mhurhangee/patent-ind-claim-en huggingface dataset:
An adaptor , comprising: an input segment of a conductive material, the input segment provided for coupling to an oscillator arrangement ; a first coaxial portion having a first diameter, the first coaxial portion including a first inner conductor coupled to the input segment and a first outer shielding segment ; a second coaxial portion having a second diameter, the second coaxial portion including a second inner conductor and a second outer shielding segment ; and a capping portion coupled to the second coaxial portion to electrically couple the second inner conductor and the second outer shielding segment , the capping portion adapted for being disposed within a waveguide , characterized in that the second diameter is different from the first diameter, and the capping portion includes an opening aligned with the inner conductor to provide an air gap at an end of the inner conductor . an input segment of a conductive material, the input segment provided for coupling to an oscillator arrangement ; a first coaxial portion having a first diameter, the first coaxial portion including a first inner conductor coupled to the input segment and a first outer shielding segment ; a second coaxial portion having a second diameter, the second coaxial portion including a second inner conductor and a second outer shielding segment ; and a capping portion coupled to the second coaxial portion to electrically couple the second inner conductor and the second outer shielding segment , the capping portion adapted for being disposed within a waveguide , characterized in that the second diameter is different from the first diameter, and the capping portion includes an opening aligned with the inner conductor to provide an air gap at an end of the inner conductor .
A planetary push-pull electric motor, hereinafter "PPPEM" , comprising: a ring stator fixedly mounted on a central axis of said PPPEM, wherein said central axis defines a centerline of said ring stator ; a planetary rotor arranged to be magnetically movable, rotatably mounted on an eccentric rotor axis in respect to said ring stator centerline ; whereby said planetary rotor and said stator are equipped with toothed gear ; a series of electromagnets radially mounted about said ring stator centerline for generating radial magnetic force upon the magnetic fields of said planetary rotor when said series of electromagnets is activated; and a means for transferring rotation of said eccentric planetary rotor axis to directly power an output shaft of said PPPEM, wherein when said series of electromagnets is activated, radial push-pull magnetic forces are generated, magnetically impelling said planetary rotor in proximal radial contact with at least one electromagnet in said series such that said planetary rotor pivots from one of said proximal tangential contact to an adjacent one in sequence, effecting a continuous rolling motion of said planetary rotor about said eccentric rotor axis and creating a rotary moment, such motion being translated into rotational motion which, when applied to said output shaft of said PPPEM utilizing said rotation transferring means, provides a source of power output from said PPPEM; and characterized in that said rotor axis is radially loaded upon said stator such that the pull forces pull said planetary rotor toward said stator in order to ensure zero backlash. a ring stator fixedly mounted on a central axis of said PPPEM, wherein said central axis defines a centerline of said ring stator ; a planetary rotor arranged to be magnetically movable, rotatably mounted on an eccentric rotor axis in respect to said ring stator centerline ; whereby said planetary rotor and said stator are equipped with toothed gear ; a series of electromagnets radially mounted about said ring stator centerline for generating radial magnetic force upon the magnetic fields of said planetary rotor when said series of electromagnets is activated; and a means for transferring rotation of said eccentric planetary rotor axis to directly power an output shaft of said PPPEM, wherein when said series of electromagnets is activated, radial push-pull magnetic forces are generated, magnetically impelling said planetary rotor in proximal radial contact with at least one electromagnet in said series such that said planetary rotor pivots from one of said proximal tangential contact to an adjacent one in sequence, effecting a continuous rolling motion of said planetary rotor about said eccentric rotor axis and creating a rotary moment, such motion being translated into rotational motion which, when applied to said output shaft of said PPPEM utilizing said rotation transferring means, provides a source of power output from said PPPEM; and characterized in that said rotor axis is radially loaded upon said stator such that the pull forces pull said planetary rotor toward said stator in order to ensure zero backlash.
An aircraft surface having a deicing module for an aircraft , the aircraft surface suitable for defining an interior of an aircraft wing , the deicing module comprising: a casing operably coupled to the aircraft surface ; at least two moveable members located between the casing and the aircraft surface , wherein the at least two moveable members includes multiple moveable members in the form of a first moveable member and a second moveable member, and wherein the first moveable member and the second moveable member are opposing moveable members that move in opposite directions; a set of tracks configured to be located in the interior of the aircraft wing , wherein the set of tracks is configured to guide the multiple moveable members; wherein each of the at least two moveable members comprises an upper portion and a lower portion , the lower portion being received within a track of the set of tracks , the upper portion being configured to abut the casing and comprising a curved face and a tip ; the deicing module further comprising; a driving mechanism comprising a cable system comprising a cable operably coupled to the at least two movable members , wherein the driving mechanism is configured to move the at least two moveable members beneath the casing such that the at least two moveable members distort the casing to an extent sufficient to release accumulations of ice thereon. a casing operably coupled to the aircraft surface ; at least two moveable members located between the casing and the aircraft surface , wherein the at least two moveable members includes multiple moveable members in the form of a first moveable member and a second moveable member, and wherein the first moveable member and the second moveable member are opposing moveable members that move in opposite directions; a set of tracks configured to be located in the interior of the aircraft wing , wherein the set of tracks is configured to guide the multiple moveable members; wherein each of the at least two moveable members comprises an upper portion and a lower portion , the lower portion being received within a track of the set of tracks , the upper portion being configured to abut the casing and comprising a curved face and a tip ; the deicing module further comprising; a driving mechanism comprising a cable system comprising a cable operably coupled to the at least two movable members , wherein the driving mechanism is configured to move the at least two moveable members beneath the casing such that the at least two moveable members distort the casing to an extent sufficient to release accumulations of ice thereon.
A gas turbine engine (20; 120; 220) comprising: a drive turbine (36; 136; 236) configured to drive a fan section (22; 122; 222); a speed change mechanism (38; 138; 238) connected to the drive turbine (36; 136; 236) and located immediately aft of the drive turbine (36; 136; 236) and aft of the fan section (22; 122; 222), an output of the speed change mechanism (38; 138; 238) connected to the fan section (22; 122; 222), wherein the drive turbine (36; 136; 236) is a fixed stator turbine and the speed change mechanism (38; 138; 238) is an epicyclical gearbox, characterized in that : a turbine drive shaft (45; 145; 245) connects the drive turbine (36; 136; 236) to a sun gear of the epicyclical gearbox. a drive turbine (36; 136; 236) configured to drive a fan section (22; 122; 222); a speed change mechanism (38; 138; 238) connected to the drive turbine (36; 136; 236) and located immediately aft of the drive turbine (36; 136; 236) and aft of the fan section (22; 122; 222), an output of the speed change mechanism (38; 138; 238) connected to the fan section (22; 122; 222), wherein the drive turbine (36; 136; 236) is a fixed stator turbine and the speed change mechanism (38; 138; 238) is an epicyclical gearbox, characterized in that : a turbine drive shaft (45; 145; 245) connects the drive turbine (36; 136; 236) to a sun gear of the epicyclical gearbox.
Handle for a cover of a medical sieve basket, comprising a base body comprising or forming a handle bar and a holding portion adjoining the handle bar , and at least one eyelet-shaped or curved fixing lug arranged at an end of the holding portion opposite the handle bar for pivot mounting of the handle , characterized in that the base body including the handle bar and the holding portion consists of a planar metal sheet which, at the end of the holding portion opposite the handle bar , is formed as a single piece of material into at least one lug-like projection extending it in a direction opposite the handle bar , said projection being bent to form the at least one fixing lug with respect to the holding portion , preferably to form an eyelet, so that the at least one bent fixing lug is formed over its width for pivot mounting of the handle . a base body comprising or forming a handle bar and a holding portion adjoining the handle bar , and at least one eyelet-shaped or curved fixing lug arranged at an end of the holding portion opposite the handle bar for pivot mounting of the handle , characterized in that the base body including the handle bar and the holding portion consists of a planar metal sheet which, at the end of the holding portion opposite the handle bar , is formed as a single piece of material into at least one lug-like projection extending it in a direction opposite the handle bar , said projection being bent to form the at least one fixing lug with respect to the holding portion , preferably to form an eyelet, so that the at least one bent fixing lug is formed over its width for pivot mounting of the handle .
A modular pressure washing system , comprising a base unit and an accessory unit , wherein the accessory unit is removably attachable to the base unit , the base unit comprising a housing a pump a motor a power source, an input valve and an output valve , wherein the housing contains the pump and the motor ,wherein the housing at least partially contains the power source , wherein the motor is operatively-connected to the power source , wherein the pump is operatively-connected to the motor , wherein the pump is fluidly connected to the input valve , and wherein the pump is fluidly connected to the output valve and the accessory unit is a frame with wheels ; characterized in that the housing further comprises a top portion and the power source is a plurality of electric batteries located within the top portion , the top portion contains a door which opens to allow access to the batteries . a base unit and an accessory unit , wherein the accessory unit is removably attachable to the base unit , the base unit comprising a housing a pump a motor a power source, an input valve and an output valve , wherein the housing contains the pump and the motor ,wherein the housing at least partially contains the power source , wherein the motor is operatively-connected to the power source , wherein the pump is operatively-connected to the motor , wherein the pump is fluidly connected to the input valve , and wherein the pump is fluidly connected to the output valve and the accessory unit is a frame with wheels ; characterized in that the housing further comprises a top portion and the power source is a plurality of electric batteries located within the top portion , the top portion contains a door which opens to allow access to the batteries .
A method of controlling an access attempt to a network by a user equipment , UE, in a wireless communication system, the method comprising: receiving first mapping information for at least one access category defined by an operator of the network; receiving barring information; determining an access category for an access attempt type that is associated with the access attempt from among a plurality of access categories based on mapping information; and determining whether to perform the access attempt to the network based on (i) the determined access category for the access attempt type that is associated with the access attempt and (ii) the barring information, wherein the plurality of access categories includes (i) the at least one access category defined by the operator of the network and (ii) access categories defined in a standard specification for the wireless communication system, wherein the mapping information defines mapping relation between the plurality of access categories and a plurality of access attempt types, respectively, wherein the mapping information includes (i) the first mapping information for the at least one access category defined by the operator of the network and (ii) second mapping information for the access categories defined in the standard specification, wherein the at least one access category defined by the operator of the network includes an access category for a network slice, and wherein the first mapping information at least defines mapping relation between the access category for the network slice and the network slice. receiving first mapping information for at least one access category defined by an operator of the network; receiving barring information; determining an access category for an access attempt type that is associated with the access attempt from among a plurality of access categories based on mapping information; and determining whether to perform the access attempt to the network based on (i) the determined access category for the access attempt type that is associated with the access attempt and (ii) the barring information, wherein the plurality of access categories includes (i) the at least one access category defined by the operator of the network and (ii) access categories defined in a standard specification for the wireless communication system, wherein the mapping information defines mapping relation between the plurality of access categories and a plurality of access attempt types, respectively, wherein the mapping information includes (i) the first mapping information for the at least one access category defined by the operator of the network and (ii) second mapping information for the access categories defined in the standard specification, wherein the at least one access category defined by the operator of the network includes an access category for a network slice, and wherein the first mapping information at least defines mapping relation between the access category for the network slice and the network slice.
A method of modulating cooling of gas turbine engine components in a gas turbine engine comprising the steps of: identifying an input indicative of a usage rate for at least a first gas turbine engine component of a plurality of gas turbine engine components; operating a cooling system (100;550) for at least the first gas turbine engine component; and moving said cooling system (100;550) from a higher cooling potential mode to a lower cooling potential mode once a set point is reached, and the set point is selected based upon said identified usage rate; characterised in that the usage rate is a maintenance condition of said at least a first gas turbine engine component. identifying an input indicative of a usage rate for at least a first gas turbine engine component of a plurality of gas turbine engine components; operating a cooling system (100;550) for at least the first gas turbine engine component; and moving said cooling system (100;550) from a higher cooling potential mode to a lower cooling potential mode once a set point is reached, and the set point is selected based upon said identified usage rate; characterised in that the usage rate is a maintenance condition of said at least a first gas turbine engine component.
A system , comprising: a power plant system including: a gas turbine system having a turbine component ; and at least one computing device in communication with the power plant system , the at least one computing device configured to control the power plant system by performing processes including: defining a turbine inlet temperature range for a combustion gas flowing through the turbine component of the gas turbine system , the turbine inlet temperature range based on a desired operational load for the power plant system ; determining a fuel cost range based on the turbine inlet temperature range; determining a maintenance cost range based on the turbine inlet temperature range; calculating a desired turbine inlet temperature range for the combustion gas flowing through the turbine component of the gas turbine system based on the determined fuel cost range and the determined maintenance cost range; and adjusting an actual turbine inlet temperature of the combustion gas flowing through the turbine component to be within the calculated, desired turbine inlet temperature range for the combustion gas flowing through the turbine component . a gas turbine system having a turbine component ; and at least one computing device in communication with the power plant system , the at least one computing device configured to control the power plant system by performing processes including: defining a turbine inlet temperature range for a combustion gas flowing through the turbine component of the gas turbine system , the turbine inlet temperature range based on a desired operational load for the power plant system ; determining a fuel cost range based on the turbine inlet temperature range; determining a maintenance cost range based on the turbine inlet temperature range; calculating a desired turbine inlet temperature range for the combustion gas flowing through the turbine component of the gas turbine system based on the determined fuel cost range and the determined maintenance cost range; and adjusting an actual turbine inlet temperature of the combustion gas flowing through the turbine component to be within the calculated, desired turbine inlet temperature range for the combustion gas flowing through the turbine component . defining a turbine inlet temperature range for a combustion gas flowing through the turbine component of the gas turbine system , the turbine inlet temperature range based on a desired operational load for the power plant system ; determining a fuel cost range based on the turbine inlet temperature range; determining a maintenance cost range based on the turbine inlet temperature range; calculating a desired turbine inlet temperature range for the combustion gas flowing through the turbine component of the gas turbine system based on the determined fuel cost range and the determined maintenance cost range; and adjusting an actual turbine inlet temperature of the combustion gas flowing through the turbine component to be within the calculated, desired turbine inlet temperature range for the combustion gas flowing through the turbine component .
A battery formation system comprising: a battery module ; an energy storage system electrically coupled to the battery module, the energy storage system operable in a first operating state in which energy is transferred from the energy storage system to the battery module to charge the battery module, and a second operating state in which energy is transferred from the battery module to the energy storage system to discharge the battery module; a power source electrically coupled to the energy storage system and configured to transfer energy from the power source to the energy storage system based on an amount of stored energy in the energy storage system; and a controller operably coupled to the battery module and configured to monitor and control a charging state of the battery module. a battery module ; an energy storage system electrically coupled to the battery module, the energy storage system operable in a first operating state in which energy is transferred from the energy storage system to the battery module to charge the battery module, and a second operating state in which energy is transferred from the battery module to the energy storage system to discharge the battery module; a power source electrically coupled to the energy storage system and configured to transfer energy from the power source to the energy storage system based on an amount of stored energy in the energy storage system; and a controller operably coupled to the battery module and configured to monitor and control a charging state of the battery module.
Use of a color conversion sheet for agriculture, wherein said color conversion sheet comprises at least one inorganic fluorescent material having the peak emission light wavelength in the range from 660 nm to 730 nm, and a matrix material comprising a polymer selected from the group consisting of photosetting polymer, a thermosetting polymer, a thermoplastic polymer, and a combination of thereof.
A reinforcing strip for a moulded body made of an injectable moulding compound, comprising a strip-shaped base body made of an aluminium-magnesium alloy according to the alloy group EN AW-5xxx, characterized in that the aluminium-magnesium alloy of the strip-shaped base body has a yield strength and/or a tensile strength which is higher and/or lower than the yield strength and/or the tensile strength of a corresponding aluminium-magnesium alloy according to the alloy group EN AW-5xxx.
A cutting frame including a plurality of cutters for cutting one or more kinds of rectangular unit pieces having a relatively small size from a rectangular base material at a predetermined inclination, the cutters being mounted or formed in the cutting frame such that the cutters correspond to the rectangular unit pieces, characterized in that the cutters are mounted or formed in the cutting frame based on an offset array structure of the rectangular unit pieces in which the rectangular unit pieces are offset from one another such that each side of any arbitrary rectangular unit piece is adjacent to not more than one different rectangular unit piece , wherein the rectangular unit pieces are inclined at an angle of 20 to 70 degrees, wherein at least some combinations of adjacent four rectangular unit pieces form an approximately rectangular-shaped island-type residue defined by the respective sides of the rectangular unit pieces, wherein the width ('cutting width') between the upper end vertex of the uppermost row rectangular unit pieces and the lower end vertex of the lowermost row rectangular unit pieces is 95% to 100% of the effective width of the base material.