mhurhangee/ep-ind-claims huggingface dataset:
An orthopedic locking screw configured for a cooperation with an implant thread of an orthopedic implant, the orthopedic locking screw comprising: a longitudinally extending shaft comprising a thread pattern section extending at least partially along the shaft, the thread pattern section comprising a first thread with a first direction and a second thread with a second direction opposite to the first direction of the first thread, the first thread being configured for the cooperation with the implant thread of the orthopedic implant and the second thread is superimposed on the first thread and intersects the first thread, characterized in that the orthopedic locking screw further comprises a screw head having a counter screw thread with a direction opposite to the first thread, the direction being opposite to the fastening direction of the locking screw, wherein the counter screw thread is arranged outwardly on the screw head and is configured to be threaded onto a screw driver. a longitudinally extending shaft comprising a thread pattern section extending at least partially along the shaft, the thread pattern section comprising a first thread with a first direction and a second thread with a second direction opposite to the first direction of the first thread, the first thread being configured for the cooperation with the implant thread of the orthopedic implant and the second thread is superimposed on the first thread and intersects the first thread, characterized in that the orthopedic locking screw further comprises a screw head having a counter screw thread with a direction opposite to the first thread, the direction being opposite to the fastening direction of the locking screw, wherein the counter screw thread is arranged outwardly on the screw head and is configured to be threaded onto a screw driver.
A dynamic stretching, strengthening and stabilization device for postural correction and retraining in a user, comprising: a central harness member having a middle panel, and two side sleeves (6, 6'); characterized by a pair of closed loop resistance tubes or cords (1, 1'), each closed loop resistance tube or cord being slidably received in one of the side sleeves (6, 6') of the central harness member; flexible handles (2,2') disposed on each closed loop resistance tube or cord and slidable along the closed loop resistance tube or cord; wherein the pair of closed loop resistance tubes or cords (1, 1') are spaced apart from each other by the side sleeves (6, 6') of the central harness member; wherein the handles (2,2') are configured to be gripped by the user and to be pulled in opposing directions to actively engage the closed loop resistance tubes or cords (1,1') in a stretching/strengthening mode; and each closed loop resistance tube or cord (1,1') being positionable over one of the user's arms so that the central harness member is positionable flat against the user's back and the handles (2,2') are positionable to cushion where the closed loop resistance tube or cords (1,1') engages the user's pectoral or underarm region in a stabilization mode; the closed loop resistance tubes or cords (1, 1') being sized so as to fit snugly on the user and providing passive resistance against forward shoulder curvature in the stabilization mode. a central harness member having a middle panel, and two side sleeves (6, 6'); characterized by a pair of closed loop resistance tubes or cords (1, 1'), each closed loop resistance tube or cord being slidably received in one of the side sleeves (6, 6') of the central harness member; flexible handles (2,2') disposed on each closed loop resistance tube or cord and slidable along the closed loop resistance tube or cord; wherein the pair of closed loop resistance tubes or cords (1, 1') are spaced apart from each other by the side sleeves (6, 6') of the central harness member; wherein the handles (2,2') are configured to be gripped by the user and to be pulled in opposing directions to actively engage the closed loop resistance tubes or cords (1,1') in a stretching/strengthening mode; and each closed loop resistance tube or cord (1,1') being positionable over one of the user's arms so that the central harness member is positionable flat against the user's back and the handles (2,2') are positionable to cushion where the closed loop resistance tube or cords (1,1') engages the user's pectoral or underarm region in a stabilization mode; the closed loop resistance tubes or cords (1, 1') being sized so as to fit snugly on the user and providing passive resistance against forward shoulder curvature in the stabilization mode.
Cup grinding wheel having a substantially circular main wheel and a plurality of grinding segments, wherein the grinding segments each have a V shape that is open towards the outside in the radial direction, said V shape being formed by in each case two arms (4, 5) of the grinding segments, preferably wherein the arms (4, 5) are arranged in an axially symmetric manner to a respective axis of symmetry extending in the radial direction, in particular wherein the respective arms (4, 5) of a grinding segment are in contact towards the inside in the radial direction, characterized in that passages that narrow in a funnel-like manner in the radial direction are formed between the grinding segments by respective outer edges (15, 16) of the arms (4, 5).
A brush-type circular composite seal, comprising: - a circular casing made of two crimped portions, a first portion of which, called a cage, comprising a cylindrical part and a radial return joined to the cylindrical part and comprising a first radial bearing face internal to the casing, and a second portion, called a chock, centred on the cylindrical part, radially extending and comprising a second bearing face internal to the casing and facing the first bearing face; - a composite structure consisting in a core internal to the casing and a network of bristles disposed into a winding around the core and comprising two parallel strands (21, 22) coming out of the casing between the cage and the chock; characterised in that: - the cylindrical part and the chock have a mutual stop radially extending interface; - the winding is in contact with the bearing faces (9, 10); - and the bearing faces (9, 10) are curved into concave tubs, having radiuses of curvature at least equal to the one of the winding. - a circular casing made of two crimped portions, a first portion of which, called a cage, comprising a cylindrical part and a radial return joined to the cylindrical part and comprising a first radial bearing face internal to the casing, and a second portion, called a chock, centred on the cylindrical part, radially extending and comprising a second bearing face internal to the casing and facing the first bearing face; - a composite structure consisting in a core internal to the casing and a network of bristles disposed into a winding around the core and comprising two parallel strands (21, 22) coming out of the casing between the cage and the chock; - the cylindrical part and the chock have a mutual stop radially extending interface; - the winding is in contact with the bearing faces (9, 10); - and the bearing faces (9, 10) are curved into concave tubs, having radiuses of curvature at least equal to the one of the winding.
A genetically engineered fusion molecule comprising a tumor associated antigen antibody (Ab) attached to an interferon alpha (IFN-α) mutant molecule, the IFN-α mutant molecule consisting of the amino acid sequence set forth in SEQ ID NO: 13 wherein R149 is A and wherein R162 is A, and wherein said antibody is attached directly to said IFN-α mutant molecule, wherein said fusion molecule when contacted to a tumor cell results in the killing or inhibition of growth or proliferation of said tumor cell.
A work vehicle comprising a fuel tank, wherein the fuel tank of the work vehicle is characterized by: a drain port which is open to an outside on a side surface and through which fuel is discharged to the outside; a suction port which is open to the outside on the side surface and has a center positioned lower than a center of the drain port and through which the fuel is sucked by an engine, wherein the drain port is formed on a side surface which faces one side in the right-left direction. a drain port which is open to an outside on a side surface and through which fuel is discharged to the outside; a suction port which is open to the outside on the side surface and has a center positioned lower than a center of the drain port and through which the fuel is sucked by an engine, wherein the drain port is formed on a side surface which faces one side in the right-left direction.
A coupling system, comprising: a transfer box having a transfer box body and a transfer box door; and an apparatus having an apparatus body and an apparatus door; said coupling system having structures wherein: the transfer box has a first sealing structure hermetically sealable by means of tight coupling of the transfer box body and transfer box door; the apparatus has a second sealing structure hermetically sealable by means of tight coupling of the apparatus body and apparatus door; the transfer box and apparatus have a third sealing structure hermetically sealable by means of tight coupling of both, as formed between the transfer box body and apparatus body; and only when the transfer box and apparatus are tightly coupled, one undivided coupling chamber is formed hermetically by the first, second and third sealing structures, i.e. the coupling chamber is formed by a mechanism requiring sealing of only three locations, where a means (15, 16) for cleaning the coupling chamber is provided, and while the coupling chamber is formed, the transfer box door magnetically contacts the apparatus door, and the transfer box door is adapted to be separated from the transfer box body and to be taken into the apparatus. the transfer box has a first sealing structure hermetically sealable by means of tight coupling of the transfer box body and transfer box door; the apparatus has a second sealing structure hermetically sealable by means of tight coupling of the apparatus body and apparatus door; the transfer box and apparatus have a third sealing structure hermetically sealable by means of tight coupling of both, as formed between the transfer box body and apparatus body; and only when the transfer box and apparatus are tightly coupled, one undivided coupling chamber is formed hermetically by the first, second and third sealing structures, i.e. the coupling chamber is formed by a mechanism requiring sealing of only three locations, where a means (15, 16) for cleaning the coupling chamber is provided, and while the coupling chamber is formed, the transfer box door magnetically contacts the apparatus door, and the transfer box door is adapted to be separated from the transfer box body and to be taken into the apparatus.
A compound having the formula I: wherein k, m, n and p are each independently 0, 1 or 2, provided that at least one of k, m, n and p is not 0; R and R' are each independently selected from H and C 1-3 alkyl, or, when taken together, R and R' are -CR 1 R 1' -X-CH 2 -, wherein CR 1 R 1' is attached to the backbone nitrogen, R 1 and R 1' are each independently selected from H and C 1-3 alkyl, and X is selected from -CH 2 -, -CH 2 CH 2 -, -CH -, -O-, -S- and -NH-; R" and R"' are each independently selected from H and C 1-3 alkyl, or, when taken together, R" and R'" are -CR 2 R 2' -X'-CH 2 -, wherein CR 2 R 2' is attached to the backbone nitrogen, R 2 and R 2' are each independently selected from H and C 1-3 alkyl, and X' is selected from -CH 2 -, -CH 2 CH 2 -, -CH -, -O-, -S- and -NH-; and R 3 and R 4 are each independently selected from aryl, substituted aryl, heteroaryl and substituted heteroaryl; or a pharmaceutically acceptable salt thereof. k, m, n and p are each independently 0, 1 or 2, provided that at least one of k, m, n and p is not 0; R and R' are each independently selected from H and C 1-3 alkyl, or, when taken together, R and R' are -CR 1 R 1' -X-CH 2 -, wherein CR 1 R 1' is attached to the backbone nitrogen, R 1 and R 1' are each independently selected from H and C 1-3 alkyl, and X is selected from -CH 2 -, -CH 2 CH 2 -, -CH -, -O-, -S- and -NH-; R" and R"' are each independently selected from H and C 1-3 alkyl, or, when taken together, R" and R'" are -CR 2 R 2' -X'-CH 2 -, wherein CR 2 R 2' is attached to the backbone nitrogen, R 2 and R 2' are each independently selected from H and C 1-3 alkyl, and X' is selected from -CH 2 -, -CH 2 CH 2 -, -CH -, -O-, -S- and -NH-; and R 3 and R 4 are each independently selected from aryl, substituted aryl, heteroaryl and substituted heteroaryl;
A fire alarm system, comprising: a socket (2, 22, 24) including at least one electrical conductor (10, 11, 12, 14) configured to electrically connect to a component received by the socket; a temperature sensor configured to detect a temperature of the electrical conductor; and a fire alarm control panel in communication with the temperature sensor, wherein the fire alarm control panel is configured to take a first action when the detected temperature of the electrical conductor exceeds a first threshold for a first period of time; and wherein the fire alarm control panel is configured to take a second action when the detected temperature of the electrical conductor exceeds a second threshold for a second period of time, the second threshold being higher than the first threshold. a socket (2, 22, 24) including at least one electrical conductor (10, 11, 12, 14) configured to electrically connect to a component received by the socket; a temperature sensor configured to detect a temperature of the electrical conductor; and a fire alarm control panel in communication with the temperature sensor, wherein the fire alarm control panel is configured to take a first action when the detected temperature of the electrical conductor exceeds a first threshold for a first period of time; and wherein the fire alarm control panel is configured to take a second action when the detected temperature of the electrical conductor exceeds a second threshold for a second period of time, the second threshold being higher than the first threshold.
Method for ascertaining a concentration (c A) of potentially infectious aerosol particles in a volume, wherein the volume comprises one or more emitters (E1,..., En) of the aerosol, comprising the following steps: - recording at least one time profile of an acoustic variable in the volume, said variable being associated with one or more of the emitters (E1,...,En), - ascertaining an emission of aerosol particles for at least one of the emitters (E1,...,En) on the basis of the recorded time profile of the acoustic variable, wherein the emission is ascertained by integrating an emission rate (q), wherein the emission rate (q) is ascertained as a function of the at least one time profile of the acoustic variable, and - ascertaining the concentration (c A) on the basis of the at least one emission, wherein an emission is determined for each of a plurality of emitters (E1,..., En) and wherein the concentration (c A) is ascertained on the basis of the largest of the determined emissions. - recording at least one time profile of an acoustic variable in the volume, said variable being associated with one or more of the emitters (E1,...,En), - ascertaining an emission of aerosol particles for at least one of the emitters (E1,...,En) on the basis of the recorded time profile of the acoustic variable, wherein the emission is ascertained by integrating an emission rate (q), wherein the emission rate (q) is ascertained as a function of the at least one time profile of the acoustic variable, and - ascertaining the concentration (c A) on the basis of the at least one emission, wherein an emission is determined for each of a plurality of emitters (E1,..., En) and wherein the concentration (c A) is ascertained on the basis of the largest of the determined emissions.
A build material for use in a three-dimensional printing system comprising: 10 to 30 percent by weight of an oligomeric curable material; 50 to 75 percent by weight of at least one diluent; 3 to 15 percent by weight of an isocyanurate (meth)acrylate; and less than 5 percent by weight of a non-reactive wax component, wherein the build material when cured exhibits a tensile modulus of 2250-3150 MPa when measured according to ASTM D 638, and wherein the build material when cured exhibits a tensile strength of 46-76 MPa when measured according to ASTM D 638. 10 to 30 percent by weight of an oligomeric curable material; 50 to 75 percent by weight of at least one diluent; 3 to 15 percent by weight of an isocyanurate (meth)acrylate; and less than 5 percent by weight of a non-reactive wax component, wherein the build material when cured exhibits a tensile modulus of 2250-3150 MPa when measured according to ASTM D 638, and wherein the build material when cured exhibits a tensile strength of 46-76 MPa when measured according to ASTM D 638.
A method of accelerating a gas turbine engine of an aircraft, comprising: adding torque to a core of the gas turbine engine to accelerate rotation of the core by controlling fuel flow to a plurality of fuel injectors of the gas turbine engine; and adding torque to the core by powering an electric machine that is operatively connected to the core to drive the core, characterized in that: the controlling fuel flow to the plurality of fuel injectors is based on feedback from the electric machine including a torque feedback and a rotational speed feedback; powering the electric machine includes controlling the electric machine based on an engine core speed feedback from the core to reach a target core speed of the core; and the controlling fuel flow based on feedback from the electric machine includes controlling fuel flow to achieve a target torque generated by the electric machine. adding torque to a core of the gas turbine engine to accelerate rotation of the core by controlling fuel flow to a plurality of fuel injectors of the gas turbine engine; and adding torque to the core by powering an electric machine that is operatively connected to the core to drive the core, characterized in that: the controlling fuel flow to the plurality of fuel injectors is based on feedback from the electric machine including a torque feedback and a rotational speed feedback; powering the electric machine includes controlling the electric machine based on an engine core speed feedback from the core to reach a target core speed of the core; and the controlling fuel flow based on feedback from the electric machine includes controlling fuel flow to achieve a target torque generated by the electric machine. the controlling fuel flow to the plurality of fuel injectors is based on feedback from the electric machine including a torque feedback and a rotational speed feedback; powering the electric machine includes controlling the electric machine based on an engine core speed feedback from the core to reach a target core speed of the core; and the controlling fuel flow based on feedback from the electric machine includes controlling fuel flow to achieve a target torque generated by the electric machine.
A distributed propulsion system (110, 210) with thermal management for an aircraft, the system comprising: two or more motors, (211a-d, 311a-d); two or more rotors (212a-d, 312a-d) being each associated with one of the two or more motors (211a-d, 311a-d), each motor (211a-d, 311a-d) being individually controlled, and each motor (211a-d, 31 1a-d) comprising a temperature sensor; a pilot input control connected to the associated motors (211a-d, 311a-d) to demand the associated motors (211a-d, 311a-d) to produce a demanded thrust, a control system comprising a control logic with thermal management connected to the pilot input control, to the temperature sensors and to the motors (211a-d, 311a-d), wherein the control logic is configured to control independently a motor power output of each motor of the associated motors (211a-d, 311a-d) to produce the demanded thrust and to control a motor temperature of one or more of the associated motors (21 1a-d, 31 1a-d); a liquid cooling system including regulators, conduits and a coolant reservoir, the regulators in communication with conduits between a coolant reservoir and each of the motors (21 1a-d); and the control system being further connected to the regulators and wherein the control logic is configured to manipulate one or more of the regulators to increase a cooling capacity circulated through one or more of the motors (21 1a-d) in response to a temperature read by one or more of the temperature sensors of the one or more of the motors (211a-d) being above a threshold temperature. two or more motors, (211a-d, 311a-d); two or more rotors (212a-d, 312a-d) being each associated with one of the two or more motors (211a-d, 311a-d), each motor (211a-d, 311a-d) being individually controlled, and each motor (211a-d, 31 1a-d) comprising a temperature sensor; a pilot input control connected to the associated motors (211a-d, 311a-d) to demand the associated motors (211a-d, 311a-d) to produce a demanded thrust, a control system comprising a control logic with thermal management connected to the pilot input control, to the temperature sensors and to the motors (211a-d, 311a-d), wherein the control logic is configured to control independently a motor power output of each motor of the associated motors (211a-d, 311a-d) to produce the demanded thrust and to control a motor temperature of one or more of the associated motors (21 1a-d, 31 1a-d); a liquid cooling system including regulators, conduits and a coolant reservoir, the regulators in communication with conduits between a coolant reservoir and each of the motors (21 1a-d); and the control system being further connected to the regulators and wherein the control logic is configured to manipulate one or more of the regulators to increase a cooling capacity circulated through one or more of the motors (21 1a-d) in response to a temperature read by one or more of the temperature sensors of the one or more of the motors (211a-d) being above a threshold temperature.
A method for data transmission performed by a User Equipment, UE, the method comprising: detecting a scheduling assignment, SA, for other UEs within a sensing window which includes a plurality of time units, TUs; selecting, based on the detected SA, a set of resources for data transmission; determining, if the UE does not perform data transmission on one resource of the selected set of resources, whether a resource subsequent to the one resource in the selected set of resources is occupied based on the detected SA, a received power, and a received energy on the resource, before transmitting data on the subsequent resource in the selected set of resources; and transmitting the data on the subsequent resource in the selected set of resources if it is determined that the resource is not occupied. detecting a scheduling assignment, SA, for other UEs within a sensing window which includes a plurality of time units, TUs; selecting, based on the detected SA, a set of resources for data transmission; determining, if the UE does not perform data transmission on one resource of the selected set of resources, whether a resource subsequent to the one resource in the selected set of resources is occupied based on the detected SA, a received power, and a received energy on the resource, before transmitting data on the subsequent resource in the selected set of resources; and transmitting the data on the subsequent resource in the selected set of resources if it is determined that the resource is not occupied.