bhlim/patentmatch_for_finetuning huggingface dataset:
Patent claim: The subsea electrical system according to claim 10 or 11 wherein the subsea terminating device 201 has a line insulation monitor 25 coupled to the first electrical powerconnection 11 of the first subsea electrical unit 101 the line insulation monitor 25 being configured to be operable online while subsea electrical units 101 102 103 104 which are electrically connected to the subsea terminating device 201 receive electrical power via the subsea terminating device 201 and the respective electric power connections.

Related passage: The distribution unit 3 may be provided with electrical protection circuitry to isolate any electrical short circuits arising for example as a result of the breakdown of the insulation of one or more of the cables 5 or a failure within one or more of the output connectors 6b.It may also incorporate a transformer to step down high voltage transmissions from the surface and umbilical 1 to lower voltages that are better suited for use by the devices 4.
Patent claim: The induction heat cooking apparatus according to claim 7 wherein to drive the second and third heating coils 242 243 in parallel the controller 280 is configured to control the third switching device 223 to be closed and during a half resonant period to control the first and second switching devices 221 222 to be in a closed state and to control the fourth switching device 224 to be in an opened state and during the other half resonant period to control the first and second switching devices 221 222 to be in the opened state and to control the fourth switching device 224 to be in the closed state.

Related passage: Referring to Table 5 the switching controller 270 controls the first second and third switches S1 S2 and S3 in response to the third switching signal such that not only the first heating coil 230 and the first resonant capacitors Cr11 and Cr12 but also the second heating coil 240 and the second resonant capacitors Cr21 and Cr22 are driven.
Patent claim: The downconversion circuit 30 according to any preceding claim wherein the second passive switching mixer 80 has an enabled and a disabled mode and wherein the downconversion circuit 30 is arranged to selectively set the second passive switching mixer 80 inthe enabled mode when an interference level exceeds a threshold for counteracting the interference andthe disabled mode for saving power compared with the enabled mode.

Related passage: As can be seen using a dutycycle of 13 gives no harmonic downconversion due to 3rd order harmonic from the square wave LO.It is alsoclear that the dutycycle can be adjusted to remove any harmonic in the Fourier series.
Patent claim: The IMS network entity of claim 9 or claim 10 wherein the charging priority value is a predetermined value stored in the network entity based on a property or type of message of the messaging transaction.

Related passage: When the CSCF charges for the SIP service request the CSCF charging information shall include the priority service ID information when the operator charges different priority service classes with different rates the CSCF charging information also includes the priority service class of the UE.When the operator charges different priority service classes with the same rate the CSCF charging information can include or exclude the priority service class of the UE.
Patent claim: The method of claim 1 further comprising selecting a set of existing LI sessions associated with the lowest priority determining whether there exists at least one LI session in an idle state in the selected set of existing LI sessions andselecting an LI session associated with a longest idle time as the particular LI session to terminate when there exists at least one LI session in an idle state in the selected set of existing LI sessions.

Related passage: In a second manner the interception center assigns the interception task of intercepting the target users A and B to an interception gateway after receiving the interception task sent from the interception center the interception gateway forwards the interception task to the interception NE.
Patent claim: The method 700 of any of claims 1012 wherein the haptic output device 310 is coupled to a wearable device and wherein the wearable device comprises a shoe an armband a sleeve a jacket glasses a glove a ring a watch a wristband 314 an article of clothing a hat a headband or jewelry.

Related passage: In some embodiments a haptic effect may be triggered in response to a flex gesture only if the flex gesture is valid.A flex gesture may be invalid for example if it has no application action associated with it.In some embodiments a default haptic effect e.g.vibration of actuator 144 for 2 seconds at intensity level of 3 may be triggered to indicate to a user that the gesture is invalid.
Patent claim: A method as recited in Claim 7 further comprising the step of automatically electronically adjusting the video image wherein optionally the method further comprises the step of using image recognition software to identify the airplane in the video image.

Related passage: The fifth video camera 80 is located at the leading edge 82 of the horizontal stabilizer 84.The fifth video camera 80 is focused forward and downward for viewing of the left wing landing gear 36.Alternatively or additionally the fifth video camera 80 could be mounted on the starboard side of the airplane 24.The sixth video camera 88 is located substantially on the centerline of the fuselage 22 of the airplane 24 between the main landing gear and the underside of the aft fuselage section 52B.The sixth video camera 88 has a viewing angle 90 for generating images of the tires 26 of the nose landing gear 28 the tires 72 of the center post main landing gear 70 the tires 40 and 42 of the left and right wing landing gear 36 and 38 and the runway or taxiway edges in the forward direction.While some foreshortening of the image seen by a pilot on a cockpit display device is likely the sixth video camera 88 provides a substantial amount of realtime information particularly about the crosswise position of the airplane 24 on a runway or taxiway and obstacles ahead.
Patent claim: A plasma source comprisingan outer surface interrupted by an aperture for delivering an atmospheric plasma from the outer surfacea transport mechanism configured to transport a substrate and the plasma source relative to each other parallel to the outer surface with a surface to be processed of the substrate in parallel with at least a part of the outer surface that contains the aperturea first electrode having a first and second surface extending from an edge of the first electrode that runs along the aperture the first surface defining the outer surface on a first side of the aperture the distance between the first and second surface increasing with distance from the edgea second electrode and a dielectric layer covering at least part of the second electrode at least part of a surface of the dielectric layer facing the second surface of the first electrode substantially in parallel with the second surface of the first electrode leaving a plasma initiation space on said first side of the aperture between the surface of the dielectric layer and the second surface of the first electrodea gas inlet in communication with the plasma initiation space to provide gas flow from the gas inlet to the aperture through the plasma initiation space.

Related passage: In the configuration as illustrated in Figure 1A the first plasma 1 may be used for cleaning andor activating the substrate surface whereas the second plasma 1 is used for the actual coating process.
Patent claim: A secure access method for an application app program and to be implemented by a secure access device 1 which includes first authentication data and a first control regulation the secure access method characterized by the steps of A making a determination as to whether a tobeauthenticated app program which is executed in an operating system 311 is provided with the first authentication data and the first control regulation and B when a result of the determination made in step A is negative identifying the tobeauthenticated app program as an unauthenticated illegitimate app program and disallowing the illegitimate app program to access a tobeaccessed device.

Related passage: The operations of server 40 and information processing terminal 30 according to Embodiment 6 will be explained with reference to FIG.7 and FIG.8 and with reference to step numbers in FIG.7 and FIG.8.
Patent claim: A pouch according to claim 1 wherein the mixture of the complexing agent and the eRH reducing agent comprises at least about 10 by weight thereof of the complexing agent.

Related passage: Preferably the hygroscopic material is an organic material.Preferably the hygroscopic material is a dispersant more preferably a salt of a carboxylic acid.Preferred carboxylic acid salts for use herein include organic polymers containing carboxylate monomers carboxylates such as citrate aminocarboxylates such as salts of MGDA GLDA etc.The hygroscopic material not only contributes to the stability of the pack but it is also an active ingredient in thecleaning process.Preferably the first composition comprises from 10 to 60 more preferably from 20 to 60 and especially from 30 to 60 by weight of hygroscopic material.
Patent claim: The ultrasound apparatus of claim 1 wherein the display unit displays the measuring device image in a halftransparent way so that an area of the ultrasound image which overlaps the measuring device image is not covered by the measuring device image.

Related passage: Afterward the ultrasound apparatus 100 may activate all of the first reference point 810 the second reference point 820 the third reference point 830 and the fourth reference point 840.Thus the user may move a position of the first reference point 810 by instantly touching and dragging the first reference point 810 in a right direction without separate manipulation.
Patent claim: A method as recited in Claim 12 further comprising the step of applying anairplane reference mark to the airplane so that the at least one reference mark and the airplane reference mark are configured to visually indicate a level of airplane alignment.

Related passage: The third video camera 50 is located substantially on the centerline of the airplane fuselage on the leading edge of the vertical tail 52 of the airplane 24.Like the first video camera 20 the third video camera 50 views forward.As a result the images produced by the third video camera 50 provide prospective forward looking guidance.The viewing angle 54 of the third video camera 50 is adjusted so that the tires 40 and 42 of the left and right wing landing gear 36 and 38 are simultaneouslyvisible.A pilot viewing an image produced by the third video camera 50 can visually judge main landing gear to pavement edge margins as needed in taxiway turns and at the start of runway or turnpad Uturns.
Patent claim: The battery pack of any of claims 1 to 13 wherein each of the battery cells includes a first side portion through which an electrode tap is withdrawn and the battery pack optionally further include lead plates extending along first side portions of the battery cells to electrically connect neighboring battery cells to each other optionally the lead plates include a first lead plate for electrically connecting the protective circuit module when present and the battery cells disposed at a side of the protective circuit module and a second lead plate for electrically connecting the protective circuit module when present and the battery cells disposed at the other side of the protective circuit module.

Related passage: The PCM 31 has external terminals 31a electrically connected with the outside.Further the PCM assembly 30 has the electrode lead 32 extending from the PCM 31 to be connected with the bottom 223 of the secondary battery cell 200.Theends 32a 32b of the electrode lead 32 are separated and electrically connected to the bottoms 223 of the two secondary battery cells 200 respectively.
Patent claim: The apparatus of claim 9 wherein a user associated with the wireless node assigns priority to services.

Related passage: According to one embodiment of the present invention every peer Ni implements a socalled service announcement message pool Pi.Thereby any service announcement message Mik received by this peer Ni is tagged with a relevance value rik.After that all relevance values rik in the pool are summedup thus yielding a cumulative relevance value wherein Ki denotes the total number of service announcement messages Mik stored in said peers pool Pi.Once this cumulative relevance value Ri exceeds a predefined threshold value Rthi all messages in the pool Pi are aggregated and sent to any neighboring peer Ni.Said relevance values rik can be very small for service announcements that are not of high importance and higher for more important ones.The speed with which messages are distributed in the network can thus be controlled in a finegrained way.
Patent claim: The turbomachine secondary ring seal assembly 46 of claim 1 wherein the sealing surface 70 is an axially extending sealing surface.

Related passage: Figure 3 is an enlarged view of Section 3 of Figure 2.A carbon seal 40 is located axially between the bearing 30 and the air compartment 34 to retain any leakage oil 39 from the bearing compartment 32.The carbon seal 40 has an annular shape and is mounted about the engine shaft 28.The carbon seal 40 seals with the rotating spacer 401 and contacts a static liner housing 44 of the turbine engine 10.Seal 40 is static and seal points x and y are formed.The arrows show the direction of buffer air flow.
Patent claim: Server computer configured to perform the method according to claim 2 or any one of claims 4 to 28 when depending from claim 2.

Related passage: Typically in accordance with the present disclosure the registration means is adapted to optionally present the user with a plurality of questionsprompts the registration means further adapted to enable the user to input a plurality of personal details in the form of numbers as answers for the questionsprompts the registration means further adapted to store the numbers along with the corresponding questionsprompts.
Patent claim: The method according to any one of claims 1 to 10 wherein the other object comprises an invehicle cradle and the one or more actions comprising any one or more of initiating a global positioning system application having a Bluetooth radio activated activating a synchronization with a vehicle system and changing to a notification profile having a relatively loud profile tone.

Related passage: Fig.9 is another embodiment of a portable information device 900 comprising a processor 902 that communicates with a magnetic field sensing device 910 that comprises both a magnetic switch and a three axis electronic compass integrated into one component.The electronic compass 906 is a three axis compass made up of a Yaxis sensor 916 an Xaxis sensor 918 and a Zaxis sensor 920 in communication with the processor 902.A magnet 914 is used in combination with the Zaxis sensor 920 to realize a magnetic switch.Similar to the previous embodiments when the portable device is open the Zaxis serves as an electronic compass component.When the device is closed the Zaxis sensor 920 provides a signal corresponding to the device being closed.Alternatively the Xaxis sensor 918 or Yaxis sensor 916 could be used instead and a signal representing other information besides the device being closed can be generated using any one of the sensors.
Patent claim: The apparatus of claim 1 wherein supposing that a plane displaying the interest tags is the XY plane the general broadcast information is displayed on a firstplane parallel to the ZX plane a second plane touching the ZX plane and the YZ plane and parallel to a Z axis and a third plane parallel to the YZ plane.

Related passage: FIG.1A illustrates an example of program information which may be included in a broadcast stream.In this example the program information included in the broadcast stream is related to different types of sports programs e.g.baseball football soccer etc.In addition to different types of sports programs more detailed information may also be included in the program information.
Patent claim: The method of claim 1 further comprising in the location management computer in response to reception of the information identifying the consumer product from the personal electronic device and determining the location of the personal electronic device at the time of acquiring the information identifying the consumer product checking a consumer product location database for a current location of the consumer products of the same type as said consumer product if the current location of the consumer products of the same type as said consumer product matches with the determined location of the personalelectronic device at the time of acquiring the information identifying the consumer product maintaining the current location of the consumer products and if the current location of the consumer products of the same type as said consumer product does not match with the determined location of the personal electronic device at the time of acquiring the information identifying the consumer product updating the determined location of the personal electronic device as the current location of the consumer products of the same type as said consumer product.

Related passage: According to a first aspect there is provided a method for updating a retail planogram comprising the steps of reading an electronic transmission from at least one RFID tag in a retail environment located in proximity to a product using a personal shopper device having a location sensing mechanism a memory a software means and an RFID reader wherein an initial planogram is stored therein collecting said read electronic location information transmitted from said at least one RFID tag by said shopper device analyzing and comparing said collected location information by said software means of said shopper device with said initial planogram inrelation to initial location information of said product with collected location information for said product from said collected information updating said initial location information for said product in said initial planogram in response to collected location information to provide an updated planogram to display current location information for said product in a current planogram arrangement in said retail environment.
Patent claim: A method 300 for operating a multishaft aeronautical gas turbine engine having an electrical machine the electrical machine including a starterelectric generator driven by at least one of the shafts of the gas turbine engine the method comprising determining 302 a desired amount of thrust to be produced from the gas turbine engine determining 304 a desired amount of electrical power to be drawn from the starterelectric generator of the gas turbine engine producing 306 the desired amount of thrust using the gas turbine engine and drawing 308 less than the desired amount of electrical power from the starterelectric generator of the gas turbine engine to allow the gas turbine engine to produce the desired amount of thrust to produce the desired amount of thrust more quickly or to maintain a stall margin.

Related passage: The power control device 29 calculates a total electricity generation torque required from the total power consumption of the loads detected by the power detection circuit 27 power loss in the electric systemelectrical characteristics of the first and second electric motors 21 22 and others.The total electricity generation torque required is a torque required to generate power corresponding to the total power consumption and thus the sum of electricity generation torques required to be applied to the first and second electric generators 21 22.The power control device 29 also calculates a surge margin on the basis of the total electricity generation torque required operating conditions of the jet engine 10 flight conditions of the aircraft and the like obtained from the engine control device 35.Then the power control device 29 manipulates the first and second power regulation devices 25 26 to ensure a specified amount or greater of jet engine 10 surge margin.
Patent claim: The tower section 100 of any of the preceding claims wherein the first set of coupling elements 20 is pivotable to the tower section 100 and the second set of coupling elements 30 is fixed to the platform 10.

Related passage: In a further aspect a platform for a tower is provided wherein the tower includes an inner surface that defines a cavity therethrough wherein the cavity has a first crosssectional area and a second crosssectional area that is different from the first crosssectional area.The platform includes a support frame and a floor coupled to the support frame.The platform also includes a plurality of mounting assemblies coupled to the support frame and the floor the mounting assemblies configured to mount the platform within the tower at one of the first crosssectional area and the second crosssectional area of the cavity.
Patent claim: Apparatus according to any of claims 1 to 12 the apparatus further comprising a further blister 14 whereinthe further blister 14 is for either housing at least part of one or more sensors or having at least part of one or more sensors mounted to or integrated with an outer surface of the blister 14 the further blister 14 is positioned on an underside portion of the aircraft wing 10 at a different spanwise location to the blister 14 and the further blister 14 is positioned on an underside portion of the aircraft wing 10 such that the further blister 14 does not project from the underside of the aircraft wing 10 beyond a leading edge 12 of the aircraft wing 10 in a direction parallel to a roll axis of the aircraft 2 and the further blister 14 does not project from the underside of the aircraft wing 10 beyond a lowermost surface of the aircraft wing 10 in a direction parallel to a yaw axis of the aircraft 2.

Related passage: Angle of sideslip AOS could be measured directly by mounting an additional unit on the bottom of the aircraft instead of on the side.Alternatively AOS could be derived by comparing differential static pressures or AOA angles between sensors on opposite sides of the aircraft.
Patent claim: The display apparatus according to claim 1 wherein if a multiview function is set the controller searches for and displays on the display multiview devices which pair with the display apparatus and controls the display to display thereon the UI to select the channel and the display mode of the at least one multiview device selected from the searched multiview devices.

Related passage: FIG.13C illustrates an operation for performing pairing between the second viewing device 195b and the image display device 100 while an image 1330 of a specific channel CH 9 is being displayed on the display 180 in synchronization with the first viewing device 195a.In one example a pairing signal 1335 may be transmitted from the image display device 100 to the second viewing device 195b.In another example a pairing signal 1335 may be transmitted from second viewing device 195b to the image display device 100.