bhlim/patentmatch_for_finetuning huggingface dataset:
Patent claim: A landing gear assembly 200 comprising a first wheel and a second wheel a first wheel sensor coupled to the first wheel and a second wheel sensor coupled to the second wheel a controller 110 coupled to the first wheel sensor and the second wheel sensor and a tangible nontransitory memory configured to communicate with the controller the tangible nontransitory memory having instructions stored thereon that in response to execution by the controller cause the controller 110 to perform operations comprising receiving 302 by the controller 110 data from the first wheel sensor and the second wheel sensor calculating 304 by the controller 110 a wheel speed characteristic for each of the first wheel and the second wheel based on the data identifying 306 by the controller 110 a lowest value for the wheel speed characteristic determining 308 by the controller 110 a moving average for the wheel speed characteristic comparing 310 by the controller 110 the lowest value to the moving average and determining 312 by the controller 110 whether the lowest value for the wheel speed characteristic indicates a dragging brake.

Related passage: Step 510 comprises comparing the deviation from the slip ratio average to a predetermined threshold value.In this regard if the deviation from the slip ratio average exceeds the threshold value it may be determined that a dragging brake is present.In response to the determination a dragging brake signal may be send to another aircraft component.A pilot or other crew member may then use the dragging brake signal to delay landing gear retraction to allow the dragging brake additional time to cool.In various embodiments a value is set to true or false in response to the determination of a dragging brake.
Patent claim: The apparatus according to claim 1 or the method according to claim 4 wherein the first windings are directed about the longitudinal axis of the first coil.

Related passage: Console 34 uses magnetic sensing to determine pressure and position data including i axial displacement and angular deflection of the distal section 13 due to pressure from contact with endocardial tissue 70 and ii position coordinates of the distal section 13 in the heart.For the purpose of generating pressure data including axial displacement and angular deflection of the distal section 13 of the catheter 28 the driver circuit 38 in console 34 drives a miniature magnetic field generator MF housed in a distal portion 13D of the tip section 13 as shown in FIG.3.In the disclosed embodiment the field generator MF comprises a coil whose axis is aligned with the Z axis coaxial with a longitudinal axis 25 of the catheter.
Patent claim: The system of any of claims 10 to 12 further comprising a second engine system 204 utilizing an oil for heat transfer wherein the fueloil heat exchanger of the fuel system 206 is a first fueloil heat exchanger 218 wherein the fuel system 206 further comprises a second fueloil heat exchanger 220 wherein the second fueloil heat exchanger 220 is in thermal communication with the oil from the second engine system 204 and the fuel from the fuel system 206 for removing heat from the second engine system 204.

Related passage: The fuel is typically a hydrocarbon such as a liquid jet fuel.The FSU 14 includes a deoxygenation system 28 which permits the fuel to remain stable at much higher temperatures without coking by removing dissolved oxygen from the liquid fuel which enables higher temperature loads to reject their heat to the fuel.It should be understood that various deoxygenation systems will benefit from the present invention.
Patent claim: The RFID tag according to claim 15 wherein the length I of the protector is a length along a longitudinal direction of the substrate.

Related passage: The reinforcing member 50A is adhered to a portion of a surface 10A a bottom surface as illustrated in FIG.2A of the base 10.The portion to which the reinforcing member 50A is adhered is located under the IC chip 30 and the connecting portion 20A which connects the IC chip 30 and the antenna 20.The reinforcing member 50A covers the IC chip 30 and the connecting portion 20A through the base 10.
Patent claim: The adapter assembly of any preceding claim wherein the first cam assembly includes a cam member having an eccentric outer surface and the second drive member includes an engagement portion for engaging the eccentric outer surface.

Related passage: In particular as seen in FIGS.5 and 6 adapter assembly 100 further includes a drive coupling assembly 112 at a proximal end portion thereof which operatively couples adapter assembly 100 to powered actuator device 20.Drive coupling assembly 112 includes rotatably supported and distally extending first and second proximal drive shafts 116 118 respectively.Proximal drive shafts 116 118 may be made flexible to act as shock absorbers allowing for reduced peak loads yet sufficiently rigid to transmit rotational forces.First and second proximal drive shafts 116 118 each include at a proximal portion thereof a tapered neck portion not shown having a noncircular crosssectional profile e.g.square shaped.Each of first and second proximal drive shafts 116 118 is provided with a biasing means not shown disposed about the respective neck portion and a sleeve not shown disposed proximal of the biasing means.The sleeves each define a bore having a crosssectional profile that corresponds to that of the neck portion of proximal drive shafts 116 118.The distal ends of the first and second drive shafts of powered actuator device 20 include coupling cuffs 120 122 each defining a recess 120a 122a corresponding to the noncircular crosssectional profile of the neck portion of proximal drive shafts 116 118.Coupling cuffs 120 122 of actuator device 20 engage theproximal end portions not shown of proximal drive shafts 116 118 wherein each proximal end portion of the proximal drive shafts 116 118 has a noncircular crosssectional profile for engaging respective recess 120a 122a of coupling cuffs 120 122 whereby rotation of drive shafts not shown of powered actuator device 20 results in concomitant rotation of coupling cuffs 120 122 and concomitant rotation of first and second proximal drive shafts 116 118.
Patent claim: The method of any preceding claim further comprising passing a cooling fluid 75 through the heat exchanger 76.

Related passage: FIG.5 illustrates a crosssectional and schematic view of the cooling system 250 according to an aspect of the present invention.The heat pipe 252 is located in the nozzle 134 and is in thermal communication with heat pipe 254.A plurality of heat pipes 252 e.g.a first subgroup of heat pipes are located in a plurality of nozzles for example there may be one heat pipe in one nozzle.The heat pipes 254 e.g.a second subgroup of heat pipes may be contained within the turbine casing or attached to the turbine casing.The manifold 256 is thermally connected to multiple heat pipes 254 and the heat pipes 254 may be arranged circumferentially about the turbine casingshell 131.The manifold 256 includes a coolantheat transfer medium such as water steam glycol or oil.The manifold 256 is thermally connected to a heat pipe heat exchanger 240.A conduit 310 connects the heat pipe heat exchanger 240 to a plurality of other heat exchangers.For example the other heat exchangers may be a fuel heating heat exchanger 241 a fuel preheating heat exchanger 242 a HRSG heat exchanger 243 and any other desired heat exchanger 244.The heat pipe heat exchanger 240 transfers the heat from the manifolds 256 to the heat transfer medium in conduit 310.As examples only the conduits heat transfer medium may be water glycol oil steam or any other suitable fluid or gas.A pump 320 may be used to force the fluid through the conduit 310 and the heat exchangers.The heat exchangers may also include valve controlled bypass lines 260 only one is shown for clarity.A valve 261 can be operated so that it directs flow around the heat exchanger e.g.242 via bypass lineconduit 260.This feature may be desirable if specific heat exchangers are to be removed possibly temporarily from the flow along conduit 310.The valves 261 can be manually controlled or remotely controlled.
Patent claim: A method of producing the beverage composition the food composition the functional food the cosmetic the supplement the quasi drug or the pharmaceutical product according to claim 14 the method comprising adding an extract of one or more types of plants selected from the group consisting of fenugreek fennel and hibiscus to a beverage composition a food composition a functional food a cosmetic a supplement a quasi drug or a pharmaceutical product in order to provide it with at least one of an oxidized protein hydrolase activity enhancing effect and a glycation stress inhibitory function.

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 semiconductor device 10 50 according to claim 1 wherein the semiconductor element 20 90 100 includes a diode the first electrode 21 91 101 includes an anode electrode of the diode and the second electrode 22 92 102 includes a cathode electrode of the diode.

Related passage: One side of the diode chip 2 is provided with the electrode surface 21a of the anode electrode 21 and the other side thereof is provided with an electrode surface 22a of a cathode electrode 22.The electrode surface 21a of the anode electrode 21 is connected with solder 7 on the same plane as that of the first bus bar 3 where the IGBT chip 1 is connected.The electrode surface 22a of the cathode electrode 22 is connected with solder 8 on the same plane as that of the second bus bar 4 where the IGBT chip 1 is connected.
Patent claim: The turbine stage 10 according to claim 6 wherein each of the trailing edge ridge structures 50 adjoins said pressure side 20 said suction side 22 and said trailing edge 26 of each respective airfoil 14 with the respective platforms 16.

Related passage: In the embodiment the front edges 12a and 12b of the blade bodies 11a and 11b are provided with coatings 14a and 14b which laterally extend from the front edges 12a and 12btoward the upstream side and have cross sections formed as the protruded portions 16a and 16b each raised to the heights of the front edges 12a and 12b.The wall surface 13 for supporting the blade bodies 11a and 11b includes the downward inclined surface 19 linearly angled so as to extend from the edge line of the front edges 12a and 12b toward the upstream side.The flow rate of the working fluid flowing to the coatings 14a 14b and the inclined surface 19 is accelerated to suppress generation of the horseshoe vortex.This makes it possible to further reduce the secondary flow loss by diminishing the strength of the passage vortex.
Patent claim: The clock circuit according to claim 5 wherein a highlayer metal is used for the Hshaped clock network.

Related passage: Fig.3 is a logic diagram of one embodiment of a clockgating unit.The configuration of clockgating unit 25 shown in Fig.3 may be used to implement the coarse clockgating units 14 and the fine grain clockgating units 16 discussed above.However it is noted that in some embodiments the coarse and fine grain clockgating units may be implemented using different configurations.
Patent claim: The device according to claim 14 wherein the determining module is specifically configured to when there are at least two MAC entities determine that the third mapping is specifically a mapping between a logic channel identity and a transport channel identity or the third mapping is specifically a mapping between an RB identity and a transport channel identity or the third mapping is specifically a mapping between a logic channel identity and a MAC entity identity or the third mapping is specifically a mapping between an RB identity and a MAC entity identity or the fourth mapping is specifically a mapping between a transport channel identity and a physical entity identity or the fourth mapping is specifically a mapping between a transport channel identity and a cell identity or the fourth mapping is specifically a mapping between a MAC entity identity and a physical entity identity or the fourth mapping is specifically a mapping between a MAC entity identity and a cell identity.

Related passage: In the uplink user equipment has to signal Node B with a rate indicator message information that is necessary to decode the transmitted packets correctly e.g.transport block size TBS modulation and coding scheme MCS level etc.Furthermore in case HARQ is used the user equipment has to signal HARQ related control information e.g.Hybrid ARQ process number HARQ sequence number referred to as New Data Indicator NDI for UMTS Rel.5 Redundancy version RV Rate matching parameters etc.
Patent claim: The heat exchanger system 1100 of any preceding Claim wherein said outlet connection is configured to receive said flow of cooled fluid from said second heat exchanger assembly 300.

Related passage: Numeral 2 designates an inlet pipe of cooling steam and numeral 3 designates an outlet pipe of same.The inlet pipe 2 connects to an upstream end of the steam supply passage 31 of the steam chamber unit 1 and the outlet pipe 3 connects to a downstream end of the steam recovery passage 33 of same.A high pressure exhaust steam from a steam turbine not shown or steam from a boiler not shown etc.is supplied into the inlet pipe 2 as a cooling steam and a recovered cooling steam is supplied into a reheating portion of boiler or a downstream intermediate pressure steam turbine etc.not shown via the outlet pipe 3.
Patent claim: The device according to Claim 3 wherein the arrangement of icons corresponds to the selected application interface and the circuitry is configured to display the arrangement of icons within the selected application interface based on the determined tilt angle.

Related passage: Note that as the gradient detection portion 106 in the present invention a smaller component for detecting gradients is preferably used particularly.In such a case it is preferable to use a triaxial acceleration sensor using a MEMS technology because reduction in size of the mobile phone can also be achieved.
Patent claim: A gas turbine engine 100 comprising a core engine 116 including a multistage compressor 124 and a stall margin modulation SMM control system 180 in communication with said core engine 116 said SMM control system 118 comprising a processor 402 in communication with a memory 404 said processor 402 programmed to determine the stall margin 304 of the compressor 124 operate the gas turbine engine 100 using the determined stall margin 304 assess a health of the compressor 124 and modify the stall margin 304 based on the assessed health of the compressor 124.

Related passage: In yet another embodiment a gas turbine engine for use in an aircraft is provided.The gas turbine engine includes at least one sensor configured to sense an engine parameter and to generate a sensor input representing the engine parameter a control system configured to control at least one of the gas turbine engine and the aircraft and an estimation system coupled in communication with the control system.The estimation system is configured to output an estimated operating parameter to the control system.The estimation system includes a primary model configured to receive at least the sensor input and to estimate the operating parameter using at least the sensor input and a redundancy system configured to receive the estimated operating parameter and to determine whether an anomaly is present within the estimated operating parameter.
Patent claim: Ethylene copolymer composition according to any proceeding claims wherein the ethylene copolymer is a bimodal ethylene copolymer comprising a low average molecular weight ethylene homopolymer fraction and a high average molecular weight ethylene copolymer fraction.

Related passage: A base resin was produced in a multistage reaction comprising a first prepolymerisation stage in slurry in a 50 dm3 loop reactor followed by transferring the slurry to a 500 dm3 loop reactor wherein polymerisation was continued in slurry to produce the low molecular weight component and a second polymerisation in a gas phase reactor in the presence of the product from the second loop reactor to produce the comonomer containing high molecular weight component.As comonomer hexene1 has been used.
Patent claim: The fiber according to any of claims 19 wherein the depressed inner cladding comprises at least one additional portion located between the central core and the first portion of the depressed inner cladding said at least one additional portion having a refractive index difference with the outer optical cladding that lies between n1 and n3.

Related passage: Also referring now to Figs.6ab shown is a crosssectional view Fig.6a and corresponding refractive index profile Fig.6b of the refractive index profile of anoptical fiber 55 according to other embodiments of the invention.Like the profiles of the previouslydiscussed embodiments of the invention the fiber profile shown in Figs.6ab has a dopedsilica core 56 a first region 57 with an index of refraction less than that of the core region a second region 58 with an index of refraction less than that of the first region and an outer cladding 59 with an index of refraction greater than those of the first and second regions and less than that of the core region.Also the first region 57 has an outer radius d2 and an inner radius is d1.The second region 58 has an outer radius d3 and an inner radius d2.As shown in Fig.5b 10.148 20.187 and 30.200.Also in this particular arrangement d16.00 m d210.013 m and d329.013 m.Accordingly the width of the first region is 4.013 m 10.013 m6.00 m and the width of the second region is 19.000 m 29.013 m10.013 m.
Patent claim: The catheter of claim 1 wherein each spine has a first region that curves to change the orientation of the spine from being directed towards the distal end of catheter body at a first end of the first curved region to being directed towards the proximal end of the catheter body at a second end of the first curved region.

Related passage: In the depicted embodiment the mapping assembly 18 comprises five spines 14.Each spine 14 has a proximal end attached at the distal end of the catheter body 12 and a free distal end i.e.the distal end is not attached to any of the other spines to the catheter body or to any other structure that confines movement of the distal end.Each spine 14 contains a support arm 24 comprising a metal or plastic material that has shape memory such that the support arm 24 forms an initial shape when no external forces are applied forms a deflected shape when an external force is applied and returns to its initial shape when the external force is released.In a preferred embodiment the support arm 24 comprises a superelastic material for example a nickeltitanium alloy such as nitinol.Each spine 14 also comprises a nonconductive covering 26 in surrounding relation to the support arm 24.In a preferred embodiment the nonconductive covering 26 comprises a biocompatible plastic tubing such as a polyurethane or polyimide tubing.
Patent claim: The method of Claim 1 wherein determining the current state of the vehicle further comprises determining a current speed of the vehicle based on the sensor data.

Related passage: FIG.2 is a visual display 200 generated by the aircraft system 100 of FIG.1 in accordance with a first exemplary embodiment.The visual display 200 may be producedfor example on the display unit 170 FIG.1 discussed above and in this embodiment may correspond to a primary flight display.
Patent claim: A wind turbine power generating apparatus comprising the wind turbine blade according to claim 8 or 9.

Related passage: Referring now to FIG.2 another embodiment of the rotor blade 22 for use with the wind turbine 10 is illustrated in accordance with aspects of the present subject matter.In particular FIG.2 illustrates a perspective view of the rotor blade 22 including one embodiment of an airflow modifying assembly 30 mounted thereon.As shown the rotor blade 22 generally includes a blade root 25 configured to be mounted or otherwise secured to the hub 20 FIG.1 of the wind turbine 10 and a blade tip 27 disposed opposite the blade root 25.A body shell 17 of the rotor blade 22 generally extends between the blade root 25 and the blade tip 27.The body shell 17 may generally serve as the outer casingcovering of the rotor blade 22 and may define a substantially aerodynamic profile such as by defining a symmetrical or cambered airfoilshaped crosssection.
Patent claim: The seal as recited in any preceding claim wherein each of the seal arc segments 186 include an internal cooling passage 180 that opens at one of the sloped first and second circumferential sides 72a.

Related passage: As seen with particular reference to Figures 1 and 2 and as noted above the outer air seal 10 of the present invention incorporates several boundary members 12 grouped in a ringshaped arrangement to reduce unwanted leakage of working fluid 44 out of the turbine section 16 of an industrial gas turbine engine 18.More particularly the boundary members 12 are disposed proximate to but radiallyoutwardof the turbine section blades 14.In the present embodiment the boundary members 12 are identical and located at a uniform radial distance Rbm from a central axis 48.It is noted that while the present discussion is directed to an arrangement of uniform boundary members 12 arrangements involving nonuniform boundary members would also suffice.
Patent claim: The system 200 of claim 14 wherein each optical probe 100 is configured to obtain images of a plurality of turbine blades 68 located at one of the plurality of stages of the turbine 28 32.

Related passage: Then in the endoscopic inspection while the plurality of rotor blades are rotated around the rotating shaft AR by using the turning tool T the plurality of rotor blades provided on the rotating shaft AR are photographed by the borescope 2 inserted into the compressor portion E2 and the endoscopic inspection is conducted.
Patent claim: Use of an agent comprising as an active ingredient an extract of one or more types of plants selected from the group consisting of fenugreek fennel and hibiscus for enhancing oxidized protein hydrolase activity.

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.