bhlim/patentmatch_for_finetuning huggingface dataset:
Patent claim: The image forming unit 100 according to any one of claims 2 to 4 wherein the first surface 502 and the second surface 402 are brought into the proximity to each other when each of the protrusions 51L 51R of the developer container 50 is located at the upstream end of the second linear part 425L 425R of the corresponding groove in the attachment direction A.

Related passage: The color image carried on the intermediate transfer belt 41 is subsequently transferred onto a sheet of paper P supplied from the sheetfeeding unit 3 as the sheet passes between the intermediate transfer belt 41 and secondary transfer roller 38 as a secondary transfer.
Patent claim: The device of any preceding claim wherein the electromagnetic device further includes a communications system and wherein the impedance is configured to maximize a signal to noise ratio in the communications system.

Related passage: Coil circuit 280 comprises a sense coil 320 and a generator coil 300.Sense coil 320 senses the magnetic field in the vicinity of the connector.Based on the sensed magnetic field driver circuit 290 drives generator coil 300 so as to generate an opposing magnetic field that counteracts the sensed magnetic field.In other words coil 300 generates an opposing magnetic field that cancels or at least considerably reduces the magnetic field sensed by coil 320.As a result the net magnetic field that affects the connector terminals and wiring is canceled or considerably reduced.
Patent claim: A method for receiving buffer status information by an access point in a wireless communication system the method comprising determining a contention subslot and a dedicated subslot for each of stations connected to the access point generating a data trigger action frame based on a first element including allocation information on the dedicated subslot to be used by a related station in a buffer status report BSR phase where each of the stations transmits buffer status information to the access point broadcasting the generated data trigger action frame to the stations and receiving a BSR frame transmitted based on the data trigger action frame from each of the stations.

Related passage: The above explanations apply e.g.to VoIP data on the other hand it is not excluded that radio bearers carrying data suitable to be transmitted on semipersistently configured resources that show a stable data size from the beginning of the data transmission are not subject to header compression.
Patent claim: The catheter of claim 4 wherein each spine comprises a strut having a varying cross sectional area.

Related passage: If desired the catheter may include a steering mechanism for deflection of the distal end of the catheter body 12.With such a design the distal end of the catheter body 12 preferably comprises a short length of tubing e.g.50mm to 100mm 2 to 4 inches in length that is more flexible than the remainder of the catheter body 12.A suitable steering mechanism comprises a puller wire not shown that extends from a proximal end in the control handle 16 through the central lumen 15 in the catheter body 12 and into an off axis lumen in the short length of tubing.Within the catheter body 12 the puller wire extends through a closely wound coil that is bendable but substantially noncompressible.The coil is fixed near the proximal and distal ends of the catheter body 12 and prevents deflection of the catheter body 12.The distal end of the puller wire is anchored at the distal end of the short length of tubing in the off axis lumen.The proximal end of the puller wire is anchored to a movable member in the handle 16 that can be moved relative to the catheter body 12.Proximal movement of the movable member relative to the catheter body 12 results in deflection of the short length of tubing.An example of such a steering mechanism and construction is described in more detail in U.S.Patent No.6064905 the disclosure of which is incorporated herein by reference.When incorporating a steering mechanism into the inventive catheter 10 it may be desirable to include a location sensor at the distal end of the catheter body 12.As would be recognized by one skilled in the art of a slurring mechanism is not including the handle 16 can be eliminated although it is described to maintain the handle for ease of use by the cardiologist.
Patent claim: The honeycomb structure according to claim 7 wherein the inorganic bonding material includes the alumina derived from basic aluminum lactate and alumina derived from boehmite and a value of A1A2 which is a ratio of a volume A1 of the alumina derived from basic aluminum lactate to a volume A2 of the alumina derived from boehmite is 0.6 or more.

Related passage: In the honeycomb catalyst of the present invention preferably the honeycomb unit further includes at least one selected from the group consisting of an inorganic fiber a scalelike material a tetrapodshaped material and a threedimensional needleshaped material for increasing the strength.
Patent claim: The method 100 of any one of claims 1 to 8 further comprising forming 182 shims 64 to fit between a wing root 20 of the wing assembly 14 and a wing stub 30 of a body assembly 16 of the aircraft 12 and further comprising installing shims on at least one of the wing root and the wing stub before the b iteratively repeating.

Related passage: Configuration analyzer 943 then determines whether the current configuration identified is within selected tolerances of selected configuration 941.If the current configuration of structure 912 is within selected tolerances of selected configuration 941 support system 908 may not need to be reconfigured.
Patent claim: The method of any of claims 9 to 13 wherein the first linear translation element 208 304 is a ball screw.

Related passage: Each adjusting unit 8 comprises a differential 14 connected to the main shaft 6 for receiving an input torque and is connected to two rotary actuators 16 for outputting torque.Exemplarily both rotary actuators 16 from each adjusting unit 8 are arranged relative to each other e.g.facing each other such that one end of an adjustment lever can be connected to both rotary actuators 16 at the same time.
Patent claim: The terminal connection assembly according to either claim 1 or claim 2 wherein the convex is engaged with a positioning concave provided in the positioning structure.

Related passage: The folding structure of the conductive elements 258 at the lower end of the deviceside terminal assembly 250 enables the respective terminals 261 to 269 and 271 to 279 to be located relatively on the upper side of the deviceside terminal assembly 250 while ensuring the pressing force of the conductive elements 258.Locating the respective terminals 261 to 269 and 271 to 279 on the upper side of the deviceside terminal assembly 250 causes the position of contact with a circuit substrate 130 as shown in Figs.13 and 19 of each of the cartridges 100a and 100b to be made close to the engagement position of the lever member 230 with the main engagement part 120.This enhances the electrical connectivity between the deviceside terminal assembly 250 and the circuit substrate 130.This configuration also enables the circuit substrate 130 of each of the cartridges 100a and 100b to be located at a position away from the lower end of each cartridge 100a or 100b and additionally enables the circuit substrate 130 to be located at a position close to the main engagement part 120.This configuration enhances the protection of the circuit substrate 130 of each of the cartridges 100a and 100b.
Patent claim: The medium of claim 2 wherein the one or more predetermined criteria can specify a low power consumption preference for the positioning system to be selected.

Related passage: At step 214 the optimum SG performs authentication.In one embodiment the optimum SG performs device authentication e.g.authenticating the UD to verify that the UD is permitted to access the network and associated network services.In another embodiment the optimum SG performs user authentication e.g.authenticating the user attempting to access the network via the authenticated UD.In another embodiment the optimum SG performs application authentication e.g.authenticating an application used for accessing network services.In another embodiment the optimum SG performs service authentication e.g.authenticating at least one service request initiated by the user via the authenticated application.
Patent claim: The system of claim 3 wherein the airoil heat exchanger 256 of the main lubrication oil system is located downstream of the fueloil heat exchanger of the fuel system 206.

Related passage: From the main fuel pump 3 8 the fuel serves as a coolant for the third liquidtoliquid heat exchanger subsystems 22.The third liquidtoliquid heat exchanger subsystem 22 includes an engine oil loop 40.The components cooled by the engine oil loop 40 are the most resistant to temperature and are permitted to exceed approximately 325 degrees Fahrenheit 163 C.Preferably the components cooled by the engine oil loop 40 utilize an optimized high temperature esterbased oil which operates at temperatures in excess of approximately 325 degrees Fahrenheit 163 C.Such an optimized high temperature esterbased oil is produced by NYCO S.A.Paris France under the trade name of GTO7.The optimized high temperature esterbased oil combined with the deoxygenated fuel temperature thermal retention capabilities permitsassociated components to operate above the conventional 325 degrees Fahrenheit 163 C temperature limit.
Patent claim: The energy storage apparatus of claim 1 wherein the chamber comprises a first sidewall a second sidewall positioned perpendicularly to the first sidewall a third sidewall facing the first sidewall and positioned perpendicularly to thesecond sidewall and a fourth sidewall facing the second sidewall and positioned perpendicularly to the first sidewall and the third sidewall wherein a plurality of cooling units are provided on an outer side of the first sidewall and the third sidewall.

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: A hedge trimmer comprising a trimming blade extending along a longitudinal axis configured for carrying out a reciprocating motion a first housing being formed or connected with a first handle having a first locking portion a second housing being formed or connected with a second handle and rotatable with respect to the first handle around a rotation axis wherein a plane perpendicular to the rotation axis is obliquely intersected with a plane perpendicular to a longitudinal axis of the trimming blade a transmission mechanism being combined to the first housing for driving the trimming blade an electric motor being combined to the first housing for driving the transmission mechanism a battery pack being combined to the second housing for supplying the electric motor with electric power a trigger configured for controlling the electric motor and a control member being movably connected to the first housing or the second housing comprising a stopper portion and a second locking portion cooperable with the first locking portion wherein the control member has a first position and a second position with respect to the second housing whereby when the control member is at the first position the first locking portion and the second locking portion are engaged with each other and the firsthousing and the second housing are relatively fixed and when the control member is at the second position the stopper portion stops movement of the trigger the first locking portion and the second locking portion are disengaged with each other and the second housing is allowed to rotate with respect to the first housing around the rotation axis.

Related passage: Japanese Patent Application Publication No.2007275063
Patent claim: The liquid laundry detergent composition according to any preceding claims wherein the anionic surfactant is selected from linear alkylbenzene sulphonate alkyl sulphate alkoxylated alkyl sulphate or a mixture thereof preferably wherein the anionic surfactant comprises linear alkylbenzene sulphonate and ethoxylated alkyl sulphate most preferably wherein the anionic surfactant comprises linear alkylbenzene sulphonate and ethoxylated alkyl sulphate in a weight ratio of linear alkylbenzene sulphonate to ethoxylated alkyl sulphate of between 31 and 11 more preferably between 21 and 11.

Related passage: A multicompartment unit dose article may also be prepared by fitting a first piece of film material into a mould.A composition or component thereof can then be poured into the mould.A preformed compartment can then be placed over the mould containing the composition or component thereof.The preformed compartment also preferably contains a composition or component thereof.The preformed compartment and said first piece of watersoluble or dispersible film material are sealed together to form the multicompartment unit dose article.
Patent claim: The method of Claim 1 further comprising determining with the processor a future state of the vehicle with respect to a second one of the plurality of legs of the selected flight plan based on the determined current state and determining with the processor a future target state for the vehicle with respect to the second one of the plurality of legs based on the flight plan data.

Related passage: Now that the components of the aircraft system 100 have been generally described the deviation module 140 will be described in greater detail.As described above the deviation module 140 generally determines the difference between the current state ofthe aircraft and the anticipated or predicted state of the aircraft according to the flight plan and provides this information to the pilot.Since the flight plan includes lateral vertical and time profiles the deviation may include any combination of lateral altitude or time deviation.As such the deviation module 140 receives the current latitude longitude and altitude of the aircraft provided by the navigation system 120 and compares these values to the appropriate latitude longitude and altitude of the aircraft according to the flight plan generated by the guidance system 130.The deviation module 140 further calculates an estimated time of arrival for a subsequent waypoint or destination and compares the estimated time of arrival to the anticipated or required time of arrival for the waypoint or destination.The estimated time of arrival may be based on for example the current and anticipated speed of the aircraft weather conditions fuel load mechanical performance or capabilities speed limits and others parameters that may impact the time of arrival.The time deviation is the difference between the estimated time of arrival and the required time of arrival.
Patent claim: The coated glass article of any of claim 1 to 4 wherein the coated glass article demonstrates a reduction in average particle count of at least 75 compared to the average particle count for the uncoated glass article preferably a reduction in average particle count of at least 90 compared to the average particle count for the uncoated glass article more preferably a reduction in average particle count of at least 99 compared to the average particle count for the uncoated glass article.

Related passage: In another embodiment the coupling agent may be an inorganic material such as metal andor a ceramic film.Nonlimiting examples of suitable inorganic materials used as the coupling agent include titanates zirconates tin titanium andor oxides thereof.
Patent claim: The computerreadable medium of claim 14 further comprising analyzing the haptic track for a future occurrence of a zeroforce interval.

Related passage: At 360 a vibrotactile haptic effect pattern is assigned to each haptic effect pattern of the plurality of haptic effect patterns or the single haptic effect pattern included within the haptic signal.Each vibrotactile haptic effect pattern can include data that causes a standarddefinition haptic output device such as an ERM to produce a vibrotactile haptic effect for a predefined duration identified as an active duration and to cease producing the vibrotactile haptic effect for a predefined duration identified as a silent duration.Thus according to the embodiment a collection of vibrotactile haptic effect patterns is generated or rendered where each vibrotactile haptic effect pattern is assigned to a haptic effect pattern included within the haptic signal.In certain embodiments the rendering of a vibrotactile haptic effect pattern includes limiting the active duration of the vibrotactile haptic effect pattern to a predefined maximum duration identified as a maximum duration.The limiting of the active duration can be performed because long vibrotactile haptic effects are generally unpleasant when output on ERMs or other types of standarddefinition haptic output devices.According to theembodiment the limiting of the active duration can be performed after the splitting of large haptic effect patterns before the assigning of the vibrotactile haptic effect pattern to a haptic effect pattern and either before or after the shifting back of the start time of each haptic effect pattern by a shift duration.Further in some embodiments the collection of vibrotactile haptic effect patterns can be stored in a computer file such as a text file or an audio file e.g.PCM file.
Patent claim: The ROM sensor system of claim 10 further comprising additional computer readable instructions comprising generating in the aircraft system controller corrective control signals to protect the aircraft system based on the error value andtransmitting the corrective control signals to one or more components of the aircraft system.

Related passage: Example fault associated with module performance includes one of the engine modules 46 operating at a reduced efficiency.For example the high pressure compressor 18 has a particular flow capacity and efficiency that experiences a change in performance due to contamination or fouling in the high pressure compressor.
Patent claim: The method of any preceding claim wherein engaging the ACC mechanism includes at least one of activating the ACC mechanism adjusting one or more outputs of the ACC mechanism based on one or more inputs or deactivating the ACC mechanism.

Related passage: Figure 8 is a graph showing engine power against time.An exemplary engine power demand curve 80 is shown which may be an oscillation due to autothrottle.The engine power response curve 82 has substantially the same shape as the demand curve 80.However the engine power response curve 82 lags behind the engine power demand curve 80 by a time period indicated by the doubleheaded arrow 84.The time lag 84 is dependent on the engine 10 the control iteration engine power condition environmental and other factors.In a typical aircraft gas turbine engine 10 the time lag 84 is in the range 1002000ms preferably 500ms to 1000ms.
Patent claim: The method of claim 1 wherein the transmission of one or more data messages is on a first channel frequency and the transmission of the voice message is on a second channel frequency different than the first channel frequency.

Related passage: The procedure of Fig.3 may be started in two different ways.One way is according to a third embodiment of the invention which is when an operator of a fighter aircraft which includes said radio communication system 1 wants to stop voice transmission using the present invention.The operator then uses the radio communication system 1 in the same way as if it was used exclusively for voice communication that is he simply releases the PTT 10 in the user communication device 5.The other way is according to a fourth embodiment of the invention wherein during the transmission using the voice communication service on the predetermined fixed frequency the onboard system computer 3 monitors the carrier information provided by the radio communication device 2 via the data bus 7.The onboard system computer 3 operator is then able to detect when the voice transmission has stopped being received that is the carrier on the predetermined fixed frequency has ceased.
Patent claim: An induction heating device comprising a working coil 70 for creating a magnetic field for induction of eddy current in a cooking utensil so as to heat the cooking utensil a power supply unit 80 for providing induction voltage to operate the working coil 70 a temperature sensor 21 for measuring a temperature of the cooking utensil a first lighting unit 40 for emitting visually perceivable light a second lighting unit 50 for emitting visually perceivable light and a control unit 93 for controlling the first lighting unit 40 based on the temperature of the cooking utensil transmitted from the temperature sensor 21.

Related passage: Subsequently the cooking apparatus 1 generates flame images FI according to the received cooking method 1430.
Patent claim: The oxidation catalyst for exhaust gas purification according to any one of claims 3 to 7 wherein the catalyst component is analloyof platinum and palladium whenplatinum and palladium are used.

Related passage: From the table 3 of FIG.7 it can be understood that the catalysts prepared by EXAMPLES 1 to 22 have high catalytic activity and are superior in the HC purification efficiency especially the cold HC purification efficiency.In particular according to the catalyst in EXAMPLE 19 the best HC purification characteristic can be achieved.
Patent claim: An optical fiber comprising an optical core surrounded by an outer optical cladding said optical core comprising from the center to the periphery a central core and a depressed inner claddingsaid central core having a radius r1 and a refractive index difference n1 with respect to the outer optical claddingsaid depressed inner cladding comprising at least a first and a second portionsaid first portion is adjacent to the central core and has a radius r2 and a refractive index difference n2 with respect to the outer optical cladding that is negativesaid second portion is adjacent to the first portion having a radius r3 and a refractive index difference n3 with respect to the outer optical cladding that is negative and wherein the refractive index difference n3 is more negative than the refractive index difference n2 wherein the depressed inner cladding comprises a third portion located between the second portion and the outer optical cladding said third portion having a radius r4 and a refractive index difference n4 with the outer optical cladding wherein the refractive index difference n4 is less negative than the refractive index difference n3 of the second portion wherein the outer radius of the depressed inner cladding is between 28 and 40 m wherein the LP01 mode leakage losses at a wavelength of 1550 nm are less than 0.01 dBkm and wherein the cable cutoff wavelength is less than 1530 nm.

Related passage: According to embodiments of the invention the inventive refractive index profile provides a positive dispersion optical fiber with a relatively large effective transmission area that is effective core area Aeff and transmission characteristics at least as desirable as conventional fibers but without the disadvantages of those same conventional fibers for example as discussed hereinabove.For example according to embodiments of the invention as shown in Fig.5a 10.303 20.026 and 30.075.Also in this particular arrangement c16.343 m c28.343 m and c323.343 m.Thus the width of the first annular ring is 2.000 m 8.343 m6.343 m and the width of the second annular ring is 15 m 23.343 m8.343 m.