bhlim/patentmatch_for_finetuning huggingface dataset:
Patent claim: An antiicing system 64 of a nacelle inlet 44 of an engine 10 of an aircraft wherein the antiicing system 64 comprises a valve assembly 66 100 fluidly connected to the nacelle inlet 44 wherein the valve assembly 60 100 comprises a first direct acting valve 102A comprising a first inlet 108A a first valve chamber 114A fluidly connected to the first inlet 108A a first internal valve body 112A circumferentially surrounding the first valve chamber 114A a first outlet 110A and a first piston 118A for adjusting a rate of flow WI of air through the first direct acting valve 102A wherein the first piston 118A is slidably engaged with the first internal valve body 112A a first control valve assembly 104A fluidly connected to the first valve chamber 114A of the first direct acting valve 102A a second direct acting valve 102B comprising a second inlet 108B a second valve chamber 114B fluidly connected to the second inlet 108B a second internal valve body 112B circumferentially surrounding the second valve chamber 114B a second outlet 110B and a second piston 118B for adjusting a rate of flow of air WPR through the second direct acting valve 102B wherein the second piston 118B is slidably engaged with the second internal valve body 112B and further wherein the second direct acting valve 102B is fluidly connected to the first direct acting valve 102A in a series configuration suchthat the second inlet 108B of the second direct acting valve 102B is directly connected to the first outlet 110A of the first direct acting valve 102A and a second control valve assembly 104B fluidly connected to the second valve chamber 114B of the second direct acting valve 102B.

Related passage: A regulating or control chamber 74 is defined between the piston head 76 and the closed end 52 of the regulating bore 40.In addition a side wall 78 of the piston 66 comprises a plurality of apertures 80 which are movable axially with the piston 66 into and out of alignment with the openings 48 in the regulating bore 40 to regulate the flow of bleed air through the pressure regulating valves 32 34.
Patent claim: The electronic circuit according to claim 1 or claim 2 wherein said first coupling circuit RD1 RD2 is configured so that said switching occurs at said second instant t3 and between said first and second instants t2 t3 the first coupling circuit RD1 RD2 operates in the respective first operating mode.

Related passage: The trimming capacitors 41 each have a terminal connected respectively to the first feedback sensing terminal 14a and to the second feedback sensing terminal 14b and receive on the other terminal compensation signals VC VC in phase opposition from the phase generator 30.In one embodiment the compensation signals VC VC are equal respectively to the reading signal VR and to the negated reading signal VR.The trimming capacitances CTRIM of the trimming capacitors 41 are adjustable in the factory and enable compensation of the offsets caused by the microstructure 2 basically capacitive unbalancings due to process imperfections and spreads and residual offsets of the subsequent reading chain charge amplifier 20 phaseshift module 21 lowpass filter 22.
Patent claim: Hearing aid according to any of the preceding claims wherein the polarization element is shaped as a strip having a width and a length and wherein the length of the strip corresponds to a distance along an inner surface of the hearing aid shell from a first end of the hearing aid shell to a second end of the hearing aid shell.

Related passage: Furthermore at least a part of the primary antenna element 7 andor the parasitic antenna element may extend along the supporting element.Preferably the first section 19 of the supporting element is between one sixteenth wavelength and a full wavelength of the emitted electromagnetic field the length being measured along the path of maximum current between the excitation points 1718.
Patent claim: A downhole system according to claim 7 further comprising a power read out unit 41 configured to detect the power used by 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: The method of any preceding claim further comprising routing the liquid coolant 98 100 114 through an intercooler 88 located within the gas turbine engine 10.

Related passage: The intercooler aftercooler and cooling systems may be connected to heat exchangers 2140 which may be one heat exchanger or more than one heat exchanger.In addition all or any combination of intercooler aftercooler andor cooling systems may be employed in the desired application.As nonlimiting examples only a turbomachine may only employ the intercooler 220 and cooling system 250 or the turbomachine may employ intercooler 220 cooling system 250 and second cooling system 1450 or the turbomachine may employ intercooler 220 cooling system 250 second cooling system 1450 and aftercooler 1420 or the turbomachine may employ intercooler 220 cooling system 250 second cooling system 1450 aftercooler 1420 and third cooling system 1440 or any subcombination of the intercooler aftercooler cooling system second cooling system and third cooling system.
Patent claim: The furnace according to any of the preceding claims being a steam methane reforming furnace.

Related passage: Fig.4 shows the simulated average tube duty per row for a reformer furnace having a firebox with 24 tube rows only half of the firebox has been simulated for symmetry reasons.To counter the phenomenon of the bending effect the momentum from the side burner rows has been increased step by step up to 78of the inner burner power.The flame bending is not suppressed and the power increase creates an overheated region at the side of the furnace whose peak value is located on the second tube row from the wall due to the hot flue gas flowing through the first tube row and heating the next row.
Patent claim: The method according to any of the preceding claims wherein the determining the estimate of a number of wireless devices is based on an estimate of a probability density function model of the number of wireless devices.

Related passage: The frequency hopping sequence to be applied on a given frame may be statically or dynamically defined.When the frequency hopping sequence to be applied on the given frame is dynamically defined signalling information has to be transmitted from the APs and the mobile terminals in order to indicate the frequency hopping sequence to be applied on the given frame so that said mobile terminals are able to determine which time and frequency resources of the grid are used to performthe transmissions.In this case such signalling information consists of a code in a codebook representing an alphabet of all allowable frequency hopping sequences for the given frame.The part of the frame in which signalling information is provided is of limited size which therefore reduces the quantity of allowable frequency hopping sequences compared with an exhaustive quantity of frequency hopping sequences made possible by the grid and therefore limits the size of the alphabet.
Patent claim: The method according to claim 2 further comprising outputting a result of the comparison of the first current draw waveform and the second current draw waveform through a user interface.

Related passage: Step 1136 represents a waiting step during which a predetermined wait time is permitted to elapse.This wait time permits the driving and driven elements of electromechanical surgical device 10 and circular surgical stapler attachment 250 to come to rest before proceeding to step 1138 in which step the firing motor is stopped.
Patent claim: The medical device kit according to claim 5 wherein the first and second locking members are configured to completely encircle the artificial caput femur surface.

Related passage: A head contacting portion 60 of the locking element 48 may be a spherical surface portion that when the locking element is in its first position defines a surface portion on a projection of the spherical inner surface 20 of the liner 26.In this way the head contacting portion 60 will contact the spherical head 18 along a contact region.A person of ordinary skill in the art will understand however that other head contacting portion 60 configurations may be used included including a rounded contacting portion not shown that contacts the spherical head 18 only at a point or along a line around the periphery of the inferior aperture 34.
Patent claim: The gas turbine engine 10 of claim 1 wherein the wing 114 214 314 414 divides the buffer cavity 112 212 312 412 into at least two portions 122 124 222 224 322 324 422 424 and the set of protuberances 116 117 216 217 316 317 416 417 are in the same portion.

Related passage: Referring now to FIGS.2 and 3 an inner cavity 50 is located radially inward of the annular duct 30 and axially between a firststage vane support 52 and a firststage rotor assembly 54.The rotor assembly 54 comprises a disk 56 and a plurality of outwardly extending blades 58 rotationally disposed about the central axis11.As best shown in FIGS.4 and 5 the disk 56 includes a radially outermost rim 60 a plurality of fir tree profiled slots 62 and a plurality of lugs 64 alternating with the slots 62 about the circumference of the rim 60.Each slot 62 accepts a radially lower most attachment 66 of a blade 58 in a sliding arrangement.One or more teeth 67 extend between a forward axial face 68 and a rearward axial face 69 of the attachment 66 engaging adjacent lugs 64 to prevent loss of the blade 58 as the disk 56 rotates.The one or more teeth 67 project a complementary fir tree profile about a periphery of each face 68 69.
Patent claim: The material according to any one of the preceding claims wherein the second amine has a primary heterocyclic amine structure or secondary heterocyclic amine structure.

Related passage: In the above formula 1 R2 is unsubstituted C3C10 more preferably C3C8 cyclic alkyl.The temperaturesensitive nitrogencontaining compound A produces various reaction products with acid gases to thereby absorb the acid gases.The temperaturesensitive nitrogencontaining compound A has steric hindrance and the steric hindrance greatly influences the kinds of the reactionproducts.For example when the temperaturesensitive nitrogencontaining compound A absorbs CO2 bicarbonate ions are advantageously produced due to the steric hindrance of the compound.Since heat of reaction is comparatively low in the reaction of to producing bicarbonate ions from the temperaturesensitive nitrogencontaining compound A and CO2 the heat of reaction in the absorption of CO2 can be reduced to improve CO2 absorption power due to the adequate steric hindrance of the temperaturesensitive nitrogencontaining compound A.
Patent claim: The surgical stapling system of Claim 16 or 17 wherein said anvil is rotatable relative to said jaw to place said end effector in said clamped configuration.

Related passage: Referring again to FIG.8 the first staples 285a are comprised of wire for example.The wire can be comprised of stainless steel andor titanium for example.The wire has a circular crosssection however alternative crosssections may be utilized.Each first staple 285a can comprise any suitable configuration such as for example a Vshaped configuration or a Ushaped configuration.A first staple 285a comprising a Vshaped configuration can include a base a first leg extending from a first end of the base and a second leg extending from a second end of the base wherein the first leg and the second leg extend in directions which are nonparallel to one another.A first staple 285a comprising a Ushaped configuration can include a base a first leg extending from a first end of the base and a second leg extending from a second end of the base wherein the first leg and the second leg extend in directions which are parallel to one another.
Patent claim: Laundry treatment appliance 2 comprising a user interface 62 said user interface 62 comprising an assembly 66 said assembly 66 comprising at least one fixed element 68 72 80 at least one rotary element 76 88 and a display 70 whereby at least one said rotary element 76 88 is a built as user interface element 44 whereby said display 70 is arranged inside said user interface element 44 characterized in that said at least one said rotary element 76 88 is axially constrained by at least one said fixed element 68 72 80.

Related passage: In the illustrated example the electronic display 16 is fixed in position relative to the knob shell 24 and the circuit board 20 and does not rotate with rotation of the rotary knob 12.The electronic display 16 is preferably an LCD display or a vacuum fluorescent display.However any electronic display 16 is contemplated.The electronic display 16 includes a display portion 80 for displaying any image capable of being displayed by the electronic display 16.The electronic display 16 also includes a clip 82 connected to a bottom of the display portion 80.The clip 82 includes a front Ushaped clip portion 86 accepting a bottom of the display portion 80 therein and plurality of rearwardly extending lead pins 84 extending from the clip portion 86 at a bottom of the display portion 80.The rearwardly extending lead pins 84 are configured to be inserted into a connector block 90 on the front of the circuit board 20.The connector block 90 includes a plurality of pin openings 92 for accepting therearwardly extending lead pins 84 therein to power the electronic display 16 and to change the image on the electronic display 16.The illustrated electronic display 16 preferably includes a protective appliqu 100 connected to a front of the display portion 80 for protecting the display portion 80.The display portion 80 of the electronic display 16 is configured to fit between a plurality of vertical flanges 96 and horizontal flanges 98 that form a square and that extend from the front of the inner cylinder 26 of the knob shell 24 as illustrated in FIGS.1 3 and 4.
Patent claim: The polyurethane foam according to claim 8 or claim 9 wherein the polyurethane foam has a total density of 28 to 50 kgm3 and a central density of 25 to 45 kgm3.

Related passage: The invention is characterized by use of polyurethane rigid and flexible foams PUR which are obtainable from wood origin raw materialstall oil derived polyols or lignin as immobilizing support for microorganisms that produce ligninolytic enzymes.The offered PUR see claims from 1 to 8 and method of their production see claims 11 to 13 ensure that produced open cell PUR structure as composite with natural fibres or produced by lignin facilitates colonization of microorganism inside the foam and stimulates the production of ligninolytic enzymes.There is verified that these properties of produced foams together with the presence therein of natural fibres or lignin source which induce ligninolytic enzymes production by the microorganisms makes these foams a valuable and completely new material for the application.
Patent claim: A method of modulating a compressor stall margin of a compressor based on a health of a gas turbine engine 100 including the compressor 124 said method comprising determining the stall margin 304 of the compressor 124 operating the gas turbine engine 100 using the determined stall margin 304 assessing a health of the compressor 124 and modifying the stall margin 304 based on the assessed health of the compressor 124.

Related passage: Further the estimation systems described herein is sufficiently accurate that design margins are facilitated to be decreased as compared to gas turbine engines that include known control system.As such the reduced design margins facilitate increasing the performance andor condition of a gas turbine engine that includes the estimation system.Moreover the abovedescribed estimation system can include a databased model that is easier to certify lowers central processing unit CPU timeandor is simpler to implement andor maintain than at least some physicsbased models.However the physicsbased models described herein provide for substantially accurate operating parameter estimations that take into account enginetoengine variations.Accordingly the estimation system described herein can be adjusted to the application for which the gas turbine engine is used by providing a plurality of model types.Additionally the abovedescribed redundancy system provides an alternate model that will avoid any anomalies within the primary model to facilitate ensuring that accurate estimated operating parameters are provided to a control system.
Patent claim: The method of claim 1 wherein said crosslinker is at least one selected from the group consisting of an amine carboxylic acid sulfate sulfite sulfonate aldehyde hydrazide sulfhydryl diazirine aryl azide acrylate epoxide phenol chromium compound vegetable tannin and syntan.

Related passage: The regenerated collagen fibers are made of the skin bones tendons and the like of animals such as bovines pigs horses deer rabbits birds and fish.A solubilized collagen solution which is produced from these materials is spun into regenerated collagen fibers followed by crosslinking with an aluminum compound.By the dense aluminum crosslinking performed immediately after the spinning the regenerated collagen fibers of the present invention can be obtained.
Patent claim: The wearable neutron detector according to claim 1 wherein the neutron detection parts are set onto a flexible clothlike material.

Related passage: Figure 3 illustrates schematically the neutron detector 8 illustrated in Figure 1.The neutron detector 8 in this example comprises two of the neutron detection elements 14 illustrated in Figure 2 with their associated photodetectors 20.The neutron detector 8 further includes a tubular sleeve 24 of neutron moderating material generally surrounding the neutron detection elements 14.The sleeve 24 is generally elongate having a similar length to the neutron detection elements 14 and a diameter similar to the width of the neutron detection elements 14.
Patent claim: The electronic circuit according to claim 1 or claim 2 wherein said first coupling circuit RD1 RD2 is configured to operate in the respective second operating mode starting from said first instant t2 and subsequentlyto switch into the respective first operating mode and for operating in said respective first operating mode for a time interval t that terminates with said switching.

Related passage: The sensing mass 8 is drawn in motion along the driving axis X by the driving mass 7.Consequently when the microstructure 2 rotates about a gyroscopic axis perpendicular to the plane of the axes X Y with a certain instantaneous angular velocitythe sensing mass 8 is subject to a Coriolis force which is parallel to the sensing axis Y and is proportional to the angular velocityof the microstructure 2 and to the velocity of the two masses 7 8 along the driving axis X.More precisely the Coriolis force FC is given by the equation FC2MSx where MS is the value of the sensing mass 8is the angular velocity of the microstructure 2 and x is the velocity of the two masses 7 8 along the driving axis X.The velocity x varies sinusoidally at the driving frequency D with a phase shift of 90 with respect to the position x along the driving axis X and amplitude that are substantially constant as the temperature varies the variations are usually less than 1.The displacements to which the sensing mass 8 is subject on account of the Coriolis force are read through the signal sensing units 15 Figure 3 and the reading device 5.In response to the excitation of the sensing mass 8 by the reading signal VRthe signal sensing units 15 transfer to the charge amplifier 32 differential sensing charge packets QRS1 QRS2 which are proportional to the capacitive unbalancing caused by the displacement of the sensing mass 8 along the sensing axis Y.The sensing charge packets QRS1 QRS2 are hence correlated to the Coriolis force and to the instantaneous angular velocityof the microstructure 2.The sensing charge packets QRS1 QRS2 are converted and processed by the reading device 5 for generating the reading signal SOUT which indicates the angular velocitysee also Figure 5.
Patent claim: Method according to any one of claims 913 characterized in that the runtime is at the beginning of a scan cycle of a userdefined control program.

Related passage: The following presents a simplified summary in order to provide a basic understanding of some aspects described herein.This summary is not an extensive overview nor is intended to identify keycritical elements or to delineate the scope of the various aspects described herein.Its sole purpose is to present some concepts in a simplified form as a prelude to the more detailed description that is presented later.