mhurhangee/patent-ind-claim-en huggingface dataset:
A diffuser of a volatile liquid substance of the type including a container of the volatile liquid substance, closed by at least one permeable membrane which is permeable to the vapours of said volatile liquid substance and in direct contact with the external environment, wherein said container is at least partly flexible and contains a plurality of capsules filled with said volatile liquid substance and made of a pressure-breakable plastic material impermeable to liquids and vapours, wherein said container includes an annular edge portion and a cup-shaped central portion containing said capsules , characterized in that the angle formed between said annular edge portion and said cup-shaped central portion of the container is between 30° and 45° and in that the diffuser further includes a flat ring stably fixed to said annular edge portion of the container .
A method of fuel system protection for an internal combustion engine comprising: introducing a directly injected fuel into a combustion chamber through a direct fuel injector ; introducing a fumigated fuel trough a fuel injector upstream of an intake valve ; and selectively operating said internal combustion engine with at least one of said directly injected fuel and said fumigated fuel. determining a temperature of said direct fuel injector as a function of engine operating parameters; advancing intake valve timing from a normal intake valve timing when said temperature rises above a first predetermined value such that an overlap between an opened intake valve and an opened exhaust valve of said combustion chamber increases; and returning intake valve timing to said normal intake valve timing after said temperature is below a second predetermined value; wherein the first predetermined value is greater than the second predetermined value. introducing a directly injected fuel into a combustion chamber through a direct fuel injector ; introducing a fumigated fuel trough a fuel injector upstream of an intake valve ; and selectively operating said internal combustion engine with at least one of said directly injected fuel and said fumigated fuel. determining a temperature of said direct fuel injector as a function of engine operating parameters; advancing intake valve timing from a normal intake valve timing when said temperature rises above a first predetermined value such that an overlap between an opened intake valve and an opened exhaust valve of said combustion chamber increases; and returning intake valve timing to said normal intake valve timing after said temperature is below a second predetermined value; wherein the first predetermined value is greater than the second predetermined value.
A surgical instrument , comprising: a handle assembly having a protruding portion ; and a battery pack , detachably assembled on the handle assembly, and operatively coupled to the protruding portion, and having at least one battery unit ; wherein, the battery pack comprises at least one discharging system comprising: a discharge element , and a switching member , operable to electrically connect the discharge element to the battery unit of the battery pack to form a discharge circuit; wherein, the switching member has an initial open state, in which the discharge circuit is non-conductive; an intermediate open state, in which the switching member cooperates with the protruding portion to make the discharge circuit non-conductive, and a closed state, in which the switching member is released from the protruding portion to make the discharge circuit conducting; wherein the discharging system further comprises a discharging circuit board , on which the discharge element is arranged, and the switching member is configured to have at least one conductive movable member , wherein at least a part of the movable member is operably movable, and one end of the movable member is fixed on the discharging circuit board and electrically connected to the discharge element, and the other end thereof is operably connectable to the discharge element electrically; wherein when the switching member is in the intermediate open state, the protruding portion forces the movable member at a position where the movable member is in non-conductive connection with the discharge element. wherein the discharging system further comprises a discharging circuit board , on which the discharge element is arranged, and the switching member is configured to have at least one conductive movable member , wherein at least a part of the movable member is operably movable, and one end of the movable member is fixed on the discharging circuit board and electrically connected to the discharge element, and the other end thereof is operably connectable to the discharge element electrically; wherein when the switching member is in the intermediate open state, the protruding portion forces the movable member at a position where the movable member is in non-conductive connection with the discharge element.
Container closure having - a pouring element which merges into a container body or can be fastened to a container body, - at least one external thread , which is formed on the pouring element , and - a closure cap for closing a pouring opening , which is provided within the pouring element , the closure cap having - a cylindrical threaded part having an open periphery and an internal thread, which interacts with the external thread of the pouring element , - a tamper-evident band , which is connected to the open periphery of the threaded part by means of a plurality of predetermined breaking lugs , opening of the container closure for the first time being evident from the breaking of the predetermined breaking lugs and the tamper-evident band has a first and a second end , wherein the first end is fixed to the open periphery of the threaded part characterized in that the second end can be connected to the pouring element . - a pouring element which merges into a container body or can be fastened to a container body, - at least one external thread , which is formed on the pouring element , and - a closure cap for closing a pouring opening , which is provided within the pouring element , - a cylindrical threaded part having an open periphery and an internal thread, which interacts with the external thread of the pouring element , - a tamper-evident band , which is connected to the open periphery of the threaded part by means of a plurality of predetermined breaking lugs , opening of the container closure for the first time being evident from the breaking of the predetermined breaking lugs and the tamper-evident band has a first and a second end , wherein the first end is fixed to the open periphery of the threaded part
A rotating electric machine comprising: a rotary shaft member that rotates about an axis; a rotor including an annular rotor core in which a plurality of pairs of magnet housing holes is arranged in a circumferential direction in an outer periphery and which is fixed to the rotary shaft member , each of the pairs of magnet housing holes respectively housing permanent magnets and being arranged in such a manner as to be opened in a V-shape toward an outer side in a radial direction (D2); a stator including an annular stator core arranged at an interval in the radial direction (D2) with respect to the rotor , and a stator coil provided around the stator core ; a field yoke arranged on an outer side of the rotor in an axial direction (D1) of the rotary shaft member ; and a field coil that is provided in the field yoke and that generates field magnetic flux when energized, wherein a bridge portion is provided between two magnet housing holes that form the pair of magnet housing holes in the rotor core , an axially facing end surface at one end in the radial direction (D2) of the field yoke and an axially facing end surface of the bridge portion face each other in the axial direction (D1), and an axially facing end surface at another end in the radial direction (D2) of the field yoke , and an axially facing end surface in the axial direction (D1) of the stator core face each other in the axial direction (D1), characterized in that positions of the field coil and the stator coil in the axial direction (D1) at least partially overlap with each other. a rotary shaft member that rotates about an axis; a rotor including an annular rotor core in which a plurality of pairs of magnet housing holes is arranged in a circumferential direction in an outer periphery and which is fixed to the rotary shaft member , each of the pairs of magnet housing holes respectively housing permanent magnets and being arranged in such a manner as to be opened in a V-shape toward an outer side in a radial direction (D2); a stator including an annular stator core arranged at an interval in the radial direction (D2) with respect to the rotor , and a stator coil provided around the stator core ; a field yoke arranged on an outer side of the rotor in an axial direction (D1) of the rotary shaft member ; and a field coil that is provided in the field yoke and that generates field magnetic flux when energized, wherein a bridge portion is provided between two magnet housing holes that form the pair of magnet housing holes in the rotor core , an axially facing end surface at one end in the radial direction (D2) of the field yoke and an axially facing end surface of the bridge portion face each other in the axial direction (D1), and an axially facing end surface at another end in the radial direction (D2) of the field yoke , and an axially facing end surface in the axial direction (D1) of the stator core face each other in the axial direction (D1), characterized in that positions of the field coil and the stator coil in the axial direction (D1) at least partially overlap with each other.
A method of affixing a gasket to a flange of a heat exchanger core, the method comprising: aligning the gasket with the flange of the heat exchanger core, wherein the gasket comprises: a body; and a tab extending outward from the body; contacting the flange of the heat exchanger core with the gasket; and securing the gasket to the flange by bending the tab of the gasket around an outer edge of the flange and such that relative motion between the gasket and the flange is prevented by the tab; and characterized in that bending the tab is connected to the body by a weld interface, the body being formed from a first metallic material and the tab being formed from a second metallic material different from the first metallic material. aligning the gasket with the flange of the heat exchanger core, wherein the gasket comprises: a body; and a tab extending outward from the body; a body; and a tab extending outward from the body; contacting the flange of the heat exchanger core with the gasket; and securing the gasket to the flange by bending the tab of the gasket around an outer edge of the flange and such that relative motion between the gasket and the flange is prevented by the tab; and characterized in that bending the tab is connected to the body by a weld interface, the body being formed from a first metallic material and the tab being formed from a second metallic material different from the first metallic material.
A method for producing an artificial gingiva , wherein a 3D model of the artificial gingiva is already available, wherein a dental model with a corresponding internal structure for inserting the artificial gingiva is designed manually by a user or fully automatically by means of a computer , wherein the designed dental model is produced by means of a subtractive production process, such as a CAM production machine, or by means of an additive production process, such as a 3D printer , characterised in that a gingival template is designed on the basis of the 3D model of the artificial gingiva , which gingival template reproduces at least sub-regions of the 3D model of the artificial gingiva as a negative mould, wherein the gingival template is designed from at least two parts , wherein the parts of the gingival template are designed to be connectable to one another using connecting means , wherein a gingival material such as silicone is introduced into the produced gingival template and cured.
Method for assisting in the piloting of an aircraft (AC) in an approach of the aircraft (AC), with a view to a landing on a landing runway , characterized in that it comprises the following steps implemented iteratively: - a first determination step (E1), implemented by a first determination module , consisting in determining a current state of the aircraft (AC), the current state comprising at least one current position (Pc) of the aircraft (AC); - a second determination step (E2), implemented by a second determination module , consisting in determining a first distance (dstd) between a target state and the current state from a first approach strategy; - a third determination step (E3), implemented by the second determination module , consisting in determining a first ellipse contained in a horizontal plane in which the aircraft (AC) is moving, the first ellipse being formed by points determined in such a way that a sum, on the one hand, of a distance (d1) between the current position (Pc) of the aircraft (AC) and the points of the first ellipse and, on the other hand, of a distance (d2) between the points of the first ellipse and a projection onto the horizontal plane of the target position (PFAF) is equal to the first distance (dstd); - a display step (E14), implemented by a display module , comprising the display of at least the first ellipse on a screen of the display module . - a first determination step (E1), implemented by a first determination module , consisting in determining a current state of the aircraft (AC), the current state comprising at least one current position (Pc) of the aircraft (AC); - a second determination step (E2), implemented by a second determination module , consisting in determining a first distance (dstd) between a target state and the current state from a first approach strategy; - a third determination step (E3), implemented by the second determination module , consisting in determining a first ellipse contained in a horizontal plane in which the aircraft (AC) is moving, the first ellipse being formed by points determined in such a way that a sum, on the one hand, of a distance (d1) between the current position (Pc) of the aircraft (AC) and the points of the first ellipse and, on the other hand, of a distance (d2) between the points of the first ellipse and a projection onto the horizontal plane of the target position (PFAF) is equal to the first distance (dstd); - a display step (E14), implemented by a display module , comprising the display of at least the first ellipse on a screen of the display module .
A method for resource indication, comprising: receiving (S201), by a terminal device, a first instruction from a network device, wherein the first instruction is used for activating a semi-persistently configured resource of a first bandwidth part, BWP, in a non-activated state; activating, by the terminal device, the semi-persistently configured resource of the first BWP according to the first instruction, when the first BWP is in the non-activated state; receiving, by the terminal device, a BWP switching instruction from the network device; and activating, by the terminal device, the first BWP in response to reception of the BWP switching instruction; and, in response to the terminal device switching from a second BWP in an activated state to the first BWP, transmitting, by the terminal device, data on the first BWP by adopting the semi-persistently configured resource. receiving (S201), by a terminal device, a first instruction from a network device, wherein the first instruction is used for activating a semi-persistently configured resource of a first bandwidth part, BWP, in a non-activated state; activating, by the terminal device, the semi-persistently configured resource of the first BWP according to the first instruction, when the first BWP is in the non-activated state; receiving, by the terminal device, a BWP switching instruction from the network device; and activating, by the terminal device, the first BWP in response to reception of the BWP switching instruction; and, in response to the terminal device switching from a second BWP in an activated state to the first BWP, transmitting, by the terminal device, data on the first BWP by adopting the semi-persistently configured resource.
Method for operating a voice control system , having the steps of: - the user requesting a change of activation command; - the user inputting the new activation command; - accepting the new activation command; and the characterizing steps of: - determining the word gender of an activation word included in the new activation command; - stipulating the voice output voice according to the word gender if the word gender is explicitly masculine or explicitly feminine; and - retaining the previous voice output voice if the word gender is not explicitly masculine and not explicitly feminine. - the user requesting a change of activation command; - the user inputting the new activation command; - accepting the new activation command; - determining the word gender of an activation word included in the new activation command; - stipulating the voice output voice according to the word gender if the word gender is explicitly masculine or explicitly feminine; and - retaining the previous voice output voice if the word gender is not explicitly masculine and not explicitly feminine.
A vehicle glazing unit comprising a glazed element having an outer face , an edge face and an inner face , said glazing unit comprising, along at least a part of a bottom edge, a profiled bead comprising a groove for clip-fastening a covering piece on said profiled bead , said covering piece comprising, as seen in cross section, a barbed hook that passes into said groove during clip-fastening, said profiled bead being situated against said edge face of said glazed element , said profiled bead comprising, as seen in cross section, an inner leg situated beneath said inner face of said glazed element , characterized in that said inner leg comprises, at least in a bottom part of said profiled bead , at least one hole passing through said inner leg , said hole preferably having a length of between 2.0 and 50.0 mm and a width (l 66 ) of between 2.0 and 10.0 mm, said hole being void of solid material and being situated in plumb with the groove , outside the latter, just at the junction between the inner leg and the groove .
Detector of smoke, gas or particles, that comprises: - a detection chamber connected to a suction device and to an opening allowing a flow of air and particles or gas to pass; - a means for retaining particles in the chamber; - a detector of the presence of smoke, gas or particles in the detection chamber; and - an emitter of a signal representative of the detection of smoke, gas or particles in the detection chamber, characterized in that the retention means comprises a volume inside the chamber configured such that a flow of air sucked in forms a vortex, between an inlet and an outlet of said chamber, to increase the time that smoke particles occupy the chamber. - a detection chamber connected to a suction device and to an opening allowing a flow of air and particles or gas to pass; - a means for retaining particles in the chamber; - a detector of the presence of smoke, gas or particles in the detection chamber; and - an emitter of a signal representative of the detection of smoke, gas or particles in the detection chamber,
A container for liquids comprising a cap , wherein the cap includes: a body configured to be attached to an upper surface of the container , and a perforation platform comprising a plurality of protruding perforating elements , so that the perforation platform is displaced vertically with respect to the cap body from a resting position to a working position, wherein the perforating elements perforate the upper surface of the container ; in the resting position, the perforation platform is horizontally aligned with the upper surface of the cap body, while, in the working position, the perforation platform is displaced vertically, and in its entirety, a distance so that the protruding perforating elements exclusively penetrate the upper surface of the container and with the perforation platform remaining in a parallel position to the upper surface of the cap ; and which is characterised in that the perforation platform also comprises a drinking orifice which cooperates with one of the protruding perforating elements when the protruding perforating element perforates the upper surface of the container . a body configured to be attached to an upper surface of the container , and a perforation platform comprising a plurality of protruding perforating elements , so that the perforation platform is displaced vertically with respect to the cap body from a resting position to a working position, wherein the perforating elements perforate the upper surface of the container ; in the resting position, the perforation platform is horizontally aligned with the upper surface of the cap body, while, in the working position, the perforation platform is displaced vertically, and in its entirety, a distance so that the protruding perforating elements exclusively penetrate the upper surface of the container and with the perforation platform remaining in a parallel position to the upper surface of the cap ; and which is characterised in that the perforation platform also comprises a drinking orifice which cooperates with one of the protruding perforating elements when the protruding perforating element perforates the upper surface of the container .
A method for operating a turboprop engine for an aircraft, the method comprising: controlling a propeller of the turboprop engine based on a selected one of a reference propeller rotational speed and a minimum propeller blade angle while the turboprop engine is running; detecting an inflight restart of the turboprop engine ; and characterized in that it further comprises controlling the propeller during the inflight restart in accordance with at least one of a modified reference propeller rotational speed and a modified minimum propeller blade angle to maintain an actual propeller blade angle above an aerodynamic disking angle during the inflight restart. controlling a propeller of the turboprop engine based on a selected one of a reference propeller rotational speed and a minimum propeller blade angle while the turboprop engine is running; detecting an inflight restart of the turboprop engine ; and characterized in that it further comprises controlling the propeller during the inflight restart in accordance with at least one of a modified reference propeller rotational speed and a modified minimum propeller blade angle to maintain an actual propeller blade angle above an aerodynamic disking angle during the inflight restart.