mhurhangee/ep-ind-claims huggingface dataset:
Bearing unit, having - an outer guide sleeve which has an opening, and - an inner receiving sleeve which is arranged rotatably within the opening of the outer guide sleeve and has a recess for receiving a fastening means, - a rotational axis of the inner receiving sleeve in the outer guide sleeve and a centre axis of the recess in the inner receiving sleeve for receiving the fastening means being spaced apart from one another by an eccentricity, - an apparatus for non-positive and/or positively locking positional securing of a set position of the receiving sleeve relative to the guide sleeve being provided between the outer guide sleeve and the inner receiving sleeve, the apparatus for non-positive and/or positively locking positional securing being formed from an apparatus for latching the inner receiving sleeve in relation to the outer guide sleeve, the apparatus for latching being formed by way of a toothing system (8, 9) of the contact face (6, 7) of the inner receiving sleeve and/or outer guide sleeve, characterized in that the toothing system (8, 9) is formed from an elastic material and deforms elastically during the rotation of the inner receiving sleeve in relation to the outer guide sleeve, a required torque for overcoming the tooth engagement preferably lying considerably above a frictional moment between the inner receiving sleeve and the outer guide sleeve during operation, the inner receiving sleeve and/or the outer guide sleeve being formed at least partially, preferably completely from an elastic plastic with a high strength. - an outer guide sleeve which has an opening, and - an inner receiving sleeve which is arranged rotatably within the opening of the outer guide sleeve and has a recess for receiving a fastening means, - a rotational axis of the inner receiving sleeve in the outer guide sleeve and a centre axis of the recess in the inner receiving sleeve for receiving the fastening means being spaced apart from one another by an eccentricity, - an apparatus for non-positive and/or positively locking positional securing of a set position of the receiving sleeve relative to the guide sleeve being provided between the outer guide sleeve and the inner receiving sleeve,
Reinforced product comprising one or more reinforcing threads, the said thread or threads being covered individually or collectively with a sheath comprising a sheathing composition comprising one or more thermoplastic block copolymers comprising at least one polyamide block, at least one polyolefin block, at least one alkylene block, and exhibiting a melt viscosity ranging from 300 Pa.s to 20 000 Pa.s, in particular from 300 to 15 000 Pa.s, measured at 230°C by oscillatory rheology, the sheathed thread or threads being themselves embedded in a rubber composition.
An applicator, comprising: a nozzle including an elongated nozzle main body to which gas and a plurality of kinds of liquids may be supplied and a nozzle head provided at a distal end of the nozzle main body and configured to jet mixed solution of the gas and the plurality of kinds of liquids supplied to the nozzle main body; and a sheath in which the nozzle main body is fitted for relative movement along a longitudinal axial direction of the nozzle main body; the applicator being adapted to be inserted into a living body to apply the mixed solution to a region in the living body; characterized in that the nozzle main body has at least two radially deformed crushed portions (28a, 28b) being provided along the longitudinal axial direction contiguously to each other at a proximal end portion of the nozzle main body; wherein the radial deformation directions of the crushed portions are different from each other; and wherein the at least two crushed portions (28a, 28b) individually are in diametrical contact with an inner surface of the sheath. a nozzle including an elongated nozzle main body to which gas and a plurality of kinds of liquids may be supplied and a nozzle head provided at a distal end of the nozzle main body and configured to jet mixed solution of the gas and the plurality of kinds of liquids supplied to the nozzle main body; and a sheath in which the nozzle main body is fitted for relative movement along a longitudinal axial direction of the nozzle main body; the applicator being adapted to be inserted into a living body to apply the mixed solution to a region in the living body; characterized in that the nozzle main body has at least two radially deformed crushed portions (28a, 28b) being provided along the longitudinal axial direction contiguously to each other at a proximal end portion of the nozzle main body; wherein the radial deformation directions of the crushed portions are different from each other; and wherein the at least two crushed portions (28a, 28b) individually are in diametrical contact with an inner surface of the sheath.
An image processing method comprising: determining image gradient indications for at least two images; determining filter costs for image regions based on the determined image gradient indications for the images; and processing data relating to the images including applying a filtering operation using the determined filter costs for the image regions, so that the processing is performed for image regions in dependence upon image gradients of the images; characterised by: wherein at least one initial blending mask indicates initial blending factors for use in combining the images; and wherein said processing data relating to the images comprises smoothing transitions in the at least one initial blending mask at smoothing rates in accordance with the filter costs for the image regions at the respective transitions to form at least one smoothed blending mask for use in blending the images to form a blended image. determining image gradient indications for at least two images; determining filter costs for image regions based on the determined image gradient indications for the images; and processing data relating to the images including applying a filtering operation using the determined filter costs for the image regions, so that the processing is performed for image regions in dependence upon image gradients of the images; characterised by: wherein at least one initial blending mask indicates initial blending factors for use in combining the images; and wherein said processing data relating to the images comprises smoothing transitions in the at least one initial blending mask at smoothing rates in accordance with the filter costs for the image regions at the respective transitions to form at least one smoothed blending mask for use in blending the images to form a blended image. wherein at least one initial blending mask indicates initial blending factors for use in combining the images; and wherein said processing data relating to the images comprises smoothing transitions in the at least one initial blending mask at smoothing rates in accordance with the filter costs for the image regions at the respective transitions to form at least one smoothed blending mask for use in blending the images to form a blended image.
Method for detecting uncontrolled combustion processes in an internal combustion engine, which combustion processes occur independently of the ignition by means of a spark plug, wherein the pressure oscillations in the combustion chamber which are triggered by the combustion processes are detected and evaluated, and in order to determine an uncontrolled combustion process before the ignition by means of the spark plug and/or before the normal start of combustion the rotational speed (n) of a crankshaft of the internal combustion engine which is influenced by the pressure oscillations is evaluated for a given ignition time, characterized in that a gas torque profile T(φ) is derived from the rotational speed and evaluated.
Anti-theft module for a battery-operated electric machine tool, comprising at least one first data interface for transmitting data, in particular position data, to an external device, and comprising a position determination unit for determining a geographical position of the anti-theft module, wherein the anti-theft module is installable as an adapter between a rechargeable battery interface of the electric machine tool and a replaceable battery and comprises at least one locking or latching element, which engages with a corresponding mating latching element of the rechargeable battery interface or the replaceable battery, when the anti-theft module is connected to the rechargeable battery interface of the electric machine tool or the replaceable battery, wherein releasing the at least one locking or latching element takes place via the external device.
An air vehicle comprising: a fuselage; a pair of control surfaces movable relative to the fuselage; an actuator having a movable actuator shaft (42, 44); and a coupler that selectively mechanically couples the actuator shaft (42, 44) to the control surfaces, wherein the coupler is in a disengaged condition when the actuator shaft (42, 44) and the control surfaces are not coupled by the coupler, and wherein the coupler is in an engaged condition when the actuator shaft and the control surfaces are coupled by the coupler; wherein the coupler is able to shift between the disengaged condition in which the control surfaces move independently of the actuator shaft such that movement of the actuator shaft (42, 44) does not cause movement of the control surfaces, and the engaged condition in which the actuator shaft (42, 44) and the control surfaces are mechanically coupled such that movement of the actuator shaft (42, 44) causes movement of the control surfaces. a fuselage; a pair of control surfaces movable relative to the fuselage; an actuator having a movable actuator shaft (42, 44); and a coupler that selectively mechanically couples the actuator shaft (42, 44) to the control surfaces, wherein the coupler is in a disengaged condition when the actuator shaft (42, 44) and the control surfaces are not coupled by the coupler, and wherein the coupler is in an engaged condition when the actuator shaft and the control surfaces are coupled by the coupler; wherein the coupler is able to shift between the disengaged condition in which the control surfaces move independently of the actuator shaft such that movement of the actuator shaft (42, 44) does not cause movement of the control surfaces, and the engaged condition in which the actuator shaft (42, 44) and the control surfaces are mechanically coupled such that movement of the actuator shaft (42, 44) causes movement of the control surfaces.
A transparent conductor comprising: an insulating substrate having a surface; and a patterned layer on the surface of the insulating substrate, characterized in that the patterned layer is arranged on the surface in a predetermined pattern including one or more conductive regions and one or more non-conductive regions, wherein each conductive region has a plurality of metal nanowires embedded in a matrix, wherein the plurality of metal nanowires form a network, and each non-conductive region comprises an exposed portion of the surface of the insulating substrate. an insulating substrate having a surface; and a patterned layer on the surface of the insulating substrate, characterized in that the patterned layer is arranged on the surface in a predetermined pattern including one or more conductive regions and one or more non-conductive regions, wherein each conductive region has a plurality of metal nanowires embedded in a matrix, wherein the plurality of metal nanowires form a network, and each non-conductive region comprises an exposed portion of the surface of the insulating substrate.
An incubator-based phototherapy device, comprising: an enclosure portion enclosing a receiving space that is configured to receive an infant, the enclosure portion at least partially comprising a transparent material; and at least one illumination portion integrated with the enclosure portion, the illumination portion comprising multiple organic light emitting diode panels that project light having a wavelength between 400nm and 550nm and having an irradiance of between 10microWatt/cm2/nm and 35microWatt/cm2/nm when energized, wherein each of the multiple organic light emitting diode panels includes a separate mechanism for energizing/de-energizing, wherein the multiple organic light emitting diode panels are integrated between layers of the enclosure portion. an enclosure portion enclosing a receiving space that is configured to receive an infant, the enclosure portion at least partially comprising a transparent material; and at least one illumination portion integrated with the enclosure portion, the illumination portion comprising multiple organic light emitting diode panels that project light having a wavelength between 400nm and 550nm and having an irradiance of between 10microWatt/cm2/nm and 35microWatt/cm2/nm when energized, wherein each of the multiple organic light emitting diode panels includes a separate mechanism for energizing/de-energizing, wherein the multiple organic light emitting diode panels are integrated between layers of the enclosure portion.
A cabin enabling steam bathes to individuals and including at least two exterior walls (3a, 3b), one access door, one cabin floor and one cabin roof, • the cabin containing a vapour feed aperture, a fresh air aperture, a discharge, and an exhaust-air discharge, and • a seat unit enabling cabin occupants to sit in the cabin, and • the surface materials of the cabin being made of water-resistant material, and • the cabin being equipped with steering and control systems (13, 14) enabling to precisely control vapour content in the cabin and the yield of which is adapted to the cabin dimensions, and • the cabin being equipped with equipotential bonding equalising electric and electrostatic charges, characterised in that • the cabin includes another foam entry arranged downstream said vapour feed aperture, said fresh air feed aperture, and downstream said exhaust air discharge, and • the cabin is equipped with steering and control systems (13, 15) enabling generation of foam to be introduced into the cabin in defined quantities. • the cabin containing a vapour feed aperture, a fresh air aperture, a discharge, and an exhaust-air discharge, and • a seat unit enabling cabin occupants to sit in the cabin, and • the surface materials of the cabin being made of water-resistant material, and • the cabin being equipped with steering and control systems (13, 14) enabling to precisely control vapour content in the cabin and the yield of which is adapted to the cabin dimensions, and • the cabin being equipped with equipotential bonding equalising electric and electrostatic charges, characterised in that • the cabin includes another foam entry arranged downstream said vapour feed aperture, said fresh air feed aperture, and downstream said exhaust air discharge, and • the cabin is equipped with steering and control systems (13, 15) enabling generation of foam to be introduced into the cabin in defined quantities.
A current collector, comprising an insulation layer; and a conductive layer at least located on at least one surface of the insulation layer, wherein the conductive layer has a thickness of D2, where 30nm≤D2≤3μm, and the current collector is provided with a plurality of holes penetrating through the insulation layer and the conductive layer, wherein the conductive layer is further arranged on wall surfaces of the plurality of holes, and for each of the plurality of holes having the conductive layer disposed on its wall surface, the conductive layer is located on a part or an entirety of the wall surface. an insulation layer; and a conductive layer at least located on at least one surface of the insulation layer, wherein the conductive layer has a thickness of D2, where 30nm≤D2≤3μm, and the current collector is provided with a plurality of holes penetrating through the insulation layer and the conductive layer, wherein the conductive layer is further arranged on wall surfaces of the plurality of holes, and for each of the plurality of holes having the conductive layer disposed on its wall surface, the conductive layer is located on a part or an entirety of the wall surface.
A gas turbine engine comprising: a compressor section, a combustor and a turbine section, the turbine section downstream of the combustor section; a shaft connecting the turbine section to the compressor section; a bore tube disposed within the shaft downstream of the compressor section, the bore tube including an inlet connected to an air source for passing cooling air in an upstream direction of the shaft, wherein the shaft includes an aft end and the inlet of the bore tube is disposed at the aft end of the shaft; and characterised in that the gas turbine engine further comprises: a fan; a cooling air supply conduit and a rotating seal sealing between the cooling air supply conduit and the bore tube. a compressor section, a combustor and a turbine section, the turbine section downstream of the combustor section; a shaft connecting the turbine section to the compressor section; a bore tube disposed within the shaft downstream of the compressor section, the bore tube including an inlet connected to an air source for passing cooling air in an upstream direction of the shaft, wherein the shaft includes an aft end and the inlet of the bore tube is disposed at the aft end of the shaft; and characterised in that the gas turbine engine further comprises: a fan; a cooling air supply conduit and a rotating seal sealing between the cooling air supply conduit and the bore tube. a fan; a cooling air supply conduit and a rotating seal sealing between the cooling air supply conduit and the bore tube.
A waveguide comprising: planar surfaces including a top planar surface and a bottom planar surface; joining surfaces, each joining surface having flat surface areas and a number of gaps, each gap comprising a pit, and extending from the top planar surface to the bottom planar surface; each joining surface is tilted at a same angle with respect to the top planar surface; each gap of each joining surface reflecting out of the waveguide light received by the gap within a first angle range; and each gap of each joining surface passing for total internal reflection down the waveguide light received within a second angle range. planar surfaces including a top planar surface and a bottom planar surface; joining surfaces, each joining surface having flat surface areas and a number of gaps, each gap comprising a pit, and extending from the top planar surface to the bottom planar surface; each joining surface is tilted at a same angle with respect to the top planar surface; each gap of each joining surface reflecting out of the waveguide light received by the gap within a first angle range; and each gap of each joining surface passing for total internal reflection down the waveguide light received within a second angle range.
A tool for use in a powder metal process, said tool including: an upper tool; and a lower tool, said lower tool having a predetermined cross sectional profile that continuously expands outward from or near a center point of said lower tool; lower tool has a punch including an inner lower punch and an outer lower punch, wherein said punch is secured to said tool by a clamping mechanism, characterized in that said outer lower punch has a plurality of strengthening webs to increase the strength of said outer lower punch, said clamping mechanism including an upper clamp member, a lower clamp member, and a clamp spike member in which said clamp spike member has a plurality of locking members or spikes with predetermined angled surfaces on at least one surface thereof. an upper tool; and a lower tool, said lower tool having a predetermined cross sectional profile that continuously expands outward from or near a center point of said lower tool; lower tool has a punch including an inner lower punch and an outer lower punch, wherein said punch is secured to said tool by a clamping mechanism, characterized in that said outer lower punch has a plurality of strengthening webs to increase the strength of said outer lower punch, said clamping mechanism including an upper clamp member, a lower clamp member, and a clamp spike member in which said clamp spike member has a plurality of locking members or spikes with predetermined angled surfaces on at least one surface thereof.
A downhole screen (405") comprising a pipe (425") and a plurality of ceramic discs (470") stacked on each other around the pipe (425"), wherein the pipe (425") comprises a plurality of ports (440"), wherein at least one spacer (499") is provided between each two adjacent discs (470") such that adjacent discs (470") are spaced from one another, and wherein the/each spacer (499") is aligned with a respective port (440") of the plurality of ports (440") in the pipe (425") and shaped to diffuse fluid flow exiting the port (440") in the pipe (425"). wherein the pipe (425") comprises a plurality of ports (440"), wherein at least one spacer (499") is provided between each two adjacent discs (470") such that adjacent discs (470") are spaced from one another, and wherein the/each spacer (499") is aligned with a respective port (440") of the plurality of ports (440") in the pipe (425") and shaped to diffuse fluid flow exiting the port (440") in the pipe (425").
A polysiloxane comprising a hydrolytic condensate of a silicon compound containing a cyclic alkoxysiloxane having the formula: wherein each R 1 independently is a substituted or unsubstituted C 1 -C 3 alkyl group, each R 2 independently is a substituted or unsubstituted C 1 -C 6 alkyl group and n is an integer of 3 to 8, the polysiloxane having at least two hydrosilylable carbon-carbon unsaturated groups per molecule and at least two hydrosilyl groups per molecule, wherein provided that t1 is a molar fraction of T units having group R 1 relative to all siloxane units in the hydrolytic condensate, t1 is in the range 0.25 ≤ t1 < 1.
A vertical take-off and landing (VTOL) aerial vehicle, comprising: an energy source; a propulsion system configured to generate a lift force; a control system including electronics to control the aerial vehicle; an outer frame; a decoupling mechanism; and an inner frame connected to the outer frame by the decoupling mechanism, the inner frame comprising the propulsion system, the control system, and the energy source; the decoupling mechanism comprising a beam coupled to the inner frame and forming a first rotation axis (A,A) for rotation of the inner frame with respect to the beam, and the beam being rotationally coupled to the outer frame by a second rotation axis (B-B) substantially orthogonally disposed with respect to the first rotation axis, the beam comprising a rotation joint located near the center of the beam, the first rotation axis being formed by one or more bearings located within the rotation joint. an energy source; a propulsion system configured to generate a lift force; a control system including electronics to control the aerial vehicle; an outer frame; a decoupling mechanism; and an inner frame connected to the outer frame by the decoupling mechanism, the inner frame comprising the propulsion system, the control system, and the energy source; the decoupling mechanism comprising a beam coupled to the inner frame and forming a first rotation axis (A,A) for rotation of the inner frame with respect to the beam, and the beam being rotationally coupled to the outer frame by a second rotation axis (B-B) substantially orthogonally disposed with respect to the first rotation axis, the beam comprising a rotation joint located near the center of the beam, the first rotation axis being formed by one or more bearings located within the rotation joint.