bhlim/patentmatch_for_finetuning huggingface dataset:
Patent claim: A method of mounting one or more sensors to an aircraft wing 10 the method comprising providing a blister 14 either housing at least part of the one or more sensors in the blister 14 or mounting at least part of the one or more sensors to or integrating at least part of the one or more sensors with an outer surface of the blister 14 and positioning the blister 14 on an underside portion of the aircraft wing 10 such that the 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 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 method according to any one of claims 9 to 12 wherein turbine exhaust air is discharged to a heat source present on board the aircraft so as to cool the heat source.

Related passage: In one embodiment the aircraft airconditioning system 10 also includes a discharge device 26 which may be located in the aircraft cabin 20.The discharge device 26 may be controlled by the controller 24 which can instruct the discharge device 26 to forward the circulated air from the aircraft cabin 20 to either the turbine 18 or out of the aircraft.In one embodiment the controller 24 may instruct the discharge device 26 to forward the circulated air from the aircraft cabin 20 to the turbine 18 if the ambient air pressure is lower than the cabin air pressure and to forward the circulated air from the aircraft cabin 20 out of the aircraft if the ambient air pressure is equal to or approximately equal to the cabin air pressure.In another embodiment the controller 24 may instruct the discharge device 26 to forward the circulated air from the aircraft cabin 20 to the turbine 18 if the difference in the ambient air pressure and the cabin air pressure exceeds a threshold value and to forward the circulated air from the aircraft cabin 20 out of the aircraft if the difference in the ambient air pressure and the cabin air pressure is below a threshold value.
Patent claim: The method according to claim 1 characterized in that the method includes forming a chalcogenide semiconductor film 1220 selected from a group consisted of IVVI IIIIVI and IIIIVVI compound.

Related passage: The method of preparing a Group 1a1b3a6a material comprises providing a substrate optionally providing a Group 1a source comprising sodium providing aseleniumGroup 1b ink of the present invention providing a Group 3a source optionally providing a Group 6a source forming at least one Group 1a1b3a6a precursor material on the substrate by optionally using the Group 1a source to apply sodium to the substrate using the seleniumGroup 1b source to apply selenium and a Group 1b material to the substrate wherein the Group 1b material selected from copper and silver preferably copper using the Group 3a source to apply a Group 3a material to the substrate optionally using the Group 6a source to apply at least one of sulfur and selenium to the substrate treating the precursor material to form a Group 1a1b3a6a material having a formula NaLXmYnSpSeq wherein X is at least one Group 1b material selected from copper and silver preferably copper Y is at least one Group 3a material selected from aluminum gallium and indium preferably indium and gallium 0L0.75 0.25m1.5 n is 1 0p lt 2.5 and 0 lt q2.5.Preferably 0.5Lm1.5 and 1.8pq2.5.Preferably Y is In1bGab wherein 0b1.More preferably the Group 1a1b3a6a material is according to the formula NaLCumIn1dGadS2e1fSe2ef wherein 0L0.75 0.25m1.5 0d1 0.2e0.5 0 lt f1 wherein 0.5Lm1.5 and 1.82ef2e1f2.5.Optionally one or more of the Group 1a source the seleniumGroup 1b ink the Group 3a source and the Group 6a source of the present invention are combined before application to the substrate.The components of the precursor material can be treated by known methods to form the Group 1a1b3a6a material having formula NaLXmYnSpSeq.The components of the precursor material can be treated individually or in various combinations.Annealing temperatures for the deposited components can range from 200 to 650C with annealing times of 0.5 to 60 minutes.Optionally additional Group 6a material can be introduced during the annealing process in the form of at least one of a selenium ink selenium vapor selenium powder hydrogen selenide gas sulfur powder and hydrogen sulfide gas.The precursor materials can optionally be heated to the annealing temperature by use of a rapid thermal processing protocol such as with the use of a highpowered quartz lamp a laser or microwave heating methods.The precursor materials can optionally be heated to the annealing temperature using traditional heating methods for example in a furnace.
Patent claim: The induction heat cooking apparatus according to claim 10 wherein to drive the first and second heating coils 341 342 in parallel the controller 380 is configured to control the second switching device 322 to be closed and during a half resonant period to control the first switching device 321 to be in a closed state and to control the third switching device 323 to be in an opened state and during the other half resonant period to control the first switching device 321 to be in the opened state and to control the third switching device 323 to be in the closed state.

Related passage: Referring to FIGS.10 and 11 in response to the third operation mode being selected the switching controller 270 outputs a third switching signal to the first second and third switches S1 S2 and S3.
Patent claim: The method as claimed in any one of claims 9 to 12 further comprising displaying a graphic user interface GUI image for editing the file according to execution of the file editing application.

Related passage: However one or more exemplary embodiments are not limited thereto thus when the device 1000 enlarges and displays the partial region of the content the device 1000 may perform image processing on the partial region of the content into a high imagequality image and may display the partial region.
Patent claim: A washing machine comprising a cabinet a tub provided within the cabinet a support member for supporting the tub and a laundry weight sensing apparatus having a first portion attached to the support member and a second portion attached to the cabinet the laundry weight sensing apparatus being configured to use load of the tub transmitted to the support member to sense the weight of laundry within the tub.

Related passage: FIG.2 is a schematic view of a weight sensing unit.As shown in FIG.2 one end 140a of the spring 140 may be hung on a weight sensing unit 160 to be coupled to a frame 103 of the cabinet 100.That is the spring 140 may be installed between the tub 110 and the frame 103 of the cabinet 100.
Patent claim: The induction heater as claimed in any of claims 16 wherein the induction heater fits within the following size envelope about 15inches 381mm long and about 12.5 inches 24.4 mm63.5mm in variable width.

Related passage: In a particularly preferred embodiment a heater apparatus 10 is provided and may be used for automotive repair.Apparatus 10 may be powered by a 240volt AC power source and may utilize a frequency in a range of 1550 KHz.Apparatus 10 may include an eddy currenthysteretic circuit with an induction work coil 19.The circuit may be engaged to the power source.A plurality of handheld manipulable applicators 18 may also be provided and may be functionally engaged to the circuit for use in applying heat generated by the circuit to desired areas of automotive vehicles.
Patent claim: A control device according to any of claims 110 wherein the processor is configured to carry out the forming of the control quantities for a flow 130 of the timing messages transferred towards the control device and transmitted in accordance with the second clock signal and also for another flow 131 of timing messages transferred in the opposite direction and transmitted in accordance with the first clock signal produced with the clock signal generator and wherein the processor is configured to calculate a weighted sum of all the control quantities and control the clock signal generator with the weighted sum of all the control quantities.

Related passage: In a computer program according to an embodiment of the invention the software means also includes instructions readable by a programmable processor for making said programmable processordetermine which portion of the reference value of the control variable corresponds to synchronisation messages received from each of the at least two other network elements and in response to a situation where the reception from one of the at least two other network elements of synchronisation messages meeting a predetermined quality criterion ceases change the reference value of the control variable by an amount equalling a portion of the reference value of the control variable which portion corresponds to the network element from which the reception of synchronisation messages meeting the predetermined quality criterion has ceased.
Patent claim: A vehicle driving mode display device that has a screen where a running speed pattern a tolerance range of the running speed pattern and a vehicle speed at a moment when a measurement is conducted are plotted on a graph where time and the vehicle speed are plotted on each axes wherein the display device judges whether or not a following first condition or a following second condition is satisfied in a case that the vehicle is driven within the tolerance range and if satisfied issues a warning.The first condition in a case that a difference between a standard speed indicated by the running speed pattern and the vehicle speed is gradually widened as time elapses.The second condition in a case that the vehicle speed exceeds the tolerance range within a predetermined allowable time period when an acceleration at the moment is presumed to be kept.

Related passage: Fig.7 shows one example of the vehicle testing apparatus.In Fig.7 the symbol 21 represents a rotation roller on which the driving wheel 22a of a vehicle 22 under test is mounted and the symbol 23 represents a chassis dynamometer operatively connected to the rotation roller 21 through the shaft24.This chassis dynamometer 23 corresponds to the dynamometer 3 of the engine testing apparatus 1.The symbol 25 represents a flywheel provided on a shaft24 and the symbol 26 represents a speed sensor provided on the shaft 24.The speed sensor 26 corresponds to a sensor not shown for outputting a rotation measurement value in Fig.4 showing the engine testing apparatus 1.This sensor is provided in an engine 2 shown in Fig.4 in the engine testing apparatus 1.The symbol 27 represents a torque sensor provided in the chassis dynamometer23 and this corresponds to the torque measuring device 8 of the engine testing apparatus 1.The symbol 28 represents a running resistance generator for generating a target running resistance signal T corresponding to an actual running speed signal v sent from the speed sensor 26.The symbol 29 represents a chassis dynamo controller for driving and controlling the chassis dynamometer 23 such that a running resistance target running resistance corresponding to the actual running speed is applied to the driving wheel 22a based on a difference signal between an actual running resistance signal t sent from the torque sensor 27 and a target running resistance signal T sent from the running resistance generator 28.The chassis dynamo controller 29 corresponds to thedynamo controller 3 of the engine testing apparatus 1.The symbol X represents a drivers aid display unit on which a set target driving pattern V0 corresponding to running speed pattern I in Figs.10 and 11 and the running speed pattern J in Fig.9 and a variation of data position V showing driving state of actual current time actual running speed signal v of current time sent from the speed sensor 26 are displayed such that the driver of the vehicle can visually check.
Patent claim: The environmental control system as recited in claim 9 wherein a check valve is disposed within said first passage associated with said low pressure tap.

Related passage: As illustrated the auxiliary compressor 42 is mechanically connected to a motor 48 via shaft 50.The auxiliary compressor 42 powered by the aircraft electricity source not shown augments the compressed LPC bleed air when the bleed air cannot provide adequate pressurization to the ECS 38.It is to be appreciated that air entering bleed passage 40 is at a pressure and temperature substantially higher than what is needed by ECS 38.In one embodiment the minimum bleed air pressure is at 20 psi 137.9 kPa in order for ECS 38 to maintain cabin pressure to 11.8 psi 81.4 kPa and provide fresh air at 0.55 Pounds 0.25 kg MassMinutePerson.
Patent claim: A cartridge buttress retention system 30 to retain a cartridge buttress material 26 on a staple cartridge 122 prior to stapling of tissue comprising a staple cartridge 122 including a Ushaped outer channel 108 surrounding a staple containing insert 110 a post 116 formed at a distal end 118 of the staple containing insert 110 distally extending fingers or projections 124 126 formed in a proximal end 128 of the staple containing insert 110 and a cartridge buttress material 26 retained on the staple cartridge 122.

Related passage: Perforated buttress strip 100 is a rectangular sheet formed from any of the buttress materials described above and has rows of spacedapart openings 101 extending therethrough.Perforated buttress strip 100 is attached onto the carrier shell 91 by threading each horizontal arm 94 fully into each respective opening 101 within the perforated buttress strip 100 until the openings 101 are brought into contact with the first member 93a or vertical portion of the L shaped hooks 93.Moving the perforated buttress strip 100 distally relative to the carrier shell 91 moves the openings 101 off of the arms 94 and releases the perforated buttress strip 100 from the carrier shell 91.Thus the perforated buttress strip 100 is detachable from the carrier shell 91 by linear motion in one direction.Arrows are provided in FIG.7 to show the path of the openings 101 as the perforated buttress strip 100 is threaded onto the arms 94.
Patent claim: An apparatus for reproducing data from a disc the apparatus comprising a storage which stores discless application data including program data which corresponds to a discless application that is not recorded in the disc and a discless application description DAD which is used to access the program data and an application driver which executes an application recorded in the disc by using application data recorded in the disc executes the discless application by using the discless application data stored in the storage and controls a life cycle of the discless application in such a manner that the life cycle of the discless application is not dependent upon whether the disc has been loaded.

Related passage: The lifecycle of the interactive application started within the first diagram in Fig.3 is continued by one of the two next flow charts of Fig.4 and Fig.5 but always only one out of the two.Any end state B in a diagram is followed by either a start state B1 or a start state B2.
Patent claim: The information processing system 100 according to any one of claims 1 to 6 wherein the first information is identification information indicating a character string that is shorter than a character string that constitutes the IP information or name information indicating a name of the secondinformation processing device 1210 the second information is information in which the identification information the name information and the IP information are associated with one another the first receiving unit 1211 includes a second receiving unit 1212 that receives input of the identification information a third receiving unit 1213 that receives input of the name information and an input distributing unit 1214 that distributes the input character string to the second receiving unit and the third receiving unit and the determining unit 1421 compares the input character string received by the second receiving unit 1212 and the third receiving unit 1213 with the identification information and the name information included in the second information for each of at least one piece of the second information stored in the second storage unit 141 and determines a first information processing device 10 identified by IP information included in any one of pieces of second information that include the identification information or the name information corresponding to the input character string as the first information processing device 10 to execute the process requested from the user.

Related passage: When it is determined that a response returns the process assigns another IP address and checks if there is a conflicting network device.The process repeats the retrieval until no conflicting network device is detected.After the IP address has been finally assigned the process outputs a connection response to the server 20 step S745.This establishes a TCPIP connection with the server 20 and starts intercommunication with the server 20 step S750.When it is determined at steps S710 and 720 that there is no matching unique information or keyword the process projects a message indicating an unsuccessful connection allowing the user of the server 20 to visually confirm the message step S755.When the intercommunication with the server 20 starts at step S750 the server 20 can input imagedata.Then the client executes the image display process to be described next.
Patent claim: A method for implementing an antenna structure 100 FIG.1FIG.2 along a loop 102 comprising placing a feed terminal d1 for connecting a feed signal Sf1 placing an intermediate grounding terminal hg1 placing a tail grounding terminal g1 for connecting a ground plane G1 so as to form a head section sa1 being conductive extending from the feed terminal to the intermediate grounding terminal along the loop capable of supporting a third electromagnetic resonance FIG.5c with two antinodes respectively at the feed terminal and the intermediate grounding terminal during a second operation mode and an intermediate section sb1 being conductive extending from the intermediate grounding terminal to the tail grounding terminal along the loop capable of supporting a second electromagnetic resonance FIG.5b with two antinodes respectively at the intermediate grounding terminal and the tail grounding terminal during the second operation mode wherein during a first operation mode the head section and the intermediate section are further capable of jointly supporting a first electromagnetic resonance FIG 5a with two antinodes respectively at the feed terminal and the tail grounding terminal without antinodes locatedbetween the feed terminal and the tail grounding terminal on the head section and the tail section.

Related passage: A graph in which the impedance Z for a resonant circuit such as resonant circuit 42 of FIG.6 has been plotted as a function of operating frequency f is shown in FIG.7.As shown by line 58 of FIG.7 the impedance of the resonant circuit may be relatively low at higher frequencies such as frequency fb and may be relatively high at lower frequencies such as frequency fa that are at or near the resonance frequency for the circuit in this example.Due to the frequencydependent behavior of the impedance Z of the resonant circuit resonantcircuitbasedcomponents such as component 42 of FIG.6 may be used to form short circuits or nearly short circuits at some frequencies of antenna operation e.g.one or more bands of frequencies in the vicinity of frequency fb and may be used to form open circuits or nearly open circuits at other frequencies of antenna operation e.g.one or more bands of frequencies in the vicinity of frequency fa.The openclosed behavior of resonantcircuitbased components such as component 42 may be used in implementing frequencydependent antenna configuration changes in antenna 40 instead of or in addition to using the openclose behavior of switched based components such as component 42 of FIG.5 in antenna 40.
Patent claim: The device according to claim 1 wherein the gate insulating film is a silicon oxide film.

Related passage: In the following embodiments of the invention are described with reference to the drawings.First a MISFET according to a first embodiment of the invention is described with reference to the drawings.With reference to Fig.1 A to Fig.4J a method for manufacturing the MISFET of the first embodiment is described.As shown in Fig.1 A on a 4HSiC0001Si substrate 1 a just substrate or a substrate having an offset angle of 15 or less in an arbitrary crystal direction if the offset angle is greater problems regarding the proximity of steps or the formation of facets would arise which would require consideration of other crystal growth mechanisms.The SiC crystal structure may be 6H instead of 4H.there is formed a SiC layer 1a by homoepitaxial growth for example.The epitaxial layer is a highquality singlecrystal layer.As shown in Fig.1B on the SiC layer 1a there is formed a mask R having openings in at least those regions where sourcedrain are to be later formed.Then N and P for example which are Group V elements are ionimplanted as impurities for forming an ntype conduction band in SiC.Thereafter a hightemperature annealing process is performed so as to electrically activate the ionimplanted atoms whereby sourcedrain regions 3a3b are formed as shown in Fig.1C.
Patent claim: The turbine blade damping system of claim 3 further comprising a first lip extending radially outwardly from a first of the feet proximate a free end thereof and a second lip extending radially outwardly from a second of the feet proximate a free end thereof.

Related passage: Referring now to the drawings in which like numerals refer to like elements throughout the several views Figs.1 and 2 illustrate a bucket damping system 100 as is described herein.The bucket damping system 100 includes a number of buckets 105.The buckets 105 may include a bucket airfoil 110 a platform 120 a shank 130 a dovetail 140 and other elements.It will be appreciated that the bucket 105 shown is one of a number of circumferentially spaced buckets 105 secured to and about the rotor of a turbine.As described above turbines generally have a number of rotor wheels having axial or slightly off axis dovetailshaped openings for receiving the dovetail 140 of the bucket 105.Likewise the airfoils 110 project into the gas stream so as to enable the kinetic energy of the stream to be converted into mechanical energy through the rotation of the rotor.
Patent claim: A control method in which a predetermined drive voltage waveform is applied to a piezoelectric element and ejection of a pulsed liquid jet from a liquid ejection device that uses the piezoelectric element and ejects a liquid having a pulsed shape is controlled the control method comprising inputting a first instructing value related to kinetic energy of the pulsed liquid jet inputting a second instructing value related to the number of times of ejection of the pulsed liquid jets per unit time and setting an index value related to rising of the drive voltage waveform such that the kinetic energy becomes the first instructing value based on voltage magnitude of the drive voltage waveform and the second instructing value.

Related passage: There are surgical instruments fluid ejection devices configured to incise or excise a living tissue by ejecting fluid at a high speed in a pulsed manner.The fluid ejection device includes a pulsed flow generating unit configured to transform fluid into a pulsed flow.The fluid ejection device is configured to eject the fluid at a high speed in the pulsed manner by driving the pulsed flow generating unit.