mhurhangee/ep-ind-claims huggingface dataset:
Turbine blade with a ceramic thermal barrier coating system, at least comprising: a substrate designed as a blade platform and as a blade airfoil, optionally a metallic bond coat on the substrate, wherein on the substrate or optionally on the metallic bond coat there is a first ceramic layer as a thermal barrier coating, which protects the substrate for the most part or completely in the exposed high temperature region and that there is locally an increase (36, 36', 36") of the thermal barrier coating for locally reinforcing the thermal barrier, wherein the increase (36, 36', 36") comprises a material that is different from the material of the first ceramic layer, wherein the local reinforcement is arranged over the first ceramic layer, without the first ceramic layer having a reduced layer thickness, characterized in that the local reinforcement (36, 36', 36") is provided at most on 30% of the area of the thermal barrier coating and in that the local reinforcement (36, 36', 36") is arranged close to a platform extending over the entire pressure side in the direction of flow and with an extent thereto which in the radial direction of the blade airfoil is at most 30%. a substrate designed as a blade platform and as a blade airfoil, optionally a metallic bond coat on the substrate, wherein on the substrate or optionally on the metallic bond coat there is a first ceramic layer as a thermal barrier coating, which protects the substrate for the most part or completely in the exposed high temperature region and that there is locally an increase (36, 36', 36") of the thermal barrier coating for locally reinforcing the thermal barrier, wherein the increase (36, 36', 36") comprises a material that is different from the material of the first ceramic layer, wherein the local reinforcement is arranged over the first ceramic layer, without the first ceramic layer having a reduced layer thickness, characterized in that the local reinforcement (36, 36', 36") is provided at most on 30% of the area of the thermal barrier coating and in that the local reinforcement (36, 36', 36") is arranged close to a platform extending over the entire pressure side in the direction of flow and with an extent thereto which in the radial direction of the blade airfoil is at most 30%.
A ham stand comprising a support structure of the piece of ham with holding means for said piece of ham, a base structure for the assembly, and a connection element of the support structure to the base structure, said connection element comprising: a spherical joint on the side area of that joint connected to one of the structures (2, 4); and a housing piece of the joint, said housing piece being attached to the other structure (2, 4), such that it presents multiple degrees of freedom due to the combination of pivoting and rotational movements of the support structure with respect to the base structure; wherein the distance between the support structure and the base structure is such that the rotation angle around any axis parallel to the base structure, for the pivoting movement of the support structure with respect to the base structure, is at least between 0 and 55°; wherein the rotation angle for the rotational movement of the support structure with respect to the base structure, according to any axis comprised in the rotation angle of said pivoting movement, is between 0 and 360°; wherein the joint comprises a connection piece to the support structure or the base structure; wherein the joint has a spherical shape along its entire surface except in the area that joins to the connection piece; characterized in that: the housing piece is at least partially complementary to the geometry of the joint; and wherein the connection piece to the support structure or to the base structure is formed by a truncated cone. a spherical joint on the side area of that joint connected to one of the structures (2, 4); and a housing piece of the joint, said housing piece being attached to the other structure (2, 4), such that it presents multiple degrees of freedom due to the combination of pivoting and rotational movements of the support structure with respect to the base structure; wherein the distance between the support structure and the base structure is such that the rotation angle around any axis parallel to the base structure, for the pivoting movement of the support structure with respect to the base structure, is at least between 0 and 55°; wherein the rotation angle for the rotational movement of the support structure with respect to the base structure, according to any axis comprised in the rotation angle of said pivoting movement, is between 0 and 360°; wherein the joint comprises a connection piece to the support structure or the base structure; wherein the joint has a spherical shape along its entire surface except in the area that joins to the connection piece; characterized in that: the housing piece is at least partially complementary to the geometry of the joint; and wherein the connection piece to the support structure or to the base structure is formed by a truncated cone. the housing piece is at least partially complementary to the geometry of the joint; and wherein the connection piece to the support structure or to the base structure is formed by a truncated cone.
A bowed rotor prevention system for a gas turbine engine, the bowed rotor prevention system comprising: a core turning motor operable to drive rotation of an engine core of the gas turbine engine; and a full authority digital engine control (FADEC) comprising at least two channels, each of the at least two channels (72A, 72B) comprising a separate processing system, the FADEC configured to control operation of the gas turbine engine in a full-power mode and to control operation of the core turning motor to drive rotation of the engine core using a reduced power draw when the FADEC is partially depowered in a low-power bowed rotor prevention mode that depowers one of the at least two channels (72A, 72B). a core turning motor operable to drive rotation of an engine core of the gas turbine engine; and a full authority digital engine control (FADEC) comprising at least two channels, each of the at least two channels (72A, 72B) comprising a separate processing system, the FADEC configured to control operation of the gas turbine engine in a full-power mode and to control operation of the core turning motor to drive rotation of the engine core using a reduced power draw when the FADEC is partially depowered in a low-power bowed rotor prevention mode that depowers one of the at least two channels (72A, 72B).
Form I of 6-((6,7-dimethoxyquinazolin-4-yl)oxy)- N,2-dimethylbenzofuran-3-carboxamide, wherein the X-ray powder diffractogram of the Form I comprises diffraction angles expressed in degrees 2-theta (2θ) at: 5.3, 10.7, 13.9, and 14.6, each of the diffraction angles having an error of about ± 0.2 degrees (2θ).
A dialysis machine (100, 200, 300) comprising: tubing or a fluid container, or both, being connectable to a patient for flowing fluid to or from the patient; and a controller (105, 350); wherein a masking sound is activatable in response to noise generated during operation of the dialysis machine (100, 200, 300); characterized in that the dialysis machine (100, 200, 300) comprises one or more sensors (140, 310, 314) configured to detect one or more patient parameters; and that the controller (105, 350) is configured to determine a sleep state of the patient based on the one or more patient parameters detected by the one or more sensors (140, 310, 314); and adjust the masking sound in response to the sleep state of the patient. tubing or a fluid container, or both, being connectable to a patient for flowing fluid to or from the patient; and a controller (105, 350); wherein a masking sound is activatable in response to noise generated during operation of the dialysis machine (100, 200, 300); determine a sleep state of the patient based on the one or more patient parameters detected by the one or more sensors (140, 310, 314); and adjust the masking sound in response to the sleep state of the patient.
Arrangement having an electric motor, which comprises a rotor, a stator and an output stage having output stage switches (28, 34) and which is assigned a motor control and a supply line which are configured, on the one hand, to enable a power supply of the motor control and of the electric motor and, on the other hand, a transmission of a digital signal sequence to the electric motor by means of changing the potential of the supply line in the form of a pulse-shaped change between at least one first higher and one second lower potential, further having a signal sequence-receiving device, which is configured to evaluate a signal sequence transmitted via the supply line and from this to determine at least one motor parameter for the operation of the electric motor, and having a storage element for storing energy from the supply line, in order to enable the operation of the signal sequence-receiving device even when the second lower potential is present temporarily at the signal sequence-receiving device, which signal sequence-receiving device is configured to enable the initiation of the transmission of a motor parameter to the electric motor by a change of the potential at the supply line from the first higher to the second lower potential, and which signal sequence-receiving device is configured to switch off the output stage switch (28, 34) of the output stage during the transmission of a digital signal sequence to the electric motor and thus interrupt the energy supply to the output stage of the electric motor via the supply line.
A grinder/polisher apparatus comprising first and second sets of grinding elements (2, 3) facing each other under an angle (a) and spaced apart in overlapping relation so as to form a V-groove between the sets of grinding elements in which the cutting edge of a knife is insertable for grinding in a back and forward movement upon grinding, wherein the grinding elements (2, 3) are supported in holders (5, 6) that are movable in opposite directions and biased by springs (9, 10) towards the V-groove, and wherein the grinding elements (2,3)have grinding front faces, characterized in that the grinding elements (2, 3) have rear faces comprising coupling means (26, 27) by which the grinding elements are pivotally hinged to the holders (5, 6) about axes (R, R') the inclinations of which correspond with the opening angle (a) of the V-groove, and wherein said coupling means comprises a ridge which partially has a circular sectional profile protruding above the rear face and running centrally along the rear face of the grinding element, or comprising engagement lugs, circular in shape, and extending the whole length of the grinding element.
A substrate bonding method comprising the steps of: forming an insulating film for bonding including depositing an SiO 2 film made of TEOS by a CVD method on at least one of a first substrate and a second substrate; bonding the first substrate and the second substrate with the insulating film for bonding being in contact with the first substrate and the second substrate; the method characterised in comprising forming an electrode for bonding made of a plastically deformable metal on one of an electrode of the first substrate and an electrode of the second substrate, wherein the bonding step comprises the step of abutting the electrode for bonding against the electrode of the substrate on which the electrode for bonding is not formed and on which the electrode is surrounded by the insulating film for bonding, before the insulating film for bonding abuts against a surface of the substrate surrounding the electrode on which the insulating film for bonding is not formed, and then press-fitting to the electrode of the substrate on which the electrode for bonding is not formed. forming an insulating film for bonding including depositing an SiO 2 film made of TEOS by a CVD method on at least one of a first substrate and a second substrate; bonding the first substrate and the second substrate with the insulating film for bonding being in contact with the first substrate and the second substrate; the method characterised in comprising forming an electrode for bonding made of a plastically deformable metal on one of an electrode of the first substrate and an electrode of the second substrate,
A combination of at least two direct acting antiviral agents (DAAs) and ribavirin for use in a method for treatment of hepatitis C virus infection, said method comprising administering the said combination of at least two DAAs and ribavirin to an hepatitis C virus patient, wherein said treatment does not include administration of interferon to said patient, and said treatment lasts for 8, 9, 10, 11, 12 or 16 weeks, and wherein said at least two DAAs comprise: or a pharmaceutically acceptable salt thereof, and
A bactericidal or bacteriostatic composition for use in the treatment or the prevention of bacterial infections by Gram-positive bacteria, characterized in that it comprises a mixture of regioisomers of an alkyl acetal or an alkyl ether of sorbitan, or a pharmaceutically acceptable salt thereof, said alkyl group comprising between 11 to 18 carbon atoms, said alkyl acetal or an alkyl ether radical being on 2-O-; 3-O-,5-O- and/or 6 - O - position.
A cell culture or cell delivery composition, characterized in that the composition comprises cellulose nanofibers and/or derivatives thereof, based on microbial cellulose, in a form of a hydrogel, and the cellulose nanofibers and/or derivatives thereof comprise mechanically disintegrated microbial cellulose.
An apparatus comprising: an interface configured to receive particle acceleration data; one or more processors; one or more storage media storing instructions, which, when executed by the one or more processors, cause the apparatus to perform: transforming the particle acceleration data from a time domain to a frequency domain; characterised in that the instructions further cause the apparatus to perform: in the frequency domain, by determining a deterministic Weiner filter having a damping factor based on the particle acceleration data, the damping factor to provide stability to the filter in the presence of noise in the particle acceleration data; and applying the deterministic Wiener filter to the particle acceleration data to generate one of particle velocity data and particle displacement data in the frequency domain. an interface configured to receive particle acceleration data; one or more processors; one or more storage media storing instructions, which, when executed by the one or more processors, cause the apparatus to perform: transforming the particle acceleration data from a time domain to a frequency domain; characterised in that the instructions further cause the apparatus to perform: in the frequency domain, by determining a deterministic Weiner filter having a damping factor based on the particle acceleration data, the damping factor to provide stability to the filter in the presence of noise in the particle acceleration data; and applying the deterministic Wiener filter to the particle acceleration data to generate one of particle velocity data and particle displacement data in the frequency domain. in the frequency domain, by determining a deterministic Weiner filter having a damping factor based on the particle acceleration data, the damping factor to provide stability to the filter in the presence of noise in the particle acceleration data; and applying the deterministic Wiener filter to the particle acceleration data to generate one of particle velocity data and particle displacement data in the frequency domain.
A rotary wing aircraft control system comprising: an airframe; a main rotor assembly supported by the airframe; a control system arranged in the airframe and operatively connected to the main rotor assembly, the control system including a flight control computer, at least one control inceptor device and a touchdown orientation control system, the touchdown orientation control system including a computer readable program code embodied therewith, the computer readable program code, when executed by the flight control computer, causes the flight control computer to: sense, by a sensor operatively connected to a flight control computer, an altitude of the rotary wing aircraft relative to a landing surface; determine, through the flight control computer, one of a landing state rearward velocity reference limit value and a landing state lateral velocity reference limit value associated with the altitude; and selectively limit, by the flight control computer, an in-detent flight envelope of the rotary wing aircraft to the one of the landing state rearward velocity reference limit value and the landing state lateral velocity reference limit value. an airframe; a main rotor assembly supported by the airframe; a control system arranged in the airframe and operatively connected to the main rotor assembly, the control system including a flight control computer, at least one control inceptor device and a touchdown orientation control system, the touchdown orientation control system including a computer readable program code embodied therewith, the computer readable program code, when executed by the flight control computer, causes the flight control computer to: sense, by a sensor operatively connected to a flight control computer, an altitude of the rotary wing aircraft relative to a landing surface; determine, through the flight control computer, one of a landing state rearward velocity reference limit value and a landing state lateral velocity reference limit value associated with the altitude; and selectively limit, by the flight control computer, an in-detent flight envelope of the rotary wing aircraft to the one of the landing state rearward velocity reference limit value and the landing state lateral velocity reference limit value. sense, by a sensor operatively connected to a flight control computer, an altitude of the rotary wing aircraft relative to a landing surface; determine, through the flight control computer, one of a landing state rearward velocity reference limit value and a landing state lateral velocity reference limit value associated with the altitude; and selectively limit, by the flight control computer, an in-detent flight envelope of the rotary wing aircraft to the one of the landing state rearward velocity reference limit value and the landing state lateral velocity reference limit value.
A method, performed by a node, of controlling the node for joining a wireless network, comprising: controlling the node to wait for a predetermined length of time; receiving beacon messages communicated by nodes of the wireless network during the predetermined length of time; analysing the number of received beacon messages with respect to a congestion condition, and determining whether to control the node to join the wireless network based on the result of the analysis. controlling the node to wait for a predetermined length of time; receiving beacon messages communicated by nodes of the wireless network during the predetermined length of time; analysing the number of received beacon messages with respect to a congestion condition, and determining whether to control the node to join the wireless network based on the result of the analysis.
An aluminum-air battery unit comprising: at least one aluminum-air electrochemical cell comprising a rectangular aluminum anode, at least one corresponding air cathode, and alkaline electrolyte, a frame configured to mechanically support the anode of the cell, and a housing configured to support mechanically the frame and the at least one air cathode and to sealably hold the electrolyte within the housing and in fluid communication with openings in the housing; wherein the frame comprises a protective strap configured to protect edges of the rectangular anode against corrosion by the electrolyte during operation, and wherein the frame has an external trapezoid shape that is configured to fit into a trapezoid cavity in the housing and is configured to press the protective strap against the edges of the rectangular anode upon insertion of the frame with the anode into the housing. at least one aluminum-air electrochemical cell comprising a rectangular aluminum anode, at least one corresponding air cathode, and alkaline electrolyte, a frame configured to mechanically support the anode of the cell, and a housing configured to support mechanically the frame and the at least one air cathode and to sealably hold the electrolyte within the housing and in fluid communication with openings in the housing; wherein the frame comprises a protective strap configured to protect edges of the rectangular anode against corrosion by the electrolyte during operation, and wherein the frame has an external trapezoid shape that is configured to fit into a trapezoid cavity in the housing and is configured to press the protective strap against the edges of the rectangular anode upon insertion of the frame with the anode into the housing.
A pre-sintered or fully-sintered blank (28, 48) for use in preparing a dental restoration, such as a dental framework, crown, partial crown, bridge, cap, veneer, abutment, pin construction, in particular crown or partial crown, which has regions of different compositions, wherein one first region of a first ceramic material and at least one second region (34, 52, 54, 56) of a second ceramic material are of different compositions and the regions are sited next to one another, wherein the ceramic materials contain zirconium dioxide doped with yttrium oxide(Y 2 O 3), and optionally calcium oxide (CaO), magnesium oxide (MgO) and/or ceroxide (CeO 2), and wherein the first ceramic material differs from the material of the second ceramic material in terms of color and proportions of stabilized crystal forms present at room temperature, and wherein the at least one second region (34, 52, 54, 56) extends within the first region and have an external geometry that tapers from a base region or base surface, and wherein percentage of yttrium oxide in the second ceramic material lies between 4.5 wt% and 7.0 wt% and in the first ceramic material between 7.0 wt% and 9.5 wt%, wherein the percentage of yttrium oxide in the first ceramic material is greater than in the second ceramic material.