mhurhangee/ep-ind-claims huggingface dataset:
Primary structure for a spacecraft comprising an interface ring and a predetermined number of panels (1a, 1b, 1c) defining a box arranged so as to close an interior volume of the spacecraft, the box being connected to the interface ring, the side panels of the box being parallel to a geometric axis of the interface ring, the interface ring being intended to be temporarily fastened to a system supporting the spacecraft in a launcher, each panel (1a, 1b, 1c) being a one-piece panel and being obtained by machining a single solid metal block, the side panels (1a, 1b) at the base of the box being connected to the interface ring via damping inserts, each panel comprising a network of intersecting ribs (3a, 3b, 3c, 3d) connected to one another by thinned plates (4a, 4b), the network of ribs being arranged, in each panel, so as to induce at least a determined stiffness as well as a transfer of forces between a proximal edge and a distal edge relative to the interface ring, the side panels (1a, 1b) at the base of the box comprise open recesses for receiving the damping inserts, each of these recesses being defined by a rib, the latter rib being continued by at least one rib extending in a longitudinal direction relative to the geometric axis of the interface ring.
A galvanic sensor comprising: a housing an anode including antimony, the anode including a plurality of holes extending through the anode, the plurality of holes having a diameter within a range of from 0.5 millimeters to about 2 millimeters, wherein the anode is substantially free from lead; a cathode including at least one of platinum, silver and gold; and an electrolyte. a housing an anode including antimony, the anode including a plurality of holes extending through the anode, the plurality of holes having a diameter within a range of from 0.5 millimeters to about 2 millimeters, wherein the anode is substantially free from lead; a cathode including at least one of platinum, silver and gold; and an electrolyte. extending through the anode, the plurality of holes having a diameter within a range of from 0.5 millimeters to about 2 millimeters, wherein the anode is substantially free from lead; a cathode including at least one of platinum, silver and gold; and an electrolyte.
An in-vehicle apparatus for restricting at least one vehicle function, said apparatus comprising: - a switch adapted to switch between a first operative position and a second operative position; - a control unit for receiving said operation of said switch; wherein said switch generates a first signal when the switch is in first operative position to enable restriction of at least one vehicle function; wherein said switch generates a second signal when the switch is in second operative position to disable said restriction of at least one vehicle function; - said control unit being adapted to communicate with a transponder and an authentication unit to execute an authentication process to restrict at least one vehicle function in dependence of operation of said switch in said first operative position, characterized in that - said control unit is associated with a keypad to input a password, and - said control unit is adapted to execute a second authentication process based on said second signal to disable restriction of said vehicle function, wherein a password is received before the execution of said second authentication process to validate the disabling of the restriction of vehicle function. - a switch adapted to switch between a first operative position and a second operative position; - a control unit for receiving said operation of said switch; wherein said switch generates a first signal when the switch is in first operative position to enable restriction of at least one vehicle function; wherein said switch generates a second signal when the switch is in second operative position to disable said restriction of at least one vehicle function; - said control unit being adapted to communicate with a transponder and an authentication unit to execute an authentication process to restrict at least one vehicle function in dependence of operation of said switch in said first operative position, - said control unit is associated with a keypad to input a password, and - said control unit is adapted to execute a second authentication process based on said second signal to disable restriction of said vehicle function, wherein a password is received before the execution of said second authentication process to validate the disabling of the restriction of vehicle function.
Method for separating a dental deep drawing model from a deep drawing film, characterized in that at least one pulling means which extends at least in sections between the deep drawing model and the deep drawing film and which comprises a stop for a puller is arranged on the deep drawing model, in that the deep drawing model is positioned along with the deep drawing film over a removal opening, the edge of which forms a stop limit for the free deep drawing edge of the deep drawing film, and then a movable puller is brought into an engagement position, in which the puller engages in the stop of the pulling means and is moved beyond this engagement position into a removal position, in which the deep drawing model is pulled out of the deep drawing film through the removal opening.
A removable closure device for a space inside an aircraft, comprising: - a frame including at least one fixing interface (15.1, 15.2) for a structural element, - a curtain assembly including a flexible curtain (16.1), - a roller around which the flexible curtain (16.1) can be wound, wherein said frame includes at least one strut (12.1, 12.2), said strut (12.1, 12.2) including the fixing interface (15.1, 15.2), - at least one guiding device including an electric motor actuator, said guiding device being able to guide in translation the flexible curtain (16.1) relative to the strut (12.1, 12.2), such that the flexible curtain (16.1) can be moved along a direction of movement parallel to a longitudinal direction of the strut (12.1, 12.2) between a stored position in which the flexible curtain (16.1) is mainly wound around the roller and a deployed position in which the flexible curtain (16.1) is mainly unrolled relative to the roller. - a frame including at least one fixing interface (15.1, 15.2) for a structural element, - a curtain assembly including a flexible curtain (16.1), - a roller around which the flexible curtain (16.1) can be wound, wherein said frame includes at least one strut (12.1, 12.2), said strut (12.1, 12.2) including the fixing interface (15.1, 15.2), - at least one guiding device including an electric motor actuator, said guiding device being able to guide in translation the flexible curtain (16.1) relative to the strut (12.1, 12.2), such that the flexible curtain (16.1) can be moved along a direction of movement parallel to a longitudinal direction of the strut (12.1, 12.2) between a stored position in which the flexible curtain (16.1) is mainly wound around the roller and a deployed position in which the flexible curtain (16.1) is mainly unrolled relative to the roller.
- A duct for a bleed system of an aircraft, wherein the duct extends at least partially along a longitudinal axis (z-z'), the duct comprising: - an inlet section for entering a fluid flow into the duct; - an outlet section distanced from the inlet section, through which such fluid flow exits the duct; and - at least one continuous piece (4, 5) arranged on an internal wall of the duct and protruding therefrom, the at least one continuous piece (4, 5) having: ∘ a first end (4.1, 5.1) located at a position adjacent to the inlet section and ∘ a second end (4.2, 5.2) located at a position close to the outlet section, wherein the continuous piece (4, 5) is slantly extended from the first end (4.1, 5.1) to the second end (4.2, 5.2) along the longitudinal axis (z-z') direction of the duct so that first and second ends are substantially opposed in transversal cross-section of the duct; the duct being characterised in that at least one continuous piece (4, 5) has three portions: - a first portion (4.3, 5.3) starting at the first end (4.1, 5.1) of the continuous piece, - a second portion (4.4, 5.4), and - a third portion (4.5, 5.5) ending at the second end (4.2, 5.2) of the continuous piece, wherein each portion (4.3, 5.3; 4.4, 5.4; 4.5, 5.5) of the continuous piece (4, 5) has a different tilting degree in relation to the longitudinal axis (z-z') of the duct. - an inlet section for entering a fluid flow into the duct; - an outlet section distanced from the inlet section, through which such fluid flow exits the duct; and - at least one continuous piece (4, 5) arranged on an internal wall of the duct and protruding therefrom, the at least one continuous piece (4, 5) having: ∘ a first end (4.1, 5.1) located at a position adjacent to the inlet section and ∘ a second end (4.2, 5.2) located at a position close to the outlet section, ∘ a first end (4.1, 5.1) located at a position adjacent to the inlet section and ∘ a second end (4.2, 5.2) located at a position close to the outlet section, wherein the continuous piece (4, 5) is slantly extended from the first end (4.1, 5.1) to the second end (4.2, 5.2) along the longitudinal axis (z-z') direction of the duct so that first and second ends are substantially opposed in transversal cross-section of the duct; the duct being characterised in that at least one continuous piece (4, 5) has three portions: - a first portion (4.3, 5.3) starting at the first end (4.1, 5.1) of the continuous piece, - a second portion (4.4, 5.4), and - a third portion (4.5, 5.5) ending at the second end (4.2, 5.2) of the continuous piece, - a first portion (4.3, 5.3) starting at the first end (4.1, 5.1) of the continuous piece, - a second portion (4.4, 5.4), and - a third portion (4.5, 5.5) ending at the second end (4.2, 5.2) of the continuous piece,
An implantable medical device comprising: a hermetically sealed housing containing electronic circuitry; a feedthrough disposed on an external surface of said housing; an antenna wire having a first distal end, a second distal end and an external surface, said antenna wire being disposed around said external surface of said housing, said antenna wire having said one end connected to said feedthrough so that said antenna wire is in electric communication with at least a portion of said electronic circuitry; characterised by a tube sealingly disposed about said entire external surface of said antenna wire to prevent fluids from contacting the wire and thereby detuning the antenna wire; and an antenna surround (44, 46) disposed about said tube. a hermetically sealed housing containing electronic circuitry; a feedthrough disposed on an external surface of said housing; an antenna wire having a first distal end, a second distal end and an external surface, said antenna wire being disposed around said external surface of said housing, said antenna wire having said one end connected to said feedthrough so that said antenna wire is in electric communication with at least a portion of said electronic circuitry; characterised by a tube sealingly disposed about said entire external surface of said antenna wire to prevent fluids from contacting the wire and thereby detuning the antenna wire; and an antenna surround (44, 46) disposed about said tube.
A liquid formulation comprising an antibody and a compound which prevents oxidation of the antibody in the liquid formulation, wherein the compound is of formula: wherein R 2 and R 3 are independently selected from hydrogen, hydroxyl, -COOH, and -CH 2 COOH; and R 4, R 5, R 6, and R 7 are independently selected from hydrogen and hydroxyl; provided that one of R 2, R 3, R 4, R 5, R 6, and R 7 is hydroxyl; or a pharmaceutically acceptable salt thereof. wherein R 2 and R 3 are independently selected from hydrogen, hydroxyl, -COOH, and -CH 2 COOH; and R 4, R 5, R 6, and R 7 are independently selected from hydrogen and hydroxyl; provided that one of R 2, R 3, R 4, R 5, R 6, and R 7 is hydroxyl; or a pharmaceutically acceptable salt thereof.
A fortifying powder comprising: a. a lipophilic nutrient, b. a monoglyceride and diglyceride oil present at a concentration of 6 wt% to 50 wt% of the fortifying powder, c. a phospholipid present at a concentration of 1 wt% to 12 wt% of the fortifying powder, and d. a carrier. a. a lipophilic nutrient, b. a monoglyceride and diglyceride oil present at a concentration of 6 wt% to 50 wt% of the fortifying powder, c. a phospholipid present at a concentration of 1 wt% to 12 wt% of the fortifying powder, and d. a carrier.
A formulation for substantially stable storage of one or more nucleic acid molecule in a native, non-denatured state in a blood sample at ambient temperatures, wherein the one or more nucleic acid molecule is stabilized in a native, non-denatured state substantially free of contaminating intracellular nucleic acids after storage at room temperature for a period of at least four days, wherein the formulation comprises: (i) a pH buffer; (ii) a phosphatase inhibitor; (iii) a purine; (iv) a zwitterionic compound, a cationic compound, or a combination thereof; and (v) a compound selected from: (v.a) an apoptosis inhibitor or a caspase inhibitor; and/or (v.b) a nuclease inhibitor; and wherein said formulation does not comprise a chelating agent, such as EDTA. (i) a pH buffer; (ii) a phosphatase inhibitor; (iii) a purine; (iv) a zwitterionic compound, a cationic compound, or a combination thereof; and (v) a compound selected from: (v.a) an apoptosis inhibitor or a caspase inhibitor; and/or (v.b) a nuclease inhibitor; (v.a) an apoptosis inhibitor or a caspase inhibitor; and/or (v.b) a nuclease inhibitor;
A protective apparatus, comprising a bracket and a cover, the upper side of the cover being hinged with the upper side of the bracket, wherein said protective apparatus comprises a pull-down apparatus, the pull-down apparatus comprises a fixed pulley, a movable pulley, a push rod and a pull rope, wherein the fixed pulley is fixedly connected to the cover, the movable pulley is located above the fixed pulley, the movable pulley is slidingly connected to the cover, the fixed end of the pull rope bypassing the movable pulley is connected to the fixed pulley, the upper end of the push rod is connected to the movable pulley, the push rod and the movable pulley cause a handle end of the pull rope to hang down under the action of gravity, and wherein by pulling down the handle end of the pull rope to move the cover downwards, after the lower end of the push rod contacts the bracket, the push rod pushes the movable pulley upwards to drive the handle end of the pull rope upwards.
A data communication method based on a distribution point unit, DPU, comprising: dividing the DPU into a plurality of virtual DPUs, vDPUs, wherein a data transmission channel of a vDPU is mutually isolated from a data transmission channel of another vDPU; receiving, by the data transmission channels of the plurality of vDPUs of the DPU, a respective data transmission configuration parameter from the OLT; and transmitting data, by the data transmission channels of the plurality of vDPUs, according to the respective data transmission configuration parameter. dividing the DPU into a plurality of virtual DPUs, vDPUs, wherein a data transmission channel of a vDPU is mutually isolated from a data transmission channel of another vDPU; receiving, by the data transmission channels of the plurality of vDPUs of the DPU, a respective data transmission configuration parameter from the OLT; and transmitting data, by the data transmission channels of the plurality of vDPUs, according to the respective data transmission configuration parameter.
A subsea leak detection system for an off-shore operation facility, comprising at least one leak detector operatively connected to a controller located on a subsea assembly characterised in that said system is provided with a floating member on which said leak detector is attached, said floating member being adapted to be installed, and stably positioned, above said assembly that said subsea assembly includes a X-mas tree and a protective structure having a template hatch extending above the X-mas tree, the protective structure acting to collect hydrocarbon leakages, said floating member is a buoy anchored by a locking unit via wires, and said leak detector is positioned above a roof of said x-mas tree and beneath said template hatch.
An item (10; 11) having - a change-in-environment part and - a barcode (12; 13) which contains data relating to the change-in-environment part, said change-in-environment part being a part that changes in accordance with environmental conditions, characterised in that the barcode (12; 13) includes information about the position of the change-in-environment part. - a change-in-environment part and - a barcode (12; 13) which contains data relating to the change-in-environment part,
A labelling machine comprising: a main supporting frame; a carrousel rotatably mounted on the main supporting frame according to a vertical axis of rotation, the outside of the carrousel being equipped with a plurality of supporting means for the objects to be labelled; means for feeding the objects to be labelled to the supporting means and means for picking up the labelled objects from the supporting means; and a plurality of labelling devices positioned radially along the edge of the carrousel which in practice apply labels to objects placed on the supporting means which pass them during carrousel rotation; the main supporting frame having a guiding and supporting track to which the labelling devices are slidably connected so that they can be placed at different positions along the edge of the carrousel; a plurality of connecting modules equipped with first coupling means allowing sliding coupling to the track; second coupling means for reversibly coupling each labelling device to a connecting module; and means for the controlled movement of each connecting module along the track; the machine being characterised in that the controlled movement means comprise mechanical meshing between each connecting module and the main frame. a main supporting frame; a carrousel rotatably mounted on the main supporting frame according to a vertical axis of rotation, the outside of the carrousel being equipped with a plurality of supporting means for the objects to be labelled; means for feeding the objects to be labelled to the supporting means and means for picking up the labelled objects from the supporting means; and a plurality of labelling devices positioned radially along the edge of the carrousel which in practice apply labels to objects placed on the supporting means which pass them during carrousel rotation; the main supporting frame having a guiding and supporting track to which the labelling devices are slidably connected so that they can be placed at different positions along the edge of the carrousel; a plurality of connecting modules equipped with first coupling means allowing sliding coupling to the track; second coupling means for reversibly coupling each labelling device to a connecting module; and means for the controlled movement of each connecting module along the track; the machine being characterised in that the controlled movement means comprise mechanical meshing between each connecting module and the main frame.
A method for acquiring a sharable power in a cell, characterized by comprising: acquiring, by a network side device, transmit powers of all carriers in the cell; allocating, by the network side device, each carrier, which has not been allocated yet to any power amplifier of the cell, and whose transmit power is the maximum among said transmit powers of all carriers, to a power amplifier, among all power amplifiers of the cell, having a maximum available power; updating, by the network side device, an available power of said power amplifier, said available power being obtained by calculating a difference between said maximum available power of said power amplifier and a sum of transmit powers of all carriers allocated onto that said power amplifier; repeatedly executing, by the network side device, the allocating and updating steps until allocating of all the carriers is complete; and acquiring, by the network side device, a minimum value among values of available powers of all the power amplifiers as the sharable power of the cell. acquiring, by a network side device, transmit powers of all carriers in the cell; allocating, by the network side device, each carrier, which has not been allocated yet to any power amplifier of the cell, and whose transmit power is the maximum among said transmit powers of all carriers, to a power amplifier, among all power amplifiers of the cell, having a maximum available power; updating, by the network side device, an available power of said power amplifier, said available power being obtained by calculating a difference between said maximum available power of said power amplifier and a sum of transmit powers of all carriers allocated onto that said power amplifier; repeatedly executing, by the network side device, the allocating and updating steps until allocating of all the carriers is complete; and acquiring, by the network side device, a minimum value among values of available powers of all the power amplifiers as the sharable power of the cell.
Use of a copolymer containing a unit comprising (i) an optionally neutralised styrene sulphonic acid unit and (ii) a unit containing an optionally neutralised (poly)carboxylic acid unit and/or a (poly)amido-amine unit, to inhibit or slow the formation of sulphide deposits, in particular of lead, iron and/or zinc sulphides, during the extraction of gas or oil.
An environmental control system for an aircraft, comprising: a first turbine configured to be coupled to an engine; a second turbine and a compressor, the second turbine coupled to the compressor; and one or more ducts configured to provide bleed air from the engine to the first and second turbines and the compressor such that the first and second turbines and the compressor condition the bleed air; characterized in that the first and second turbines, and the compressor are configured to be situated in a common compartment of an aircraft with the engine and the first turbine is configured to power the engine via a gearbox. a first turbine configured to be coupled to an engine; a second turbine and a compressor, the second turbine coupled to the compressor; and one or more ducts configured to provide bleed air from the engine to the first and second turbines and the compressor such that the first and second turbines and the compressor condition the bleed air; characterized in that the first and second turbines, and the compressor are configured to be situated in a common compartment of an aircraft with the engine and the first turbine is configured to power the engine via a gearbox.