Abstract: A plate closes the main part of a vane in two parts. An internal cavity is closed by the plate. Around a bearing surface of the plate, a groove receives an elastic seal, and the outer edge of the plate extends over the groove to compress the seal and to establish excellent leak proofing. The position of the plate may be guaranteed by centring pins penetrating into holes adjacent to the seal and which it fills when the pins have been removed, which completes the closing of the cavity. The plate has application in particular to stationary gas guide vanes in turbine engines.

Abstract: Method for producing a woven structure having at least one woven wall, includes: weaving one first portion including warp and weft threads intertwined according to the fundamental weave of each portion of woven wall corresponding to this first portion, stopping introduction of weft threads after insertion of a weft thread associated with the positioning of one elongated element having a main axis, with this weft thread being intertwined with the warp threads of each portion of woven wall, introducing each elongated element between the warp threads defining with the associated weft thread, the insertion position of this elongated element, maintaining in position each elongated element and introducing one new weft thread intertwining warp threads of the structure according to the fundamental weave of each wall portion or according to at least one new weave, to resume production of the structure, with each elongated element not being taken in the structure.

Abstract: This invention relates to an assembly (100) for an aircraft turbofan comprising a flowpath splitter (40) downstream from which there is firstly a fan flowpath (31) inner delimitation ring (44) and secondly a compressor case (42), the assembly comprising a plurality of outlet guide vanes (34) provided with an inner platform (50) located in the downstream continuity of the delimitation ring. According to the invention, the assembly comprises at least one part (52) to support the delimitation ring (44), comprising a radially outer end (52b) fixed to a downstream part of this ring (44) and a radially inner end (52a) fixed to the compressor case (42).

Abstract: A transmission system for avionics application data is disclosed. In one aspect, the system is for transmitting avionics application data between data producing means and data consuming means, the application data being transmitted in the form of data transmission units, each including: at least one portion of an application message, and an additional message containing identification and control information. The additional message includes: an identification sequence including a static part making it possible to identify the application message and its source and a variable part making it possible to distinguish the message in a unique manner, and a control sequence designed to check the integrity of the application message and based on a sequence representing a cyclic redundancy control code of the concatenation of at least one portion of the application message corresponding to said unit, with the identification sequence.

Abstract: A data security system for securing the critical data of an on-board airplane avionics system comprising access control means for controlling access to the said data on the basis of the security related information of a user, wherein the security related information is selected from the group consisting of: a list of authorised users; a maximum number of allowed accesses, as well as the types of allowed accesses; a time window allowed for access; a series/concatenation allowed for access, by various different users; and a hierarchical prioritisation of the zones associated with the data storage means.

Abstract: A circuit board assembly for installation in a cabinet includes a first standards based size first mounting frame portion having a PCB mounted thereto. A second mounting frame portion is connected to the first mounting frame portion having no portion of the PCB connected thereto. A combination size of the first and second mounting frames defines a larger second standards based size. Multiple heat transfer components may be connected to the first or second mounting frame portion provide a conduction/convection cooling path. The first mounting frame portion may include a first false board edge and the second mounting frame portion includes one or more false board edge(s) positioned laterally and oppositely directed to the first false board edge. The first and second false board edges are slidably received in opposed slots created in a cabinet.

Abstract: A hybrid architecture for avionics data transmission and a corresponding system are disclosed. In one aspect, the architecture includes a plurality of subscriber stations connected by a data transmission capability. The stations are connected on the one hand by a first capability for transmitting data to their neighbors to form at least a first data transmission network in a closed ring between the stations and on the other hand by a second capability for transmitting data to a capability forming a central communication plan switch to form at least one second data transmission network in a star between the stations and the capability forming the central plan switch.

Abstract: A battery having a display indicating an amount of time the battery can be used before needing to be recharged and/or replaced. The amount of time can be displayed in minutes. An end of life indicator indicating whether the battery should be replaced can also be provided on the battery. The battery can determine the amount of time and an end of life indication based on environmental conditions and/or use. The battery can include sensors for measuring and/or monitoring environmental conditions, as well as a global positioning system (GPS) transponder. The battery can also include a communication link for transmitting data to a central location, a specified location and/or a pre-selected location, which data can include the amount of time the battery can be used before needing to be recharged and/or replaced. The battery can be coupled to and configured to power a device.

Abstract: The present invention relates to a method that may be used in a digital data communication system comprising a communication network constituted of a plurality of nodes, and a plurality of subscriber equipment units each connected to a node, includes: a transmission phase (P1) including the steps of limiting of the size of each frame to be transmitted, adding identification-authentication credentials, and transmitting the frames with a predetermined transmission interval; and a transmission phase (P2) including the steps of monitoring-checking for compliance with the input conditions; removal of each frame that is non-compliant, replicating each frame that is compliant, monitoring-checking for compliance with the output conditions, removing each frame that is non-compliant, transmitting each frame that is compliant, and recording and storing of the identification-authentication credential for each frame transmitted.

Abstract: This system for transmitting avionic information of the type including means for transmitting data frames through at least one transmission network based on avionic switches, intended for corresponding receiving means. The system further includes means for determining the crossing time by at least some of the data frames of at least some of the switches and means on the network for transmitting a corresponding crossing time information frame associated with this data frame, intended for corresponding receiving means.

Abstract: Variable displacement systems, utilizing a phase relationship controller to determine and control the volumetric displacement of liquid and gas compression systems, including applications of said systems to continuously variable, constant speed power transmissions and to variable compression-ratio internal combustion engines.

Abstract: A support structure suitable for interposing between the engine and the nacelle of an aeroengine and suitable for being fastened on an intermediate casing, the structure comprising a shroud having a plurality of sectors (12A, 12B, 12C, 12D), a plurality of radial arms (14A, 14B, 14C, 14D) each installed between two adjacent shroud sectors, and a plurality of fastener means (16) for fastening the plurality of shroud sectors to the plurality of radial arms, the shroud sectors and radial arms forming a skeleton (10) suitable for transmitting structural forces within the intermediate casing, the structure including non-structural fairings mounted on the skeleton and suitable for reconstituting the airflow passage.

Abstract: This digital data exchange architecture includes at least one communication network having at least one communication plane, a plurality of pieces of subscriber electronic equipment, and several switches. Each switch includes means forming a time referencing server able to: generate a local current time reference; transmit this local current time reference generated on the corresponding communication plane via a frame; receive via one or several frames the current time references generated by at least some of the switches of the corresponding communication plane; analyze the received current time references, in order to generate a local following time reference according to a predetermined generation law; and associate the local following time reference with the local current time reference.

Abstract: Cycling, self-checking, fail-open block valve system that continuously cycles such that the user of the block valve system can determine if the system is operational at all times. A dual port, tandem block valve body contains two block valves which alternate between full open and fully closed. The full open and full closing cycle is monitored for any changes, and the operator is alerted if one of the valves is not operating properly.

Abstract: This multi-user processor system for processing information, of the type including a data exchange engine (3) associated with multiple users (1) of shared resources (2), is characterized in that it includes means (4) for controlling data exchange in the processor, associated with each user, the exchange engine and the shared resources, in order to authorize transactions or not and in that the engine includes means (5) for breaking down authorized transactions into elementary sub-transactions, means (6) for interlacing the sub-transactions obtained from the breaking down of the authorized transactions of several users and the means (6) for distributing these interlaced sub-transactions among the different resources.

Abstract: A closer for an attachment orifice of an OGV in a turbine engine, the vane having a blade fixed to a root provided with attachment orifices, the closer including a cup adapted to be fixed in the attachment orifice of an OGV; a cylindrical shaped plug engaging in the cup, the plug including an upper face inclined relative to the ground plane of the plug; a guide adapted to position the plug on the cup by rotation into a working position, in which the upper face of the plug coincides with the surface level of the vane root; a blocking system to block the plug in the working position.

Abstract: Described herein are embodiments of methods, devices and systems of phase functionality for a meter. One aspect comprises a method of phase functionality for a meter. One embodiment of the method comprises determining a load value for each phase of a poly-phase electrical system; comparing, using a processor, the load value for each phase of a poly-phase electrical system with a respective threshold value for each phase of the poly-phase electrical system; and opening or closing one or more relays based on the comparison, wherein the one or more relays are each associated with respective phase of the poly-phase electrical system.

Abstract: A data collection device (100) is described which monitors the environmental conditions and the operations of a medical device (10). The data collection device may be arranged to communicate wirelessly via a cloud computing environment with a central computer (210). The central computer compares the reported use data with a preventive maintenance model to predict when or how the medical device will fail. In addition, the central computer may integrate reports from many data collection devices operating in various environments for the purpose of analyzing and improving the predictive maintenance model.

Abstract: A system includes a first floating unit and at least one second floating unit. The first floating unit includes at least one system of connection to the second floating unit, this connecting system including a projectile connected to a free end of a mooring line and at least one male and/or female coupling element placed at a first of its ends. The second floating unit includes at least one element for receiving-retaining the projectile from the first floating unit, these receiving-retaining elements including a housing, the shape of the projectile ensuring its placement in the housing in a non-destructive manner, and a female and/or male coupling element complementary to the male and/or female coupling element of the first floating unit, the at least one complementary female and/or male coupling element being separate from the projectile, so as to immobilize degrees of freedom of movement between floating units thus coupled.

Abstract: A light device includes a light engine having light emitting device, an optical device, and at least a first magnetic element disposed between the light emitting device and the optical device. The light device further includes a support holder having a magnetic material adapted to couple to the at least one magnetic element, to magnetically attach the light engine to the support holder.