mhurhangee/patent-ind-claim-en huggingface dataset:
Method of detecting the presence of at least one propellant gas in a gaseous sample, comprising the steps of: - receiving the sample in a sample chamber ; - generating test light pulses and reference light pulses, the spectrum of the light pulses being at least partially within a wavelength range wherein absorption is indicative for the presence of said propellant gas, especially in the range of 3.30-3.55 μm wavelength; - passing the test light pulses through the sample chamber and letting the reference light pulses bypass the sample chamber ; - detecting the test light pulses and the reference light pulses with a detector ; - comparing the amplitude (A Test ) of at least one detected test light pulse with the amplitude (A ref ) of at least one detected reference light pulse so as to determine the presence or absence of said propellant gas above a predetermined threshold concentration in the sample chamber , wherein the test light pulses and the reference light pulses are detected by the same, single, detector , characterised in that the test light pulses and the reference light pulses are generated by beam splitting pulsed laser light from a single laser source to generate test laser light pulses travelling along a test optical path (P1) and reference laser light pulses travelling along a reference optical path (P2), in that the length of an optical path in ambient air travelled by the test laser light pulses is equal to the length of an optical path in ambient air travelled by the reference laser light pulses, and in that the total length of the test optical path (P1) travelled by the test laser light pulses is different from the total length of the reference optical path (P2) travelled by the reference laser light pulses. - receiving the sample in a sample chamber ; - generating test light pulses and reference light pulses, the spectrum of the light pulses being at least partially within a wavelength range wherein absorption is indicative for the presence of said propellant gas, especially in the range of 3.30-3.55 μm wavelength; - passing the test light pulses through the sample chamber and letting the reference light pulses bypass the sample chamber ; - detecting the test light pulses and the reference light pulses with a detector ; - comparing the amplitude (A Test ) of at least one detected test light pulse with the amplitude (A ref ) of at least one detected reference light pulse so as to determine the presence or absence of said propellant gas above a predetermined threshold concentration in the sample chamber ,
An oral treatment device for use in providing treatment to a person's teeth and/or gums, comprising: a dental treatment tray configured for placement over at least a portion of a user's teeth and formed from a wax-based composition containing 40% to 95% by combined weight of paraffin wax and microcrystalline wax and 5% to 60% by weight of a thermoplastic elastomer homogeneously blended with the paraffin wax and microcrystalline wax, wherein the dental treatment tray is thermally stable to a temperature of at least 45°C and plastically deformable at room temperature (25°C); and an oral treatment composition adjacent to and/or impregnated within the dental treatment tray. a dental treatment tray configured for placement over at least a portion of a user's teeth and formed from a wax-based composition containing 40% to 95% by combined weight of paraffin wax and microcrystalline wax and 5% to 60% by weight of a thermoplastic elastomer homogeneously blended with the paraffin wax and microcrystalline wax, wherein the dental treatment tray is thermally stable to a temperature of at least 45°C and plastically deformable at room temperature (25°C); and an oral treatment composition adjacent to and/or impregnated within the dental treatment tray.
Agricultural transport vehicle , with a load compartment , with a tailgate positioned at a rear region of the load compartment , and with a hydraulic tailgate actuator for moving the tailgate , with an unloading device designed in particular as a scraper floor or retractable floor or push unit, and with an unloading device actuator for driving the unloading device , with a hydraulic module shared by the tailgate actuator and the unloading device actuator , and a tailgate sensor , depending on which the unloading device actuator of the unloading device can be operated in such a manner that the unloading device actuator can be driven by the hydraulic module whenever the tailgate sensor detects a defined opening position of the tailgate , characterized in that metering rollers are arranged in the rear region of the load compartment , in that a rotational speed sensor monitors the rotational speed of the metering rollers , and in that the unloading device actuator can be activated by the hydraulic module in such a manner that the unloading device actuator can be driven whenever the tailgate sensor detects the defined opening position of the tailgate and whenever, furthermore, the rotational speed sensor detects a defined rotational speed of the metering rollers .
Method for manufacturing a gas fired radiant emitter with increased emissivity, comprising the steps of - providing a porous ceramic burner deck , - applying a wet coating layer on said porous ceramic burner deck , wherein said wet coating layer comprises ceramic particles and/or metallic particles, that will form a coating layer with increased emissivity compared to the porous ceramic burner deck without the coating layer; wherein sintering and/or curing of said coating layer is performed by operating said gas fired radiant emitter in which the porous ceramic burner deck is mounted, via supplying combustible gas to said radiant emitter and igniting said combustible gas after it has flown through the porous ceramic burner deck , whereby the uncured and/or unsintered coating layer is transformed into a sintered and/or cured coating layer adhering to said porous ceramic burner deck via sintered and/or cured bonds. - providing a porous ceramic burner deck , - applying a wet coating layer on said porous ceramic burner deck , wherein said wet coating layer comprises ceramic particles and/or metallic particles, that will form a coating layer with increased emissivity compared to the porous ceramic burner deck without the coating layer;
Grinding device for a slice-cutting machine (10', 10") for cutting off slices of in particular strand-like cutting material, preferably food, the grinding device comprising a grinding stone for sharpening a rotating circular blade of the slice-cutting machine (10', 10") and a honing stone for deburring the circular blade , the grinding device comprising a grip in order to move the grinding stone and/or the honing stone to the circular blade , and the grinding device having a holder for fastening to a stop plate of the slice-cutting machine (10', 10") with an insertion device for form-fitting insertion into the stop plate , the holder having a U-shaped plate receptacle with a gap for insertion of the stop plate into the gap when the grinding device is pushed onto the stop plate , characterized in that the insertion device has at least one lug for engaging in an associated deepening of the stop plate , or in that the stop plate has at least one lug for engaging in an associated deepening of the insertion device .
A method of operating User Equipment, UE, in a wireless communication network, characterized by : receiving from the network a first value for a Time Alignment Timer, TAT, , and a second value for the TAT for non delay-tolerant data, wherein the first value indicates a shorter duration than the second value; and when data to the network is determined delay-tolerant, applying the first value to the Time Alignment Timer . receiving from the network a first value for a Time Alignment Timer, TAT, , and a second value for the TAT for non delay-tolerant data, wherein the first value indicates a shorter duration than the second value; and when data to the network is determined delay-tolerant, applying the first value to the Time Alignment Timer .
An electric power steering apparatus that calculates a current command value based on at least a steering torque, driving-controls a motor , which applies an assist torque to a steering system based on said current command value, by an inverter with respective phase duties of a pulse width modulation (PWM), and detects an angle of said steering system or said motor , characterised by : an angle estimating section to detect a regenerative current of said motor by fixing said respective phase duties to 0% or 100% and to estimate said angle when a detecting system of said angle is failed, wherein said electric power steering apparatus performs an assist-control based on an estimating angle that is estimated at said angle estimating section . an angle estimating section to detect a regenerative current of said motor by fixing said respective phase duties to 0% or 100% and to estimate said angle when a detecting system of said angle is failed, wherein said electric power steering apparatus performs an assist-control based on an estimating angle that is estimated at said angle estimating section .
A mobile monitoring device comprising: - a data signal interface adapted to - be coupled to a data line arranged in an aircraft and carrying one or more sensor signals, such that, in operation, the data signal interface branches off and receives as input signal part of the energy of the one or more sensor signals carried on the data line such that the input signal is characteristic of the one or more sensor signals, and - provide an output signal characteristic of the input signal, and - a wireless communication interface connected to the data signal interface for receiving the output signal and adapted to wirelessly transmit the output signal to a remote location, wherein the data signal interface comprises a processing means which is arranged and adapted to receive the input signal and to process the input signal to generate the output signal, wherein the processing means implements a decoding module which is operable to calculate for one or more of the sensor signals, of which the input signal is characteristic, corresponding measurement values and to generate the output signal such that it is characteristic of the one or more measurement values. - a data signal interface adapted to - be coupled to a data line arranged in an aircraft and carrying one or more sensor signals, such that, in operation, the data signal interface branches off and receives as input signal part of the energy of the one or more sensor signals carried on the data line such that the input signal is characteristic of the one or more sensor signals, and - provide an output signal characteristic of the input signal, and - be coupled to a data line arranged in an aircraft and carrying one or more sensor signals, such that, in operation, the data signal interface branches off and receives as input signal part of the energy of the one or more sensor signals carried on the data line such that the input signal is characteristic of the one or more sensor signals, and - provide an output signal characteristic of the input signal, and - a wireless communication interface connected to the data signal interface for receiving the output signal and adapted to wirelessly transmit the output signal to a remote location,
A surgical robotic cart assembly including: a base , the base configured to support a robotic arm thereon and including a plurality of casters attached thereto to allow the surgical robotic cart assembly to move along a floor; characterised by at least one vacuum cup (610; 710) coupled to the base; an actuator configured to move the at least one vacuum cup away from the base and towards the floor to engage the at least one vacuum cup with the floor; and a vacuum source (630; 730) in fluid communication with the at least one vacuum cup and configured to remove air from the at least one vacuum cup thereby securing the at least one vacuum cup to the floor, when the at least one vacuum cup is in contact with the floor, and immobilizing the surgical robotic cart assembly. a base , the base configured to support a robotic arm thereon and including a plurality of casters attached thereto to allow the surgical robotic cart assembly to move along a floor; characterised by at least one vacuum cup (610; 710) coupled to the base; an actuator configured to move the at least one vacuum cup away from the base and towards the floor to engage the at least one vacuum cup with the floor; and a vacuum source (630; 730) in fluid communication with the at least one vacuum cup and configured to remove air from the at least one vacuum cup thereby securing the at least one vacuum cup to the floor, when the at least one vacuum cup is in contact with the floor, and immobilizing the surgical robotic cart assembly.
A kit of parts comprising a shark avoidance system , a bag with at least one access panel and a life vest or buoyancy compensator device , wherein the bag is configured to receive and retain the shark avoidance system , wherein the bag is removably connected with the life vest or buoyancy compensator device with a release device in the form of a rip cord device , such that pulling of the rip cord device releases the bag from attachment with the life vest or buoyancy compensator device , and wherein the shark avoidance system comprises: a.) at least one open ended enclosure with at least a top , sides , and at least one bottom , wherein especially said sides and said bottom forming at least one interior enclosed space ; and b.) at least one buoyant device and at least one inflatable device , wherein said buoyant device and said inflatable device are connected to form a combination and/or wherein said combination is connected with said top of the open ended enclosure ; c.) wherein said sides connect said top and said bottom , wherein said sides form at least one flexible wall and wherein said flexible wall comprises and/or consists of a combination of at least three layers , at least one first, preferably outer, layer , at least one second, preferably middle, layer and at least one third, preferably inner, layer , especially said third layer connected to said second layer and/or said second layer connected to said first layer , wherein one of said layers is a water impervious layer, wherein one of said layers is a bioelectrical blocking layer and/or wherein one of said layers is a sound emission blocking layer. a.) at least one open ended enclosure with at least a top , sides , and at least one bottom , wherein especially said sides and said bottom forming at least one interior enclosed space ; and b.) at least one buoyant device and at least one inflatable device , wherein said buoyant device and said inflatable device are connected to form a combination and/or wherein said combination is connected with said top of the open ended enclosure ; c.) wherein said sides connect said top and said bottom , wherein said sides form at least one flexible wall and wherein said flexible wall comprises and/or consists of a combination of at least three layers , at least one first, preferably outer, layer , at least one second, preferably middle, layer and at least one third, preferably inner, layer , especially said third layer connected to said second layer and/or said second layer connected to said first layer , wherein one of said layers is a water impervious layer, wherein one of said layers is a bioelectrical blocking layer and/or wherein one of said layers is a sound emission blocking layer.
A method for receiving an enhanced downlink physical control channel, EPDCCH, in a wireless access system supporting an unlicensed band, the method performed by a user equipment, UE, and comprising: receiving (S2530), through an unlicensed band cell, UCell, configured in the unlicensed band, the EPDCCH including control information for scheduling the UCell; and receiving (S2540) downlink data in the UCell based on the control information, characterised in that the EPDCCH is transmitted in a partial subframe, pSF, which is configured in a smaller size than one subframe, wherein enhanced resource element groups, EREGs, included in the EPDCCH are indexed, starting from a starting symbol of the pSF, and wherein a starting position of the pSF is not aligned with a subframe boundary of a primary cell, PCell, configured in a licensed band. receiving (S2530), through an unlicensed band cell, UCell, configured in the unlicensed band, the EPDCCH including control information for scheduling the UCell; and receiving (S2540) downlink data in the UCell based on the control information, characterised in that the EPDCCH is transmitted in a partial subframe, pSF, which is configured in a smaller size than one subframe, wherein enhanced resource element groups, EREGs, included in the EPDCCH are indexed, starting from a starting symbol of the pSF, and wherein a starting position of the pSF is not aligned with a subframe boundary of a primary cell, PCell, configured in a licensed band.
A method of wireless communications using hybrid automatic repeat request, HARQ, comprising: generating a first codeword based on a first code block length, wherein the first codeword is generated using a polar code; transmitting a first signal using the first codeword; generating a second codeword with incremental redundancy information for the first codeword based on a second code block length, wherein the second codeword is generated using a polar code; generating a third codeword with repetition of at least a portion of the first codeword based on a third code block length, wherein the third codeword is generated using a polar code; determining a fourth code block length for transmitting a second signal; and transmitting the second signal using a hybrid codeword in response to a determination that the fourth code block length is not an integer multiple of the first code block length, wherein the hybrid codeword includes at least the second codeword and the third codeword. generating a first codeword based on a first code block length, wherein the first codeword is generated using a polar code; transmitting a first signal using the first codeword; generating a second codeword with incremental redundancy information for the first codeword based on a second code block length, wherein the second codeword is generated using a polar code; generating a third codeword with repetition of at least a portion of the first codeword based on a third code block length, wherein the third codeword is generated using a polar code; determining a fourth code block length for transmitting a second signal; and transmitting the second signal using a hybrid codeword in response to a determination that the fourth code block length is not an integer multiple of the first code block length, wherein the hybrid codeword includes at least the second codeword and the third codeword.
An antigen binding protein that binds to a PCSK9 protein comprising the amino acid sequence of SEQ ID NO: 1, wherein the antigen binding protein is a monoclonal antibody or fragment thereof, wherein the antigen binding protein decreases the LDLR lowering effect of PCSK9 on LDLR, and (i) wherein the antigen binding protein is an LDLR non-competitive neutralizing antigen binding protein; and/or (ii) wherein the antigen binding protein comprises: a heavy chain polypeptide comprising the following complementarity determining regions (CDRs): a heavy chain CDR1 that is a CDR1 in SEQ ID NO:89; a heavy chain CDR2 that is a CDR2 in SEQ ID NO:89; a heavy chain CDR3 that is a CDR3 in SEQ ID NO:89; and a light chain polypeptide comprising the following CDRs: a light chain CDR1 that is a CDR1 in SEQ ID NO:32; a light chain CDR2 that is a CDR2 in SEQ ID NO:32; a light chain CDR3 that is a CDR3 in SEQ ID NO:32; wherein the CDRs are identified by the Kabat definition, the Chothia definition, the AbM definition or the contact definition. (i) wherein the antigen binding protein is an LDLR non-competitive neutralizing antigen binding protein; and/or (ii) wherein the antigen binding protein comprises: a heavy chain polypeptide comprising the following complementarity determining regions (CDRs): a heavy chain CDR1 that is a CDR1 in SEQ ID NO:89; a heavy chain CDR2 that is a CDR2 in SEQ ID NO:89; a heavy chain CDR3 that is a CDR3 in SEQ ID NO:89; and a light chain polypeptide comprising the following CDRs: a light chain CDR1 that is a CDR1 in SEQ ID NO:32; a light chain CDR2 that is a CDR2 in SEQ ID NO:32; a light chain CDR3 that is a CDR3 in SEQ ID NO:32; wherein the CDRs are identified by the Kabat definition, the Chothia definition, the AbM definition or the contact definition. a heavy chain CDR1 that is a CDR1 in SEQ ID NO:89; a heavy chain CDR2 that is a CDR2 in SEQ ID NO:89; a heavy chain CDR3 that is a CDR3 in SEQ ID NO:89; and a light chain polypeptide comprising the following CDRs: a light chain CDR1 that is a CDR1 in SEQ ID NO:32; a light chain CDR2 that is a CDR2 in SEQ ID NO:32; a light chain CDR3 that is a CDR3 in SEQ ID NO:32; wherein the CDRs are identified by the Kabat definition, the Chothia definition, the AbM definition or the contact definition. a light chain CDR1 that is a CDR1 in SEQ ID NO:32; a light chain CDR2 that is a CDR2 in SEQ ID NO:32; a light chain CDR3 that is a CDR3 in SEQ ID NO:32; wherein the CDRs are identified by the Kabat definition, the Chothia definition, the AbM definition or the contact definition.
Guide vane, wherein the vane comprises an airfoil having a first airfoil portion and a second airfoil portion , and the first airfoil portion is reversibly rotatable from a first position into a second position about an axis of rotation (D), relative to the second airfoil portion , wherein, in at least one profile section of the airfoil, the axis of rotation (D) is arranged outside a profile of the first airfoil portion , and a profile of the first airfoil portion comprises a suction side having a first contour portion and a second contour portion , and a profile of the second airfoil portion comprises a pressure-side contour portion , which in the first position is covered by the first contour portion of the first airfoil portion and in the second position is instead covered by the second contour portion of the first airfoil portion in the circumferential direction, characterized in that the axis of rotation (D) is located on the side of the pressure side, and downstream of the leading edge and upstream of the trailing edge of the second blade portion . a profile of the first airfoil portion comprises a suction side having a first contour portion and a second contour portion , and a profile of the second airfoil portion comprises a pressure-side contour portion , which in the first position is covered by the first contour portion of the first airfoil portion and in the second position is instead covered by the second contour portion of the first airfoil portion in the circumferential direction, characterized in that the axis of rotation (D) is located on the side of the pressure side, and downstream of the leading edge and upstream of the trailing edge of the second blade portion .