bhlim/patentmatch_for_finetuning huggingface dataset:
Patent claim: A gazed virtual object identification determination module GVOIDM according to claim 1 wherein said Object identification Retrieving Means OIRM is configured to retrieve said object identification from an alpha channel associated with said position at said display matching said gaze coordinate P.

Related passage: Figure 1B illustrates another architecture diagram of a system embodiment according to the present invention in an exemplary distributed form.A gaze capture module 11 and gazed virtual object identification module 13 are shown comprised by a first entity 108 for instance a first terminal.A plurality of gaze distance determination modules 12 with parallel behaviour and a virtual object modification module 15A are shown comprised by a second entity 101 and may for instance be implemented as a static library.The skilled person will understand that this second entity need not be the same entity for the gaze distance determination modules 12 and the virtual object modification module 15A but that these modules may be comprised by separate entities shared libraries.Also the skilled person will understand that these modules may be otherwise implemented for instance as interface implementations by one or more virtual object or rather program code instances representing virtual objects.A gaze translucency algorithm module 14 is shown comprised by a third entity for instance a central server 109.Further another virtual object modification module 15B is shown comprised by a fourth entity 102.The skilled person will appreciate that the interrelationships of these modules are analogous to those described above for figure 1A.Moreover the skilled person will appreciate that the arrows shown to cross from one entity to another may in practice be implemented as communications between the separate distributed entities via a network using various network modules configured to transmit and receive information to each other.
Patent claim: A computer program product comprising code tangibly embodied thereon that when executed on a processor causes the processor to perform a method 40 according to one of claims 1 to 6.

Related passage: In a case where a load is constant a current on rotation coordinates that is output from the coordinate converter 8 is constant but if the load pulsates by a frequency of two times the voltage that is applied to the AC motor 6 a current on rotation coordinates pulsates at the same frequency and the components of two times the applied voltage frequency have a value other than zero.Thus if a fault phase is determined using the frequency components of the current on rotation coordinates there is a case where stepout and false detection is performed in a case where a load pulsates.In contrast to this the current phase on rotation coordinates is constant even in a case where the load pulsates and the components of two times the applied voltage frequency are zero.Thus by using the frequency components of the current phase on rotation coordinates a false detection is not performed even in a case where the load pulsates and it is possible to perform a constant fault phase detection.
Patent claim: The slide rail assembly of claim 5 or 6 characterized in that the rear blocking part 27 of the guide rail 22 is extended with a rear supporting part 27a an upper edge of the rear supporting part 27a is configured to abut against the fixing member 43 on the chassis 42.

Related passage: The said recess may be provided with stops for stopping the second slide rail 20 in the first slide rail.It can be seen from Fig.3 that on the first web plate 11 of the first slide rail 10 there is punched out a first protruding panel 16 protruding toward the back surface of the first web plate 11 and extending from the back surface of the first web plate 11 into the recess 22.When the second slide rail 20 slides within the first slide rail 10 the third end surface 223 and the fourth end surface 224 form stop means for stopping the movement of the first protruding panel 16 in the length direction preventing the over insertion of the second slide rail 20 when being retracted into the first slide rail 10 and the pulling off of the second slide rail 20 when being deployed from the first slide rail 10.Meanwhile the distances between the first end surface 23 and the third end surface 223 and between the second end surface 24 and the fourth end surface 224 determines the length of the overlapping portion of the second slide rail 20 and the first slide rail 10.
Patent claim: A method for maintenance operation of an elevator the elevator comprising a car 10 moving upwards and downwards between landings L1 in a shaft 20 being provided with a pit 22 at a bottom of the shaft 20 the method comprising unlocking and opening landing door 25 at a lowermost landing L1 manually whereby normal operation of the car 10 is prevented activating a first stop button P1 at the lowermost landing L1 in the shaft 20 whereby a safety circuit S1 S2 of the elevator is opened so that operation of the car 10 is prevented entering into the shaft 20 from the lowermost landing L1 closing the landing door 25 and climbing down to the bottom of the pit 22 turning a drive switch SW1 in a maintenance control unit 100 positioned in the pit 22 into a maintenance drive mode whereby the first stop button P1 is bypassed so that the car 10 can be driven in maintenance mode from the maintenance control unit 100 upwards and downwards in the shaft 20.

Related passage: FIG.1 shows an elevator arranged within a building.The elevator comprises a car 1 and a counterweight 5 which are supported on a load carrying element 3 by pulleys 6.The load carrying element 3 is fixed at either end and is driven by a traction sheave 4 to vertically displace the car 1 and the counterweight 5 in opposite directions along associated guide rails not shown mounted within a shaft 2.When the car 1 is level with any landing passengers can enter or exit the car 1 through the respective landing door 13a 13b 13c 13d.
Patent claim: A downhole system according to any of claims 711 wherein the well tubular metal structure comprises two annular barriers each annular barrier comprisinga tubular part mounted as part of the first well tubular metal structurean expandable tubular surrounding the tubular part each end section of the expandable tubular being connected with the tubular partan annular barrier space between the tubular part and the expandable tubular andan expansion opening in the tubular part through which pressurised fluid passes for expanding the expandable tubular and bringing the annular barrier from an unexpanded position to an expanded position.

Related passage: As shown in Fig.14 the detection tool 50 in the downhole system 100 may further comprise a downhole driving unit 73 an anchoring tool section 74 having radial extension anchors 75 and a key tool 76 having keys 77 engaging grooves in the completion component 1.The key tool 76 is operated by a stroking tool 79.The detection tool 50 is powered through a wireline 78.The key tool 76 is able to both open and close a completion component in one run that is without the tool having to be retracted from the well.By the detection tool 50 and the key tool being in the same tool string the key tool can change the position of the completion component and the detection tool can verify that the performed operation of the key tool has resulted in the planned position change of the completion component.
Patent claim: The method according to claim 1 characterized in that the first fine particles 101 are obtained by emulsion polymerization of at least a binder resin.

Related passage: Three parts by weight of the microcapsules 1 part by weight of a charge control agent E1 manufactured by NIPPON KAYAKU CO.LTD.and 1 part by weight of polypropylene wax as a wax component were dispersed in 500 parts by weight of an acetone solution prepared by dissolving 10 wt of styrenebutylacrylate acrylate content 40 wt as a polymer filler and 10 wt of cholic acid.This dispersion was sprayed to form a powder having an average particle size of about 10 m.One wt of hydrophobic silica was externally added to the resultant powder to manufacture a black electrophotographic toner.
Patent claim: The airfoil of any of the preceding claims wherein at least a portion of the core ceramic fibers comprise a plurality of multifiber tows.

Related passage: FIG.3 is a flow chart illustrating a method of manufacture of a CMC turbine blade of the present invention using a method of silicon carbidesilicon carbide CMC manufacture known as a slurry cast melt infiltration process slurry cast MI.Both the core insert sections and outer shell sections of the CMC turbine blade may be manufactured using the slurry cast MI process.
Patent claim: The method according to any one of claims 5 to 8 wherein in the step 1 the conditions under which the supporter contacts with the carbon source include pressure of 0.11MPa and time of 0.16h the carbon deposition reaction happens in an oxygencontaining atmosphere the temperature of the carbon deposition reaction is 100C500C and the time of the carbon deposition reaction is 20200h the oxygen content in the oxygencontaining atmosphere is 10100vol and the oxygencontaining atmosphere is selected from a mixture of air or oxygen and an inert gas.

Related passage: The organic compound that is a source from which the carbonaceous substance is derived is not necessarily required to be the molding additives and may be other organic compounds as long as it can produce the predetermined amount of the carbonaceous substance on the catalyst.However by adopting the method of allowing the molding additivesderived carbonaceous substance to remain in the predetermined amount the hydrotreating catalyst of the present embodiment can be obtained without largely changing the conventional method for preparing a catalyst except for adjusting conditions for calcination of the catalyst support and calcination of the catalyst precursor described later thus this method is preferably adopted.
Patent claim: The method 200 of claim 14 wherein the electrical damper 124 comprises a resistor 125 wherein the method further comprises integrating the electrical damper 124 into a power converter 122 of the generator 114 and controlling via the controller 120 the resistor 125 so as to prohibit the generator 114 from being a constant power load at frequencies of torsional interaction.

Related passage: Figure 1 schematically illustrates a gas turbine engine drive schematic for a synchronous generator that utilizes a load damper.Figure 2 schematically illustrates a control configuration for the load damper.Figure 3a schematically illustrates an example electric load damper.Figure 3b schematically illustrates another example second load damper.Figure 4 is a graph showing the effect of load damping on generator rotational speed.Figure 5 is a graph showing the effect of damping on torsional oscillation.Figure 6 is a graph showing the effect of load damping on power dissipation.Figure 7 is a graph showing the effect of load damping on energy dissipation.
Patent claim: Printing unit comprising at least a printing head 20 a support plate 15 to which said printing head 20 is associated and at least one positioning member 45a 45b associated to the support plate 15 and to the printing head 20 to adjust the reciprocal position of the latter two characterized in that said support plate 15 defines an adjustment planewith respect to which said printing head 20 is positioned and in that said positioning member 45a 45b comprises at least an actuation device 50 which can be selectively actuated above the adjustment planeand a kinematic conversion device 46 configured to convert the actuation of said actuation device 50 into an adjustment of the position of the printing head 20 with respect to the support plate 15 in at least one direction lying on the adjustment planesaid actuation device 50 being associable with a cam element 48 able to engage in a suitably shaped seating 58 made in said printing head 20.

Related passage: The eccentric shaft 11a is thereby eccentrically rotated to move the positioning block 10 causing the positioning pin 9 fastenedthereto to push the V shaped flange 5 thereby displacing the line head 3 in the nozzle row direction.There is then set a displacement that is equal to one half of the nozzle pitch namely that is 0.021 mm.
Patent claim: The gas turbine engine 10 of claim 2 wherein there are at least two sets of protuberances 116 117 216 217 316 317 416 417 which are located in different portions 122 124 222 224 322 324 422 424.

Related passage: Although an exemplary seal 80 is shown positioned between a stationary member and a rotating member it is to be understood that an exemplary seal 80 may also be located between two rotating members or two stationary members as well.
Patent claim: A computer implemented method to determine aircraft sensor failure and correct aircraft sensor measurement in an aircraft system the computer implemented method comprising determining using a physicsbased highfidelity model a highfidelity system response over operating conditions during which sensor drift of a sensor of interest can be detected creating using an aircraft system controller a reduced order model ROM using the highfidelity system response wherein the ROM correlates with the sensor of interest when operating normally calculating using the ROM at least one reduced order sensor value determining an error value between the reduced order sensor value and a sensor measurement reading from the sensor of interest and comparing the error value to an error threshold wherein the sensor of interest has failed when the error value is greater than the error threshold.

Related passage: The diagnosis method 100 then determines if the difference yz in the step 136 is less than or equal to an established model driven gas path threshold value at a step 138.If yes the diagnosis method 100 diagnoses an actuator failure at a step 140.A user is then able to focus a repair or replacement procedure to the particular actuator within the engine 10 for example.
Patent claim: The terminal connection assembly according to any one of claims 1 to5 wherein the convex has a side portion arranged to abut on the positioning structure.

Related passage: The circuit substrate 130 is placed below the main engagement part 120 on the fourth wall 104 to transmit electrical signals to and from the printing device 10 as shown in Fig.13.The circuit substrate 130 is fixed to the fourth wall 104 to face its surface down at an inclination angle of for example 10 to 45 degrees relative to the direction of the arrow Z.
Patent claim: The system of claim 11 wherein the first locationupdaterequest includes context information related to the locationinformationrequest and wherein the one or morepredetermined criteria specify a location precision preference for the positioning system to be selected based on the context information.

Related passage: In one embodiment a SG maintains a datalink layer state for at least a portion of the UDs serviced by that SG.For example during initial connection establishment with ON 102 a UD establishes a PPP session with one of the SGs 110.In one embodiment a PPP session is statefull such that the SG maintains datalink layer state information associated with each PPP session with a mobile UD.In one embodiment datalink layer state information comprises at least one of a link state characteristic parameter a compression protocol a compression protocol state a mobile user device IP address and like information.
Patent claim: The method according to claim 7 or 8 wherein the clock circuit further comprises a second multiplexer wherein an output end of the second multiplexer is connected to the input end of the buffer module and the method further comprises inputting a clock selection signal from an address input end of the second multiplexer inputting a clock source signal from the first data input end of the second multiplexer inputting a testing clock signal from the second data input end of the second multiplexer and outputting the clock source signal or the testing clock signal from the output end receiving by the input end of the buffer module the clock source signal or the testing clock signal that is output from the output end of the second multiplexer when the second multiplexer outputs the testing clock signal from the output end outputting by the clock gating cell connected to the at least one first multiplexer a clock signal from the output end of the clock gating cell according to a testing logic signal received by the testing enabling end and the testing clock signal received by the data end from the output end of the buffer module and when the second multiplexer outputs the clock source signal from the output end outputting by the clock gating cell connected to the at least one first multiplexer a clock signal from the output end of the clock gating cell according to the frequency division logic signal or the gating logic signal received by the enabling end from the output end of the corresponding first multiplexer and the clock source signal received by the data end from the output end of the buffer module.

Related passage: Turning now to Fig.2 a diagram illustrating one embodiment of a clock tree that may be implemented in IC 10 is shown.In the illustrated embodiment clock generator 11 is configured to generate a clock signal that is conveyed to the root clock signal node via clock driver 13.Clock generator 11 may be any suitable type of clock generating circuit such as a phase locked loop PLL or a ring oscillator.
Patent claim: The energy storage apparatus of claim 4 wherein a plurality of battery modules are stacked on one another and positioned within the rack housing and the cooling fan is positioned on an outer side of the rear plate.

Related passage: The housing 72 has a generally hexahedral body.An inlet 72a through which a cooling medium is introduced is formed at one end of the housing 72 and an outlet 72b through which the cooling medium is discharged is formed at the other end of the housing 72.The blower 75 compulsorily introducing the cooling medium into thehousing 72 is installed in the inlet 72a.The cooling medium is formed by air and the blower 75 may be formed by a fan compulsorily transferring air.
Patent claim: The system for weighing and cutting food dough of claim 1 wherein the controller stops the inlet conveyor and the first and the second weighing conveyors when the cutting apparatus is operated.

Related passage: The second weighing conveyor 25 measures the part of the food dough F2 that is cut by the first weighing conveyor 23 after it is cut by the cutting apparatus 27.Similarly to the first weighing conveyor 23 the second weighing conveyor 25 is supported on a base 25S by a load cell 25L.The level of the second weighing conveyor 25 is the same as that of the first weighing conveyor 23.The second weighing conveyor 25 is longer than the first weighing conveyor 23 so that the second weighing conveyor 25 can hold the entire part of the food dough F2 that is cut out.
Patent claim: A hearing assistance device according to claim 13 configured to provide that in case it is concluded that substantial feedback is present in the electric input signal IN the hearing assistance device is brought into a FEEDBACK mode where the electric input signal IN is chosen to be one of or a weighted combination of the supplementary input signals SIN1 SIN2 or a weighted combination of all three electric input signals SIN1 SIN2 AIN in a timefrequency representation.

Related passage: The earpiece 24 also holds one ITE microphone 26 that is positioned at the entrance to the ear canal when the earpiece is positioned in its intended position in the ear canal of the user.The ITE microphone 26 is connected to an AD converter not shown and optional to a prefilter not shown in the BTE housing 12 with electrical wires not visible contained in the sound transmission member 20.
Patent claim: The image processing terminal of claim 6 wherein the control signal includes three or more dimensional coordinate and wherein the processor determines a coordinate of the corresponding key of the remote controller by using a first axis coordinate information and a second axis coordinate information and determines whether the normal input or the force input is applied to the corresponding key of the remote controller by using a third axis coordinate information.

Related passage: The controller 180 may perform a channel conversion operation registered in a channel list if the pressure is smaller than a preset pressure threshold.However the controller 180 may change the currently set channel list LIST 1 230 to a different channel list LIST 2 231 and simultaneously perform channel conversion on the changed channel list if the touch pressure of the soft key 211 or 212 is greater than the preset pressure threshold.
Patent claim: The method for producing the oxidation catalyst for exhaust gas according to any one of claims 9 to 11 wherein the amount of calcium is 0.01 to 0.09 mol per 1L of the catalyst in Ca conversation preferably the amount of calcium is 0.015 to 0.08 mol per 1L of the catalyst in Ca conversion and most preferably the amount of calcium is 0.02 to 0.055 mol per 1L of the catalyst in Ca conversion.

Related passage: The conditions for the HC purifying characteristic evaluation will be given in the following.In this case the zeolite average thickness in the cell flat portion in FIG.6 indicates an average value of YRf in the catalytic layer structures shown in FIG.3A to FIG.3C.Endurance conditionsEngine exhaust amount 3000 ccFuel gasoline Nisseki dash gasolineCatalyst inlet gas temperature 650 CTest period 100 hoursPerformance evaluation conditionsCatalyst capacity for one bank threeway catalystcatalyst 20 1.3 litercatalyst of the present invention catalyst 10 2.6 literTest vehicle inline 4 cylinder 2.0 liter engine manufactured by Nissan Motor Co.Ltd.Carbon number of the hydrocarbons discharged in the engine startup contained in the catalyst inlet gasC2C3 21.0C4C6 33.0C7C9 40.0
Patent claim: An aircraft cabin blower system 30 having a hydraulic circuit 36 comprising a first hydraulic device 38 and a second hydraulic device 40 wherein the first hydraulic device 38 is mechanically coupled to a cabin blower compressor 52 and the second hydraulic device 40 is arranged in use to be mechanically coupled to a spool of a gas turbine engine 10 and where further the first hydraulic device 38 is capable of performing as a hydraulic motor and the second hydraulic device 40 is capable of performing as a hydraulic pump such that when in use the system 30 is operating in a cabin blower configuration a driving force supplied by the spool of the gas turbine 10 causes the second hydraulic device 40 to pump liquid provided in the hydraulic circuit 36 and thereby to drive the first hydraulic device 38 which in turn rotates the cabin blower compressor 52.

Related passage: According to Fig.2 during flight operation of the helicopter the running engine 1 drives the electric motorgenerator 10 as an electric generator via the main gearbox 5 the accessory gear box 12 and the additional freewheel assembly 11 respectively connected by the axle 3.The rotary wing 7 is driven via the main gearbox 5 and the output 6.The main gearbox 5 and the electric motorgenerator 10 drive as well directly and mechanically the pump 8 coupled via the drive shaft 9.During flight operation the driven electric motorgenerator 10 feeds any electric on board consumers e.g.the battery while the driven pump 8 providesenergy to its respective hydraulic consumers 13 e.g.an air concompressor.The electric engines starter motorgenerator 2 is driven by the engine 1 and feeds the helicopters electric on board consumers.