bhlim/patentmatch_for_finetuning huggingface dataset:
Patent claim: The method according to any of the preceding claims wherein the determining the respective estimates of trajectory is based on an estimate joint probability density of the position and speed of each of the wireless devices.

Related passage: Fig.3 schematically represents a communication device 350 of the wireless communications network.The communication device 350 may be a representation of an AP such as the AP 110 andor may be a representation of a mobile terminal such as the mobile terminal 120 andor may be a representation of the server 100.
Patent claim: The isolator system according to claim 1 or 2 wherein the connection means includes an outer tubular member and an inner tubular member which can be fitted to each other and seal means for sealing a gap at a fitted portion and the outer tubular member is provided at an outside of any one of the first opening connector and the second opening connector and the inner tubular member is provided at an outside of another one of the connectors.

Related passage: A processing system for cell cultures of the present invention is characterized by comprising a plurality of modules that can be mutually connected a first closed space provided in each of the modules a door that openscloses an aperture possessed by the first closed space a connecting member provided at a peripheral part of the aperture and a decontaminatingagent supplying module that supplies a decontaminating agent wherein the decontaminating agent is supplied to the first closed space by the decontaminatingagent supplying module the decontaminating agent is supplied to a second closed space formed by the connecting member and the door of one module and the connecting member and the door of the other module connected to the one so as to form an integrated closed space maintaining the connected modules in a sterile state.
Patent claim: The adapter assembly of any preceding claim wherein the first drive assembly includes a first drive screw having a threaded portion and a trocar member operably received about the threaded portion rotation of the first drive screw causes longitudinal movement of the trocar member.

Related passage: With reference to FIGS.59 drive coupling assembly 110 has a cylindrical profile and is configured to selectively secure adapter assembly 100 to surgical device 10 FIG.1.Drive coupling assembly 110 includes a connector housing 112 and a connector extension 114 fixedly connected to connector housing 112 by a mounting plate 113.Connector housing 112 and connector extension 114 operate to rotatably support a first rotatable proximal drive shaft 116 a second rotatable proximal drive shaft 118 and a third rotatable proximal drive shaft 120.Connector housing 112 and connector extension 114 of drive coupling assembly 110 also rotatably supports first second and third connector sleeves 116 118 and 120 respectively.Each of connector sleeves 122 124 126 is configured to mate with respective first second and third drive connectors not shown of surgical device 10 FIG.1.Each connector sleeve 122124 126 is further configured to mate with a proximal end 116a 118a 120a of respective first second and third proximal drive shafts 116 118 120.
Patent claim: The tool according to claim 1 wherein the load adjusting mechanism is configured to move the load sensor along a pressing direction of the switch manipulation part.

Related passage: The electric power tool 10 according to the present embodiment is an impact driver rotary striking tool using a DC brushless motor 20 hereinafter termed the DC motor 20 as the drive source.As shown in FIG.1 the electric power tool 10 includes a tubular housing main body portion 12 and a handle portion 15 formed so as to protrude from the lower portion of the housing main body portion 12.The handle portion 15 includes a grip portion 15h that can be held by a user when using the electric power tool 10 and also includes a battery connection portion 15p located on the lower side distal end side of the grip portion 15h.And at the distal end portion of the grip portion 15h there is provided the variable speed switch 30 that can be pulled by the user with a fingertip.Further at the battery connection portion 15p of the handle portion 15 there is provided a connection mechanism not shown by means of which a battery 16 is connected to the battery connection portion 15p.The DC motor 20 refer to FIG.2 is housed in the rear portion of the housing main body portion 12.Further a drive device not shown including a planetary gear mechanism for increasing a rotational force of the DC motor 20 and a striking force generation mechanism etc.are housed in front of the DC motor 20.And an output shaft of the drive device is linked to a tool attachment portion 13 attached to the distal end position of the housing main body portion 12.
Patent claim: The multiplexer 200 of claim 1 wherein the first and second three port devices 220 2321 each comprisea circulator a ferrite waveguide circulator a ferrite waveguide circulator switch a frequency selective circulator a frequency selective circulator switch a directional filter a transmission line junction a tee junction or a manifold.

Related passage: With the embodiments provided by this disclosure no one load element needs to be rated to handle the full power of a reflected wave.For example in one implementation where reflected RF power is split evenly by waveguide power divider 165 between loads 152 and 154 i.e.a 3dB power divider then each of the loads need only be rated for absorbingof the maximum potential reflected RF power.In some embodiments waveguide loads 152 and 154 are implemented for example using attenuating wave guides that comprises a tapered wedge design andor absorbent material that substantially absorbs and spreads out the energy from reflected RF power along the length of the waveguide.It should also be appreciated that in other embodiment waveguide power divider 165 may divide power between more than just two waveguide loads.
Patent claim: A process according to claims 7 to 10 to be performed in a bottom fired furnace.

Related passage: Fig.13 shows different burner configurations which can be implemented in a concave formed burner roof.The crosssection view for two radiating oblique walls 1c is illustrated in Fig.13a wherein the optimum angle Ca is below or about 50 and the horizontal cave roof width Cw is designed based on the tube corridor width W and the Ca angle so that enough space is kept to arrange the burners accordingly.
Patent claim: The inorganic thermoset resin according to claim 10 or 11 comprising an antishrinkage additive.

Related passage: In general phenolic resins and glass fibre prepregs comprise the outer skins of such panels.Alternatively skins may be made from a composite of glass fibre with epoxy or carbon fibre with epoxy.All these skin materials have known environmental limitations.Phenolic resins are regarded as highly noxious and can cause skin problems such as dermatitis.Glass fibres cause irritation of the skin eyes and upper respiratory system producing skin eruption similar in appearance to poison ivy pneumoconiosis and silicosis.If ingested glass fibres can also cause gastrointestinal conditions.
Patent claim: The landing gear assembly of claim 2 wherein the operations further comprise evaluating 352 by the controller 110 the lowest value and the moving average against a threshold wherein the threshold is based on the moving average and preferably wherein the threshold is 50 to 70 of the moving average.

Related passage: A slip ratio beyond a given threshold value may indicate a dragging brake.While the selection of a threshold value may be based upon aircraft size weight engine power brake size and other suitable factors in various embodiments a threshold value may range from about 0.5 to 15 more preferably from about 1 to about 10 and more preferably from about 1.5 to about 4.The threshold value may be compared to the slip ratio of a particular wheel on an aircraft though in various embodiments the threshold value may be compared to an average slip ratio of one or more of the wheels of an aircraft.For example the threshold value may be compared to the average of the left outboard and left inboard wheel or the average of all aircraft wheels.
Patent claim: The gas turbine engine 10 of any preceding claim wherein the protuberances 118 218 318 418 120 220 320 420 extend radially into the buffer cavity 112 212312412.

Related passage: The segmented ring 86 is radially located in a neck region 96 of the blades 58.The neck region 96 extends radially outward above the rim 60 from the attachment 66 to a platform 98 that supports an airfoil 100 and defines the inner radial contour of the annular duct 30.Individual ring segments 186 extend axially outward from the neck region 96 of each blade 58 and are formed by casting turning grinding broaching electrodischarge EDM or other suitable process.With the blades 58 interposed with the lugs 64 adjacent ring segments 186 substantially align defining a complete segmented ring 86.A single segmented ring 86 as shown in FIG.2 may be used or multiple segmented rings 86 as shown in FIG.3 may also be used.The addition of multiple segmented rings 86 provides a greater leakage restriction but the actual number may be limited by space and weight requirements.
Patent claim: The image processing terminal of claim 1 wherein the modes include two or more of a standby mode an active standby mode or a deep standby mode.

Related passage: FIG.10 illustrates a method for converting a channel while broadcast data is received and displayed in a mobile terminal 100 according to a sixth embodiment of the present invention in which a corresponding operation is performed according to a pressure at which a key for performing channel conversion is pressed.For example the controller 180 checks the pressure of an input key or touch region when a soft key 211 or 212 for channel conversion is input or touched while the soft menu 20 for a channel manipulation is displayed.
Patent claim: The rotary electric shaver according to Claim 1 wherein the outer blade 22 includes the rib portion 27 having the upper surface 27a formed into a curved shape at both end portions 27b 27c in the circumferential direction.

Related passage: The term electric shaver refers to both rotary type shavers and reciprocating type shavers and in the embodiments below the present invention will be described on an electric rotary shaver.
Patent claim: The image processing terminal of claim 1 wherein the control signal includes three or more dimensional coordinate and wherein the processor determines a coordinate of the specific 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 specific key of the remote controller by using a third axis coordinate information.

Related passage: FIG.10 illustrates a method for converting a channel while broadcast data is received and displayed in a mobile terminal 100 according to a sixth embodiment of the present invention in which a corresponding operation is performed according to a pressure at which a key for performing channel conversion is pressed.For example the controller 180 checks the pressure of an input key or touch region when a soft key 211 or 212 for channel conversion is input or touched while the soft menu 20 for a channel manipulation is displayed.
Patent claim: A seal 66 for a gas turbine engine comprising a plurality of seal arc segments 66 166 266 366 each of the seal arc segments 66 166 266 366 including radially inner and outer sides 70a 70b and sloped first and second circumferential sides 72a 72b the seal arc segments 66 166 266 366 being circumferentially arranged about an axis A such that the sloped first and second circumferential sides 72a 72b define gaps 74 circumferentially between adjacent ones of the seal arc segments 66 166 266 366 each of the gaps 74 extending from the radially inner sides 70a along a respective central gap axis A1 that slopes with respect to a radial direction R from the axis A.

Related passage: Reference is made to the Figures generally in which an outer air seal 10 according to the present invention is shown.By way of overview the seal 10 includes a set 20 of boundary members 12 grouped in a ringshaped arrangement to prevent leakage within the turbine section 16 of an associated gas turbine engine 18.Each boundary member 12 is separated from adjacent boundary members by interface gaps 22 formed therebetween.The interface gaps 22 allow contraction and expansion of individual boundary members 12 as well as relative motion between the boundary members collectively during operation.The interface gap 22 includes a radiallyskewed portion 24 formed by angled portions 2628 of cooperating adjacent boundary member interface edges 3032.The interface gap 22 may also include a radiallyaligned portion 34 and one or more partition members 36 may extend into the interface gap 22 to form a serpentineshaped pathway 38 within the gap.Cooling fluid conduits 40 disposed within the boundary members 12 provide a pathway for cooling fluid 42 to enter the interface gap 22 thereby providing supplemental cooling without reducing engine operating efficiency.Itis noted that while the outer air seal 10 is described in the context of an industrial gas turbine engine 18 and specifically within an engine turbine section 16 the seal will provide benefits in other settings including other stationary interfaces such as intervane interfaces and end wall to downstream component interfaces as well.Furthermore as a matter of convention rotation of blades 14 will be shown as occurring in a counterclockwise fashion during operation of the reference engine 18.Clockwise rotation is possible however and in settings with clockwise rotation the various aspects of the invention would be achieved mosteffectively if the orientation of the radiallyskewed portion 24 of the interface gap 22 is commensurately reversed from that shown and described herein.Additionally in the context of counterclockwise rotation the terms rotationallyupstream and rotationallydownstream shall refer to locations that are displaced respectively clockwise and counterclockwise from a given reference point.The outer air seal 10 of the present invention will now be described in detail.
Patent claim: A seal arc segment 66 166 266 366 for a gas turbine engine comprising a seal arc segment body 66a defining radially inner and outer sides 70a 70b and sloped first and second circumferential sides 72a 72b extending from the radially inner side 70a.

Related passage: As seen with continued reference to Figure 2 and with additional reference to Figures 3 and 4 the boundary members 12 are essentiallyrectangular elements that cooperatively form a substantiallycontinuous band adapted for encircling a longitudinallyextending region within the turbine section 16.The boundary members 12 include a front edge 50 and a rear edge 52 that each extend between the interface edges 3032 noted above.The boundary members 12 havea curved crosssection characterized by a radiallyinward surface 54 which is oriented toward the engine central axis 48 and an opposite radiallyoutward surface 56.The interface edges 3032 of adjacent boundary members 12 have complementary contours.As noted above interface edges of adjacent boundary members form interface gaps 22 that allow relative motion as well as cyclic growth and contraction of the boundary members during engine operation.Although not required the present embodiment also includes a radiallyaligned portion 34 disposed proximate the boundary member radiallyoutward surface 56.A blocking panel 58 disposed within the interface gap 22 provides a physical barrier that helps prevent unwanted radiallyoutward motion of working fluid 44 traveling through the turbine section 16.Blocking panels 58 may be omitted in settings where additional fluid flow obstructions are not desired.Where used however the panels 58 may be held in place by a variety of methods such as notches 6062 cut into the boundary member interface edges 3032.Other fixing methods including welding brazing interference fits and the use of fastening components may also hold the panels 58 in place if desired.As will be more fully described below the interface gap 12 of the present invention also provides extended component life by reducing pulse loading of blocking panels 58.Although the radial position of the blocking panels 58 may vary the panel protection feature described below is most effective when the blocking panel 58 is located radially outward of the radiallyskewed portion 24.In this application the term radiallyskewed means an orientation that is rotated to be offset from a radial orientation by a desired amount.In the present embodiment the radiallyskewed portion of the interface gap 22 is offset from radial orientation by an anglewithin the range of about fifteen to fiftyfive degrees.It is noted that the radiallyskewed portion 24 need not be proximate the radiallyinward surface 54 of the boundary members 12 however shifting the radial position of the radiallyskewed portion may reduce the film cooling feature described below.
Patent claim: A control method of a display apparatus the method comprising receiving an image signal displaying on a display at least one candidate profile from among a plurality of candidate profiles each of which comprises different setting information for a plurality of setting items of the display apparatus selecting one from among the displayed at least one candidate profile according a user input and in response to the selecting storing the setting information for the plurality of setting items comprised in the selected candidate profile.

Related passage: The abovedescribed steps are only carried out upon first powerup.In subsequent uses the stored control parameter settings will be used to control the display panel.By using this method both the stores and the consumers can properly set the relevant parameters of the television device to proper settings optimum for the intended viewing environment.The television device may allow the user to further adjust these parameters at any time.Other control parameters that are not affected by the viewing environment may be preset at the factory and are not affected by the above initialization process.
Patent claim: The method of any of claims 10 to 14 wherein emitting by the optical transmitter the optical signal comprises emitting the optical signal as a single laser pulse at a fixed wavelength and wherein determining using the controller the at least one temperature for each of the plurality of zones comprises determining the at least one temperature for each of the plurality of zones using optical time domain reflectometry OTDR.

Related passage: FIG.2 depicts scanning method 100 a method whereby data processor 22 controls optical switch 14 to scan sensing elements 16a 16b...16N at variable rates.In many fire and overheat detection systems impermissible delays in overheat or fire detection can result in dangerous conditions developing before fire suppression or extinguishing apparatus can be deployed.It is therefore essential that such systems be capable of a high interrogator scan rate so as to minimize the time delay between subsequent checks of each sensing element 16a 16b...16N.It is well known in the art however that spatial and temperature resolution are inversely related to interrogator scan rate in distributed optical fiber sensing systems.Although a high fast scan rate is necessary to ensure that all monitored components are interrogated frequently the greater resolution provided by slower scanning rates may be needed to identify and localize a fire or overheat condition.Scanning method 100 allows optical fiber sensing system 10 to provide high spatial and temperature resolution when necessary while maintaining a high normal scan rate as described below.
Patent claim: Use of a glycation stress inhibitor comprising extracts of fenugreek and fennel as active ingredients for inhibiting glycation stress.

Related passage: It is known that oxidation reactions and glycation reactions in vivo adversely affect cells and tissues.In particular the production and accumulation of proteins having undergone an oxidation reaction or a glycation reaction i.e.oxidized proteins or glycated proteins cause diseases such as diabetes complications Alzheimers disease cataracts and arteriosclerosis as well as aging and hypofunction of tissues such as skin.On this account the oxidized proteins and glycated proteins are called damaging proteins.In particular accumulation of AGEs Advanced Glycation Endproducts which are end products produced by a nonenzymatic addition reaction of a carbohydrate to a protein is seen as a problem.
Patent claim: The material according to any one of the preceding claims wherein the first amine is represented by a general formula R1R2NR3 wherein R1 R2 and R3 are all bonded to a nitrogen atom R1 is represented by Cs1Ht1Ou1Nv1 wherein s1 t1 u1 and v1 respectively satisfy 0s120 1t150 0u110 and 0v15 R2 is represented by Cs2Ht2Ou2Nv2 wherein s2 t2 u2 and v2 respectively satisfy 0s220 1t250 0u210 and 0v25 and R3 is hydrogen or a functional group represented by Cs3Ht3Ou3Nv3 wherein s3 t3 u3 and v3 respectively satisfy 1s320 1t350 0u310 and 0v35.

Related passage: In the present embodiment based on a correlation between the solubility of the reaction accelerator with water and a solidification effect and the like when the absorbing liquid is at 20 to 60C preferably 20 to 50C more preferably 30 to40C the absorbing liquid becomes in a state in which the reaction accelerator in the absorbing liquid is solidified to disperse a precipitate containing the reaction accelerator in the absorbing liquid so that the absorbing liquid becomes a slurry solution containing the precipitate containing the solidified reaction accelerator in the state of being dispersed.The shape of the precipitate is a granular shape or the like without particular limitation.When the absorbing liquid is at 60 to 120C a state in which the reaction accelerator in the absorbing liquid is dissolved in the absorbing liquid is maintained.The absorbing liquid is preferably at not less than 67C or not more than 100C.When the absorbing liquid is at 60 to 120C the absorbing liquid becomes a solution in which there is formed a mixed phase including two phases of an amino groupcontaining compound rich phase containing a large amount of an amino groupcontaining compound compared to the first rich solution 23A and a reaction accelerator rich phase containing a large amount of the reaction accelerator compared to the first rich solution 23A and containing the reaction accelerator in the state of being dissolved.