mhurhangee/ep-ind-claims huggingface dataset:
An airfoil for a gas turbine engine, the airfoil comprising: an airfoil body extending between a platform and a tip, the airfoil body having a leading edge, a trailing edge, a pressure side, and a suction side; a serpentine cavity formed within the airfoil body and having an up-pass serpentine cavity, a down-pass serpentine cavity, and a trailing edge cavity; and a dead-end tip flag cavity extending in a direction between the leading edge and the trailing edge, the dead-end tip flag cavity arranged between the serpentine cavity and the tip, wherein the dead-end tip flag cavity ends at a dead-end wall located at a position between the leading edge and the trailing edge of the airfoil body, wherein the dead-end tip flag cavity is defined by an outer wall, an inner wall, and the dead-end wall, with the outer wall and the inner wall extending in a direction between the leading edge and the trailing edge and the dead-end wall extending in a direction between the platform and the tip, characterized by a squealer pocket arranged at the tip of the airfoil body, wherein the outer wall of the dead-end tip flag cavity forms a pocket surface of the squealer pocket, and at least one tip cooling hole formed within the outer wall and configured to enable fluid connection between the dead-end tip flag cavity and the squealer pocket. an airfoil body extending between a platform and a tip, the airfoil body having a leading edge, a trailing edge, a pressure side, and a suction side; a serpentine cavity formed within the airfoil body and having an up-pass serpentine cavity, a down-pass serpentine cavity, and a trailing edge cavity; and a dead-end tip flag cavity extending in a direction between the leading edge and the trailing edge, the dead-end tip flag cavity arranged between the serpentine cavity and the tip, wherein the dead-end tip flag cavity ends at a dead-end wall located at a position between the leading edge and the trailing edge of the airfoil body, wherein the dead-end tip flag cavity is defined by an outer wall, an inner wall, and the dead-end wall, with the outer wall and the inner wall extending in a direction between the leading edge and the trailing edge and the dead-end wall extending in a direction between the platform and the tip, characterized by a squealer pocket arranged at the tip of the airfoil body, wherein the outer wall of the dead-end tip flag cavity forms a pocket surface of the squealer pocket, and at least one tip cooling hole formed within the outer wall and configured to enable fluid connection between the dead-end tip flag cavity and the squealer pocket.
A method for displaying images used prior to an administration of radiation treatment to a patient, the method comprising the steps of: (a) obtaining a 3D image of one or more internal anatomical features of the patient, and generating a beam's-eye view image, i.e. a projection of the 3D image from the viewpoint of a treatment beam; (b) obtaining a digitized representation of one or more external features of the patient; (c) annotating the beam's-eye view image with the representation of the one or more external features, the annotated beam's-eye view image being based on, or at least in part on, one or more treatment parameters relating to the administration of radiation treatment to the patient; and (d) displaying the annotated beam's-eye view image; the method further comprising the step of: (e) in response to the displayed annotated beam's-eye view image iteratively (i) adjusting the one or more treatment parameters and (ii) displaying an updated annotated beam's-eye view image, wherein the updated annotated beam's-eye view image is based at least in part on the parameter adjustments thereby providing a visual indication of effects of the parameter adjustments on the delivery of radiation therapy with respect to both internal anatomical and external features of the patient on one image. (a) obtaining a 3D image of one or more internal anatomical features of the patient, and generating a beam's-eye view image, i.e. a projection of the 3D image from the viewpoint of a treatment beam; (b) obtaining a digitized representation of one or more external features of the patient; (c) annotating the beam's-eye view image with the representation of the one or more external features, the annotated beam's-eye view image being based on, or at least in part on, one or more treatment parameters relating to the administration of radiation treatment to the patient; and (d) displaying the annotated beam's-eye view image; (e) in response to the displayed annotated beam's-eye view image iteratively (i) adjusting the one or more treatment parameters and (ii) displaying an updated annotated beam's-eye view image, wherein the updated annotated beam's-eye view image is based at least in part on the parameter adjustments thereby providing a visual indication of effects of the parameter adjustments on the delivery of radiation therapy with respect to both internal anatomical and external features of the patient on one image.
Vehicle seat, wherein the vehicle seat comprises at least one recess and one movable carrier platform, wherein - the carrier platform can be moved out of a park position into a use position, wherein - the carrier platform is held in the recess when in the park position, - the carrier platform comprises a mechanical connector, wherein - in the use position, on the carrier platform, a carrier module comprising a mechanical connection device can be connected to the connector of the carrier platform and can be removed again, wherein - in the park position, carrier modules cannot be connected, characterised in that - the carrier module can be connected to an electric power supply circuit via the connection device and the connector of the carrier platform, wherein - control signals can be transmitted to the carrier module as an alternative to, in addition to or alternately with the connection to the electric power supply circuit. - the carrier platform can be moved out of a park position into a use position, wherein - the carrier platform is held in the recess when in the park position, - the carrier platform comprises a mechanical connector, wherein - in the use position, on the carrier platform, a carrier module comprising a mechanical connection device can be connected to the connector of the carrier platform and can be removed again, wherein - in the park position, carrier modules cannot be connected, characterised in that - the carrier module can be connected to an electric power supply circuit via the connection device and the connector of the carrier platform, wherein - control signals can be transmitted to the carrier module as an alternative to, in addition to or alternately with the connection to the electric power supply circuit.
A system for the image-based display of information in the form of a display of a telephone, wherein a) the system comprises an image output device comprising at least one first section (S1_1, S1_2) and at least one second section (S2_1, S2_2), wherein b) the first section is configured so that the display of the information is optimized for high-quality imaging, and the second section (S2_1, S2_2) is configured so that it is optimized for imaging of reduced quality, and c) the first section (S1_1, S1_2) is configured so that it can be actively switched on and off by a user in accordance with an energy saving scheme and on a supplementary basis, characterized in that d) the energy saving scheme is configured to achieve a switching off of parts of the first section (S1_1, S1_2) and e) the switching off of parts of the first section (S1_1, S1_2) occurs when the displayed content of the first section (S1_1, S1_2) has not changed over a period of time, wherein the second section (S2_1, S2_2) has no backlighting and is always actively operated. a) the system comprises an image output device comprising at least one first section (S1_1, S1_2) and at least one second section (S2_1, S2_2), wherein b) the first section is configured so that the display of the information is optimized for high-quality imaging, and the second section (S2_1, S2_2) is configured so that it is optimized for imaging of reduced quality, and c) the first section (S1_1, S1_2) is configured so that it can be actively switched on and off by a user in accordance with an energy saving scheme and on a supplementary basis, characterized in that d) the energy saving scheme is configured to achieve a switching off of parts of the first section (S1_1, S1_2) and e) the switching off of parts of the first section (S1_1, S1_2) occurs when the displayed content of the first section (S1_1, S1_2) has not changed over a period of time,
A device for converting wind energy into energy of another type, the device comprising: - a base, - a hollow mast, mounted on the base, extending along a substantially vertical axis, - at least one module with a general shape of revolution around an axis, positioned coaxially around the mast, and movable in rotation around that mast, said module comprising: ∘ at least one flap extending between an end connected by a pivot link, and a free end, said flap being movable around the pivot link between a retracted position and a deployed position, ∘ means for moving the flap between its deployed and retracted positions, based on the angular position of that flap around the mast, said movement means being able to be deactivated, - a shaft, positioned in the hollow mast coaxially to the module, connected in rotation with that module around the axis, and cooperating with a converter converting the mechanical rotational energy of the shaft into another type of energy. - a base, - a hollow mast, mounted on the base, extending along a substantially vertical axis, - at least one module with a general shape of revolution around an axis, positioned coaxially around the mast, and movable in rotation around that mast, said module comprising: ∘ at least one flap extending between an end connected by a pivot link, and a free end, said flap being movable around the pivot link between a retracted position and a deployed position, ∘ means for moving the flap between its deployed and retracted positions, based on the angular position of that flap around the mast, said movement means being able to be deactivated, ∘ at least one flap extending between an end connected by a pivot link, and a free end, said flap being movable around the pivot link between a retracted position and a deployed position, ∘ means for moving the flap between its deployed and retracted positions, based on the angular position of that flap around the mast, said movement means being able to be deactivated, - a shaft, positioned in the hollow mast coaxially to the module, connected in rotation with that module around the axis, and cooperating with a converter converting the mechanical rotational energy of the shaft into another type of energy.
Angle measuring device (1, 20) as a rotary encoder and/or position encoder for determining an absolute angle of rotation, comprising: one field element which generates a magnetic field and is rotatably mounted about a first axis of rotation, whereby the field element is rotatably mounted about a second axis of rotation, which is offset with respect to the first axis of rotation, so that the field element rotates in a plane of rotation about the second axis of rotation, with a sensor array with at least two sensors (10, 11, 12, 13, 14, 15) positioned offset with respect to the plane of rotation, whereby the sensor array is designed to determine the position of the field element in the plane of rotation and its orientation with respect to its north-south pole orientation by measuring the magnetic field generated by the field element as a function of the position of the field element in the plane of rotation and/or as a function of the north-south pole orientation of the field element about the first axis of rotation, whereby the angle measuring device comprises a housing and a gear unit, and whereby the field element is rotatably mounted about the first and second axis of rotation (6, 7) relative to the housing through the gear unit. one field element which generates a magnetic field and is rotatably mounted about a first axis of rotation, whereby the field element is rotatably mounted about a second axis of rotation, which is offset with respect to the first axis of rotation, so that the field element rotates in a plane of rotation about the second axis of rotation, with a sensor array with at least two sensors (10, 11, 12, 13, 14, 15) positioned offset with respect to the plane of rotation, whereby the sensor array is designed to determine the position of the field element in the plane of rotation and its orientation with respect to its north-south pole orientation by measuring the magnetic field generated by the field element as a function of the position of the field element in the plane of rotation and/or as a function of the north-south pole orientation of the field element about the first axis of rotation, whereby the angle measuring device comprises a housing and a gear unit, and whereby the field element is rotatably mounted about the first and second axis of rotation (6, 7) relative to the housing through the gear unit.
Method for configuring a resource for the use thereof by a first virtual runtime environment of a hardware platform, a management device for virtual runtime environments (VM1, VM2, CVM) being provided, characterized in that a second virtual runtime environment with a configuration device is provided, and in that - in a first step the resource is assigned to the second runtime environment by the management device, - in a second step the resource is configured by the configuration device, and - in a third step the configured resource is assigned to the first runtime environment. - in a first step the resource is assigned to the second runtime environment by the management device, - in a second step the resource is configured by the configuration device, and - in a third step the configured resource is assigned to the first runtime environment.
A method for use in surveying a subsurface region beneath a body of water by detecting secondary S and primary P waves propagating through the subsurface region, the method characterized by: deploying a sensor system onto the seabed, the sensor system comprising a first sensor configuration in mechanical contact with the seabed and a second sensor configuration attached to the first sensor configuration and floating in the water above the seabed; using the first sensor configuration to detect mixed S and P waves on or in the subsurface region; and using the second sensor configuration to detect P waves in the water; applying scaling and/or conditioning to the detected P waves; and using the scaled and/or conditioned P waves to compensate the detected mixed S and P waves, and thereby attenuate the effects of P waves in the mixed S and P waves. deploying a sensor system onto the seabed, the sensor system comprising a first sensor configuration in mechanical contact with the seabed and a second sensor configuration attached to the first sensor configuration and floating in the water above the seabed; using the first sensor configuration to detect mixed S and P waves on or in the subsurface region; and using the second sensor configuration to detect P waves in the water; applying scaling and/or conditioning to the detected P waves; and using the scaled and/or conditioned P waves to compensate the detected mixed S and P waves, and thereby attenuate the effects of P waves in the mixed S and P waves.
LED semiconductor component (LEDA) comprising - an n-doped substrate layer (N-SUB), - a first, n-doped casing layer (N-MAN), wherein the casing layer (N-MAN) is arranged on the substrate layer and an active layer, wherein the active layer comprises a light-emitting layer and is arranged on the first casing layer (N-MAN), - a second, p-doped casing layer (P-MAN), wherein the second casing layer (P-MAN) is arranged on the active layer, - a p-doped current expansion layer (P-VERT), wherein the current expansion layer (P-VERT) is arranged on the second casing layer (P-MAN), and - a p-doped contact layer (P-KON), wherein the p-doped contact layer (P-KON) is arranged on the current expansion layer (P-VERT), wherein the p-doped contact layer (P-KON) consists of a layer with aluminium content and has carbon as doping substance, and wherein the concentration of aluminium is higher in the contact layer (P-KON) than in the current expansion layer (P-VERT) and the casing layers (N-MAN, P-MAN), which are arranged on the substrate layer, and the current expansion layer (P-VERT) each comprise an AlGaAs compound. - an n-doped substrate layer (N-SUB), - a first, n-doped casing layer (N-MAN), wherein the casing layer (N-MAN) is arranged on the substrate layer and an active layer, wherein the active layer comprises a light-emitting layer and is arranged on the first casing layer (N-MAN), - a second, p-doped casing layer (P-MAN), wherein the second casing layer (P-MAN) is arranged on the active layer, - a p-doped current expansion layer (P-VERT), wherein the current expansion layer (P-VERT) is arranged on the second casing layer (P-MAN), and - a p-doped contact layer (P-KON), wherein the p-doped contact layer (P-KON) is arranged on the current expansion layer (P-VERT), wherein the p-doped contact layer (P-KON) consists of a layer with aluminium content and has carbon as doping substance, and wherein the concentration of aluminium is higher in the contact layer (P-KON) than in the current expansion layer (P-VERT) and the casing layers (N-MAN, P-MAN), which are arranged on the substrate layer, and the current expansion layer (P-VERT) each comprise an AlGaAs compound.
An apparatus configured to mount a windshield to a vehicle, the apparatus comprising: a foam configured to be positioned between the windshield and a frame of the vehicle along at least a portion of an interior perimeter of the windshield, characterized by one or more rigid components (1104A, 1104B) configured to move towards a location of an impact to compress the foam when the windshield is deformed by the impact, wherein the one or more rigid components are positioned at least partially within the foam, and an attachment component configured to attach the foam to the frame of the vehicle. a foam configured to be positioned between the windshield and a frame of the vehicle along at least a portion of an interior perimeter of the windshield, characterized by one or more rigid components (1104A, 1104B) configured to move towards a location of an impact to compress the foam when the windshield is deformed by the impact, wherein the one or more rigid components are positioned at least partially within the foam, and an attachment component configured to attach the foam to the frame of the vehicle.
Source for generating ionizing radiation, comprising: • a vacuum chamber (12; 153); • a cathode that is able to emit an electron beam into the vacuum chamber (12; 153); • an anode (16; 76; 154; 174) that receives the electron beam and that comprises a target (20; 21) that is able to generate ionizing radiation from the energy received from the electron beam; • an electrode (24; 166) that is placed in the vicinity of the cathode and forming a wehnelt, characterized in that the electrode is formed from a conductive surface adhering to a concave face (26; 168) of a dielectric, the outside of the concavity of the face (26; 168) being oriented toward the anode (16; 76; 154; 174). • a vacuum chamber (12; 153); • a cathode that is able to emit an electron beam into the vacuum chamber (12; 153); • an anode (16; 76; 154; 174) that receives the electron beam and that comprises a target (20; 21) that is able to generate ionizing radiation from the energy received from the electron beam; • an electrode (24; 166) that is placed in the vicinity of the cathode and forming a wehnelt,
A lithium polymeric membrane comprising a fluorinated and semi-crystalline polymeric matrix, a lithium salt and a non-ionic surfactant as a plasticizer, wherein the fluorinated and semi-crystalline polymeric matrix is poly(vinyliden fluoride-co-hexafluoropropylene), the lithium salt is lithium hexafluorophosphate, and characterised in that the non-ionic surfactant is polyethylene glycol tert-octylphenyl ether.
Nanocomposite paints with micro slime layer control properties in the form of fouling release coatings, which are two-part epoxy coatings where the first part is the epoxy resin (component A) and the second part is the curing agent (hardener) which contains aromatic- and/or alkyl- functionalized polyamines (component B) Where the hardener is modified with - hydrophobic nanoparticles based on hyperbranched dendritic polymers with symmetric or asymmetric architecture or - inorganic nanoparticles decorated with hydrophobic moieties, characterized in that the hydrophobic polymeric nanoparticles used to modify component B, comprise functionalized dendritic polymers with symmetrical or asymmetrical architecture, derived from commercially available dendritic polymers, such as: • Hyperbranched polyethylenimine with molecular weight 400-750.000 Da, • Diaminobutane propyleneimine dendrimers with molecular weight 200-7.000 Da, • Poly(amido amine) (PAMAM) dendrimers with molecular weight 200-150.000 Da, • Hyperbranched dendritic polyglycerols with molecular weight 200-100.000 Da • Hyperbranched dendritic polyesters with molecular weight 200-200.000 Da • other dendritic polymers exhibiting similar characteristics, which are functionalized with hydrophobic groups such as alkyl chains with 8 to 22 carbon atoms or fluoroalkyl chains with 11 to 45 fluoro atoms or other hydrophobic groups, at 40-100% molecular coverage. wherein such nanocomposite paints are used as fouling release coating applied to objects submerged in water such as the vessel hulls, sea platforms, bridge, underwater structures (e.g. propeller, aquaculture chambers) etc - hydrophobic nanoparticles based on hyperbranched dendritic polymers with symmetric or asymmetric architecture or - inorganic nanoparticles decorated with hydrophobic moieties, characterized in that the hydrophobic polymeric nanoparticles used to modify component B, comprise functionalized dendritic polymers with symmetrical or asymmetrical architecture, derived from commercially available dendritic polymers, such as: • Hyperbranched polyethylenimine with molecular weight 400-750.000 Da, • Diaminobutane propyleneimine dendrimers with molecular weight 200-7.000 Da, • Poly(amido amine) (PAMAM) dendrimers with molecular weight 200-150.000 Da, • Hyperbranched dendritic polyglycerols with molecular weight 200-100.000 Da • Hyperbranched dendritic polyesters with molecular weight 200-200.000 Da • other dendritic polymers exhibiting similar characteristics, • Hyperbranched polyethylenimine with molecular weight 400-750.000 Da, • Diaminobutane propyleneimine dendrimers with molecular weight 200-7.000 Da, • Poly(amido amine) (PAMAM) dendrimers with molecular weight 200-150.000 Da, • Hyperbranched dendritic polyglycerols with molecular weight 200-100.000 Da • Hyperbranched dendritic polyesters with molecular weight 200-200.000 Da • other dendritic polymers exhibiting similar characteristics,
Propylene polymer grafted by at least one grafting monomer chosen from unsaturated carboxylic acids or their functional derivatives, unsaturated dicarboxylic acids having 4 to 10 carbon atoms and their functional derivatives, C 1 -C 8 alkyl esters of unsaturated carboxylic acids or glycidyl ester derivatives of unsaturated carboxylic acids, or metal salts of unsaturated carboxylic acids, characterized in that it comprises an amount of carbon resulting from renewable raw materials (resulting from living natural resource - animals or plants - which are a mixture of 3 isotopes: 12 C representing approximately 98.892%, 13 C approximately 1.108% and 14 C as traces: 1.2 x 10 -10 %) of greater than 20%, preferably of greater than 50% by weight relative to the total weight of carbon of the propylene polymer, this amount of carbon resulting from renewable raw materials being measured according to the standard ASTM D 6866-06.