bhlim/patentmatch_for_finetuning huggingface dataset:
Patent claim: Fiber reinforced composition comprising a 5.0 to 89.5 wt.of a heterophasic polypropylene copolymer HECO b 5.0 to 89.5 wt.of a propylene polymer PP having a melt flow rate MFR2 230 C measured according to ISO 1133 of 1150 g10min c 5.0 to 65.0 wt.of Glass fibers GF and d 0.5 to 5.0 wt.of a polar modified polypropylene as adhesion promoter AP based on the total weight of the fiber reinforced composition wherein i the heterophasic polypropylene copolymer HECO having a xylene cold soluble XCS content in the range of 10.0 to lower than 25.0 wt.based on the heterophasic polypropylene copolymer HECO ii the xylene cold soluble XCS fraction of the heterophasic polypropylene copolymer HECO having a comonomer content in the range of 15.0 to 35.0 wt.and an intrinsic viscosity IV of lower than 2.0 dlg.

Related passage: It has been surprisingly found out that the fiber reinforced composition possesses very good flowabilty by keeping the other properties like stiffness and impact on the desired levels.In particular the flexural modulus the Charpy impact and the elongation at break fulfill the requirements set for instance by the automobile industry and the appliance industry see tables 2 to 4.
Patent claim: A component according to any one of the previous claims wherein each sheath of each protector segment is formed of a different material to the material of which the component is formed.

Related passage: The locking member 42 has a first end region 76 adjacent the first platform 16.The first end region adapts the locking member to engage a first cooling air hole 36a at the trailing edge of the airfoil.The first end region also adapts the locking member to engage in the spanwise direction a first front opening 78 in the shield 44.The locking member has a second end region 82 adjacent the second platform which adapts the locking member to engage a second cooling air hole 36b at the trailing edge of the airfoil.The second end region also adapts the locking member to engage in the spanwise direction a second front opening 84 in the shield.Fig.2 shows the stator vane 10 shown in Fig.1 and the shield assembly 12 in the installed condition.As shown in Fig.2 the long second side 62 of the shield overlaps the first side 52.The upper portion 72 and lower portion 74 of the long second side overlap each other in the spanwise direction.The tabs 5658 on the first side extend at a location past the rear edge of the second side through the openings 6668 in the second side.The tabs are bent over into a faying relationship with the second side to urge the second side toward the pressure surface of the airfoil.
Patent claim: The wireless device of claim 3 wherein the privacy condition module further comprises a privacy condition module for analyzing audio received by the wireless device to determine that the wireless device is in a nonprivate location.

Related passage: According to one aspect of the present invention there is also provided an apparatus and method for automatically transmitting a predetermined voice message from a portable wireless terminal to a calling partners terminal over a currentlyestablished traffic channel when the portable wireless terminal enters a speakerphone call mode.
Patent claim: A method of using a communication device 100 the communication device 100 being used at a one hub to share information by transmitting and receiving image data and sound data among a plurality of hubs via a communication network the method comprising determining whether a receiving device 150 250 that is connected to the communication device 100 and that supports a predetermined standard is any one of adedicated receiving device 150 that is previously specified and that has an image recordingsound recording function or a receiving device 250 that does not have an image recordingsound recording function and when a determination result is positive at the determining converting at least one selected form a group consisting of image data and sound data from the one hub and image data and sound data transmitted from a different hub other than the one hub into a digital signal in accordance with the predetermined standard so as to transmit the digital signal from the communication device 100 to the receiving device 150 250.

Related passage: Further a series of processes as described in the present specification can be carried out by hardware software or a combination of both.When performing the process by software the program having recorded therein a processing sequence can be implemented by installing it in the memory of the computer in which the dedicated hardware is built in.Alternatively the program can be installed and executed in the generalpurpose computer which can perform various processes.For example the program can be recorded in a recording medium in advance.The program can be not only installed in the computer from the recording medium programs can be also received through networks such as LAN Local Area Network and the Internet to install the programs in recording media such as a builtin hard disk.
Patent claim: The induction heater as claimed in any of claims 15 wherein the oscillator comprises two inverting amplifiers tied together.

Related passage: In another embodiment a controller may be provided for allowing only one of the applicators 18 to be in use at a time.The applicators 18 may be interchangeable in the connection of each to the eddy currenthysteretic circuit.The applicators 18 may be simultaneously engaged to the eddy currenthysteretic circuit.At least one of the applicators 18 may include a flexible pad 18 e.g.FIGURE 3 for accommodating substantially all configurations of automotive vehicle body areas.Alternatively or in addition at least one of the applicators 18 e.g.FIGURE 4 may include a magnetic ferrite structure 23 having an air gap 21 for delivering a concentrated level of heat to a mechanical part of an automotive vehicle.Each applicator 18 may also include indicia 32 for indicating an oncondition of the applicator 18.Heater apparatus 10 may also include a sensor which turns an applicator 18 off when no motion is sensed over a predetermined period of time.A housing 90 may be used to contain the eddy currenthysteretic circuit and the plurality of applicators 18 when the heater structures are not in use.
Patent claim: The rotor blade assembly 100 as in any preceding claim wherein said vortex generator accessory 102 comprises a plurality of said protrusion members 108 extending from said base portion 104.

Related passage: As seen in Fig.4 in an advantageous embodiment the vortex generator device 70 is formed as a vane VG device comprising a base 71 having when mounted to an exterior of the wind turbine blade an inner side 72 for attaching to the exterior of the wind turbine blade and an outer side 73 facing away from the exterior of the wind turbine blade.The base 71 further comprises a first side 77 or trailing edge side and a second side 78 or leading edge side as well as a first end 75 and a second end 76.The base 71 is trapeziumshaped so that the first side 77 is parallel to the second side 78 and so that a length of the second side 78 of the base 71 is smaller than a length of the first side 77 of the base 71.In an advantageous embodiment the first end 75 and the second end 76 are oriented so that they form a mutual tapering angle of approximately 38 degrees.The base may advantageously be formed with a rounded perimeter as further shown in Fig.6.
Patent claim: A positive electrode according to any one of claims 1 and 2 wherein the active carbon is in the form of particles having an average diameter of 1 to 30 m preferably of 3 to 20 m more preferably 5 to 10 m.

Related passage: Results of analysis of preferred graphites by Xray diffractometry and another technique are shown below.Lattice spacing d002 0.3330.350 nm Crystallite size in aaxis direction La 20 nm or larger Crystallite size in caxis direction Lc 20 nm or larger True density 2.002.25 gcm3
Patent claim: The ophtalmic composition according to anyone of claims 1 to 14 further containing at least one compound among decongestant eye muscle accommodator antiphlogisticstyptic vitamin and amino acid.

Related passage: In a preferred embodiment of the invention the aqueous ophthalmic solution is characterized by including latanoprost at a concentration of 0.005 a pH damper system that may be selected from boric acid citric acid sorbic acid acetic acid sodium borate monobasic sodium phosphate dibasic sodium phosphate sodium citrate and sodium acetate in a range of concentration from 0.001 to 5.0 one or more agents that increase the viscosity such as hydroxypropylcellulose carbooxylmethylcellulose sulfate chondrointin formal glycerol methyldinoglycerol and cyclodextrins in a concentration ranging from 0.05 to 20.00 one or more tensoactive agents moisturizers such as polyoxyl 40 stearate polysorbate 80 poloxamer and tyloxapol in concentrations ranging from 0.01 to 20.0 one or more osmolarity regulating agents such as sodium chloride sorbitol manitol and dextrose at a concentration ranging from 0.6 to 1.8 expressed as chemical equivalents of sodium chloride one or more preservatives such as benzalkonium chloride benzetonium chloride thiomersal phenylmercury acetate or nitrate parabens chlorohexidine gluconate ethylic alcohol cetrimide sodium perborate and chlorobutanol in adequate concentration in order to provide an antimicrobian effect.It may also contain one or more antioxidant agents such as disodic edetate sodium metabisulfite sodium bisulfite acetylcysteine sodiumthiosulfate and thiourea in adequate concentration in order to give the required effect.
Patent claim: The method according to claim 7 wherein said method comprises not further forwarding by said interdomain bridge IDB12 erroneous received packets from said first domain DOD1 towards said second domain DOD2.

Related passage: In response to the retransmission request signal NACK received from base station 30a relay station 20c transmits the decode and forward relay signal to base station 30a in frame 3.Furthermore mobile station 10 transmits the data signal retransmission signal to relay station 20b in frame 3 in response to the retransmission request signal NACK received from relay station 20b.Relay station 20b transmits the amplify and forward relay signal obtained from the retransmission signal to base station 30a in frame 3.Therefore base station 30a can receive the amplify and forward relay signal retransmitted from relay station 20b and the decode and forward relay signal transmitted from relay station20c at the same time and combine these signals.
Patent claim: The propylene ethylene random copolymer RPP according to anyone of the preceding claims wherein the xylene cold soluble XCS content of the propylene ethylene random copolymer RPP is equal or below 12 wt..

Related passage: In the present invention the polypropylene resin used as a base material resin of polypropylene resin expanded particles is preferably a low melting point resin having a high ethylene content in order to prepare the polypropylene resin foamed products under a low steam pressure.In a case where a copolymer component which is copolymerized with propylene is ethylene an ethylene content rate is preferably 3.0by weight or more but 8.0by weight or less and more preferably 3.5by weight or more but 7.0by weight or less.In a case of using the Ziegler polymerization catalyst an upper limit of the ethylene content rate is about 5by weight.However in a case of using the metallocene polymerization catalyst a polypropylene resin having an ethylene content rate of about 8by weight can beproduced.
Patent claim: The air vehicle navigation method according to claim 1 wherein at least one instruction node upon at least one thread of the aircraft trajectory is a composite node 306b comprising a set of instruction nodes 306ba 306bc with their associated trigger nodes 306ba 306bc whereina.fulfillment of a condition associated to a trigger 306ba in the thread 306 which immediately precedes the composite node 306b starts the validity of the first instruction 306ba of the composite node and b.fulfillment of a condition of a trigger 306bc in the composite node 306b which is associated to the last instruction 306bc in the composite node starts the validity of the instruction 306c in the thread 306 which immediately follows the composite node.

Related passage: At step 530 the intent generation engine 104 uses the user preferences model 105 the operational context model 106 and the aircraft performance model 118 to enrich the flight intent description.The intent generation engine 104 identifies constraints and objectives from the models 105 106 and 118 that are relevant to the flight segments e.g.not all the constraints included in the operational context are likely to apply to a specific route or to all flight segments on a particular flight path.How relevant constraints and objectives are identified is described in more detail below.The intent generation engine 104 enriches the flight intent by expanding the flight segment intent datasets either by adding further instances of flight segments or by amending the existing instance of flight intent such that the resulting instance of flight intent specifies the relevant constraints and objectives according to the syntactical and lexical rules imposed by the flight intent description language.The output of step 530 is an enriched flight intent description.
Patent claim: A composition according to any one of the preceding claims wherein the oligosaccharide mixture comprises 0.570 more preferably 120 even more preferably 25 with respect to the total weight of the composition.

Related passage: The nutritional composition of the invention preferably comprises at least 20 mg of choline per 100 g of the dry weight of the nutritional composition.According to an embodiment the nutritional composition comprises 2090 preferably 3070 more preferably 3560 mg choline per 100 g of the dry weight of the nutritional composition.
Patent claim: Ultrasonic flow meter according to any of the preceding claims wherein the membrane is disc shaped to cover the second side of the transducer.

Related passage: In one embodiment separate first and second parts of the fixing member serve to provide respective first and second electrical connections between the ultrasound transducer and the circuit board.In special embodiments one or more electrical connections are made using Surface Mounted Device SMD technology or a similar automated manufacturing process hereafter in general referred to as SMD technology.The circuit board can be preassembled in an SMD machinery capable of soldering other electrical components onto the circuit board including the ultrasound transducer.Especially the ultrasound transducer may be provided with a thin sheet steel membrane preglued onto the surface in contact with the fluid flow.In such a process the positioning of the ultrasound transducer can be done with the accuracy of the SMD machinery which is measured in the order of fractions of a millimetre such as below 1.0 mm such as below 0.1 mm possibly even below 0.01 mm and the electrical connection between the ultrasound transducer and the circuit board is established.Furthermore the use of e.g.SMD machinery for providing the electrical connections to the ultrasound transducer serves to eliminate the need for wire connections between circuit board and transducer.Wire connections in an automated assembly line make up a subject of difficulty.An advantage of mounting one or more ultrasound transducers directly on the circuit board makes the circuit board suitable for testing prior to final assembly of the flow meter.
Patent claim: A gas turbine component according to any one of claims 1 to 6 wherein the porosity of the thermal barrier layer 12 is within a range from 10 to 30.

Related passage: Of particular interest to the present invention is the susceptibility of TBC materials including YSZ to attack by CMAS.As discussed previously CMAS is a relatively low melting compound that when molten is able to infiltrate columnar and noncolumnar TBCs and subsequently resolidify to promote spallation during thermal cycling.To address this concern the TBC 26 in Figure 2 is shown as being provided with a protective deposit 30 of this invention.As a result of being on the outermost surface of the blade 10 the protective deposit 30 serves as a barrier to CMAS infiltration of the underlying TBC 26.The protective deposit 30 is shown in Figure 2 as comprising an additive portion that overlies the surface 32 of the TBC 26 so as to be available for sacrificial reaction with CMAS and further comprises an internal infiltrated portion that extends into porosity within the TBC 26 so as to maintain a level of CMAS protection in the event the additive portion is breached or lost through spallation erosion andor consumption.In the case of the columnar TBC 26 schematically represented in Figure 2 such porosity is represented in part as being defined by gaps 34 between individual columns of the TBC 26.However porosity is also likely to be present within the columns for example in the surfaces of individual columns if the TBC 26 were deposited by EBPVD to have a featherlike grain structure as known in the art.
Patent claim: The auxiliary power unit as defined in any preceding claim wherein the compressor shaft is drivingly engaged to the turbine section.

Related passage: One alternative to using the gas turbine engine as the sole source of power to operate an electrical power generator is to add in the aircraft a further intermittent combustion internal combustion engine such as gasoline engines operating on the any of the Diesel Miller Otto or Wankel cycles.Such engines can operate with a fuel efficiency on the order of seventy percent 70 better than that of a continuous combustion Brayton cycle internal combustion gas turbine engine.At high altitudes internal combustion engines of all kinds face the problem of limited power output because of the relatively small air pressures there limiting the chemical reactions of oxygen with hydrogen and oxygen with carbon in the burning the engine fuel in the engine combustion chamber or chambers.This can be solved for gas turbine engines by providing therein very large air flows through use typically of axial flow compressors usually in two stages with both a low compression compressor followed along the fluid flow path through the engine by a high compression compressor.This arrangement provides at least enough compressed air to the subsequent combustor to sustain the desired combustion process therein and a mass of airflow sufficient to combine with enough fuel to provide the energy needed to overcome the aircraft drag at the speed and altitude intended for operation.
Patent claim: The method according to claim 1 wherein the temper hard fat has a Ratio A of less than 45 more preferably less than 38 more preferably less than 30 still more preferably less than 20 and most preferably from 1 to 10 wherein the Ratio A is the proportion of saturated fatty acid residues having 16 or fewer carbon atoms relative to the total number of saturated fatty acid residues of the temper hard fat.

Related passage: Acquisition cost of adapted machines to crystallize transfree fats chocolate filling is expensive.
Patent claim: The mobile terminal of claims 1 to 10 wherein the controller is further configured to cause the display to display preset screen information corresponding to a preset application during fingerprint recognition performed when the touch input is applied to the sensing unit the touch input applied when an execution screen of the preset application is displayed on the display.

Related passage: Meanwhile if the acquired biometric information matches with any of the prestored authentication information the mobile terminal 100 operates in a second mode that allows access to the total content that is in authentication mode.
Patent claim: The surgical instrument of claim 2 or claim 3 wherein the articulation system further comprises an articulation drive shaft operably interfacing with the articulation actuation mechanism and the gear arrangement.

Related passage: According to an embodiment of the present disclosure end effector 160 includes a cartridge assembly e.g.jaw member 164 and an anvil assembly e.g.jaw member 162 including an anvil portion for deploying surgical fasteners into body tissue and forming the surgical fasteners.End effector 160 is pivotably mounted about an axissubstantially perpendicular to the longitudinal axis of endoscopic portion 140.Cartridge assembly 164 houses a plurality of staples.Anvil assembly 162 is movable in relation to cartridge assembly 164 between an open position spaced from cartridge assembly 164 and an approximated or clamped position in juxtaposed alignment with cartridge assembly 164.Preferably the staples are housed in cartridge assembly 164 to apply linear rows of staples to body tissue.End effector 160 is attached to a mounting portion which is pivotably attached to a body portion.The body portion may be integral with endoscopic portion 140 of powered surgical instrument 100 or may be removably attached thereto to provide a replaceable or disposable loading unit.The loading unit may be connectable to endoscopic portion 140 through a bayonet connection.It is envisioned that the loading unit has an articulation link connected to the mounting portion of the loading unit and the articulation link is connected to the linkage rod so that the end effector 160 is articulated as the linkage rod is translated in the distalproximal direction along the longitudinal axis.Other means of connecting end effector 160 to endoscopic portion 140 to allow articulation may be used.For example a flexible tube or a plurality of pivotable members may be used.
Patent claim: The mobile device as claimed in claim 1 wherein the first isolation element and the second isolation element each substantially have an Lshape.

Related passage: The antenna device according to the seventh embodiment is a modification of the third embodiment.Radio communication antennas 21d and 22d each are formed into a Ushape and the intermediate portions of the lower horizontal portions of the antennas are respectively connected to feed points 41 and 42 viavertical pieces.The vertical and horizontal portions of the antenna elements 21d and 22d are electrically coupled to the vertical and horizontal portions of parasitic elements 31 and 32 respectively.
Patent claim: An induction cooking hob 10 including at least one induction coil 14 characterized in that the induction cooking hob 10 includes the device according to claim 11 andor the control unit according to claim 12.

Related passage: The phase LOAD of ZCOIL can be calculated from the phase displacement ICOIL which exists between the output voltage VD and the driven current ICOIL and which can be directly measured at the converter 3A outputs.Looking at the topology of the resonant circuit 31A the following equation I can be writtenwhere VCOIL is the phase of the voltage signal across the inductor coil 2.The term VCOIL can be calculated from the phase of the driven current ICOIL according to the following equation II which can be obtained by performing a Fourier first harmonic analysis of the output voltage VD assuming that VD is a square wave with a 50 of dutycyclein which CC1C2.
Patent claim: The device according to claim 12 or 13 comprising a second body 15 bonded to said first face 7 of said first body 1.

Related passage: A sensor is formed as follows.The insulating layers 24 see Fig.4 are formed on the upper and lower surfaces of the substrate.Thereafter the temperaturemeasuring resistors 28A and 28B the heater 29 the fluid temperature detecting resistor 30 the thin metal contact film 32 and the lowersurface electrode pad 35 and the like which constitute the detecting section 27 are formed on the insulating layer 24.These components are then covered with the protective layer 37.The resultant structure is etched from the upper surface side to form the diaphragm 25 thus finishing the flow rate sensor 20.