mhurhangee/ep-ind-claims huggingface dataset:
Device for adjusting pivotable slats (14, 16), which are arranged substantially perpendicularly to one another, of an air vent, comprising a first rotatably mounted adjusting element, wherein - the first adjusting element has at least one cylindrical section, - the first adjusting element has in the at least one cylindrical section at least one guide in which a first displacing element is guided, - at least one slat extending in a first direction is coupled by way of the displacing element with the first adjusting element, and - at least one slat extending in a second direction perpendicular to the first direction is coupled with the first adjusting element, and comprising a second rotatably mounted adjusting element, wherein the first adjusting element is coupled with the second adjusting element and the second adjusting element is coupled with at least one slat extending in the second direction, characterised in that the second adjusting element has at least one cylindrical section and the second adjusting element has in the at least one cylindrical section at least one guide in which an adjusting member for pivotation of the at least one slat extending in the second direction is guided and wherein the axis of rotation of the second adjusting element extends at a right angle to the axis of rotation of the first adjusting element. - the first adjusting element has at least one cylindrical section, - the first adjusting element has in the at least one cylindrical section at least one guide in which a first displacing element is guided, - at least one slat extending in a first direction is coupled by way of the displacing element with the first adjusting element, and - at least one slat extending in a second direction perpendicular to the first direction is coupled with the first adjusting element,
A propeller assembly comprising: a plurality of propeller blades, and a pitch change mechanism including at least one motor; a drive input for driving said plurality of propeller blades to rotate about a central drive axis, said pitch change mechanism being mounted for rotation with said drive input characterized in that the pitch change mechanism is operable upon driving of said motor to rotate said propeller blades about said central drive axis relative to said drive input, and includes a drive input gear transmission (66,62,64,68,56) arranged to resist rotation of said blades so as to change a pitch angle of said blades when said blades are moved relative to said drive input by said pitch change mechanism. a plurality of propeller blades, and a pitch change mechanism including at least one motor; a drive input for driving said plurality of propeller blades to rotate about a central drive axis, said pitch change mechanism being mounted for rotation with said drive input characterized in that the pitch change mechanism is operable upon driving of said motor to rotate said propeller blades about said central drive axis relative to said drive input, and includes a drive input gear transmission (66,62,64,68,56) arranged to resist rotation of said blades so as to change a pitch angle of said blades when said blades are moved relative to said drive input by said pitch change mechanism.
A method of optimizing antenna beam shape of a first directional antenna in a communications system, said method comprising the steps of: - defining at least a handover beam sector and a main beam sector of the antenna beam of said directional antenna; - optimizing a shape of said handover beam sector based on a handover parameter setting of said communications system; and - optimizing a shape of said main beam sector by maximizing the antenna gain of said first directional antenna in said main beam sector. - defining at least a handover beam sector and a main beam sector of the antenna beam of said directional antenna; - optimizing a shape of said handover beam sector based on a handover parameter setting of said communications system; and - optimizing a shape of said main beam sector by maximizing the antenna gain of said first directional antenna in said main beam sector.
A method for isolating a section of a pipe, the method comprising: locating a first plug module of an isolation tool in a pipe in a first mode using a sealing pigging array with no or minimal bypass; urging the first plug module through the pipe in a first direction; securing the first plug module against the pipe; configuring the first plug module in a second mode to permit fluid bypass of the sealing pigging array and the first plug module; locating a second plug module in the pipe while the first plug module is in the second mode and urging the second plug module through the pipe in a second direction opposing the first direction and towards the first plug module such that fluid displaced by location of the second plug module bypasses the first plug module; configuring the first plug module in a third mode to isolate the section of the pipe, retaining pressure on one side of the isolation tool while allowing the other side to be fully vented; securing the second plug module and the first plug module to the pipe to isolate the pipe section between the modules (12,24); and configuring the first plug module in the first mode to prevent fluid bypass of the sealing pigging array for pigging both the first and second plug modules (12,24) to one end of the pipe for removal. locating a first plug module of an isolation tool in a pipe in a first mode using a sealing pigging array with no or minimal bypass; urging the first plug module through the pipe in a first direction; securing the first plug module against the pipe; configuring the first plug module in a second mode to permit fluid bypass of the sealing pigging array and the first plug module; locating a second plug module in the pipe while the first plug module is in the second mode and urging the second plug module through the pipe in a second direction opposing the first direction and towards the first plug module such that fluid displaced by location of the second plug module bypasses the first plug module; configuring the first plug module in a third mode to isolate the section of the pipe, retaining pressure on one side of the isolation tool while allowing the other side to be fully vented; securing the second plug module and the first plug module to the pipe to isolate the pipe section between the modules (12,24); and configuring the first plug module in the first mode to prevent fluid bypass of the sealing pigging array for pigging both the first and second plug modules (12,24) to one end of the pipe for removal.
A sensing membrane, to be applied to a micro-electro-mechanical system device, comprising: a body (11,21,31,41,61): a stress releasing structure (13,13',23,33,33',43,63,63') surrounding the body (11,21,31,41,61) for releasing a membrane residual stress, the stress releasing structure (13,13',23, 33,33',43,63,63') having an elastic ring (130,130',230,630,630'), a plurality of first perforations (13a,13a',23a,33a,33a',43a,63a,63a'), a plurality of second perforations (13b,13b',23b,33b,33b',43b,63b,63b') and a plurality of third perforations (23c,63c), wherein the first perforations (13a,13a',23a,33a,33a', 43a,63a,63a') are located between the body (11,21,31,41,61) and the elastic ring (130,130',230,630,630'), the elastic ring (130,130',230,630,630') is located between the first perforations (13a,13a',23a,33a,33a',43a,63a,63a') and the second perforations (13b,13b',23b,33b,33b',43b,63b,63b'), and each of the third perforations (23c,63c) is located between two neighbouring first perforations (13a,13a',23a,33a,33a',43a,63a,63a') and one of the second perforations (13b,13b',23b,33b,33b',43b,63b,63b') and the third perforations (23c,63c) are arranged in a radiated pattern at the inner rim of the elastic ring (130,130',230,630,630'), each of the third perforations is a rectangle, and a longitudinal direction of each of the third perforations passes through a substantial center of the body for releasing the membrane residual stress in a tangential direction of the body; and a connecting portion (15,25,35,35',45,65) for connecting the stress releasing structure (13,13',23,33,33',43,63,63') and a substrate of the MEMS device. a body (11,21,31,41,61): a stress releasing structure (13,13',23,33,33',43,63,63') surrounding the body (11,21,31,41,61) for releasing a membrane residual stress, the stress releasing structure (13,13',23, 33,33',43,63,63') having an elastic ring (130,130',230,630,630'), a plurality of first perforations (13a,13a',23a,33a,33a',43a,63a,63a'), a plurality of second perforations (13b,13b',23b,33b,33b',43b,63b,63b') and a plurality of third perforations (23c,63c), wherein the first perforations (13a,13a',23a,33a,33a', 43a,63a,63a') are located between the body (11,21,31,41,61) and the elastic ring (130,130',230,630,630'), the elastic ring (130,130',230,630,630') is located between the first perforations (13a,13a',23a,33a,33a',43a,63a,63a') and the second perforations (13b,13b',23b,33b,33b',43b,63b,63b'), and each of the third perforations (23c,63c) is located between two neighbouring first perforations (13a,13a',23a,33a,33a',43a,63a,63a') and one of the second perforations (13b,13b',23b,33b,33b',43b,63b,63b') and the third perforations (23c,63c) are arranged in a radiated pattern at the inner rim of the elastic ring (130,130',230,630,630'), each of the third perforations is a rectangle, and a longitudinal direction of each of the third perforations passes through a substantial center of the body for releasing the membrane residual stress in a tangential direction of the body; and a connecting portion (15,25,35,35',45,65) for connecting the stress releasing structure (13,13',23,33,33',43,63,63') and a substrate of the MEMS device.
An actuator comprising: a motor controller; a motor drive configured to receive power from a power source and to receive a command from the motor controller; at least one motor winding configured to receive a voltage from the motor drive; at least one or more sensors configured to detect a parameter associated with the actuator and communicate at least one signal containing information about the detected parameter to the motor controller; and a bus dump circuit having a resistor, the circuit configured to dissipate regenerative energy; wherein the motor controller is configured to process the at least one signal from the one or more sensors and provide control of the actuator; and characterized in that the actuator is configured to apply an additive regeneration dissipation control, RDC, voltage to the command from the motor controller, wherein the additive RDC voltage is configured to be adjusted using the temperature of the resistor in the bus dump circuit. a motor controller; a motor drive configured to receive power from a power source and to receive a command from the motor controller; at least one motor winding configured to receive a voltage from the motor drive; at least one or more sensors configured to detect a parameter associated with the actuator and communicate at least one signal containing information about the detected parameter to the motor controller; and a bus dump circuit having a resistor, the circuit configured to dissipate regenerative energy; wherein the motor controller is configured to process the at least one signal from the one or more sensors and provide control of the actuator; and characterized in that the actuator is configured to apply an additive regeneration dissipation control, RDC, voltage to the command from the motor controller, wherein the additive RDC voltage is configured to be adjusted using the temperature of the resistor in the bus dump circuit.
A method of repairing an airfoil of a compressor blade (80; 122) of a gas turbine engine, the method comprising: developing a suggested blend repair to the airfoil comprising the steps of: (a) storing history with regard to a particular airfoil of a compressor blade (80; 122) in a particular gas turbine engine, wherein the history includes a surge history for the gas turbine engine; (b) taking information with regard to new damage to the particular airfoil; (c) reaching an initial blend recommendation based upon step (b); (d) assessing whether the initial blend recommendation of step (c) would be appropriate to repair the new damage based upon a consideration of steps (a) - (c); and (e) reporting a final blend recommendation, wherein the final blend recommendation is performed utilizing borescopic blending. developing a suggested blend repair to the airfoil comprising the steps of: (a) storing history with regard to a particular airfoil of a compressor blade (80; 122) in a particular gas turbine engine, wherein the history includes a surge history for the gas turbine engine; (b) taking information with regard to new damage to the particular airfoil; (c) reaching an initial blend recommendation based upon step (b); (d) assessing whether the initial blend recommendation of step (c) would be appropriate to repair the new damage based upon a consideration of steps (a) - (c); and (e) reporting a final blend recommendation, (a) storing history with regard to a particular airfoil of a compressor blade (80; 122) in a particular gas turbine engine, wherein the history includes a surge history for the gas turbine engine; (b) taking information with regard to new damage to the particular airfoil; (c) reaching an initial blend recommendation based upon step (b); (d) assessing whether the initial blend recommendation of step (c) would be appropriate to repair the new damage based upon a consideration of steps (a) - (c); and (e) reporting a final blend recommendation, wherein the final blend recommendation is performed utilizing borescopic blending.
A system comprising an apparatus for providing a clock signal having a predefined average clock rate, the apparatus comprising: means for providing a reference signal; means for generating random numbers at a predefined distribution; means for determining a difference between at least two subsequently generated random numbers; and means for dividing the reference signal to generate the clock signal based on the difference between the at least two subsequently generated random numbers; wherein a time difference between a clock cycle and a subsequent clock cycle of the clock signal is irregular, wherein the number of cycles in the reference signal between at least two clock cycles in the clock signal corresponds to the difference between the at least two subsequently generated random numbers. means for providing a reference signal; means for generating random numbers at a predefined distribution; means for determining a difference between at least two subsequently generated random numbers; and means for dividing the reference signal to generate the clock signal based on the difference between the at least two subsequently generated random numbers; wherein a time difference between a clock cycle and a subsequent clock cycle of the clock signal is irregular, wherein the number of cycles in the reference signal between at least two clock cycles in the clock signal corresponds to the difference between the at least two subsequently generated random numbers.
A method for inspecting a blow molded container having a finish (20; 120), a base (80; 180; 310), a body (34; 134) between the finish (20; 120) and base (80; 180; 310), and etching (42; 142; 342) at the base (80; 180; 310), the method comprising: identifying where on the base (80; 180; 310) the etching (42; 142; 342) is located; designating the base (80; 180; 310) as accurately blow molded if the etching (42; 142; 342) is located at a predetermined location of the base (80; 180; 310); and designating the base (80; 180; 310) as not accurately blow molded if the etching (42; 142; 342) is not located at the predetermined location of the base (80; 180; 310); wherein the etching is confined to a flexible diaphragm of the base (80; 180; 310) arranged between a center push-up portion (82; 182; 382) at an axial center of the base (80; 180; 310) and a heel at an outer periphery of the base (80; 180; 310), the etching (42; 142; 342) extends continuously around an axial center of the base (80; 180; 310), and the etching (42; 142; 342) is configured to reduce the weight of the base at the flexible diaphragm of the base (80; 180; 310) to facilitate flexing of the flexible diaphragm. identifying where on the base (80; 180; 310) the etching (42; 142; 342) is located; designating the base (80; 180; 310) as accurately blow molded if the etching (42; 142; 342) is located at a predetermined location of the base (80; 180; 310); and designating the base (80; 180; 310) as not accurately blow molded if the etching (42; 142; 342) is not located at the predetermined location of the base (80; 180; 310); wherein the etching is confined to a flexible diaphragm of the base (80; 180; 310) arranged between a center push-up portion (82; 182; 382) at an axial center of the base (80; 180; 310) and a heel at an outer periphery of the base (80; 180; 310), the etching (42; 142; 342) extends continuously around an axial center of the base (80; 180; 310), and the etching (42; 142; 342) is configured to reduce the weight of the base at the flexible diaphragm of the base (80; 180; 310) to facilitate flexing of the flexible diaphragm.
A system for monitoring one or more passenger seats of a vehicle, the system comprising: at least one sensor (32, 33; 56a, 56b, 56c) configured to monitor an occupancy status for each of the one or more passenger seats; a first display unit (31; 54a, 54b, 54c) configured to: display an occupancy condition for each of the one or more passenger seats, and determine the occupancy condition for each of the one or more passenger seats based on the occupancy status for each of the one or more passenger seats over a predefined time period; and a second display unit (45; 55a, 55b, 55c) configured to: receive reservation conditions for each of the one or more passenger seats, and display a reservation condition for each of the one or more passenger seats; wherein the first and second display units (31,45) are positioned proximal to the one or more passenger seats. at least one sensor (32, 33; 56a, 56b, 56c) configured to monitor an occupancy status for each of the one or more passenger seats; a first display unit (31; 54a, 54b, 54c) configured to: display an occupancy condition for each of the one or more passenger seats, and determine the occupancy condition for each of the one or more passenger seats based on the occupancy status for each of the one or more passenger seats over a predefined time period; and a second display unit (45; 55a, 55b, 55c) configured to: receive reservation conditions for each of the one or more passenger seats, and display a reservation condition for each of the one or more passenger seats; wherein the first and second display units (31,45) are positioned proximal to the one or more passenger seats.
Commercial vehicle trailer, in particular a refrigerated semi-trailer or refrigerated trailer, comprising a cooling device for cooling a cargo space, which device has a user interface for inputting and displaying at least one operating variable, characterized in that the commercial vehicle trailer has a control unit which is arranged outside an electronic brake control means and is coupled to at least one remote action unit, the user interface and the control unit being connected to one another via a communication interface, the user interface being designed for data output from the control unit and data input to the control unit.
An electrical connector comprising: signal terminals and a ground terminal (14, 15); an insulating housing for holding the signal terminals and the ground terminal (14, 15); and a conductive shell covering at least a part of side outer peripheries of the signal terminals and the ground terminal (14, 15), wherein the signal terminals form pairs, the ground terminal (14, 15) is disposed between the pairs of signal terminals, and a part (14e, 15e) of the ground terminal (14, 15) is in direct contact with an inner wall (31a, 32a, 60a) of the conductive shell, characterized in that a load is applied to a part of the ground terminal (14, 15) in direct contact with the inner wall of the conductive shell toward a side in contact with the inner wall (31a, 32a, 60a) of the conductive shell to bring the part of the ground terminal (14, 15) into direct contact with the conductive shell. signal terminals and a ground terminal (14, 15); an insulating housing for holding the signal terminals and the ground terminal (14, 15); and a conductive shell covering at least a part of side outer peripheries of the signal terminals and the ground terminal (14, 15), wherein the signal terminals form pairs, the ground terminal (14, 15) is disposed between the pairs of signal terminals, and a part (14e, 15e) of the ground terminal (14, 15) is in direct contact with an inner wall (31a, 32a, 60a) of the conductive shell, characterized in that a load is applied to a part of the ground terminal (14, 15) in direct contact with the inner wall of the conductive shell toward a side in contact with the inner wall (31a, 32a, 60a) of the conductive shell to bring the part of the ground terminal (14, 15) into direct contact with the conductive shell.