mhurhangee/ep-ind-claims huggingface dataset:
Exhaust-gas turbocharger having a regulating unit for regulating the power of the exhaust-gas turbocharger, and having an actuator for operating the regulating unit, wherein the regulating unit can be operated, via an operation lever assigned thereto, by way of a thrust rod of the actuator, and the thrust rod is connected to the operation lever of the regulating unit via an adjustment member, wherein the adjustment member has a screw-nut element and an attachment element, wherein the attachment element is coupled to the operation lever and the screw-nut element has a first threaded region, via which it is coupled to the attachment element, and a second threaded region, via which it is coupled to the thrust rod, characterized in that the screw-nut element has an internal thread arranged in a passage bore and has an external thread arranged on the outer circumference of a cylindrical projection piece, and the attachment element has an internal thread corresponding to the external thread of the screw-nut element, and the thrust rod has, correspondingly thereto, an external thread corresponding to the internal thread of the screw-nut element, which internal thread and external thread are in each case screwed to the screw-nut element, wherein the internal thread in the passage bore and the external thread on the projection piece of the screw-nut element run in each case codirectionally and have the same pitch or different pitches.
A composition for use in dental tissue repair and/or regeneration, comprising a triacrylate and a porous scaffold, wherein the triacrylate promotes adhesion and/or proliferation of dental pulp stem cells (DPSCs).
Vehicle component for a vehicle, in particular a rail vehicle for high-speed traffic, comprising - a surface (102.1; 202.1; 316.3) which, during operation, is exposed to a relative wind-induced air flow having a local main flow direction, wherein - said surface (102.1; 202.1; 316.3) has a separation region in the form of a flow separation edge (107; 207; 307) at which said air flow separates from said surface (102.1; 202.1; 316.3), and - at least one perturbing element (115; 215; 315) associated upstream to said flow separation edge (107; 207; 307) is provided, which is formed in order to introduce a perturbation into said air flow, characterised in that - said perturbing element (115; 215; 315) has at least one guide face (115.1; 215.1; 315.1) protruding into said air flow, wherein - said guide face (115.1; 215.1; 315.1) being formed, and inclined by an inclination angle with respect to said local main flow direction, in such a way that a velocity component, which is oriented transversely with respect to said local main flow direction and which induces downstream of said perturbing element (115; 215; 315) a local turbulence in a shear layer of said air flow separated downstream of said perturbing element (115; 215; 315) at said flow separation edge (107; 207; 307), is imposed to said part of said air flow striking said guide face (115.1; 215.1; 315.1). - a surface (102.1; 202.1; 316.3) which, during operation, is exposed to a relative wind-induced air flow having a local main flow direction, wherein - said surface (102.1; 202.1; 316.3) has a separation region in the form of a flow separation edge (107; 207; 307) at which said air flow separates from said surface (102.1; 202.1; 316.3), and - at least one perturbing element (115; 215; 315) associated upstream to said flow separation edge (107; 207; 307) is provided, which is formed in order to introduce a perturbation into said air flow, characterised in that - said perturbing element (115; 215; 315) has at least one guide face (115.1; 215.1; 315.1) protruding into said air flow, wherein - said guide face (115.1; 215.1; 315.1) being formed, and inclined by an inclination angle with respect to said local main flow direction, in such a way that a velocity component, which is oriented transversely with respect to said local main flow direction and which induces downstream of said perturbing element (115; 215; 315) a local turbulence in a shear layer of said air flow separated downstream of said perturbing element (115; 215; 315) at said flow separation edge (107; 207; 307), is imposed to said part of said air flow striking said guide face (115.1; 215.1; 315.1).
A softside luggage article comprising: a first panel (108, 114); a frame supporting the first panel (108, 114), the frame including: a first structural member extending along a first edge of the first panel (108, 114); a second structural member extending along a second edge of the first panel (108, 114); and two or more cross braces connected to and extending between the first and second structural members; a carry handle including opposing first and second end portions (270, 272), each end portion (270, 272) of the carry handle coupled to one of the two or more cross braces; and a reinforcing strap (274, 276) coupled to an end portion (270, 272) of the carry handle, the reinforcing strap (274, 276) extending to and coupling with an edge of the first panel (108, 114). a first panel (108, 114); a frame supporting the first panel (108, 114), the frame including: a first structural member extending along a first edge of the first panel (108, 114); a second structural member extending along a second edge of the first panel (108, 114); and two or more cross braces connected to and extending between the first and second structural members; a first structural member extending along a first edge of the first panel (108, 114); a second structural member extending along a second edge of the first panel (108, 114); and two or more cross braces connected to and extending between the first and second structural members; a carry handle including opposing first and second end portions (270, 272), each end portion (270, 272) of the carry handle coupled to one of the two or more cross braces; and a reinforcing strap (274, 276) coupled to an end portion (270, 272) of the carry handle, the reinforcing strap (274, 276) extending to and coupling with an edge of the first panel (108, 114).
A method of upgrading a modular gas turbine engine, wherein the gas turbine engine comprises: a first fan module comprising a fan having plurality of fan blades; a first engine core module including an engine core and a gearbox arranged to provide drive to the fan; and a first fan case module comprising a fan case arranged to enclose the fan blades, the method including the steps of: disassembling the gas turbine engine, replacing a one of the first fan module, first engine core module or first fan case module with a replacement fan module, a replacement engine core module or a replacement fan case module; and reassembling the gas turbine engine using the replacement module (50', 52', 54'), wherein the replacement module (50', 52', 54') is compatible with the others of the first fan module, first engine core module or first fan case module; and wherein the replacement module (50', 52' 54') is designed to different parameters to the one of the first fan module, first engine core module or first fan case module, such that it improves the performance of the engine; characterised in that the method comprises subjecting each module (50, 52, 54, 50', 52', 54') to a separate passing off process to determine a power setting parameter for the respective module; and combining the contributions from each module (50, 52, 54, 50', 52', 54') to determine a combined power rating for the engine. disassembling the gas turbine engine, replacing a one of the first fan module, first engine core module or first fan case module with a replacement fan module, a replacement engine core module or a replacement fan case module; and reassembling the gas turbine engine using the replacement module (50', 52', 54'), wherein the replacement module (50', 52', 54') is compatible with the others of the first fan module, first engine core module or first fan case module; and wherein the replacement module (50', 52' 54') is designed to different parameters to the one of the first fan module, first engine core module or first fan case module, such that it improves the performance of the engine; characterised in that the method comprises subjecting each module (50, 52, 54, 50', 52', 54') to a separate passing off process to determine a power setting parameter for the respective module; and combining the contributions from each module (50, 52, 54, 50', 52', 54') to determine a combined power rating for the engine. wherein the replacement module (50', 52', 54') is compatible with the others of the first fan module, first engine core module or first fan case module; and wherein the replacement module (50', 52' 54') is designed to different parameters to the one of the first fan module, first engine core module or first fan case module, such that it improves the performance of the engine; characterised in that the method comprises subjecting each module (50, 52, 54, 50', 52', 54') to a separate passing off process to determine a power setting parameter for the respective module; and combining the contributions from each module (50, 52, 54, 50', 52', 54') to determine a combined power rating for the engine.
A package 10 for products, in which the package has a substantially truncated rectangular or square shape, and in which the package comprises: at least two flexible adjoined layers 12, 14 configured to provide a cavity extending therebetween for containing a product, in which the at least two flexible adjoined layers 12, 14 are moveable between: a first closed configuration in which the flexible adjoined layers 12, 14 are sealed around the entire periphery thereof to isolate the cavity from an external environment; and a second open configuration in which the flexible adjoined layers 12, 14 extend in a substantially cone shaped configuration defining the cavity therebetween, and in which the base of the substantially cone shaped configuration provides an opening extending into the cavity, in which the package comprises a front surface provided by a first flexible layer 12, a rear surface provided by a second flexible layer 14, and a cavity extending therebetween, in which each flexible layer comprises a top end 16, 16' and an opposed bottom end 18, and in which each of the flexible adjoined layers 12, 14 comprises a first corner 20 provided at the top end 16, 16', a diagonally opposed second corner 22 provided at an opposed bottom end 18, and an openable seam 24 extending therebetween. a first closed configuration in which the flexible adjoined layers 12, 14 are sealed around the entire periphery thereof to isolate the cavity from an external environment; and a second open configuration in which the flexible adjoined layers 12, 14 extend in a substantially cone shaped configuration defining the cavity therebetween, and in which the base of the substantially cone shaped configuration provides an opening extending into the cavity, in which the package comprises a front surface provided by a first flexible layer 12, a rear surface provided by a second flexible layer 14, and a cavity extending therebetween, in which each flexible layer comprises a top end 16, 16' and an opposed bottom end 18, and in which each of the flexible adjoined layers 12, 14 comprises a first corner 20 provided at the top end 16, 16', a diagonally opposed second corner 22 provided at an opposed bottom end 18, and an openable seam 24 extending therebetween.
Assembly of a condenser for an air conditioning circuit, and a refrigerating fluid reserve, the condenser comprising a housing which is connected to the refrigerating fluid reserve, the housing receiving a first portion for heat exchange between the refrigerating fluid and a cooling liquid, the first portion being configured to convey the refrigerating fluid to the refrigerating fluid reserve, and a second heat exchange portion which is configured to produce a heat exchange complement between the refrigerating fluid and the cooling liquid at the outlet of the reserve, the reserve being located facing a lateral side of the housing, that is to say a side of the housing located between longitudinal end sides (12, 14) of the housing, wherein the housing comprises an assembly of plates stacked along a stacking direction that is essentially orthogonal to the plates, which define between them circulation blades (21, 23) for the refrigerating fluid and the cooling fluid in the heat exchange portions (13, 15), the assembly of plates being configured to provide a circulation path of the refrigerating fluid allowing circulation in series of the refrigerating fluid in the housing, from the first heat exchange portion toward the fluid reserve, then from the latter into the second heat exchange portion, characterized in that each of the plates extends with continuity of material in the region of the first heat exchange portion and the second heat exchange portion.
Method for manufacturing a brake disc comprising the following operating steps: a) preparing a brake disc, comprising a braking band and provided with two mutually opposite braking surfaces (2a, 2b), each of which defines at least partially one of the two main faces of the disc, the braking band being made of aluminium or aluminium alloy, or being made of grey cast iron or steel; b) depositing on the disc a layer of chromium carbide and nickel-chromium in particulate form with High Velocity Oxygen Fuel technique, High Velocity Air Fuel technique or Kinetic Metallisation technique forming a base protective coating that covers at least one of the two braking surfaces of the braking band in direct contact with them; and c) depositing over said base protective coating a material in particulate form consisting of tungsten carbide and cobalt (Co) with High Velocity Oxygen Fuel technique, High Velocity Air Fuel technique or Kinetic Metallisation technique forming a surface protective coating that covers at least one of the two braking surfaces of the braking band. a) preparing a brake disc, comprising a braking band and provided with two mutually opposite braking surfaces (2a, 2b), each of which defines at least partially one of the two main faces of the disc, the braking band being made of aluminium or aluminium alloy, or being made of grey cast iron or steel; b) depositing on the disc a layer of chromium carbide and nickel-chromium in particulate form with High Velocity Oxygen Fuel technique, High Velocity Air Fuel technique or Kinetic Metallisation technique forming a base protective coating that covers at least one of the two braking surfaces of the braking band in direct contact with them; and c) depositing over said base protective coating a material in particulate form consisting of tungsten carbide and cobalt (Co) with High Velocity Oxygen Fuel technique, High Velocity Air Fuel technique or Kinetic Metallisation technique forming a surface protective coating that covers at least one of the two braking surfaces of the braking band.
Steel, which consists of (in % by weight) C: 0.4 to 0.7%, Si: 0.15 to 0.5% Mn: 0.8 to 2.0% Cr: 0.3 to 1.0%, wherein the Cr content %Cr in each case meets the following condition: %Cr≥(%Ni + %Si + %Mn + %S + %Al)/5 with %Ni: respective Ni content of the steel %Si: respective Si content of the steel %Mn: respective Mn content of the steel %S: respective S content of the steel %Al: respective Al content of the steel N: 0.0015 to 0.010% Ni: 0.04 to 2% Ti: 0.005 to 0.1% V: 0.0080 to 0.1% B: 0.0005 to 0.004% Ca: 0.0005 to 0.004% P: ≤ 0.030% S: ≤ 0.005% Al: ≤ 0.05% Cu: ≤ 0.1% Nb: ≤ 0.004% H: ≤ 0.0001% O: ≤ 0.0050% and optionally Mo: 0.006 to 0.02%, remainder iron and unavoidable impurities. with %Ni: respective Ni content of the steel %Si: respective Si content of the steel %Mn: respective Mn content of the steel %S: respective S content of the steel %Al: respective Al content of the steel
A pregrouted PC steel material (10, 10') comprising: a PC steel stranded wire composed of a plurality of steel wires (1a, 1b, 1c, 1d); a pregrout layer disposed on an outer periphery of said PC steel stranded wire so as to accommodate said PC steel stranded wire; a sheath covering an outer periphery of said pregrout layer; and a capsule including a pregrout-hardening agent and a film with which said pregrout-hardening agent is covered, said capsule being interposed among said steel wires (1a, 1b, 1c, 1d) constituting said PC steel stranded wire, said capsule having a strength such that said capsule is not broken before tensioning said PC steel stranded wire characterized in that the capsule is broken by compressive and shearing forces exerted on the capsule present in a gap among said steel wires (1a, 1b, 1c, 1d) with a narrowing of the gap during the tensioning, wherein said capsule and a binder are interposed in said gap among said steel wires (1a, 1b, 1c, 1d) constituting said PC steel stranded wire. a PC steel stranded wire composed of a plurality of steel wires (1a, 1b, 1c, 1d); a pregrout layer disposed on an outer periphery of said PC steel stranded wire so as to accommodate said PC steel stranded wire; a sheath covering an outer periphery of said pregrout layer; and a capsule including a pregrout-hardening agent and a film with which said pregrout-hardening agent is covered, said capsule being interposed among said steel wires (1a, 1b, 1c, 1d) constituting said PC steel stranded wire, said capsule having a strength such that said capsule is not broken before tensioning said PC steel stranded wire characterized in that the capsule is broken by compressive and shearing forces exerted on the capsule present in a gap among said steel wires (1a, 1b, 1c, 1d) with a narrowing of the gap during the tensioning, wherein said capsule and a binder are interposed in said gap among said steel wires (1a, 1b, 1c, 1d) constituting said PC steel stranded wire.
A femoral component for a knee prosthesis, comprising: an anterior flange; a medial condyle extending from the anterior flange to a posterior end thereof and having inner and outer edges (216, 218) defining a medial condyle width therebetween; and a lateral condyle extending from the anterior flange to a posterior end thereof and having inner and outer edges (226, 228) defining a lateral condyle width therebetween, the inner edge of the lateral condyle having a first portion, a second portion, and an intermediate portion, wherein the inner edges (226, 216) of the lateral and medial condyles (220, 210) define an intercondylar notch and lateral and medial extents of the intercondylar notch such that an intercondylar width extends between the inner edges (226, 216) of the lateral and medial condyles (220, 210), wherein the inner edge of the lateral condyle tapers toward the outer edge of the lateral condyle at the intermediate portion such that the width of the intercondylar notch is greater along the second portion of the inner edge of the lateral condyle than along the first portion of the lateral condyle, characterized in that the inner edge lies substantially along a single plane from the anterior flange to the posterior end of the medial condyle. an anterior flange; a medial condyle extending from the anterior flange to a posterior end thereof and having inner and outer edges (216, 218) defining a medial condyle width therebetween; and a lateral condyle extending from the anterior flange to a posterior end thereof and having inner and outer edges (226, 228) defining a lateral condyle width therebetween, the inner edge of the lateral condyle having a first portion, a second portion, and an intermediate portion, wherein the inner edges (226, 216) of the lateral and medial condyles (220, 210) define an intercondylar notch and lateral and medial extents of the intercondylar notch such that an intercondylar width extends between the inner edges (226, 216) of the lateral and medial condyles (220, 210), wherein the inner edge of the lateral condyle tapers toward the outer edge of the lateral condyle at the intermediate portion such that the width of the intercondylar notch is greater along the second portion of the inner edge of the lateral condyle than along the first portion of the lateral condyle,
A compound of formula wherein R 1 is phenyl, optionally substituted by one or two substituents, selected from 3 H, halogen, C 1-7 -alkyl, di-methyl-amino, NHC - C 1-7 -alkyl, C O-C 1-7 -alkyl, C 1-7 - alkoxy, OC( 3 H) 3, O 11 CH 3, OCH 2 CH 2 18 F, C 1-7 -alkoxy substituted by halogen, hydroxy, C 1-7 -alkyl substituted by hydroxy, S-C 1-7 -alkyl, or by a heterocyclyl group, selected from morpholinyl, piperazinyl, piperidinyl or pyrrolidinyl; or is benzo[d][1,3]dioxol-5-yl, 2,3-dihydrobenzo[b][1,4]dioxin-6-yl, indolin-2-one, or is heteroaryl, selected from the group consisting of thiophenyl, benzofuranyl, benzothiophenyl, pyrazinyl, or benzothiazolyl; R 2 is hydrogen, C 1-7 -alkyl or C 1-7 -alkyl substituted by halogen; R 3 is C 1-7 -alkyl, C( 3 H) 3, 11 CH 3, C 1-7 -alkyl substituted by halogen, -(CH 2) 2 -O-C 1-7 -alkyl substituted by halogen or C 3-6 -cycloalkyl; or R 2 and R 3 form together with the N-atom to which they are attach a ring containing -CH 2 CH 2 CHRCH 2 CH 2 -, -CH 2 CH 2 CH 2 CH 2 -, -CH 2 CH 2 CH 2 -, -CH 2 CH 2 -NR-CH 2 CH 2 -, -CH 2 CH 2 -O-CH 2 CH 2 -, -CH 2 CH 2 CHRCH 2 -, -CH 2 CHRCH 2 - or R is hydrogen, halogen, C 1-7 -alkyl substituted by halogen or C 1-7 -alkoxy; or a pharmaceutically acceptable acid addition salt, a racemic mixture or its corresponding enantiomer and/or optical isomers thereof. R 1 is phenyl, optionally substituted by one or two substituents, selected from 3 H, halogen, C 1-7 -alkyl, di-methyl-amino, NHC - C 1-7 -alkyl, C O-C 1-7 -alkyl, C 1-7 - alkoxy, OC( 3 H) 3, O 11 CH 3, OCH 2 CH 2 18 F, C 1-7 -alkoxy substituted by halogen, hydroxy, C 1-7 -alkyl substituted by hydroxy, S-C 1-7 -alkyl, or by a heterocyclyl group, selected from morpholinyl, piperazinyl, piperidinyl or pyrrolidinyl; or is benzo[d][1,3]dioxol-5-yl, 2,3-dihydrobenzo[b][1,4]dioxin-6-yl, indolin-2-one, or is heteroaryl, selected from the group consisting of thiophenyl, benzofuranyl, benzothiophenyl, pyrazinyl, or benzothiazolyl; R 2 is hydrogen, C 1-7 -alkyl or C 1-7 -alkyl substituted by halogen; R 3 is C 1-7 -alkyl, C( 3 H) 3, 11 CH 3, C 1-7 -alkyl substituted by halogen, -(CH 2) 2 -O-C 1-7 -alkyl substituted by halogen or C 3-6 -cycloalkyl; or R 2 and R 3 form together with the N-atom to which they are attach a ring containing -CH 2 CH 2 CHRCH 2 CH 2 -, -CH 2 CH 2 CH 2 CH 2 -, -CH 2 CH 2 CH 2 -, -CH 2 CH 2 -NR-CH 2 CH 2 -, -CH 2 CH 2 -O-CH 2 CH 2 -, -CH 2 CH 2 CHRCH 2 -, -CH 2 CHRCH 2 - or R is hydrogen, halogen, C 1-7 -alkyl substituted by halogen or C 1-7 -alkoxy;
A composition comprising a long-acting, IL-2Rβ-selective agonist compound comprised of IL-2 covalently attached to a poly(ethylene glycol) or pharmaceutically acceptable salts thereof for use in a method of treating a patient suffering from a cancer, wherein the method comprises the steps of: (a) administering to the patient an IL-2Rβ-activating amount of the composition comprising a long-acting, IL-2Rβ-selective agonist compound; and (b) administering an IL-15 receptor-activating amount of a long-acting IL-15 agonist comprised of IL-15 covalently attached to a poly(ethylene glycol), or pharmaceutically acceptable salts thereof.
Device of the exoskeleton type comprising two legs (2, 3) arranged to be coupled to the feet of a user, a connecting member between the upper ends of the legs to which it is hinged and a tool-holder arm connected to the connecting member, characterised in that the legs and the connecting member are arranged to form substantially a triangle of which an apex belongs to the connecting member, so that all forces applied to the device converge at the apex of said triangle.