Abstract: According to one aspect disclosed herein, there is provided a client device for use in an optical wireless communications network, the client device comprising a transceiver configured to receive data via an optical wireless connection. The transceiver comprises an upward facing optical transducer configured to detect or transmit an optical wireless transmission, the sensor arranged to have a coverage area with at least two 5 concentric segments. A portion of the sensor is configured to provide an outermost segment of the at least two concentric segments.

Abstract: Compounds of formula (I): wherein A1, A2, Ra, Rb, Rc, Rd, R3, R4, R5 and T are as defined in the description. Medicinal products containing the same which are useful in treating pathologies involving a deficit in apoptosis, such as cancer, auto-immune diseases, and diseases of the immune system.

Abstract: A system is provided for determining the position of an interventional device inside a lumen. The interventional device comprises a distal portion inside the lumen and a proximal portion outside the lumen and the system comprises a processor. The processor is configured to receive a first estimated position of the distal portion of the interventional device inside the lumen from a first system and receive an estimated displacement of the distal portion of the interventional device inside a lumen from a second system, wherein the estimated displacement is representative of the movement of the distal portion of the interventional device inside the lumen. The processor is further configured to determine a second estimated position of the distal portion of the interventional device inside the lumen based on the first estimated position and the estimated displacement.

Abstract: The invention relates to a foldable cot, comprising a bottom portion and a stretchable side wall. The cot further comprises a movable frame for stretching the side wall to an unfolded state. The foldable cot also comprises an adapter mounted to a side wall frame element for connecting the foldable cot to a bearing frame of a buggy, the adapter having a rotatable element that is rotatably attached to the side wall frame element, and an engaging element fixedly attached to the rotatable element such that upon pivoting the frame arm for unfolding the side wall, the frame arm also engages the engaging element inducing the rotatable element to swivel relative to the side wall frame element of the frame for bringing the cot in a mainly horizontal orientation.

Abstract: Various disclosed embodiments are directed to image-to-material translation based on delighting an input image, thereby allowing proper capturing of the color and geometry properties of the input image for generating a visual rendering. This, among other functionality described herein, improves the inaccuracies, user experience, and computing resource consumption of existing technologies.

Abstract: The invention relates to an air intake of an aircraft turbojet engine nacelle extending along an axis X, in which an air flow circulates from upstream to downstream, the air intake comprising an inner wall and an outer wall which are connected by a leading edge and an inner partition so as to delimit an annular cavity, the air intake comprising means for injecting at least one hot air flow into the inner cavity and at least one ventilation orifice formed in the outer wall in order to allow the hot air flow to escape after heating the inner cavity, the air intake comprising at least one acoustic member positioned in the inner cavity facing the ventilation orifice so as to modify the acoustic resonance frequencies and/or to attenuate the acoustic waves formed in the inner cavity via the ventilation orifice.

Abstract: The invention relates to an air intake of an aircraft turbojet engine nacelle, extending along an axis X, in which an air flow circulates from upstream to downstream, the air intake comprising an inner wall facing the axis X and an outer wall for guiding an external air flow, the walls being connected by a leading edge and an inner partition so as to delimit an annular cavity. The air intake comprises means for injecting at least one hot air flow into the inner cavity and at least one ventilation orifice formed in the outer wall to allow the hot air flow to escape after heating the inner cavity, the ventilation orifice comprising an upstream edge, the circumferential profile of which is discontinuous in order to generate turbulences, and a downstream edge, the radial profile of which is aerodynamic in order to limit the formation of pressure fluctuations.

Abstract: The invention relates to an air intake of an aircraft turbojet engine nacelle, extending along an axis X, in which an air flow circulates from upstream to downstream, the air intake extending circumferentially around the axis X and comprising an inner wall, which faces the axis X in order to guide an inner air flow, and an outer wall, which is opposite the inner wall, for guiding an external air flow, the walls being connected by a leading edge and an inner partition so as to delimit an annular cavity. The air intake comprises means for injecting at least one hot air flow into the inner cavity and at least one ventilation orifice formed in the outer wall in order to allow the hot air flow to escape after heating the internal cavity, the air intake comprising at least one disruption member of the external air flow, positioned upstream of the ventilation orifice, which extends outwardly from the outer wall.

Abstract: The invention relates to a foldable cot, comprising a bottom portion and a stretchable side wall. The cot further comprises a movable frame for stretching the side wall to an unfolded state. The foldable cot also comprises an adapter mounted to a side wall frame element for connecting the foldable cot to a bearing frame of a buggy, the adapter having a rotatable element that is rotatably attached to the side wall frame element, and an engaging element fixedly attached to the rotatable element such that upon pivoting the frame arm for unfolding the side wall, the frame arm also engages the engaging element inducing the rotatable element to swivel relative to the side wall frame element of the frame for bringing the cot in a mainly horizontal orientation.

Abstract: Various disclosed embodiments are directed to image-to-material translation based on delighting an input image, thereby allowing proper capturing of the color and geometry properties of the input image for generating a visual rendering. This, among other functionality described herein, improves the inaccuracies, user experience, and computing resource consumption of existing technologies.

Abstract: The invention relates to an air intake of an aircraft turbojet engine nacelle extending along an axis X, in which an air flow circulates from upstream to downstream, the air intake comprising an inner wall and an outer wall which are connected by a leading edge and an inner partition so as to delimit an annular cavity, the air intake comprising means for injecting at least one hot air flow into the inner cavity and at least one ventilation orifice formed in the outer wall in order to allow the hot air flow to escape after heating the inner cavity, the air intake comprising at least one acoustic member positioned in the inner cavity facing the ventilation orifice so as to modify the acoustic resonance frequencies and/or to attenuate the acoustic waves formed in the inner cavity via the ventilation orifice.

Abstract: The invention relates to an air intake of an aircraft turbojet engine nacelle, extending along an axis X, in which an air flow circulates from upstream to downstream, the air intake comprising an inner wall facing the axis X and an outer wall for guiding an external air flow, the walls being connected by a leading edge and an inner partition so as to delimit an annular cavity. The air intake comprises means for injecting at least one hot air flow into the inner cavity and at least one ventilation orifice formed in the outer wall to allow the hot air flow to escape after heating the inner cavity, the ventilation orifice comprising an upstream edge, the circumferential profile of which is discontinuous in order to generate turbulences, and a downstream edge, the radial profile of which is aerodynamic in order to limit the formation of pressure fluctuations.

Abstract: A distributor valve comprising a second element configured to be displaced relative to a first element, so as to form an overall passage opening of variable fuel passage section corresponding to the intersection of a first passage opening and a second passage opening. The head portion of the second passage opening comprises a first inclination having a first average slope, the intermediate portion of the second passage opening comprises a second inclination having a second average slope strictly greater than said first average slope, and the foot portion of the second passage opening comprises a third inclination having a third average slope, strictly less than said second average slope.

Abstract: The invention relates to an air intake of an aircraft turbojet engine nacelle, extending along an axis X, in which an air flow circulates from upstream to downstream, the air intake extending circumferentially around the axis X and comprising an inner wall, which faces the axis X in order to guide an inner air flow, and an outer wall, which is opposite the inner wall, for guiding an external air flow, the walls being connected by a leading edge and an inner partition so as to delimit an annular cavity. The air intake comprises means for injecting at least one hot air flow into the inner cavity and at least one ventilation orifice formed in the outer wall in order to allow the hot air flow to escape after heating the internal cavity, the air intake comprising at least one disruption member of the external air flow, positioned upstream of the ventilation orifice, which extends outwardly from the outer wall.

Abstract: The invention provides a method for monitoring a location of a tool in an ultrasound image. The method includes acquiring a plurality of 2D ultrasound images by way of an ultrasound transducer, wherein at least one of the plurality of 2D ultrasound images comprises a part of the tool and generating a 3D ultrasound image from said plurality of 2D ultrasound images. A first location of the tool is then identified within the 3D ultrasound image. An additional 2D ultrasound image, and location information relating to the location of the ultrasound transducer during capture of the additional 2D ultrasound image, is then acquired and the 3D ultrasound image updated based on the additional 2D ultrasound image and the location information. A location of the tool with respect to the additional 2D ultrasound image is then identified within the updated 3D ultrasound image based only on imaging data of the updated 3D ultrasound image.