mhurhangee/ep-ind-claims huggingface dataset:
A deformation structure, which is adapted for example for pedestrian protection for a motor vehicle for arrangement between a bumper cover and a bumper crossbeam, comprising a series of deformation elements arranged one behind the other in a deformation direction, characterised in that every two adjacent deformation elements are coupled together by means of a coupling mechanism in such a way that, in a first load case, two adjacent deformation elements enter into a latching engagement with one another or are positioned in a latching engagement, such that a relative displacement of the adjacent deformation elements with respect to one another in the deformation direction is prevented, or at least made more difficult, and a deforming of the deformation structure occurs at a high level of force, and, in a second load case, two adjacent deformation elements do not enter into the latching engagement or leave the latching engagement, such that a relative displacement of the adjacent deformation elements in the deformation direction is enabled, or at least made easier, and a deforming of the deformation structure occurs at a low level of force.
An aeration element for gasification or aeration of liquids, comprising: an essentially flattened, rigid support element having a substantially oval cross-section and corrugated outer surfaces (3, 4), said corrugated outer surfaces including ridges defining grooves therebetween; a threaded opening for receiving a cooperating fitting for a sealed connection to an air supply; a flexible membrane disposed around said support element, said membrane having a plurality of slits disposed therein, wherein compressed gas is introduced between said support element and said membrane and can escape via said slits into a liquid that is to be gasified; at least one retaining clamp for holding said membrane around at least one end of said support element; and a check valve assembly for preventing backflow of debris into an interior of said support element, said check valve assembly comprising an opening formed in the support element and a flexible band positioned around a circumference of said support element and covering said opening for sealing said opening from said debris, characterized in that said support element includes a stepped portion around at least one end, said stepped portion including a recessed area for receiving the flexible band of said check valve assembly. an essentially flattened, rigid support element having a substantially oval cross-section and corrugated outer surfaces (3, 4), said corrugated outer surfaces including ridges defining grooves therebetween; a threaded opening for receiving a cooperating fitting for a sealed connection to an air supply; a flexible membrane disposed around said support element, said membrane having a plurality of slits disposed therein, wherein compressed gas is introduced between said support element and said membrane and can escape via said slits into a liquid that is to be gasified; at least one retaining clamp for holding said membrane around at least one end of said support element; and a check valve assembly for preventing backflow of debris into an interior of said support element, said check valve assembly comprising an opening formed in the support element and a flexible band positioned around a circumference of said support element and covering said opening for sealing said opening from said debris, characterized in that said support element includes a stepped portion around at least one end, said stepped portion including a recessed area for receiving the flexible band of said check valve assembly.
Apparatus for performing at least one electrical or electromechanical function, preferably a communication function, wherein the apparatus comprises at least one housing and at least one pushbutton, wherein the housing comprises at least one first hinge element, wherein the pushbutton comprises at least one second hinge element, wherein the first and second hinge elements (146, 160) are adapted to interact as a hinge in an assembled state of the apparatus, characterized in that the apparatus further comprises at least one snap element physically separate from the first and second hinge elements (146, 160), wherein the snap element is adapted to hold the pushbutton and the housing together when the first and second hinge elements (146, 160) are engaged, wherein the snap element comprises at least one flexible latch element, wherein the latch element is adapted to be flexed open when the pushbutton is mounted to the housing and wherein the latch element is adapted to lock in a locked position when the first and second hinge elements (146, 160) are engaged.
A method of growing a silicon ingot comprising a dopant material having a segregation coefficient of k, the method comprising the steps of: i) providing a crucible having an inner growth zone in fluid communication with an outer feed zone; ii) providing an initial charge in the inner growth zone and the outer feed zone, the initial charge in the inner growth zone comprising silicon and the dopant material and the initial charge in the outer feed zone comprising silicon and no dopant material; iii) melting the silicon and dopant material in the inner growth zone to form a melted mixture and the silicon in the outer feed zone to form a silicon melt, the melted mixture and the silicon melt having upper melt surfaces at substantially similar heights, wherein the inner growth zone has a cross-sectional surface area at the upper melt surface of the melted mixture of A s and the crucible has a total cross-sectional surface area at the upper melt surface area of the melted mixture and the silicon melt of A t; iv) growing the silicon ingot from the inner growth zone; and v) removing the grown silicon ingot comprising the dopant material in an axially substantially constant concentration, wherein the method is a continuous Czochralski growth method comprising the step of delivering a feed comprising silicon and no dopant material into the outer feed zone in an amount M F; while growing the silicon ingot to an amount M x, and wherein dM F / dM x = 1 − k A t / A s i) providing a crucible having an inner growth zone in fluid communication with an outer feed zone; ii) providing an initial charge in the inner growth zone and the outer feed zone, the initial charge in the inner growth zone comprising silicon and the dopant material and the initial charge in the outer feed zone comprising silicon and no dopant material; iii) melting the silicon and dopant material in the inner growth zone to form a melted mixture and the silicon in the outer feed zone to form a silicon melt, the melted mixture and the silicon melt having upper melt surfaces at substantially similar heights, wherein the inner growth zone has a cross-sectional surface area at the upper melt surface of the melted mixture of A s and the crucible has a total cross-sectional surface area at the upper melt surface area of the melted mixture and the silicon melt of A t; iv) growing the silicon ingot from the inner growth zone; and v) removing the grown silicon ingot comprising the dopant material in an axially substantially constant concentration,
Vertical axis wind turbine comprising a support base, a shaft extending centrally from the support base, a support frame for a plurality of blades (4a, 4b, 4c), mounted on the base rotatable with the shaft, and a control frame for the plurality of blades (4a, 4b, 4c), mounted on the shaft, above the blade support frame; wherein each blade of the plurality of blades (4a, 4b, 4c) comprises a first half-blade and a second half-blade supported by the blade support frame; characterized in that the blade control frame comprises a control element mounted rotatably on the shaft, a pin, extending from the control element in an eccentric position with respect to the shaft, a plurality of connecting rods, one for each blade (4a, 4b, 4c), rotatably supported by the pin and a directional deflector extending from the pin and rotatable integrally with it; and in that each blade (4a, 4b, 4c) comprises a fixed rod associated with the blade support frame and a mobile rod having an end sliding on the blade support frame and another end associated with a respective connecting rod of the blade control frame; wherein, during the rotation of the turbine, the directional deflector angles toward the direction of the wind flow, thereby fixing an angular position of the pin with respect to the shaft and the mobile rod of each blade (4a, 4b, 4c) rotates following a trajectory (T M), eccentric with respect to a trajectory (T F) of the fixed rod, sliding on the blade support frame and thus causing the opening and closing of the blades (4a, 4b, 4c). wherein each blade of the plurality of blades (4a, 4b, 4c) comprises a first half-blade and a second half-blade supported by the blade support frame; characterized in that the blade control frame comprises a control element mounted rotatably on the shaft, a pin, extending from the control element in an eccentric position with respect to the shaft, a plurality of connecting rods, one for each blade (4a, 4b, 4c), rotatably supported by the pin and a directional deflector extending from the pin and rotatable integrally with it; and in that each blade (4a, 4b, 4c) comprises a fixed rod associated with the blade support frame and a mobile rod having an end sliding on the blade support frame and another end associated with a respective connecting rod of the blade control frame; wherein, during the rotation of the turbine, the directional deflector angles toward the direction of the wind flow, thereby fixing an angular position of the pin with respect to the shaft and the mobile rod of each blade (4a, 4b, 4c) rotates following a trajectory (T M), eccentric with respect to a trajectory (T F) of the fixed rod, sliding on the blade support frame and thus causing the opening and closing of the blades (4a, 4b, 4c).
An exhaust gas treatment system for an advanced humid air turbine system, the exhaust gas treatment system treating water content contained in an exhaust gas discharged from a gas turbine system in which a working fluid is humidified, comprising: an exhaust gas flow path through which the exhaust gas discharged from the gas turbine system flows; a water recovery unit (32; 32D; 32E) connected to the exhaust gas flow path, the water recovery unit being configured to cool an exhaust gas that flows in from the exhaust gas flow path by a refrigerant to thereby recover water content contained in the exhaust gas; and at least one bypass flow path (40; 40B; 40C) through which part of the exhaust gas from the exhaust gas flow path flows so as to avoid cooling by the refrigerant in the water recovery unit (32; 32D; 32E), characterized in that the at least one bypass flow path (40; 40B; 40C) has a downstream end disposed in the water recovery unit (32; 32D; 32E) at a position downstream in a flow direction of the exhaust gas with respect to a zone in which the exhaust gas is cooled in the water recovery unit (32; 32D; 32E). an exhaust gas flow path through which the exhaust gas discharged from the gas turbine system flows; a water recovery unit (32; 32D; 32E) connected to the exhaust gas flow path, the water recovery unit being configured to cool an exhaust gas that flows in from the exhaust gas flow path by a refrigerant to thereby recover water content contained in the exhaust gas; and at least one bypass flow path (40; 40B; 40C) through which part of the exhaust gas from the exhaust gas flow path flows so as to avoid cooling by the refrigerant in the water recovery unit (32; 32D; 32E), characterized in that the at least one bypass flow path (40; 40B; 40C) has a downstream end disposed in the water recovery unit (32; 32D; 32E) at a position downstream in a flow direction of the exhaust gas with respect to a zone in which the exhaust gas is cooled in the water recovery unit (32; 32D; 32E).
A hinge, comprising a first block, including first means for attachment to a frame and first bearing means for axial support of second support bearing means, belonging to a second block including second means for attachment to a door, the first and second bearing means (13, 23) being designed for mutual cooperation in relative rotation with respect to an axial direction of a geometric hinge pin axis, the first bearing means being mounted movable in axial position, within a predetermined range of axial adjustment extending along said axial direction with respect to the first attachment means and being associated with means for adjusting said axial position and with means for locking in said axial position, characterized in that the locking means include a pin arranged to be accommodated in a hinge pin hole, wherein the first bearing means include a support bearing socket with a support bearing surface turned toward the second bearing means and with a support surface turned opposite to the support bearing surface intended to be supported by the pin, wherein a hinge pin adjustment segment is intended to be rotatably mounted, and movable in axial translation, with respect to the first attachment means and includes a support ramp for adjusting axial position, inclined with respect to a plane that is purely radial to said axial direction, intended to cooperate with a support ramp relief integral with the first attachment means, wherein the pin is further functionally associated with means of abutment in rotation integral with the first attachment means, arranged to limit any parasitical rotation of the hinge pin adjustment segment.
A method for determining a data transmission delay in a plurality of data lanes, characterized in that the method comprises: parsing a received data of each data lane, according to Initial Lane Alignment, ILA, information already existing in the data of each data lane, so as to obtain a first Local Multi Frame Clock, LMFC; according to a preset frequency division multiple, performing frequency division on a first LMFC of each data lane to obtain a second LMFC corresponding to each data lane, wherein, a period of the second LMFC corresponding to each data lane is greater than a data transmission delay corresponding to a data lane having the maximum data transmission delay in all the data lanes before the frequency division; clearing a write address in each buffer corresponding to each data lane using the second LMFC, and according to the second LMFC, writing respectively the data of each data lane into a corresponding buffer; and according to a system reference, SYSREF, signal and a preset LMFC interval, generating a third LMFC; clearing a read address in each buffer corresponding to each data lane using the third LMFC, and according to the third LMFC, reading respectively the data of each data lane from the corresponding buffer, wherein the period of the second LMFC is the same as a period of the third LMFC; and in each data lane, the data transmission delay is: (N-1)*T_LMFC; where N is the preset frequency division multiple, and T_LMFC is a length of a standard LMFC. parsing a received data of each data lane, according to Initial Lane Alignment, ILA, information already existing in the data of each data lane, so as to obtain a first Local Multi Frame Clock, LMFC; according to a preset frequency division multiple, performing frequency division on a first LMFC of each data lane to obtain a second LMFC corresponding to each data lane, wherein, a period of the second LMFC corresponding to each data lane is greater than a data transmission delay corresponding to a data lane having the maximum data transmission delay in all the data lanes before the frequency division; clearing a write address in each buffer corresponding to each data lane using the second LMFC, and according to the second LMFC, writing respectively the data of each data lane into a corresponding buffer; and according to a system reference, SYSREF, signal and a preset LMFC interval, generating a third LMFC; clearing a read address in each buffer corresponding to each data lane using the third LMFC, and according to the third LMFC, reading respectively the data of each data lane from the corresponding buffer, wherein the period of the second LMFC is the same as a period of the third LMFC; and in each data lane, the data transmission delay is: (N-1)*T_LMFC; where N is the preset frequency division multiple, and T_LMFC is a length of a standard LMFC.
An epoxy resin composition comprising at least the undermentioned components to, the component accounting for 5 to 40 parts by mass, the component accounting for 20 to 95 parts by mass, and the component accounting for 1 to 25 parts by mass, relative to the total quantity of the epoxy resins which accounted for 100 parts by mass:: epoxy resin having two naphthalene backbones and mainly two epoxy groups in a repeating unit as represented by general formula. wherein X in general formulae is an alkylene group containing 1 carbon atom or a group as represented by general formula; R in general formula is one selected from the group consisting of a glycidyl ether group, a group as represented by general formula, a hydrogen atom, a halogen atom, a phenyl group, and an alkyl group containing 1 to 4 carbon atoms; Y is a naphthalene backbone; Z is a naphthalene backbone; Y and Z each have a glycidyl ether group, or either Y or Z has a substituent group as represented by general formula, and each repeating unit mainly contains two epoxy groups; the naphthalene ring in Y or Z may be bonded to the backbone chain at the ortho position or the meta position;;: a glycidyl amine type epoxy resin having three or more glycidyl groups in a molecule;: sulfone based or imide based thermoplastic resin; and: epoxy resin curing agent; and wherein the epoxy resin composition has a viscosity of 5 to 100 Pa·s at 80 °C and is measured by the method referred to in the description.: epoxy resin having two naphthalene backbones and mainly two epoxy groups in a repeating unit as represented by general formula. wherein X in general formulae is an alkylene group containing 1 carbon atom or a group as represented by general formula; R in general formula is one selected from the group consisting of a glycidyl ether group, a group as represented by general formula, a hydrogen atom, a halogen atom, a phenyl group, and an alkyl group containing 1 to 4 carbon atoms; Y is a naphthalene backbone; Z is a naphthalene backbone; Y and Z each have a glycidyl ether group, or either Y or Z has a substituent group as represented by general formula, and each repeating unit mainly contains two epoxy groups; the naphthalene ring in Y or Z may be bonded to the backbone chain at the ortho position or the meta position;;: a glycidyl amine type epoxy resin having three or more glycidyl groups in a molecule;: sulfone based or imide based thermoplastic resin; and: epoxy resin curing agent; and
A connector (10, 10A, 10B, 10C, 10D) with a coaxial cable, comprising: an electrically conductive first terminal that is crimped and fixed onto an inner conductor of said coaxial cable; an electrically conductive first conductive member (80, 80A, 80B) that is crimped and fixed onto an outer conductor of said coaxial cable; an electrically insulative housing (50, 50A, 50C, 50D) that comprises a first housing chamber housing the first terminal and the first conductive member (80, 80A, 80B); and an electrically conductive first shell to which the first conductive member (80, 80A, 80B) being housed is connected and which is configured as at least one of a ground and a shield; characterized by comprising a first protrusion which contacts the first shell and is disposed in the first conductive member (80, 80A, 80B); and a first support hole formed in the first shell, the first support hole supporting the first conductive member (80, 80A, 80B) with the first protrusion fitted into the first support hole. an electrically conductive first terminal that is crimped and fixed onto an inner conductor of said coaxial cable; an electrically conductive first conductive member (80, 80A, 80B) that is crimped and fixed onto an outer conductor of said coaxial cable; an electrically insulative housing (50, 50A, 50C, 50D) that comprises a first housing chamber housing the first terminal and the first conductive member (80, 80A, 80B); and an electrically conductive first shell to which the first conductive member (80, 80A, 80B) being housed is connected and which is configured as at least one of a ground and a shield; characterized by comprising a first protrusion which contacts the first shell and is disposed in the first conductive member (80, 80A, 80B); and a first support hole formed in the first shell, the first support hole supporting the first conductive member (80, 80A, 80B) with the first protrusion fitted into the first support hole.
A method for producing a laminate comprising at least two nonwoven layers (1, 2) of continuous filaments, in particular of continuous filaments of thermoplastic material arranged one above the other, wherein a first nonwoven layer is produced which has a higher shrinkage capacity or a higher shrinkage potential in the direction of its surface extension than a second nonwoven layer, wherein the first nonwoven layer is produced by means of a spunbond method and/or by means of a meltblown method from multicomponent filaments, in particular from bicomponent filaments, wherein the second nonwoven layer is produced by means of a spunbond method or by means of a meltblown method from multicomponent filaments - in particular from bicomponent filaments - and/or from monocomponent filaments and is directly flatly combined or brought together with the first nonwoven layer, in particular is laid directly on the first nonwoven layer, wherein the unit comprising the at least two or both nonwoven layers (1, 2) arranged one on top of the other is consolidated such that over the surface of the unit consolidation regions and consolidation-free regions are arranged in a distributed manner, wherein following the consolidation, shrinkage of the first nonwoven layer is activated so that as a result of the shrinkage of the first nonwoven layer consolidation-free regions of the second nonwoven layer are displaced or raised transversely, in particular perpendicularly to the surface extension of the unit, and wherein a laminate having a thickness D of less than 2 mm is produced.