mhurhangee/patent-ind-claim-en huggingface dataset:
A slipper retainer ball for use within a hydraulic unit and configured to turn or rotate with respect to a wobbler of the hydraulic unit when installed therein, comprising: a partial spherical body having an aperture passing through a center of the body and defining an axis, the body having a flat bottom surface , a flat top surface , an external curved surface that is a smooth arcuate surface that extends from the bottom surface to the top surface, and an interior profiled surface that extends in an axial direction from the bottom surface to the top surface; the interior profiled surface comprising: a first surface extending parallel to the axis from the bottom surface in the axial direction; a second surface extending perpendicular to the axis from the first surface and radially outward toward the external curved surface; a third surface extending from the second surface in the axial direction at a first angle that is skew from the axis; a fourth surface extending from the third surface parallel to the axis and in the axial direction; and a fifth surface extending from the fourth surface to the top surface at a second angle that is skew from the axis; wherein the axial thickness of the body extending between the bottom surface and the top surface is 1.196 cm (0.471 inches). a partial spherical body having an aperture passing through a center of the body and defining an axis, the body having a flat bottom surface , a flat top surface , an external curved surface that is a smooth arcuate surface that extends from the bottom surface to the top surface, and an interior profiled surface that extends in an axial direction from the bottom surface to the top surface; the interior profiled surface comprising: a first surface extending parallel to the axis from the bottom surface in the axial direction; a second surface extending perpendicular to the axis from the first surface and radially outward toward the external curved surface; a third surface extending from the second surface in the axial direction at a first angle that is skew from the axis; a fourth surface extending from the third surface parallel to the axis and in the axial direction; and a fifth surface extending from the fourth surface to the top surface at a second angle that is skew from the axis; a first surface extending parallel to the axis from the bottom surface in the axial direction; a second surface extending perpendicular to the axis from the first surface and radially outward toward the external curved surface; a third surface extending from the second surface in the axial direction at a first angle that is skew from the axis; a fourth surface extending from the third surface parallel to the axis and in the axial direction; and a fifth surface extending from the fourth surface to the top surface at a second angle that is skew from the axis; wherein the axial thickness of the body extending between the bottom surface and the top surface is 1.196 cm (0.471 inches).
An imaging device comprising: a plurality of pixels (P) each including a first light-receiving element (PD1) and a second light-receiving element (PD2), the plurality of pixels (P) including a first pixel (P1), wherein a size of a light-receiving region of the first light-receiving element (PD1) is different from a size of a light-receiving region of the second light-receiving element (PD2); a generating section that is able to generate a first detection value on a basis of a light-receiving result by the first light-receiving element (PD1) of each of the plurality of pixels (P), and is able to generate a second detection value on a basis of a light-receiving result by the second light-receiving element (PD2) of each of the plurality of pixels (P); and a diagnosis section that is able to perform blooming detection on a basis of a detection ratio that is a ratio between the first detection value and the second detection value in the first pixel (P1), and wherein the diagnosis section is able to perform the blooming detection also on a basis of whether the first detection value in the first pixel (P1) is saturated and whether the second detection value in the first pixel (P1) is saturated, in addition to the detection ratio in the first pixel (P1). a plurality of pixels (P) each including a first light-receiving element (PD1) and a second light-receiving element (PD2), the plurality of pixels (P) including a first pixel (P1), wherein a size of a light-receiving region of the first light-receiving element (PD1) is different from a size of a light-receiving region of the second light-receiving element (PD2); a generating section that is able to generate a first detection value on a basis of a light-receiving result by the first light-receiving element (PD1) of each of the plurality of pixels (P), and is able to generate a second detection value on a basis of a light-receiving result by the second light-receiving element (PD2) of each of the plurality of pixels (P); and a diagnosis section that is able to perform blooming detection on a basis of a detection ratio that is a ratio between the first detection value and the second detection value in the first pixel (P1), and wherein the diagnosis section is able to perform the blooming detection also on a basis of whether the first detection value in the first pixel (P1) is saturated and whether the second detection value in the first pixel (P1) is saturated, in addition to the detection ratio in the first pixel (P1).
A multilink-based communication method of a transmitter in a wireless communication system, the method comprising: receiving , at a multilink adaptation protocol, MLAP, layer of the transmitter, multilink control information from a MLAP layer of a receiver; identifying whether a difference of characteristic values between multiple links is greater than a predetermined value; determining , at the MLAP layer of the transmitter, transmission data distribution to the multiple links based on the multilink control information in case that the difference of the characteristic values between the multiple links is not greater than the predetermined value, wherein the multiple links are associated with a plurality of radio access technology, RAT, types; transmitting the distributed transmission data on the multiple links simultaneously; selecting a path from the multiple links in case that the difference of the characteristic values between the multiple links is greater than the predetermined value; and transmitting data on the selected path. receiving , at a multilink adaptation protocol, MLAP, layer of the transmitter, multilink control information from a MLAP layer of a receiver; identifying whether a difference of characteristic values between multiple links is greater than a predetermined value; determining , at the MLAP layer of the transmitter, transmission data distribution to the multiple links based on the multilink control information in case that the difference of the characteristic values between the multiple links is not greater than the predetermined value, wherein the multiple links are associated with a plurality of radio access technology, RAT, types; transmitting the distributed transmission data on the multiple links simultaneously; selecting a path from the multiple links in case that the difference of the characteristic values between the multiple links is greater than the predetermined value; and transmitting data on the selected path.
Method for conductively heating a metal sheet to prepare the metal sheet for a subsequent shaping press-hardening process, wherein the metal sheet or at least an area of the metal sheet that is to be conductively heated has an outer contour that is rectangular or nonrectangular, wherein the conductive heating is performed by virtue of at least one electrode having a contact area brought into electrical contact with the metal sheet and the contact area being used to supply the electric current for performing the conductive heating to the metal sheet and/or to remove said electric current from the metal sheet , characterized in that the electrode has an uneven, patterned contact area having a multiplicity of contact surfaces , at intervals from one another, that form a multiplicity of individual contact points, at intervals from one another, between the electrode and the metal sheet .
An aircraft comprising: a first wing , a second wing , and a fuselage, the first wing and a portion of the fuselage defining a first side , and the second wing and another portion of the fuselage defining a second side ; and an asymmetric propulsion system , the asymmetric propulsion system comprising: an electric generator ; a single turbomachine with a turbine section and a shaft rotatable with at least a portion of the turbine section, the single turbomachine being operable to drive the electric generator and a first propulsor mechanically coupled to the shaft of the single turbomachine , the single turbomachine being mounted to the first side of the aircraft ; and a second propulsor assembly mounted to the second side at a location away from the single turbomachine and the first propulsor , the electric generator in electrical communication with the second propulsor assembly for powering the second propulsor assembly. a first wing , a second wing , and a fuselage, the first wing and a portion of the fuselage defining a first side , and the second wing and another portion of the fuselage defining a second side ; and an asymmetric propulsion system , the asymmetric propulsion system comprising: an electric generator ; a single turbomachine with a turbine section and a shaft rotatable with at least a portion of the turbine section, an electric generator ; a single turbomachine with a turbine section and a shaft rotatable with at least a portion of the turbine section, the single turbomachine being operable to drive the electric generator and a first propulsor mechanically coupled to the shaft of the single turbomachine , the single turbomachine being mounted to the first side of the aircraft ; and a second propulsor assembly mounted to the second side at a location away from the single turbomachine and the first propulsor , the electric generator in electrical communication with the second propulsor assembly for powering the second propulsor assembly. a first propulsor mechanically coupled to the shaft of the single turbomachine , the single turbomachine being mounted to the first side of the aircraft ; and a second propulsor assembly mounted to the second side at a location away from the single turbomachine and the first propulsor , the electric generator in electrical communication with the second propulsor assembly for powering the second propulsor assembly.
A garment to which a blower device is detachably attachable, the garment comprising a main body including at least an outer fabric having an attachment hole through which the blower device can be partially inserted, the main body being configured to cover at least a portion of a body of a wearer, and a heat insulation material attached to the main body at least on an inner side of the outer fabric and configured to cover at least a portion of the body, wherein the garment is configured such that the heat insulation material is detachable from the main body , and wherein at least one of the main body and the heat insulation material has a positioning part configured to hold the heat insulation material at a predetermined position relative to the main body , characterized in that the positioning part is provided on the heat insulation material , and configured to be engaged with the attachment hole to hold the heat insulation material at the predetermined position relative to the main body . a main body including at least an outer fabric having an attachment hole through which the blower device can be partially inserted, the main body being configured to cover at least a portion of a body of a wearer, and a heat insulation material attached to the main body at least on an inner side of the outer fabric and configured to cover at least a portion of the body, wherein the garment is configured such that the heat insulation material is detachable from the main body , and wherein at least one of the main body and the heat insulation material has a positioning part configured to hold the heat insulation material at a predetermined position relative to the main body , characterized in that the positioning part is provided on the heat insulation material , and configured to be engaged with the attachment hole to hold the heat insulation material at the predetermined position relative to the main body .
A lighting device comprising: - at least one light guide ; - a light source coupled to a light inlet surface of the at least one light guide ; the lighting device further comprising a reflecting element for reflecting light beams (a) emitted by the light source , the reflecting element being located at an end of the at least one light guide opposite the light inlet surface wherein: - the at least one light guide is configured for emitting light beams (C) mainly in a first direction (X) through a light outlet surface of the at least one light guide , the light outlet surface being disposed at least partially at an angle (alpha) of more than 90o with respect to the first direction (X); - the light guide has at least one surface comprised of a plurality of prisms , at least a first portion of the plurality of prisms being configured for reflecting light beams (B) coming from the reflecting element , and to reflect them towards the first direction (X); - at least a second portion of the plurality of prisms is configured for refracting light beams coming from the light source ; characterized in that - the lighting device further comprises a light guide support having a reflective surface for reflecting light beams (A) coming from the light source . - at least one light guide ; - a light source coupled to a light inlet surface of the at least one light guide ; - the at least one light guide is configured for emitting light beams (C) mainly in a first direction (X) through a light outlet surface of the at least one light guide , the light outlet surface being disposed at least partially at an angle (alpha) of more than 90o with respect to the first direction (X); - the light guide has at least one surface comprised of a plurality of prisms , at least a first portion of the plurality of prisms being configured for reflecting light beams (B) coming from the reflecting element , and to reflect them towards the first direction (X); - at least a second portion of the plurality of prisms is configured for refracting light beams coming from the light source ; characterized in that - the lighting device further comprises a light guide support having a reflective surface for reflecting light beams (A) coming from the light source . - the lighting device further comprises a light guide support having a reflective surface for reflecting light beams (A) coming from the light source .
A gas turbine arrangement, in particular a micro gas turbine arrangement, comprising: - a gas turbine device comprising a combustor system , a turbine driven by an exhaust gas stream of said combustor system, and a compressor for supplying said combustor system with a compressed oxidant stream ; - a recuperator having a heat exchanger for transferring at least a portion of the thermal power of said exhaust gas stream of said turbine to said compressed oxidant stream ; - at least one exhaust gas-side bypass connecting a second inlet of said recuperator for said exhaust gas stream to a second outlet of said recuperator for said exhaust gas stream while bypassing said heat exchanger ; and - at least one control element for adjusting the flow through said at least one exhaust gas-side bypass , characterized in that said exhaust gas-side bypass is integrated into said recuperator ; and said recuperator comprises an inner shell and an outer shell enclosing said inner shell, wherein an inlet side of said inner shell is connected to said second inlet of said recuperator and an outlet side of said outer shell is connected to said second outlet of said recuperator , and wherein said exhaust gas-side bypass connects the interior of said inner shell in an axial direction to the interior of said outer shell . - a gas turbine device comprising a combustor system , a turbine driven by an exhaust gas stream of said combustor system, and a compressor for supplying said combustor system with a compressed oxidant stream ; - a recuperator having a heat exchanger for transferring at least a portion of the thermal power of said exhaust gas stream of said turbine to said compressed oxidant stream ; - at least one exhaust gas-side bypass connecting a second inlet of said recuperator for said exhaust gas stream to a second outlet of said recuperator for said exhaust gas stream while bypassing said heat exchanger ; and - at least one control element for adjusting the flow through said at least one exhaust gas-side bypass ,
A suction strainer provided inside a tank in which oil is stored, the suction strainer comprising: a tubular filtration section comprising a thin plate bended into a pleat shape; an upper plate that covers an entire upper end surface of the filtration section , the upper plate having an air vent hole ; and a moving member provided to be movable between a position of closing the air vent hole and a position of opening the air vent hole , characterized in that the upper plate includes a rod-shaped member provided with a stopper on an upper end portion; the air vent hole is provided around the rod-shaped member in plan view; the moving member is a plate-shaped member having a hole into which the rod-shaped member is inserted; and the moving member is movable between a lower end position where the moving member is adjacent to the upper plate to close the air vent hole and an upper end position where the moving member abuts on the stopper . a tubular filtration section comprising a thin plate bended into a pleat shape; an upper plate that covers an entire upper end surface of the filtration section , the upper plate having an air vent hole ; and a moving member provided to be movable between a position of closing the air vent hole and a position of opening the air vent hole , characterized in that the upper plate includes a rod-shaped member provided with a stopper on an upper end portion; the air vent hole is provided around the rod-shaped member in plan view; the moving member is a plate-shaped member having a hole into which the rod-shaped member is inserted; and the moving member is movable between a lower end position where the moving member is adjacent to the upper plate to close the air vent hole and an upper end position where the moving member abuts on the stopper .
A method for forming a membrane system having the form of a flat sheet or a tube, including (a) a porous membrane formed from at least one first polymer; and (b) particles of at least one second polymer different from the first polymer, wherein the porous membrane (a) has the particles (b) immobilized, wherein the at least one second polymer includes units (I) which are formed by polymerizing N-vinylcaprolactam, and the weight ratio of the particles (b) is at most 15 wt%, based on the total weight of the porous membrane (a) and the particles (b), the weight ratio of the particles (b) referring to the solid weight of the particles (b) and being determined by thermogravimetric analysis, said method comprising the steps of (i) providing a polymer solution containing the at least one first polymer; (ii) providing a coagulation bath; (iii) optionally providing a bore solution; (iv) shaping the polymer solution into a predetermined form of a flat sheet or a tube; and (v) immersing the polymer solution having the predetermined form into the coagulation bath; to coagulate the porous membrane (a) having the immobilized particles (b); wherein the coagulation bath and/or the bore solution, if provided, contains the particles (b) at least at the time of step (v). (a) a porous membrane formed from at least one first polymer; and (b) particles of at least one second polymer different from the first polymer, wherein the porous membrane (a) has the particles (b) immobilized, wherein the at least one second polymer includes units (I) which are formed by polymerizing N-vinylcaprolactam, and the weight ratio of the particles (b) is at most 15 wt%, based on the total weight of the porous membrane (a) and the particles (b), the weight ratio of the particles (b) referring to the solid weight of the particles (b) and being determined by thermogravimetric analysis, said method comprising the steps of (i) providing a polymer solution containing the at least one first polymer; (ii) providing a coagulation bath; (iii) optionally providing a bore solution; (iv) shaping the polymer solution into a predetermined form of a flat sheet or a tube; and (v) immersing the polymer solution having the predetermined form into the coagulation bath; (i) providing a polymer solution containing the at least one first polymer; (ii) providing a coagulation bath; (iii) optionally providing a bore solution; (iv) shaping the polymer solution into a predetermined form of a flat sheet or a tube; and (v) immersing the polymer solution having the predetermined form into the coagulation bath; to coagulate the porous membrane (a) having the immobilized particles (b); wherein the coagulation bath and/or the bore solution, if provided, contains the particles (b) at least at the time of step (v).