mhurhangee/patent-ind-claim-en huggingface dataset:
A battery device comprising: a casing having a plurality of sides (10a-10f) including a bottom side, a top side opposite to said bottom side, two lateral sides, a front side, and a rear side opposite to said front side, wherein the plurality of sides are assembled to form a sealed container, a battery cell pack located within the sealed container, wherein the casing comprises at least one outlet arranged at at least one of the plurality of sides, wherein the sealed container is configured to prevent heated gases generated upon a malfunction of the battery cell pack from escaping the casing except via said at least one outlet; wherein a filter is arranged at said at least one outlet for limiting at least flames from escaping said casing; and wherein terminals for connection of the battery device to a load, another battery device or an external power source are arranged at the front side, and wherein said at least one outlet is arranged at the rear side of the casing. a casing having a plurality of sides (10a-10f) including a bottom side, a top side opposite to said bottom side, two lateral sides, a front side, and a rear side opposite to said front side, wherein the plurality of sides are assembled to form a sealed container, a battery cell pack located within the sealed container, wherein the casing comprises at least one outlet arranged at at least one of the plurality of sides, wherein the sealed container is configured to prevent heated gases generated upon a malfunction of the battery cell pack from escaping the casing except via said at least one outlet; wherein a filter is arranged at said at least one outlet for limiting at least flames from escaping said casing; and wherein terminals for connection of the battery device to a load, another battery device or an external power source are arranged at the front side, and wherein said at least one outlet is arranged at the rear side of the casing.
A planetary gear box assembly comprising a sun gear and a plurality of planet gears (4; 32) in meshing engagement with the sun gear ; the planet gears (4; 32) in meshing engagement with a ring gear which encircles the plurality of planet gears (4; 32), each planet gear (4;32) mounted for rotation in a planet carrier by means of a bearing pin received in a parallel bore in the planet carrier , characterized in that the bearing pin including a small axially tapered section adjacent one or both ends and the assembly further comprising a tapered sleeve configured to interference fit between a radially inner wall surface of the parallel bore and a radially outer surface of the or each axially tapered section of the bearing pin, a gallery for the distribution of fluid to an interface between the wall surface of the parallel bore and a surface of the tapered sleeve , or to an interface between a radially outer surface of an axially tapered section of the bearing pin and a surface of the tapered sleeve , and a circumferential groove provided in the surface of the tapered sleeve at the interface.
A heating device comprising: a shell , with a receiving chamber formed therein; a heating element received in the receiving chamber ; a liquid transport body in contact with the heating element , the liquid transport body being configured for absorbing tobacco liquid and supplying the tobacco liquid to the heating element ; the liquid transport body comprises multiple annular liquid transport layers stacked inside the shell , along an axial direction of the shell ; outer diameters of multiple annular conductive layer are equal to an inner diameter of the receiving chamber such that the multiple annular liquid transport layers are capable of being assembled in the receiving chamber and abutting against an inner surface of the shell . a shell , with a receiving chamber formed therein; a heating element received in the receiving chamber ; a liquid transport body in contact with the heating element , the liquid transport body being configured for absorbing tobacco liquid and supplying the tobacco liquid to the heating element ; the liquid transport body comprises multiple annular liquid transport layers stacked inside the shell , along an axial direction of the shell ; outer diameters of multiple annular conductive layer are equal to an inner diameter of the receiving chamber such that the multiple annular liquid transport layers are capable of being assembled in the receiving chamber and abutting against an inner surface of the shell .
Device intended to be connected to a board which is connected by circuits to actuators , to mechanisms , and to receivers able to receive data, so that the board is able to receive signals from receivers , these signals being transmitted by receivers in response to external data received by these receivers , and that one or more mechanisms are thus able to be actuated as a function of these data, this device being characterized in that it comprises a terminal block which is adapted to be connected with said board so that said mechanisms are still capable of being actuated by said actuators via said board , and a removable box which is intended to be connected with said terminal block so that said terminal block is an interface between said board and said box , said device being able to analyze said data via said box , at least some of the connections between said box and said terminal block being redundant of at least some of the connections between said terminal block and said board allowing providing additional control functions such that at least some of said mechanisms are able to be actuated independently by means of said board and by means of said box , said terminal block and/or said box allowing the actuation of said mechanisms by said receivers .
An assembly for a turbine engine , the assembly comprising: a combustor wall including a shell , a heat shield and an annular land ; the heat shield attached to the shell ; and the land extending vertically between the shell and the heat shield and laterally between a land outer surface and an inner surface , the inner surface at least partially defining a quench aperture in the combustor wall; wherein a lateral distance between the land outer surface and the inner surface varies around the quench aperture ; wherein the land is aligned with an aperature defined by a surface of the shell that extends between opposing side surfaces of the shell ; characterised in that : a distal land surface of the land slidingly contacts one of the side surfaces of the shell . a combustor wall including a shell , a heat shield and an annular land ; the heat shield attached to the shell ; and the land extending vertically between the shell and the heat shield and laterally between a land outer surface and an inner surface , the inner surface at least partially defining a quench aperture in the combustor wall; wherein a lateral distance between the land outer surface and the inner surface varies around the quench aperture ; wherein the land is aligned with an aperature defined by a surface of the shell that extends between opposing side surfaces of the shell ; characterised in that : a distal land surface of the land slidingly contacts one of the side surfaces of the shell .
A fitting in the form of a saddle-type fitting, comprising a half-tube shaped main section , dimensioned to receive in it a section of a pipe , a tubular section extending from a circular or elliptical hole of the half-tube, at an angle to the longitudinal axis of the half-tube section, characterised in that said half-tube section comprises a first pair of circular or elliptical sealing zones and first sealing means, to form circular or elliptical seals circumscribing the hole in the half-tube section and a corresponding mating hole in a mating pipe placed in the half-tube section, between the inner surface of the half-tube section and the outer surface of the mating pipe, wherein the tubular section comprises a second pair of circular sealing zones and second sealing means to form circular seals between the inside surface of the tubular section and the outside surface of a mating pipe inserted into said tubular section, wherein in between said first pair of circular or elliptical sealing zones is a pressure testing chamber , and wherein in between said second pair circular sealing zones is a pressure testing chamber ; optionally said first and second sealing means are means to form electrofusion.
Tool steel having the following composition, wherein the components are indicated in each case in mass percent: 0.30 ≤ C (carbon) ≤ 0.55 0.02 ≤ Si (silicon) ≤ 1.00 0.05 ≤ Mn (manganese) ≤ 1.00 P (phosphorus) ≤ 0.025 S (sulphur) ≤ 0.015 0.50 ≤ Cr (chromium) ≤ 2.00 0.10 ≤ Mo (molybdenum) ≤ 1.00 0.50 ≤ Ni (nickel) ≤ 3.00 0.50 ≤ Cu (copper) ≤ 2.50 0.001 ≤ Nb (niobium) ≤ 0.100 0.01 ≤ V (vanadium) ≤ 0.60 wherein the remainder consists of iron, usual impurities and/or accompanying elements in traces up to 0.02 mass percent per accompanying element. 0.30 ≤ C (carbon) ≤ 0.55 0.02 ≤ Si (silicon) ≤ 1.00 0.05 ≤ Mn (manganese) ≤ 1.00 P (phosphorus) ≤ 0.025 S (sulphur) ≤ 0.015 0.50 ≤ Cr (chromium) ≤ 2.00 0.10 ≤ Mo (molybdenum) ≤ 1.00 0.50 ≤ Ni (nickel) ≤ 3.00 0.50 ≤ Cu (copper) ≤ 2.50 0.001 ≤ Nb (niobium) ≤ 0.100 0.01 ≤ V (vanadium) ≤ 0.60
A hot-melt anchor head, comprising an anchor ring , a guide wire , an electrical hot-melt member and a clamp piece , wherein the anchor ring is provided with at least one through hole (1-1); the guide wire can be electrified; the electrical hot-melt member is arranged on the anchor ring and connected with the guide wire ; the clamp piece is arranged in the through hole (1-1) to clamp an anchor cable reinforcement ; a bearing plate is arranged at a bottom of the anchor ring , an opening opposite to the through hole (1-1) is formed in the bearing plate , and the anchor ring is made of a metal material; the hot-melt anchor head further comprises a strain gauge connected with the guide wire and arranged on a surface of the anchor ring ; the surface of the anchor ring is integrally formed with a coating layer by injection moulding with a hot-melt material, the strain gauge is coated by the coating layer and is in close contact with the surface of the anchor ring so as to be integrally formed, and an end, close to the bearing plate , of the anchor ring extends inwards and is provided with a flange, and the flange is used for holding a part, located inside the through hole (1-1), of the coating layer ; when the hot-melt anchor head clamps the anchor cable reinforcement , the part, located inside the through hole (1-1), of the coating layer fills a space between the anchor ring and the clamp piece and is limited in the space in all directions; and when the part, located inside the through hole (1-1), of the coating layer is heated to be melted by the electrical hot-melt member , the hot-melt anchor head releases the anchor cable reinforcement .
A method for monitoring the condition of a heat exchanger in an air circuit of an aircraft , said heat exchanger being for cooling air extracted from a primary hot air source of the aircraft, said method being characterised in that it comprises the following steps: - acquiring temperature measurements made by a probe disposed at an outlet of said heat exchanger , said acquiring being performed when the air circuit is fed by a secondary hot air source downstream of said heat exchanger and the primary hot air source being cut off, - selecting a relevant temperature measurement from said temperature measurements, said relevant temperature measurement being representative of a stabilisation phase included in a predetermined observation time period, - comparing said relevant temperature measurement with an alert threshold, and - evaluating a leakage level in the heat exchanger based on said comparison. - acquiring temperature measurements made by a probe disposed at an outlet of said heat exchanger , said acquiring being performed when the air circuit is fed by a secondary hot air source downstream of said heat exchanger and the primary hot air source being cut off, - selecting a relevant temperature measurement from said temperature measurements, said relevant temperature measurement being representative of a stabilisation phase included in a predetermined observation time period, - comparing said relevant temperature measurement with an alert threshold, and - evaluating a leakage level in the heat exchanger based on said comparison.
A heat dissipator for a charging connector , comprising: a body , wherein a cooling chamber is formed in the body and a receiving hole is defined at an inner circumference of the body , the receiving hole being configured to accommodate the charging connector ; an air blower mounted on the body ; and a plurality of first heat sinks distributed on an outer surface of the body , wherein an inlet of the cooling chamber is arranged at a bottom of the body and spaced apart from the plurality of first heat sinks in the radial direction of the body , wherein an air vent is provided on the body , through which the air from the air blower flows to the plurality of first heat sinks . a body , wherein a cooling chamber is formed in the body and a receiving hole is defined at an inner circumference of the body , the receiving hole being configured to accommodate the charging connector ; an air blower mounted on the body ; and a plurality of first heat sinks distributed on an outer surface of the body , wherein an inlet of the cooling chamber is arranged at a bottom of the body and spaced apart from the plurality of first heat sinks in the radial direction of the body , wherein an air vent is provided on the body , through which the air from the air blower flows to the plurality of first heat sinks .
A pneumatic tire, comprising: a tread portion extending in a tire circumferential direction to form an annular shape; a pair of sidewall portions disposed on both sides of the tread portion ; and a pair of bead portions disposed on a tire-radial-direction inner side of the sidewall portions ; wherein one circumferential groove is formed on both sides of the tire centerline (CL) in the tread portion , wherein each circumferential groove , while extending continuously in the tire circumferential direction, is displaced periodically in a tire width direction and a plurality of lug grooves with both ends closed extending in the tire width direction is scattered along the tire circumferential direction on both sides of each circumferential groove in the tread portion , wherein a position of the lug grooves in the tire width direction is displaced periodically along the tire circumferential direction and a period of displacement (C 2 ) of the lug grooves is synchronized with a period of displacement (C 1 ) of the circumferential grooves , characterized in that the circumferential grooves and the lug grooves are respectively disposed on both sides of a centerline in the tread portion , the period of displacement of the circumferential grooves is shifted between both sides of the centerline, and a shift amount (Δ) of this period is made to be 25% to 33% of the period. a tread portion extending in a tire circumferential direction to form an annular shape; a pair of sidewall portions disposed on both sides of the tread portion ; and a pair of bead portions disposed on a tire-radial-direction inner side of the sidewall portions ; wherein one circumferential groove is formed on both sides of the tire centerline (CL) in the tread portion , wherein each circumferential groove , while extending continuously in the tire circumferential direction, is displaced periodically in a tire width direction and a plurality of lug grooves with both ends closed extending in the tire width direction is scattered along the tire circumferential direction on both sides of each circumferential groove in the tread portion , wherein a position of the lug grooves in the tire width direction is displaced periodically along the tire circumferential direction and a period of displacement (C 2 ) of the lug grooves is synchronized with a period of displacement (C 1 ) of the circumferential grooves , characterized in that the circumferential grooves and the lug grooves are respectively disposed on both sides of a centerline in the tread portion , the period of displacement of the circumferential grooves is shifted between both sides of the centerline, and a shift amount (Δ) of this period is made to be 25% to 33% of the period.
Dosing machine for preparing a mixture, in particular a two-component adhesive, comprising a housing and a mixer shaft mounted therein, on the end of which shaft a rotor is arranged, the mixer shaft being movable along a longitudinal axis from an operating position, in which the rotor engages in a mixer chamber that is detachably connected to the housing , and, after removal from the mixer chamber , into a maintenance position in which the rotor is freely accessible, characterized in that the mixer shaft is mounted within a hollow shaft and can be connected to the hollow shaft for conjoint rotation, the hollow shaft being rotatably mounted within the housing .
A vertically adjustable caster wheel apparatus having a yolk frame and a wheel frame , said yolk frame having a pivot pin connected to and extending through said yolk frame , and said wheel frame having one end pivotally connected to said yolk frame and a second end rotatably connected to a wheel , comprising: an elastic member having a first retainer connected to one end of said elastic member and a second retainer connected to an opposite end of said elastic member , wherein said first retainer is connected to said pivot pin of said yolk frame to allow said elastic member to pivot with respect to said yolk frame , characterized in that said second retainer having a threaded aperture extending there through along a longitudinal axis; a swivel plate coupled to said wheel frame and having a threaded aperture extending there through and coaxial with said longitudinal axis; a threaded fastener releasably engaging said threaded aperture in said swivel plate and said threaded aperture in said second retainer ; and a spacer positioned between said second retainer and said swivel plate for adjusting a vertical height of said wheel by adjusting an angle of said wheel frame relative to said yolk frame . an elastic member having a first retainer connected to one end of said elastic member and a second retainer connected to an opposite end of said elastic member , wherein said first retainer is connected to said pivot pin of said yolk frame to allow said elastic member to pivot with respect to said yolk frame , characterized in that said second retainer having a threaded aperture extending there through along a longitudinal axis; a swivel plate coupled to said wheel frame and having a threaded aperture extending there through and coaxial with said longitudinal axis; a threaded fastener releasably engaging said threaded aperture in said swivel plate and said threaded aperture in said second retainer ; and a spacer positioned between said second retainer and said swivel plate for adjusting a vertical height of said wheel by adjusting an angle of said wheel frame relative to said yolk frame .
A negative electrode plate comprising a negative current collector and a negative film, the negative film being provided on at least one surface of the negative current collector and comprising a negative active material; wherein the negative active material comprises graphite, and an OI value of the negative film represented by V OI and a pressing density of the negative film represented by PD satisfy a relationship: 0.7≤(80/V OI +43/PD)×PD/V OI ≤21.5, and a unit of the pressing density of the negative film represented by PD is g/cm 3 , a particle diameter of the negative active material represented by D50 and an OI value of a powder of the negative active material represented by G OI satisfy a relationship: 2.8≤100/(D50+2.8×G OI )≤12, and a unit of the particle diameter of the negative active material represented by D50 of the volume particle size distribution is μm, and, 2.8≤(X×0.8+Y×0.2)×Y/X≤15, X=(80/V OI +43/PD)×PD/V OI , Y=100/(D50+2.8×G OI ), wherein V OI and G OI are determined by the method defined in the description. wherein the negative active material comprises graphite, and an OI value of the negative film represented by V OI and a pressing density of the negative film represented by PD satisfy a relationship: 0.7≤(80/V OI +43/PD)×PD/V OI ≤21.5, and a unit of the pressing density of the negative film represented by PD is g/cm 3 , a particle diameter of the negative active material represented by D50 and an OI value of a powder of the negative active material represented by G OI satisfy a relationship: 2.8≤100/(D50+2.8×G OI )≤12, and a unit of the particle diameter of the negative active material represented by D50 of the volume particle size distribution is μm, and, 2.8≤(X×0.8+Y×0.2)×Y/X≤15, X=(80/V OI +43/PD)×PD/V OI , Y=100/(D50+2.8×G OI ), wherein V OI and G OI are determined by the method defined in the description.
A check booth system for use to determine the accuracy of a physical surgical guide manufactured based on a virtual surgical plan including at least one virtual implant and a virtual surgical guide including at least one master tube , the check booth comprising: a support surface ; and a checking support coupled to the support surface , wherein the support surface is configured to receive a check protocol form , and wherein the checking support includes a calibration member having openings and a support structure configured to engage with the physical surgical guide . a support surface ; and a checking support coupled to the support surface , wherein the support surface is configured to receive a check protocol form , and wherein the checking support includes a calibration member having openings and a support structure configured to engage with the physical surgical guide .
Method for applying a thermal insulation on a 3-dimensional structure , the 3-dimensional structure comprising at least two individual tube sections and an outward extending connecting section , the thermal insulation having a thickness of 0.5 cm-5 cm, wherein the method consists of the steps of - providing a substantially flat panel of insulation material, wherein the method is characterized by the steps of - forming one or more 2-dimensional elements from the flat insulation material, wherein forming is assisted by a motor that provides reciprocating motion to a cutting element, - applying the one or more 2-dimensional elements on the 3-dimensional structure, wherein the forming is performed at a constant angle with respect to the 2-dimensional element, by having the motor in a fixed position in view of the constant angle. - providing a substantially flat panel of insulation material, wherein the method is characterized by the steps of - forming one or more 2-dimensional elements from the flat insulation material, wherein forming is assisted by a motor that provides reciprocating motion to a cutting element, - applying the one or more 2-dimensional elements on the 3-dimensional structure,