in one or more rows in a first overview space, and the one or more second overview windows in the second space in a stack in a second overview space. The arranged overview windows may then be displayed in the overview mode of the computing device.

Abstract: The invention relates to a guide vane for a bypass aircraft turbomachine, its aerodynamic part comprising a first lubricant cooling interior passage in which heat transfer structures are arranged and a second lubricant cooling interior passage in which heat transfer structures are arranged, the aerodynamic part comprising a bent area connecting a lubricant output end of the first interior passage to a lubricant input end of the second passage, the bent area extending along a curved generatrix and being partly delimited by the intrados wall and the extrados wall of the vane. According to the invention, the bent area comprises one or more lubricant guide(s) arranged between the intrados and extrados walls of the vane, and each extending substantially parallel to the curved generatrix of the bent area.

Abstract: On a computing device, an overview mode is provided to present overview windows of all applications currently running on the computing device. When one or more applications are running in a windowed mode, a first overview window is generated for each of the one or more applications running in the windowed mode; when one or more applications are running in a full-screen mode, a second overview window is generated for each of the one or more applications running in the full-screen mode. The one or more first overview windows in the first space can be arranged in one or more rows in a first overview space, and the one or more second overview windows in the second space in a stack in a second overview space. The arranged overview windows may then be displayed in the overview mode of the computing device.

Abstract: A method for manufacturing a part by additive manufacturing, the part to be manufactured including at least one portion to be held forming an angle of less than 45° with respect to a building direction of the part to be manufactured, the portion to be held having a first lateral surface and a second lateral surface opposite each other, the method comprising the steps of: providing a digital model of the part to be manufactured, adding to the digital model at least one holding element positioned on one side of the portion to be held, so as to be in contact with said first lateral surface or said second lateral surface.

Abstract: An aircraft turbomachine blade includes an aerodynamic part manufactured in one piece by additive manufacturing, this aerodynamic part including a pressure-side wall, a suction-side wall and an internal fluid passage, this internal fluid passage being crossed by a plurality of disruptive elements that each connect the pressure-side wall to the suction-side wall, being irregularly spaced apart according to varied parameters in a chosen and optimized range, the junction of the disruptive elements with the pressure-side and suction-side walls not following a particular arrangement along the internal passage so as to form a disorderly arrangement.

Abstract: A user device incorporates a user interface platform that combines user notifications and various operational settings as part of a common display region. The notifications and settings are separated from one another, and the user interface dynamically adjusts the arrangement of these features to make it convenient for a user to quickly see the information and to manage it. The setting information may incorporate user logins, network and communication data, display and audio information, as well as other settings. And the application-related notifications may include information about active applications such as an email account, audio or video calls, texting apps, social media platforms, calendars, music players, video players, and the like. In response to a new notification, the system may consolidate the operational settings into core settings information. The system may also auto collapse (or expand) the notification list when a new notification is received.

Abstract: A user device incorporates a user interface platform that combines user notifications and various operational settings as part of a common display region. The notifications and settings are separated from one another, and the user interface dynamically adjusts the arrangement of these features to make it convenient for a user to quickly see the information and to manage it. The setting information may incorporate user logins, network and communication data, display and audio information, as well as other settings. And the application-related notifications may include information about active applications such as an email account, audio or video calls, texting apps, social media platforms, calendars, music players, video players, and the like. In response to a new notification, the system may consolidate the operational settings into core settings information. The system may also auto collapse (or expand) the notification list when a new notification is received.

Abstract: A guide vane for a twin-spool aircraft turbomachine has an aerodynamic part that includes an internal lubricant cooling passage extending along a principal lubricant flow direction. The aerodynamic part is made in a single piece and also includes heat transfer fins arranged in the passage connecting the intrados and extrados walls and extending approximately parallel to the direction, these fins being distributed in successive rows along the principal direction and made such that for two rows of staggered directly consecutive fins, a first row includes fins forming a positive acute angle A1 with a dummy reference plane, while a second row includes fins forming a negative acute angle A2 with this plane.