mhurhangee/patent-ind-claim-en huggingface dataset:
A furniture panel having an integrated or inserted flap fitting , which comprises a lever mechanism having multiple levers for guiding a flap of an item of furniture, wherein the flap fitting comprises a spring unit , which acts on at least one lever of the lever mechanism using settable pre-tension, and wherein the flap fitting comprises a housing , which comprises two parallel sides spaced apart from one another, wherein the flap fitting is inserted through an end-face opening of the furniture panel into a pocket in the furniture panel formed behind the opening , or wherein the flap fitting is integrated into this pocket during the production of the furniture panel, or wherein the flap fitting is laterally inserted through a pocket, which is introduced from a lateral face of the furniture panel and comprises an opening on the end face , wherein the lever mechanism retracts into an end-face opening of the flap fitting and into the end-face opening of the furniture panel in a closed position of the guided flap, wherein the pre-tension of the spring unit and/or the transmission ratio between the spring unit and the lever mechanism is settable via an adjustment element having a tool receptacle , characterized in that all joint axes of the lever mechanism are positioned between the sides of the housing in a closed state of the flap fitting , and in that the tool receptacle is accessible through the end-face opening of the furniture panel and the end-face opening of the flap fitting .
A method for determining whether a gas sample originates from biological processes or from a gas installation being tested and containing a utility gas, characterized in that an increased concentration of hydrogen in the sample as compared to that present in the utility gas is used as evidence that the sample originates from biological decay processes and not from the gas installation under test, and a hydrogen selective gas sensor is used for the evaluation of hydrogen content in the sample, wherein the gas sensor is several orders of magnitude more sensitive to hydrogen than to any of the gases present in natural gas and wherein the gas sensor does not react to a decreased oxygen content.
Motor vehicle, with an interior which is bounded by a floor structure , a roof structure and two side structures , wherein a support , preferably a freestanding support , is arranged in the interior , wherein the support has at least one seat belt mounting device for mounting a seat belt for securing a person sitting on a motor vehicle seat and is preferably designed for at least reducing roof deformation in the event of a crash of the motor vehicle in order to ensure a survival space in the interior , wherein the support is provided with at least one device for compensating for deformations arising in the driving state of the motor vehicle, characterized in that the device provides a degree of freedom of movement for the support in the longitudinal direction of the support , and the device comprises a guide bushing in which the support is mounted in a longitudinally displaceable manner.
A hypergolic two-component system for rocket engines, including a fuel and an oxidising agent that are provided in a manner separated from one another and can be reacted in a rocket engine by bringing them into contact with one another, characterised in that - the fuel is an ionic liquid comprising a thiocyanate anion and one or more cations, wherein the cation or cations are selected from one or more imidazolium ions of the general formula I, triazolium ions of the general formula II or III, and/or tetrazolium ions of the general formula IV: where R 1 is a C 1 - to C 6 -alkyl radical or a C 2 - to C 6 -alkenyl radical, where R 2 is hydrogen or a C 1 - to C 6 -alkyl radical or a C 2 - to C 6 -alkenyl radical, and where X 1 , X 2 and X 3 are each independently hydrogen, a C 1 - to C 6 -alkyl radical or a C 2 - to C 6 -alkenyl radical; and in that - the oxidising agent comprises hydrogen peroxide. - the fuel is an ionic liquid comprising a thiocyanate anion and one or more cations, wherein the cation or cations are selected from one or more imidazolium ions of the general formula I, triazolium ions of the general formula II or III, and/or tetrazolium ions of the general formula IV: where R 1 is a C 1 - to C 6 -alkyl radical or a C 2 - to C 6 -alkenyl radical, where R 2 is hydrogen or a C 1 - to C 6 -alkyl radical or a C 2 - to C 6 -alkenyl radical, and where X 1 , X 2 and X 3 are each independently hydrogen, a C 1 - to C 6 -alkyl radical or a C 2 - to C 6 -alkenyl radical; and in that - the oxidising agent comprises hydrogen peroxide.
A method for producing a radiation window foil, comprising the following steps: - providing a carrier , - producing an etch-stop layer on the carrier , - producing a mesh on the etch-stop layer, said mesh comprising openings being delimited by ribs , said mesh having a first upper side surface defined by the top of the ribs and a second lower side surface defined by the bottoms of the ribs, the mesh being supported by the carrier , with the etch stop layer on the second lower side of the mesh, wherein said etch stop layer is made of silicon nitride, - covering the mesh with a layer for carrying mechanical stress on the first side of the mesh, said layer covering the ribs and the etch-stop-layer , so that the openings in the mesh at a level closer to the second side surface of the mesh than the first side surface of the mesh are spanned, and - detaching a radiation window foil that comprises the etch stop layer , the mesh and said layer from said carrier , wherein - the step of detaching the radiation window foil from the carrier comprises etching away the carrier . - providing a carrier , - producing an etch-stop layer on the carrier , - producing a mesh on the etch-stop layer, said mesh comprising openings being delimited by ribs , said mesh having a first upper side surface defined by the top of the ribs and a second lower side surface defined by the bottoms of the ribs, the mesh being supported by the carrier , with the etch stop layer on the second lower side of the mesh, wherein said etch stop layer is made of silicon nitride, - covering the mesh with a layer for carrying mechanical stress on the first side of the mesh, said layer covering the ribs and the etch-stop-layer , so that the openings in the mesh at a level closer to the second side surface of the mesh than the first side surface of the mesh are spanned, and - detaching a radiation window foil that comprises the etch stop layer , the mesh and said layer from said carrier , - the step of detaching the radiation window foil from the carrier comprises etching away the carrier .
Transfer unit for containers as they leave a forming unit used for forming said containers , the containers having a bottom intended to form a supporting surface of the container , the transfer unit comprising: - upper guide means for guiding the containers along a predetermined path (T); - cooling means for cooling the bottom of the containers , characterized in that the cooling means are integrated into a lower guide for the containers , the lower guide having an upper face intended to be positioned, without contact, facing the bottoms of the containers , the upper face forming an end stop against toppling of the containers along the predetermined path (T). - upper guide means for guiding the containers along a predetermined path (T); - cooling means for cooling the bottom of the containers ,
A method for detecting optical fluorescence radiation irradiated by an object to be analyzed as an optical measurement signal with an intensity that corresponds to an autofluorescence of the object, wherein an optical excitation pulse is generated by a short-pulse laser and the optical measurement signal is converted into an electrical signal and electrically processed, characterized in that the electrical signal is temporally stretched in the step of electrical processing.
A low-carbon environmentally-friendly foamer composition, characterized in that the composition comprises the following ingredients in mass percentage: 1-chloro-3,3,3-trifluoropropene 60-98.99% 1,1,1,2,3-pentafluoropropane 1-39.9% 1,2,2,3-tetrafluoropropane 0.01-1%.
A sous vide cooker comprising: a housing extending along an longitudinal axis from an upper housing end to a lower housing end and comprising at least one display ; a bulkhead having an upper bulkhead end extending along the longitudinal axis into the lower housing end, and a lower bulkhead end extending along the longitudinal axis below the housing, the bulkhead and housing forming a first cavity therebetween; a heat sink comprising a metal material and having an upper heat sink end abutting the bulkhead and a lower heat sink end extending along the longitudinal axis below the bulkhead, the heat sink and bulkhead forming a second cavity therebetween; a skirt attached at an upper skirt end to the bulkhead and extending to a lower skirt end located below the lower heat sink end to form a third cavity between the skirt and the heat sink, the skirt surrounding the heat sink in a direction perpendicular to the longitudinal axis, and having one or more inlet openings and one or more outlet openings located below the lower heat sink end; a TRIAC physically attached in conductive thermal communication to the heat sink in the second cavity; an impeller located in the third cavity; a drive shaft extending through at least the heat sink and into the third cavity and operatively connected to the impeller; a motor operatively connected to the drive shaft; and a heating element located within the third cavity. a housing extending along an longitudinal axis from an upper housing end to a lower housing end and comprising at least one display ; a bulkhead having an upper bulkhead end extending along the longitudinal axis into the lower housing end, and a lower bulkhead end extending along the longitudinal axis below the housing, the bulkhead and housing forming a first cavity therebetween; a heat sink comprising a metal material and having an upper heat sink end abutting the bulkhead and a lower heat sink end extending along the longitudinal axis below the bulkhead, the heat sink and bulkhead forming a second cavity therebetween; a skirt attached at an upper skirt end to the bulkhead and extending to a lower skirt end located below the lower heat sink end to form a third cavity between the skirt and the heat sink, the skirt surrounding the heat sink in a direction perpendicular to the longitudinal axis, and having one or more inlet openings and one or more outlet openings located below the lower heat sink end; a TRIAC physically attached in conductive thermal communication to the heat sink in the second cavity; an impeller located in the third cavity; a drive shaft extending through at least the heat sink and into the third cavity and operatively connected to the impeller; a motor operatively connected to the drive shaft; and a heating element located within the third cavity.
A manifold of a flowmeter , comprising: a body having a first face and an opposing second face ; a first orifice defined by the body , wherein the first orifice projects into the body from the first face ; a second orifice defined by the body , wherein the second orifice projects into the body from the second face , and wherein the first and second orifices meet to define a fluid passage traversing through the body , and wherein the second orifice is configured to fluidly connect to at least two flow tubes of the flowmeter ; wherein the second orifice is bifurcated into a first minor orifice and a second minor orifice , wherein the first minor orifice and second minor orifice are each adapted to fluidly communicate with a first and second flow tube of the at least two flow tubes , respectively; and characterized by two bosses that project from the second face being configured to provide a space for the at least two flow tubes of the flowmeter and/or a brace bar of the flowmeter and/or pickoffs and/or case portions to index; wherein the two bosses are oriented such that a long axis of each of the two bosses is substantially perpendicular to an axis that bisects both the first minor orifice and the second minor orifice . a body having a first face and an opposing second face ; a first orifice defined by the body , wherein the first orifice projects into the body from the first face ; a second orifice defined by the body , wherein the second orifice projects into the body from the second face , and wherein the first and second orifices meet to define a fluid passage traversing through the body , and wherein the second orifice is configured to fluidly connect to at least two flow tubes of the flowmeter ; wherein the second orifice is bifurcated into a first minor orifice and a second minor orifice , wherein the first minor orifice and second minor orifice are each adapted to fluidly communicate with a first and second flow tube of the at least two flow tubes , respectively; and
A drug delivery system to deliver a first medicament and at least one second medicament operable through a single dispense interface, comprising, a. a primary reservoir of the first medicament containing at least one first drug agent; b. a dose button operably connected to the primary reservoir ; c. a single dispense interface configured for fluid communication with the primary reservoir ; and d. a secondary reservoir of the second medicament containing at least one second drug agent different from the at least one first drug agent configured for fluid communication to the single dispense interface ; wherein the drug delivery system is configured such that a single activation of the dose button causes the first medicament from the primary reservoir and a non-user settable dose of the second medicament to be expelled through the single dispense interface , wherein the single operation of the dose button causes the first medicament from the primary reservoir to be expelled through the single dispense interface after a therapeutic dose of the non-user settable dose of second medicament has been expelled through the single dispense interface , the drug delivery system being characterized in that the secondary reservoir and the single dispense interface are contained in a single module that is disposable and replaceable with a replacement module containing a new secondary reservoir of medicament and a new single dispense interface . a. a primary reservoir of the first medicament containing at least one first drug agent; b. a dose button operably connected to the primary reservoir ; c. a single dispense interface configured for fluid communication with the primary reservoir ; and d. a secondary reservoir of the second medicament containing at least one second drug agent different from the at least one first drug agent configured for fluid communication to the single dispense interface ;
A yarn feeder , comprising - a drum supporting a yarn (Y) wound upon itself, which is adapted to be unwound upon request from a downstream textile machine, and - a passive weft braking device , which is arranged so as to apply a predetermined uncontrolled braking action on the yarn (Y) unwinding from the drum , - an active yarn braking device , which is arranged downstream of said passive weft braking device , - a tension sensor , which is arranged downstream of said active weft braking device in order to measure the tension of the yarn (Y) that unwinds from the drum and to generate a corresponding tension signal (T), - a control unit (CU), programmed to drive by feedback said active weft braking device on the basis of said tension signal (T), characterized in that said active weft braking device comprises at least one first weft braking lamina , which is pushed against an abutment by motor means which are functionally connected to said control unit (CU), with the interposition of irreversible transmission means provided with auxiliary manual adjustment means , the yarn (Y) being adapted to slide between said first weft braking lamina and said abutment . - a drum supporting a yarn (Y) wound upon itself, which is adapted to be unwound upon request from a downstream textile machine, and - a passive weft braking device , which is arranged so as to apply a predetermined uncontrolled braking action on the yarn (Y) unwinding from the drum , - an active yarn braking device , which is arranged downstream of said passive weft braking device , - a tension sensor , which is arranged downstream of said active weft braking device in order to measure the tension of the yarn (Y) that unwinds from the drum and to generate a corresponding tension signal (T), - a control unit (CU), programmed to drive by feedback said active weft braking device on the basis of said tension signal (T),
A space launcher comprising a launcher body , an engine comprising a combustion chamber opening out onto a nozzle having a longitudinal axis (Z-Z), the engine being fixed to the launcher body by means of a grimbal , the nozzle being provided with a plate extending radially around the nozzle or the combustion chamber and isolating a internal volume of the spacecraft from an external medium, the plate delimiting an inner segment of the engine and an outer segment of the engine , the inner segment of the engine comprising all or part of the combustion chamber and being disposed in the launcher body , isolated from the external medium by the plate , the plate having an inner face and an outer face positioned respectively in the internal volume and in the external medium, characterized in that it further comprises a plurality of cables each connected to the inner face of the plate on the one hand, and to the inner segment of the engine on the other hand. the plate delimiting an inner segment of the engine and an outer segment of the engine , the inner segment of the engine comprising all or part of the combustion chamber and being disposed in the launcher body , isolated from the external medium by the plate , the plate having an inner face and an outer face positioned respectively in the internal volume and in the external medium, characterized in that it further comprises a plurality of cables each connected to the inner face of the plate on the one hand, and to the inner segment of the engine on the other hand.
A system comprising: a magnetic resonance (MR) scanner defining an examination volume ; and at least one processor programmed to: control the MR scanner to apply imaging sequences to a subject arranged in the examination volume ; in response to the imaging sequences, acquire a series of MR data sets of the subject at a plurality of mutually different echo times (TEs); reconstruct an MR phase image from each MR data set, thereby generating a series of MR phase images; phase unwrap the series of MR phase images; map the intensity of the series of MR phase images as a function of time, thereby producing a series of phase accumulation maps; and to use the change in phase over time from the series of phase accumulation maps to identify the tissue and/or material type of each pixel or voxel of interest within a volume of the subject . a magnetic resonance (MR) scanner defining an examination volume ; and at least one processor programmed to: control the MR scanner to apply imaging sequences to a subject arranged in the examination volume ; in response to the imaging sequences, acquire a series of MR data sets of the subject at a plurality of mutually different echo times (TEs); reconstruct an MR phase image from each MR data set, thereby generating a series of MR phase images; phase unwrap the series of MR phase images; map the intensity of the series of MR phase images as a function of time, thereby producing a series of phase accumulation maps; and to use the change in phase over time from the series of phase accumulation maps to identify the tissue and/or material type of each pixel or voxel of interest within a volume of the subject . control the MR scanner to apply imaging sequences to a subject arranged in the examination volume ; in response to the imaging sequences, acquire a series of MR data sets of the subject at a plurality of mutually different echo times (TEs); reconstruct an MR phase image from each MR data set, thereby generating a series of MR phase images; phase unwrap the series of MR phase images; map the intensity of the series of MR phase images as a function of time, thereby producing a series of phase accumulation maps; and to use the change in phase over time from the series of phase accumulation maps to identify the tissue and/or material type of each pixel or voxel of interest within a volume of the subject .
A gas turbine engine component comprising: an airfoil with a suction side and pressure side , and extending from a leading edge to a trailing edge ; and a plurality of cooling holes adjacent the leading edge , with said cooling holes having a non-circular shape, with a longer dimension (d 1 ) and a shorter dimension (d 2 ), and said airfoil defining a radial direction (R) from a radially outer end to a radially inner end, and radially outer of said cooling holes spaced toward said radially outer end having said longer dimension (d 1 ) extending closer to parallel to said radial direction (R), and radially inner cooling holes closer to said radially inner end having said longer dimension (d 1 ) extending to be closer to perpendicular relative to said radial direction (R) compared to said radially outer cooling holes ; characterised in that : there is a transition zone intermediate said radially inner and radially outer cooling holes , with said transition zone including a cooling hole having a longer dimension (d 1 ) that is non-perpendicular and non-parallel to said radial direction (R); said transition zone includes a plurality of cooling holes , which have said longer dimension (d 1 ) defining an angle (A, B) between 0 and 90° relative to said radial direction (R); and the angle (A, B) of said plurality of cooling holes in said transition zone increases as said cooling holes are radially closer to said radially inner most cooling hole . an airfoil with a suction side and pressure side , and extending from a leading edge to a trailing edge ; and a plurality of cooling holes adjacent the leading edge , with said cooling holes having a non-circular shape, with a longer dimension (d 1 ) and a shorter dimension (d 2 ), and said airfoil defining a radial direction (R) from a radially outer end to a radially inner end, and radially outer of said cooling holes spaced toward said radially outer end having said longer dimension (d 1 ) extending closer to parallel to said radial direction (R), and radially inner cooling holes closer to said radially inner end having said longer dimension (d 1 ) extending to be closer to perpendicular relative to said radial direction (R) compared to said radially outer cooling holes ; there is a transition zone intermediate said radially inner and radially outer cooling holes , with said transition zone including a cooling hole having a longer dimension (d 1 ) that is non-perpendicular and non-parallel to said radial direction (R); said transition zone includes a plurality of cooling holes , which have said longer dimension (d 1 ) defining an angle (A, B) between 0 and 90° relative to said radial direction (R); and the angle (A, B) of said plurality of cooling holes in said transition zone increases as said cooling holes are radially closer to said radially inner most cooling hole .