bhlim/patentmatch_for_finetuning huggingface dataset:
Patent claim: A downhole system 100 for controlling a flow of fluid in a well downhole comprisinga well tubular metal structure 3 arranged in a borehole 4a downhole flow device 1 according to any of the preceding claimsa downhole manipulation tool 40 configured to move the sliding sleeve along the axial extension anda power supply 44 configured to power an operation of the downhole manipulation tool.

Related passage: The displaceable part 4 is displaceable in the axial direction in relation to the base part by means of a key tool operating with a stroking tool shown in Fig.14 engaging a groove 31 in the displaceable part 4.The completion component comprises a projecting element 34 arranged in a groove 35 in the displaceable part 4.The projecting element projects 34 from the displaceable part 4 and is adapted to engage grooves 36 in the tubular base part 3.When the key tool or stroking tool moves the displaceable part 4 axially in relation to the tubular base part 3 the projecting element 34 is forced to revert into the groove in the displaceable part 4 and the displaceable part 4 is moved axially until the projecting element 34 faces an internal groove 36 in the tubular base part 3 closest to groove 35.When the projecting element 34 is opposite the groove 36 the projecting element engages the groove and the displaceable part 4 is again locked for movement in the axial direction.The displaceable part 4 is now in its slightly open position in which the first opening 20 and the second opening 21 are overlapping.The completion component 1 can be further adjusted so that the openings overlap even more by moving the displaceable part 4 further in the axial direction in relation to the tubular base part 3 and the projecting element 34 is forced to retract and the displaceable part 4 can move to position the projecting element 34 opposite another of the internal grooves 36 in the tubular base part 3.In this way the displaceable part 4 is moved axially in relation to the tubular base part 3 from a first and closed position in which the first and second openings do not overlap to a fully open position in which the first and second openings overlap completely.In Fig.1 the completion component 1 can be arranged in the closed position and in ten other positions in which the openings 20 21 are more or less aligned.The projecting element may be a spring element such as a circlip or circlip ring or be connected by means of a spring device so that the projecting element is able to retract into the groove in the displaceable part 4.
Patent claim: A technological line for the process according to the preceding claims characterised in that it includes a vat with the above emulsion a set of two mixers a heating climatic chamber containing emulsion water an inert material calcium hydroxide additives and an aerogel.

Related passage: According to one feature of the present invention the first mixer is provided with at least a first mixing section disposed in proximity to the first containing means and a second mixing section disposed in proximity to the introduction means.In the first section the raw materials are mixed to reduce the presence of possible cement lumps that could be present when they are introduced in the second section the raw materials are mixed at least with water to define thecement agglomerate that will be unloaded into the second mixer.
Patent claim: The method 300 of claim 5 wherein rotating the gas turbine engine 10 comprises rotating the gas turbine engine 10 about the longitudinal axis 12 as the plurality of optical probes 100 are used to obtain images of a plurality of turbine blades 68 located at each of the plurality of stages of the turbine 28 32.

Related passage: Fig.5 is a diagram for explaining a state in which the first fixture 3A and the second fixture 4A to which the plurality of borescopes 2A and 2B which are not common are attached are mounted on the corresponding external access ports respectively.
Patent claim: The arrangement according to claim 14 wherein the first grating G1 creates a periodic interference pattern with pitch p1 at a known distance Talbot effect downstream and acts as structured illumination onto the second grating G2 which further creates a periodic interference pattern with pitch p2 at the detector plane.p1 and p2 match the radius of curvature of an incident wavefront by the relation p11p1d1l1l1 p21p2d2l2l2 and p1p2d2l2 where p1 and p2 are the pitch of G1 and G2 respectively l1 is the distance between the source or G0 if G0 is used to G1 distance d1 is the distance between G1 and the created structured illumination d2 is the distance between the structured illumination and G2 l2 is the distance between G2 and the detector1 forshift grating while2 for 2 shift grating.

Related passage: The two beams interfere in the analyser plane and cause a field of standing waves i.e.a field of interference lines with high and low intensity parallel to the grating lines and a periodicity equal to that of the second beam recombiner grating.The most important aspect of this invention is the fact that the interference lines occur even when the radiation is spatially incoherent i.e.coming from large source at close distance and temporally incoherent i.e.polychromatic.The lines only occur in certain planes namely when the conditions d2d3 is at least approximately fulfilled.Furthermore the condition p2p12 has to be at least approximately fulfilled.
Patent claim: The method of any of claims 16 wherein applications hosted with flightdeckinstalled multifunction display comprise a window on the flightdeckinstalled multifunction display a window managed across multiple flightdeckinstalled multifunction displays multiple application on multiple devices a diversity of pilot control interfaces including an ability to operate without the pilot control interfaces an abstract nature of hosted applications including a nonvideo application a compositing of certified andoperationally approved information a multiple user and sharedexclusive application environment application devicebased status information sent to a gateway including additional application categories or a combination thereof.

Related passage: If there is a turbulent condition then that condition may be indicated to the flight crew at 106.This may include providing an indication on the handheld device 40.For example an indication may be displayed on the display 44 of the handheld device 40.By way of additional example an audible indication may be emitted from the handheld device 40.Further if the determination of the turbulent condition is made by the handheld device 40 and not the controller 30 providing an indication of the turbulent condition may include transmitting a turbulence signal from the handheld device 40 to the aircraft 10.The controller 30 may then provide an indication on a display 22 on the flight deck 18 of the aircraft 10 in response to the turbulence signal which was transmitted from the handheld device 40.Alternatively the flight deck 18 may emit an audible indication in response to the turbulence signal provided by the handheld device 40.
Patent claim: Polypropylene composition C according to any one of the preceding claims wherein the polypropylene composition C has an intrinsic viscosity IV determined according to DIN ISO 16281 in Decalin at 135 C of the xylene soluble content XCS in the range of 0.7 to 2.0 dlg.

Related passage: The matrix polymers of the heterophasic polymers of component a may have a ratio of matrix polymer polymer of phase 1 to polymer of phase 2 of about 973 to 8020 preferably 955 to 9010.The heterophasic polymer shows a melt flow rate of about 0.1 to 200g10 min preferably 02 to 50g10 min more preferable 0.3 to 20 g10 min according to ISO 1133.The ethylene content of the matrix polymer may be up to 7 mol and the overall ethylene content of the heterophasic polymer of component a may be up to 30 mol preferably up to 15 mol.
Patent claim: The image forming apparatus according to claim 1 wherein the controller controls the image forming means based on the predetermined mode to form the first measuring images on the plurality of the first sheets and then control the image forming means to form the second measuring images on the second sheets.

Related passage: Fig.6 is a flowchart illustrating the workflow for a process according to this exemplary embodiment.A control program not illustrated for implementing this exemplary embodiment is stored in the storage device 121.The control program is loaded onto a random access memory RAM not illustrated and is executed by the CPU 103.
Patent claim: A hearing assistance device according to any one of claims 116 wherein the predefined scheme comprises selecting the time frequency units having the largest signal to noise ratio among corresponding time frequency units of the electric input signals.

Related passage: The hearing loss compensated output signal is transmitted through electrical wires contained in a sound signal transmission member 20 to a receiver 22 for conversion of the hearing loss compensated output signal to an acoustic output signal for transmission towards the eardrum of a user and contained in an earpiece 24 that is shaped not shown to be comfortably positioned in the ear canal of a user for fastening and retaining the sound signal transmission member in its intended position in the ear canal of the user as is wellknown in the art of BTE hearing aids.
Patent claim: The exhaust gas purification catalyst according to any one of claims 1 to 3 which is a catalyst for purifying NOx.

Related passage: Now an exhaust gas cleaning catalyst of the present invention will be described in more detail with reference to the drawing.Fig.1 is a partially sectional view showing the structure of an exhaust gas cleaning catalyst of the present invention.The exhaust gas cleaning catalyst 1 is comprised of a carrier substrate 2 a catalyst carrying layer 3 formed on the carrier substrate and a noble metal catalyst carried by the catalyst carrying layer.The catalyst carrying layer 3 includes at least two layers i.e.a lower layer 4 and an upper layer 5 and may include one or more additional layers not shown between the lower layer 4 and the upper layer 5.
Patent claim: The induction heating device according to any one of claims 1 to 13 further comprisinga pressure sensor 23 for detecting a weight of the cooking utensil wherein the control unit 93 is configured to change an operational state of the first lighting unit 40 in accordance with a change in the weight of the cooking utensil.

Related passage: Subsequently the cooking apparatus 1 generates flame images FI according to the received cooking method 1430.
Patent claim: The arrangement according to any of the preceding claims wherein a mechanism is comprised to vary the distance between G1 and G2 or that between source or G0 if G0 is used and G1 or that between G2 and the detector along the optical axis so that the duty cycle of the interference pattern on the detector plane is tuned in order to obtain interference pattern with specific duty cycle.

Related passage: The afore mentioned invention therefore unites the following properties and advantagesa The setup comprising the beam splitter grating and the beam recombiner grating is achromatic and requires practically no spatial coherent light.The setup can be operated therefore with a standard xray tube.b The setup is less sensitive to phase shifts than MachZehnder type interferometers.Therefore the setup allows to investigate samples that cause large phase shifts.c The phase shift sensitivity can be tuned within certain limits by changing the sample position or the grating positions or by using grating sets with different periods.d The related materials and fabrication methods for the gratings are comparably wellknown and can be easily performed.e The setup is very well suited for mammography for the reasons given in the introduction suitable energy range screening applications radiation damage.f The setup is very well suited for applications that require many xray images tomography series of xray images etc..
Patent claim: The laser device according to claim 2 or 3 further comprising a deflection mirror configured to reflect the light from the light source toward the first mirror the first optical path being bent at the deflection mirror.

Related passage: The first and second deflection mirrors 24a and 24b are attached to a pair of opposing faces of the mirror base 26 which are opposed so as to interpose the rotation axis 22 in a direction orthogonal to a Zaxis.That is respective deflection mirrors are arranged at different positions of the mirror base 26 around the rotation axis 22.A face of each deflection mirror at an opposite side of a face attaching to the mirror base 26 is a deflection face for reflecting and thereby deflecting a laser light beam.Conveniently a deflection face of the first deflection mirror 24a may also be referred to as a first deflection face and a deflection face of the second deflection mirror 24b may also be referredto as a second deflection face below.
Patent claim: The article of manufacture of claim 6 wherein the wheel speed characteristic is a summation of an angular velocity during a time interval and preferably wherein the time interval begins after takeoff and ends prior to a gear retract braking.

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: Method for operating a gas turbine 10 the gas turbine 10 comprising a compressor 12 a combustor 13 16 with at least two burners 24 25 a turbine 14 17 downstream of the combustor 13 16 and a plurality of turbine outlet temperature measurements 18 19 the method comprising the steps ofsupplying a first fuel flow to one of the burners 2425 of one combustor 13 16 and supplying a second fuel flow to another one of the burners 24 25 of the same combustor 13 16 wherein the first fuel flow is smaller than the second fuel flowmeasuring the turbine outlet temperature of the turbine 14 17 with the turbine outlet temperature measurements 18 19 of the respective turbine 14 17selecting a number of turbine outlet temperature measurements 18 19 which is smaller than a total number of the turbine outlet temperature measurements 18 19averaging the measured temperatures of the selected turbine outlet temperature measurements 18 19 to obtain a trimmed turbine outlet temperature TAT TR andcontrolling the operation of the gas turbine 10 with the trimmed turbine outlet temperature TAT TR.

Related passage: This feature makes sure that independent from the number of operative burners and their location inside of the second combustor none of these burners is exposed to high temperatures that may cause damage or a life time reduction of this particular burner.
Patent claim: The system of any one of claims 12 wherein the first parasitic scattering element and the second parasitic scattering element each comprise a capacitive component or an inductive component of the ground planeconfigured to isolate the first antenna element and the second antenna element from one another within a same frequency range and comprises an electrical size that is about equal to a selfresonance.

Related passage: Figs.4a and 4b are graphs representing the frequency characteristics of the correlation and the frequency characteristics of the antenna efficiency for both antennas in the antenna apparatus configuration illustrated in Fig.3.
Patent claim: The method of 10 11 or 12 wherein emitting by the optical transmitter the optical signal comprises emitting laser pulses having a constant amplitude using a swept frequency methodology 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 based on optical frequency domain reflectometry IOFDR.

Related passage: Interrogator 12 is an FBG interrogator comprising broadband light source 18 high speed spectrometer 20 and data processor 22.Broadband light source 18 may for instance be a Superluminescent Light Emitting Diode SLED source capable of producing light at several wavelengths.High speed spectrometer 20 is a spectrometer capable of rapidly assessing relative shift in Bragg wavelength BB.The particular speed requirements of high speed spectrometer 20 will depend on the number of optical sensing elements 16a 16b...16N and on the sampling speed requirements of optical fiber sensing system 10 which may in turn be determined by safety or firesuppression requirements of the monitored regions or systems.Dataprocessor 22 is a microprocessor or other logiccapable device configured to calculate temperature changes T from relative shifts in Bragg wavelength BB and further configured to run scanning method 100 described below with respect to FIG.2..Data processor 22 may be a programmable logic device such as a multifunction computer or a fixedfunction processor.
Patent claim: The computer implemented method of claim 1 further comprising determining using the ROM a reduced order system response that comprises one or more reduced order sensor values and determining an aggregate error response between the reduced order system response and a plurality of sensor measurement readings from the sensor of interest.

Related passage: In this example the modeling computer 62 is configured to generate modeled gas path parameters y based on the engine inputs received from the engine 10.The example modeling computer 62 is further configured to generate modeled subsystem parameters z based on the engine inputs received from the engine 10.
Patent claim: The gas turbine engine of claim 7 and further comprising a generator 132 configured to produce electric power wherein the generator is coupled to the fan rotor such that rotation of the fan rotor drives rotation of the generator wherein the rechargeable battery receives electric power from the generator when the fan rotor rotates.

Related passage: FIG.2 is a schematic view of pump system 50.Pump system 50 includes bearing compartment 52 having a compartment cavity that contains fan drive gear system 36 including bearings 54 auxiliary pump 44 gutter 56 auxiliary reservoir 58 and first shuttle valve 60.Pump system 50 also includes second shuttle valve 62 main reservoir 64 main pump 66 and scavenge pump 67 positioned outside of bearing compartment 52.Passages 68 70 72 74 76 78 80 82 84 86 and 88 connect the various components as illustrated and as further described below.
Patent claim: The gas turbine engine of any preceding claim wherein the electric motor receives power from a ground auxiliary power unit or wherein the electric motor receives power from a cable connecting the electric motor to a ground power grid or wherein the electric motor receives power from a rechargeable battery mounted to the gas turbine engine or wherein the gas turbine engine is mounted to an aircraft and wherein the electric motor receives power from batteries mounted within the aircraft.

Related passage: In one embodiment bearings 54 are journal bearings.Journal bearings can benefit from having a supply of substantially continuous lubricating liquid.Consequently bearings 54 can benefit from having liquid supplied from auxiliary pump 44 when engine operating conditions prevent main pump 66 from supplying adequate liquid.This benefit depends on auxiliary pump 44 having an adequate supply of liquid during those engine operating conditions.
Patent claim: The gas turbine of any preceding claim wherein the end surfaces 108 face one another and are substantially coincident.

Related passage: FIG.7 shows a top view and FIG.8 shows a side view of first seal 50 and second seal 52 and connector 56 with connector 56 coupled to first seal 50 and second seal 52 with a plurality of attachments 80 in accordance with one embodiment of this invention.First seal 50 has a first seal end 74 FIG.8 and second seal 52 has a second seal end 76 FIG.8.First seal 50 and second seal 52 may be aligned first seal end 74 to second seal end 76 with a space 78 FIG.8 between first seal 50 and second seal 52.Connector 56 covers space 78 between first seal 50 and second seal 52 and first seal end 74 and second seal end 76.In one embodiment of this invention the connector 56 is substantially the same width as first seal 50 and second seal 52.However connector 56 may be a different width than first seal 50 andor second seal 52.Each attachment 80 may include for example at least one of a spot weld or a tack.Attachments 80 are illustrated in FIG.8 partially protruding above connector 56.However attachments 80 may be flush or inset relative to connector 56.Other attachments may also be used to secure connector 56 to first seal 50 and second seal 52.For example FIG.9 shows one embodiment of the invention in a top view of first seal 50 and second seal 52 and connector 56 with connector 56 coupled to the first seal 50 and the second seal 52 with an adhesive.A person skilled in the art will readily recognize many ways for coupling connector 56 to first seal 50 and second seal 52 without visible attachments.
Patent claim: The method of any preceding claim further comprising at least one of providing for display by the computing device 202 the image data on a display device 204 or storing the image data within a memory 208 associated with the computing device 202.

Related passage: Moreover the endoscopic inspection is performed by connecting a turning tool T to the engine E.The turning tool T is an apparatus for rotating a rotating shaft AR includes a motor and a gearbox and can rotate the rotating shaft AR through a shaft not shown.
Patent claim: The vehicle running test system according to claim 1 further comprising a calculation part adapted to calculate the driving index at predetermined time intervals or at predetermined distance intervals and a target speed pattern setting part adapted to on a basis of the driving index calculated by the calculation part set a target speed pattern for guiding a subsequent run such that the driving index comes close to a target value wherein the display control part displays the target speed pattern on the graph.

Related passage: Then as shown in Fig.3 the vehicle driving mode display device 2 in this embodiment is so configured to be able to display a specific area E within a predetermined time period before and after the present time in the graph G1 in an enlarged form only in the vehicle speed axis direction.Before and after the enlarged specific area E is an ordinary display area N expressed in an ordinary scale namely in a scale wherein the vehicle speed axis is expressed in the full scale.