mhurhangee/ep-ind-claims huggingface dataset:
An apparatus comprising means for: causing a first image of live viewfinder data to be displayed to a user, the first image comprising one or more selectable objects (502, 504); receiving a first user input selecting at least one selectable object from the first image; subsequent to receiving the first user input, causing a second image of live viewfinder data to be displayed to the user, the second image comprising a second instance of the at least one selected object in a changed position from the first image; in response to a user capture input, combining the at least one selected object of the first image and the second image to create a composite image comprising the at least one selectable object from the first image and the second instance of the at least one selected object in a changed position from the first image; and causing the composite image to be stored. causing a first image of live viewfinder data to be displayed to a user, the first image comprising one or more selectable objects (502, 504); receiving a first user input selecting at least one selectable object from the first image; subsequent to receiving the first user input, causing a second image of live viewfinder data to be displayed to the user, the second image comprising a second instance of the at least one selected object in a changed position from the first image; in response to a user capture input, combining the at least one selected object of the first image and the second image to create a composite image comprising the at least one selectable object from the first image and the second instance of the at least one selected object in a changed position from the first image; and causing the composite image to be stored.
A supersaturated solid solution soft magnetic material, comprising: raw materials including iron (Fe), silicon (Si), cobalt (Co) and titanium (Ti); wherein proportions of the respective raw materials comprise 72.0-78.0 atomic percent (at%) Fe, 12.0-18.0 at% Si, 4.0-12.0 at% Co and 1.0-3.0 at% Ti.
An illuminating building block with high light transmission, comprising: a base having at least two recesses defined therethrough; a top cover being hollow and light transmittable, mounted on the base, including a top portion and side walls, the top portion including at least two hollow studs corresponding to the recesses of the base, the side walls being extended from edges of the top portion to edges of the base; a circuit board disposed on a top of the base, including at least two units of electrode circuits corresponding to the recesses of the base, each unit of electrode circuit including a positive electrode circuit and a negative electrode circuit, at least one illuminating member mounted on the electrode circuit of the circuit board; characterised in that the positive electrode circuits and the negative electrode circuits are respectively connected with at least one set of electric connection members that are extended away from the base, each of the electric connection members including a projection portion, a connection portion and at least two elastic pieces, the projection portion contacting the electrode circuit of the circuit board, the connection portion electrically connecting the projection portion with the elastic pieces, the elastic pieces projecting into the hollow studs. a base having at least two recesses defined therethrough; a top cover being hollow and light transmittable, mounted on the base, including a top portion and side walls, the top portion including at least two hollow studs corresponding to the recesses of the base, the side walls being extended from edges of the top portion to edges of the base; a circuit board disposed on a top of the base, including at least two units of electrode circuits corresponding to the recesses of the base, each unit of electrode circuit including a positive electrode circuit and a negative electrode circuit, at least one illuminating member mounted on the electrode circuit of the circuit board; characterised in that the positive electrode circuits and the negative electrode circuits are respectively connected with at least one set of electric connection members that are extended away from the base, each of the electric connection members including a projection portion, a connection portion and at least two elastic pieces, the projection portion contacting the electrode circuit of the circuit board, the connection portion electrically connecting the projection portion with the elastic pieces, the elastic pieces projecting into the hollow studs.
-5,10-methylene-tetrahydrofolate for use in the treatment in a human of solid tumors, including cancer, which treatment comprises the following steps: a) On Day 1, administering an IV bolus containing 10-1000 mg/m 2 (of BSA) of a fluorinated pyrimidine base such as 5-fluorouracil (5-FU), followed, either simultaneously or after a period of 10 min - 4 hours, by b) administering two or more IV boluses, interspaced by a period of 10 - 60 minutes, each containing 5 - 1000 mg/m 2 -5,10-methylenetetrahydrofolate, followed by c) administering a continuous infusion of a fluorinated pyrimidine base such as 5-FU over a period of 46 hours, or until the end of Day 2, followed by d) optionally administering one IV bolus containing 5 - 1000 mg/m 2 (of BSA) -5,10-methylene-tetrahydrofolate before the end of Day 1, followed by e) On Day 2, optionally administering one or more IV boluses each containing 5 - 1000 mg/m 2 (of BSA) -5,10-methylene-tetrahydrofolate, wherein step b) is optionally repeated up to 4 times on Day 1 with an interval of 10 min - 4 hours between each repetition, and wherein step e) is optionally repeated up to 4 times on Day 2 with an interval of between 10 min - 60 min between each bolus being administered, and wherein all steps a) - e) are optionally repeated every 2 weeks for up to eight cycles, i.e. up to sixteen weeks. a) On Day 1, administering an IV bolus containing 10-1000 mg/m 2 (of BSA) of a fluorinated pyrimidine base such as 5-fluorouracil (5-FU), followed, either simultaneously or after a period of 10 min - 4 hours, by b) administering two or more IV boluses, interspaced by a period of 10 - 60 minutes, each containing 5 - 1000 mg/m 2 -5,10-methylenetetrahydrofolate, followed by c) administering a continuous infusion of a fluorinated pyrimidine base such as 5-FU over a period of 46 hours, or until the end of Day 2, followed by d) optionally administering one IV bolus containing 5 - 1000 mg/m 2 (of BSA) -5,10-methylene-tetrahydrofolate before the end of Day 1, followed by e) On Day 2, optionally administering one or more IV boluses each containing 5 - 1000 mg/m 2 (of BSA) -5,10-methylene-tetrahydrofolate,
A pivot hinge fitting for a roof window, comprising: a frame hinge part for fastening to a frame of the roof window and including guide means (120, 130), and a sash hinge part for fastening to a sash of the roof window and including a slide rail to cooperate with the guide means (120, 130) of the frame hinge part, an additional set of engagement means (150, 250) is provided on the frame hinge part and the sash hinge part, with a first engagement element on the sash hinge part and a second engagement element on the frame hinge part, to pull the frame hinge part and the sash hinge part together, wherein the frame hinge part is provided on an intermediate frame and in addition to the guide means (120, 130) comprises a top plate connected to a base plate of the frame hinge part, characterized in that in that the second engagement element of the additional set of engagement means is provided as a wedge-shaped portion of the top plate of the frame hinge part and arranged to enter the first engagement element of the sash hinge part during operation of the roof window, when the sash is brought from the open position towards the closed position. a frame hinge part for fastening to a frame of the roof window and including guide means (120, 130), and a sash hinge part for fastening to a sash of the roof window and including a slide rail to cooperate with the guide means (120, 130) of the frame hinge part, an additional set of engagement means (150, 250) is provided on the frame hinge part and the sash hinge part, with a first engagement element on the sash hinge part and a second engagement element on the frame hinge part, to pull the frame hinge part and the sash hinge part together, wherein the frame hinge part is provided on an intermediate frame and in addition to the guide means (120, 130) comprises a top plate connected to a base plate of the frame hinge part, characterized in that in that the second engagement element of the additional set of engagement means is provided as a wedge-shaped portion of the top plate of the frame hinge part and arranged to enter the first engagement element of the sash hinge part during operation of the roof window, when the sash is brought from the open position towards the closed position.
A plastic injection tool for producing a closure cap with a cap body and a cap cover formed integrally with and of the same material as the cap body, wherein the cap cover can be formed as cap lid, which can be moved relative to the cap body, wherein the injection tool is further divided into first and second mold halves (2, 3), which can be displaced relative to one another, and wherein an injection nozzle is formed in the first mold half, wherein sliding jaw tool parts, which can simultaneously be moved in an injection direction (r) of the produced closure cap and perpendicular to the ejection direction (r), are further formed in the second mold half radially outside to a central tool core, and a partial injection contour of the cap body is in each case formed in the sliding jaw tool parts, wherein the partial injection contours, combined in a circumferential direction of the closure cap result in a complete injection contour of the part of the cap body, which is formed by the sliding jaw tool parts, wherein an ejector is further provided assigned to the second mold half, for ejecting the produced closure cap, characterized in that partial injection contours, which differ from one another, are formed in two or more sliding jaw tool parts in such a way that individually producible and exchangeable sliding jaw tool parts are formed by means of a certain partial injection contour, which differs at least from a further sliding jaw tool part, and that a sliding jaw tool part is in contact with the tool core in the ejection direction (r) prior to the ejection of the closure cap on two regions located one behind the other in the ejection direction (r).
An operating system for an architectural covering, said operating system comprising: a first drive section comprising an input and an output, the first drive section including a first planetary gear set with a first sun gear, and a first set of planetary gears meshingly engaged with the first sun gear and carried by a first carrier positioning the first set of planetary gears about the first sun gear; a second drive section comprising an input and an output, said output of said first drive section having said input of said second drive section, the second drive section including a second planetary gear set with a second sun gear, and a second set of planetary gears meshingly engaged with the second sun gear and carried by a second carrier positioning the second set of planetary gears about the second sun gear; a ring gear shared by the first and second drive sections (164, 165), the ring gear meshingly engaged with both the first and second sets of planetary gears,, rotation of either the first set of planetary gears or the second set of planetary gears causing rotation of the ring gear and rotation of the other set of planetary gears,; and a directional control mechanism arranged to selectively lock the ring gear conveying movement between said first and second planetary gear sets (164, 165) to control movement of said output of said planetary gear set upon actuation of said input of said first planetary gear set;wherein said first and second planetary gear sets (164, 165) control rotation of said output of said planetary gear set upon rotation of said input of said first planetary gear set. a first drive section comprising an input and an output, the first drive section including a first planetary gear set with a first sun gear, and a first set of planetary gears meshingly engaged with the first sun gear and carried by a first carrier positioning the first set of planetary gears about the first sun gear; a second drive section comprising an input and an output, said output of said first drive section having said input of said second drive section, the second drive section including a second planetary gear set with a second sun gear, and a second set of planetary gears meshingly engaged with the second sun gear and carried by a second carrier positioning the second set of planetary gears about the second sun gear; a ring gear shared by the first and second drive sections (164, 165), the ring gear meshingly engaged with both the first and second sets of planetary gears,, rotation of either the first set of planetary gears or the second set of planetary gears causing rotation of the ring gear and rotation of the other set of planetary gears,; and a directional control mechanism arranged to selectively lock the ring gear conveying movement between said first and second planetary gear sets (164, 165) to control movement of said output of said planetary gear set upon actuation of said input of said first planetary gear set;wherein said first and second planetary gear sets (164, 165) control rotation of said output of said planetary gear set upon rotation of said input of said first planetary gear set.
A wearable device to be worn by an operator at a flight deck of an aircraft, said wearable device comprising: a communication unit configured to receive aircraft parameters (192, 194) for identifying an aircraft state from an aircraft system; a database configured to store adverse control rules that define at least an adverse control associated with an aircraft state, said adverse control representing a control that should not be activated or modified in the current aircraft state; a first sensor to collect data associated with at least one of movement and location relative to the flight deck of the wearable device; a haptic unit configured to communicate an alert to the operator; and a processing unit coupled to the communication unit, the database, the first sensor and the haptic unit, the processing unit configured to identify a first aircraft state based on the aircraft parameters received via the communication unit, determine at least one of the position and the motion of the wearable unit relative to the flight deck based on the data collected by the first sensor; evaluate an operator intent based on the determined at least one of position and motion of the wearable device relative to the flight deck, initiate a first alert when the operator intent corresponds to the first adverse control during the first aircraft state; and communicate the first alert to the operator via the haptic unit. a communication unit configured to receive aircraft parameters (192, 194) for identifying an aircraft state from an aircraft system; a database configured to store adverse control rules that define at least an adverse control associated with an aircraft state, said adverse control representing a control that should not be activated or modified in the current aircraft state; a first sensor to collect data associated with at least one of movement and location relative to the flight deck of the wearable device; a haptic unit configured to communicate an alert to the operator; and a processing unit coupled to the communication unit, the database, the first sensor and the haptic unit, the processing unit configured to identify a first aircraft state based on the aircraft parameters received via the communication unit, determine at least one of the position and the motion of the wearable unit relative to the flight deck based on the data collected by the first sensor; evaluate an operator intent based on the determined at least one of position and motion of the wearable device relative to the flight deck, initiate a first alert when the operator intent corresponds to the first adverse control during the first aircraft state; and communicate the first alert to the operator via the haptic unit.
Method of manufacturing a housing for an electric motor, which has a sleeve-shaped housing wall extending about a longitudinal axis of the housing and a cover disposed inside the housing wall transverse to the longitudinal axis at a predetermined position between longitudinal ends (18, 20) of the housing wall, wherein a first subspace of the interior of the housing serves to accommodate a stator of the electric motor, and a second subspace of the interior of the housing serves to accommodate a control electronics for the electric motor, and wherein the cover separates the first subspace and the second subspace, the method comprising: providing a precursor of the housing in which the cover is integrally formed with the housing wall and is arranged at one of the longitudinal ends (18, 20) of the housing wall, separating the cover from the housing wall, displacing the cover relative to the housing wall in the direction of the longitudinal axis from the one longitudinal end into the predetermined position, and joining the cover to the housing wall in the predetermined position. providing a precursor of the housing in which the cover is integrally formed with the housing wall and is arranged at one of the longitudinal ends (18, 20) of the housing wall, separating the cover from the housing wall, displacing the cover relative to the housing wall in the direction of the longitudinal axis from the one longitudinal end into the predetermined position, and joining the cover to the housing wall in the predetermined position.
A method of allocating resources for communications in a mobile telecommunication system wherein the mobile telecommunication system provides a wireless interface for a base station to communicate with communications devices (401, 402, 403) and wherein a communications device is operable to transmit signals to another communications device using time and frequency resources of the wireless interface and in accordance with a device-to-device communication protocol, wherein a first pool of the time and frequency resources is allocated to device-to-device communications of a one-to-many type and a second pool of the time and frequency resources is allocated to device-to-device communications of a one-to-one type, the second pool of resources being separate from the first pool, the method comprising: a first communications device transmitting one-to-many messages for communication to a plurality of other communications devices using resources of the first resources pool, a second communications device transmitting one-to-one device-to-device messages using resources of the second resources pool, the second communications device transmitting a first message as a one-to-many message using resources of the first resources pool, the second communications device transmitting a second message as a one-to-one message using resources of the second resources pool, wherein the first message comprises resources allocation information for indicating resources of the second resources pool used for transmitting the second message, determining that the level of collision in the second resources pool is unacceptable based on a comparison with a pool acceptability threshold, and upon determining that the level of collision in the second resources pool is unacceptable, re-allocating the resources between the first and second pools. a first communications device transmitting one-to-many messages for communication to a plurality of other communications devices using resources of the first resources pool, a second communications device transmitting one-to-one device-to-device messages using resources of the second resources pool, the second communications device transmitting a first message as a one-to-many message using resources of the first resources pool, the second communications device transmitting a second message as a one-to-one message using resources of the second resources pool, wherein the first message comprises resources allocation information for indicating resources of the second resources pool used for transmitting the second message, determining that the level of collision in the second resources pool is unacceptable based on a comparison with a pool acceptability threshold, and upon determining that the level of collision in the second resources pool is unacceptable, re-allocating the resources between the first and second pools.
An equipment management method comprising: receiving, by an equipment management apparatus, from a fuel cell system, a state message including an information element indicating a state of the fuel cell system; specifying, by the equipment management apparatus, the recommended time based on the state message, transmitting, by the equipment management apparatus, to a predetermined terminal, a notification message based on the state message, wherein the notification message includes an information element indicating a recommended time for which maintenance of the fuel cell system is recommended to be executed, and wherein the specifying the recommended time includes specifying the recommended time based on the rate at which the temperature of the fuel cell system decreases. receiving, by an equipment management apparatus, from a fuel cell system, a state message including an information element indicating a state of the fuel cell system; specifying, by the equipment management apparatus, the recommended time based on the state message, transmitting, by the equipment management apparatus, to a predetermined terminal, a notification message based on the state message, wherein the notification message includes an information element indicating a recommended time for which maintenance of the fuel cell system is recommended to be executed, and wherein the specifying the recommended time includes specifying the recommended time based on the rate at which the temperature of the fuel cell system decreases.
A splitter apparatus for a gas turbine engine, comprising: a splitter including a generally annular outer wall substantially defining a convex leading edge at a forward end thereof; a generally annular splitter support positioned radially within the outer wall, the splitter support comprising a forward end disposed substantially against a splitter inner surface of the outer wall; and a generally annular first bulkhead spanning between the outer wall and the splitter support, wherein the outer wall, the splitter support, and the first bulkhead collectively substantially define a generally annular splitter plenum; characterized in that the forward end of the splitter support comprises a plurality of circumferentially spaced apart, generally radially oriented metering slots therein; wherein the outer wall comprises an inner portion disposed generally radially inward from the splitter inner surface and extending generally aft, the inner portion comprising a plurality of spaced-apart exit slots; and wherein the splitter plenum, the metering slots, and the exit slots are arranged to conduct airflow from the plenum, through the metering slots substantially against the splitter inner surface, and through the exit slots. a splitter including a generally annular outer wall substantially defining a convex leading edge at a forward end thereof; a generally annular splitter support positioned radially within the outer wall, the splitter support comprising a forward end disposed substantially against a splitter inner surface of the outer wall; and a generally annular first bulkhead spanning between the outer wall and the splitter support, wherein the outer wall, the splitter support, and the first bulkhead collectively substantially define a generally annular splitter plenum;