mhurhangee/ep-ind-claims huggingface dataset:
A method for producing a grease composition comprising a base oil and a multiple thickener system which comprises a non-polar thickener component and a polar thickener component, which method involves the steps of: - preparing a first mixture which comprises a polar thickener and a base oil, which polar thickener is a metal based soap or a metal based complex soap, and wherein the polar thickener is present in an amount in the range of from 1-25% by weight and the base oil is present in an amount in the range of from 74-99% by weight, based on the total amount of the first mixture; - preparing at a temperature in the range of from 90-250°C a second mixture which comprises a non-polar thickener and a base oil, which non-polar thickener comprises a high molecular weight component comprising a (co- or homo-) polymer of propylene with a weight average molecular weight equal to or larger than 200,000 and a low molecular weight component comprising a (co- or homo-) polymer of propylene with a weight average molecular weight equal to or smaller than 100,000, and wherein the non-polar thickener is present in an amount in the range of from 1-25% by weight and the base oil is present in an amount in the range of from 74-99% by weight, based on the total amount of the second mixture; - preparing a third mixture which comprises the first mixture or the polar thickener which has been separated from the first mixture and the second mixture; - cooling at least the second mixture to room temperature by means of a rapid cooling process which is performed in less than 30 seconds; and - subjecting the third mixture to a mechanical shearing treatment. - preparing a first mixture which comprises a polar thickener and a base oil, which polar thickener is a metal based soap or a metal based complex soap, and wherein the polar thickener is present in an amount in the range of from 1-25% by weight and the base oil is present in an amount in the range of from 74-99% by weight, based on the total amount of the first mixture; - preparing at a temperature in the range of from 90-250°C a second mixture which comprises a non-polar thickener and a base oil, which non-polar thickener comprises a high molecular weight component comprising a (co- or homo-) polymer of propylene with a weight average molecular weight equal to or larger than 200,000 and a low molecular weight component comprising a (co- or homo-) polymer of propylene with a weight average molecular weight equal to or smaller than 100,000, and wherein the non-polar thickener is present in an amount in the range of from 1-25% by weight and the base oil is present in an amount in the range of from 74-99% by weight, based on the total amount of the second mixture; - preparing a third mixture which comprises the first mixture or the polar thickener which has been separated from the first mixture and the second mixture; - cooling at least the second mixture to room temperature by means of a rapid cooling process which is performed in less than 30 seconds; and - subjecting the third mixture to a mechanical shearing treatment.
Gas turbine comprising a wet compression device, by means of which an aqueous liquid mixture, which contains at least one surfactant, in droplet form can be introduced into a compressor of the gas turbine during the operation of the gas turbine, wherein the aqueous liquid mixture additionally contains at least a defoaming agent characterized in that the gas turbine has a first metering device, which is designed to feed a predetermined quantity of surfactant into water which is provided for use in the wet compression device, and in that the gas turbine has a second metering device, which is designed to feed a predetermined quantity of defoaming agent into water which is provided for use in the wet compression device.
A steel, for marine applications, consisting of by weight percent: Carbon: 0.05 to 0.20; Silicon: 0.15 to 0.55; Manganese: 0.60 to 1.60; Chromium: 0.75 to 1.50; Aluminum: 0.40 to 0.80; Niobium and/or vanadium: 0.01 ≤ [Nb] + ≤ 0.60; Sulphur: up to 0.045; Phosphor: up to 0.045; Optionally: up to 0.15 wt.% molybdenum, preferably up to 0.10 wt.%, and/or up to 0.05 wt.% titanium; Balance iron and incidental and/or residual impurities. Carbon: 0.05 to 0.20; Silicon: 0.15 to 0.55; Manganese: 0.60 to 1.60; Chromium: 0.75 to 1.50; Aluminum: 0.40 to 0.80; Niobium and/or vanadium: 0.01 ≤ [Nb] + ≤ 0.60; Sulphur: up to 0.045; Phosphor: up to 0.045; Optionally: up to 0.15 wt.% molybdenum, preferably up to 0.10 wt.%, and/or up to 0.05 wt.% titanium; Balance iron and incidental and/or residual impurities.
A non-azeotropic refrigerant mixture comprising a high-boiling-point refrigerant gas and a low-boiling-point refrigerant gas wherein the high-boiling-point refrigerant gas is butane; and the low-boiling-point refrigerant gas is ethane and R-14; characterized in that the butane/ethane gas ratio is in the range from 90/10 to 60/40; and the content of R-14 in the non-azeotropic refrigerant mixture is more than 0% and not more than 9%; or the high-boiling-point refrigerant gas is butane and the low-boiling-point refrigerant gas is ethylene and R-14; characterized in that the butane/ethylene ratio is in the range from 90/10 to 70/30; and the content of R-14 in the non-azeotropic refrigerant mixture is more than 0% and not more than 7.5%; or the high-boiling-point refrigerant gas is isobutane and the low-boiling-point refrigerant gas is ethylene and R-14; characterized in that the isobutane/ethylene ratio is in the range from 90/10 to 80/20; and the content of R-14 in the non-azeotropic refrigerant mixture is more than 0% and not more than 10%. the high-boiling-point refrigerant gas is butane; and the low-boiling-point refrigerant gas is ethane and R-14; characterized in that the butane/ethane gas ratio is in the range from 90/10 to 60/40; and the content of R-14 in the non-azeotropic refrigerant mixture is more than 0% and not more than 9%; or the high-boiling-point refrigerant gas is butane and the low-boiling-point refrigerant gas is ethylene and R-14; characterized in that the butane/ethylene ratio is in the range from 90/10 to 70/30; and the content of R-14 in the non-azeotropic refrigerant mixture is more than 0% and not more than 7.5%; or the high-boiling-point refrigerant gas is isobutane and the low-boiling-point refrigerant gas is ethylene and R-14; characterized in that the isobutane/ethylene ratio is in the range from 90/10 to 80/20; and the content of R-14 in the non-azeotropic refrigerant mixture is more than 0% and not more than 10%. the isobutane/ethylene ratio is in the range from 90/10 to 80/20; and the content of R-14 in the non-azeotropic refrigerant mixture is more than 0% and not more than 10%.
A method for heat treatment of powdery products, in particular of powders, characterized in that said products are heated by the flow of said products in a passage tube for current, positioned tilted with respect to a horizontal plane, and preferably substantially vertically with respect to this plane, said products flowing into said tube essentially by gravity, and wherein said products are heated in said tube by heating the walls of the tube by the Joule effect, said tube being connected and directly powered by an electric power supply device with which the walls of said tube may be heated by the Joule effect.
A method of controlling a host device, comprising: receiving a request from a CICAM connected to the host device, using the CI+ protocol, to run a CICAM application on the host device requiring a message to be displayed to a user; checking whether the host device is capable of servicing the request to run the CICAM application; and in the event that the host device is not capable of servicing the request to run the CICAM application, providing the CICAM application to a second, different, device to run thereon, wherein the providing step further comprises: accessing a local area network; establishing the presence of at least one second device located on the local area network; and providing the CICAM application to one of said second devices located on the local area network over a Low Speed Communication LSC session to run thereon. receiving a request from a CICAM connected to the host device, using the CI+ protocol, to run a CICAM application on the host device requiring a message to be displayed to a user; checking whether the host device is capable of servicing the request to run the CICAM application; and in the event that the host device is not capable of servicing the request to run the CICAM application, providing the CICAM application to a second, different, device to run thereon, wherein the providing step further comprises: accessing a local area network; establishing the presence of at least one second device located on the local area network; and providing the CICAM application to one of said second devices located on the local area network over a Low Speed Communication LSC session to run thereon. accessing a local area network; establishing the presence of at least one second device located on the local area network; and providing the CICAM application to one of said second devices located on the local area network over a Low Speed Communication LSC session to run thereon.
An engine crank pulley structure to be disposed at a vehicle front side of a longitudinally mounted engine, the structure comprising: a front pulley that is configured to transmit crank rotational force to a first accessory via a belt; a rear pulley that is disposed at a vehicle rear side of the front pulley and configured to transmit crank rotational force to a second accessory via a belt; and a connecting portion that is configured to connect the front pulley and the rear pulley, wherein the connecting portion is configured to crush and deform in a vehicle front-rear direction as a collision load toward the vehicle rear side is applied to the connecting portion, and an outer diameter of the front pulley is smaller than an inner diameter of the rear pulley, characterized in that the engine crank pulley structure further comprises an inertia ring between the front pulley and the rear pulley, and an inner diameter of the inertia ring is larger than an outer diameter of the rear pulley. a front pulley that is configured to transmit crank rotational force to a first accessory via a belt; a rear pulley that is disposed at a vehicle rear side of the front pulley and configured to transmit crank rotational force to a second accessory via a belt; and a connecting portion that is configured to connect the front pulley and the rear pulley, wherein the connecting portion is configured to crush and deform in a vehicle front-rear direction as a collision load toward the vehicle rear side is applied to the connecting portion, and an outer diameter of the front pulley is smaller than an inner diameter of the rear pulley, characterized in that the engine crank pulley structure further comprises an inertia ring between the front pulley and the rear pulley, and an inner diameter of the inertia ring is larger than an outer diameter of the rear pulley.
An aqueous polyurethane resin dispersion, the polyurethane resin having a polyalkylene oxide in a side chain thereof is obtainable by reacting a polyester polyol, a polyether diol, a polyol containing a quaternary N-atom or tertiary amino group and a polyisocyanate, and wherein the polyester polyol is obtained by reacting an aromatic polycarboxylic acid and a polyol.
Entrained-flow gasifier for the gasification of fuels in dust or liquid form using a free oxygen-containing gasifying agent at pressures between atmospheric pressure and 8 MPa and at gasification temperatures between 1200 and 1900°C, in which gasifier - a reaction chamber is connected to a quenching chamber arranged therebelow via a guide pipe in a pressure shell, - the reaction chamber is delimited by a cooling screen, - a gasification burner which can be arranged at the upper end of the reaction chamber, - the cooling screen gap between the cooling screen and pressure shell is flushed with an inert gas, - the cooling screen is configured by the winding of a number of cooling screen tubes through which a cooling liquid flows, - the cooling screen has a tapering conical cooling screen portion at the upper end, a tapering conical cooling screen portion at the lower end and a central cylindrical cooling screen portion therebetween, characterized in that the cooling screen tubes are configured as a thick-walled cooling screen tube in the region of the lower and the upper cooling screen portion and as a thin-walled cooling screen tube in the region of the central cooling screen portion. - a reaction chamber is connected to a quenching chamber arranged therebelow via a guide pipe in a pressure shell, - the reaction chamber is delimited by a cooling screen, - a gasification burner which can be arranged at the upper end of the reaction chamber, - the cooling screen gap between the cooling screen and pressure shell is flushed with an inert gas, - the cooling screen is configured by the winding of a number of cooling screen tubes through which a cooling liquid flows, - the cooling screen has a tapering conical cooling screen portion at the upper end, a tapering conical cooling screen portion at the lower end and a central cylindrical cooling screen portion therebetween,
Lattice boom crane with: - an undercarriage, - an upper carriage which is arranged to rotate on the undercarriage, - a lattice boom jib which is arranged on the upper carriage, - at least one bracing support (6, 7, 8) projecting laterally out from and disposable on the lattice boom jib, - an upper bracing means is provided which connects the bracing support (6, 7, 8) to a lattice boom jib part located in the area of the head end of the lattice boom jib and has at least one rigid, rod-shaped bracing element or a cable, and - a lower bracing means is provided which connects the bracing support (6, 7, 8) to a lattice boom jib part located in the area of the foot end of the lattice boom jib or to a component of the super structure and has at least one rigid, rod-shaped bracing element or a cable, characterised in that the bracing support (6, 7, 8; 6, 8) is attached parallel to a longitudinal axis of the lattice boom jib so that it can slide. - an undercarriage, - an upper carriage which is arranged to rotate on the undercarriage, - a lattice boom jib which is arranged on the upper carriage, - at least one bracing support (6, 7, 8) projecting laterally out from and disposable on the lattice boom jib, - an upper bracing means is provided which connects the bracing support (6, 7, 8) to a lattice boom jib part located in the area of the head end of the lattice boom jib and has at least one rigid, rod-shaped bracing element or a cable, and - a lower bracing means is provided which connects the bracing support (6, 7, 8) to a lattice boom jib part located in the area of the foot end of the lattice boom jib or to a component of the super structure and has at least one rigid, rod-shaped bracing element or a cable,
A use of a filter for filtering fluids, said filter comprising: a. nano alumina fibres; b. a plurality of second fibres comprised of a combination of a plurality of coarse and a plurality of fine fibers and mixed with said nano alumina fibres, said second fibres arranged to create asymmetrical pores; and c. a plurality of particles disposed on said nano alumina fibers, wherein the plurality of particles have an average particle size of below 0.1 μm. a. nano alumina fibres; b. a plurality of second fibres comprised of a combination of a plurality of coarse and a plurality of fine fibers and mixed with said nano alumina fibres, said second fibres arranged to create asymmetrical pores; and c. a plurality of particles disposed on said nano alumina fibers, wherein the plurality of particles have an average particle size of below 0.1 μm.
Combination - of a drive unit having - an electric motor which has - a stator and - a rotor comprising the output shaft, and - a transmission gear mechanism, - which is connected to an output shaft of the electric motor in a rotationally driving manner, - which comprises a planetary gear mechanism, and - which is arranged within the output shaft, which is designed as a hollow shaft, of the electric motor, characterized in that the combination comprises a tool unit which comprises a static part and a rotatable part, wherein the rotatable part is a tool or is connected to such a tool in a rotationally driving manner, and the static part is a tool housing which serves for rotatably mounting the tool, wherein a ring gear of the planetary gear mechanism of the drive unit is connected to the tool housing of the tool unit in a rotationally fixed manner. - of a drive unit having - an electric motor which has - a stator and - a rotor comprising the output shaft, and - a transmission gear mechanism, - which is connected to an output shaft of the electric motor in a rotationally driving manner, - which comprises a planetary gear mechanism, and - which is arranged within the output shaft, which is designed as a hollow shaft, of the electric motor, - an electric motor which has - a stator and - a rotor comprising the output shaft, and - a stator and - a rotor comprising the output shaft, and - a transmission gear mechanism, - which is connected to an output shaft of the electric motor in a rotationally driving manner, - which comprises a planetary gear mechanism, and - which is arranged within the output shaft, which is designed as a hollow shaft, of the electric motor, - which is connected to an output shaft of the electric motor in a rotationally driving manner, - which comprises a planetary gear mechanism, and - which is arranged within the output shaft, which is designed as a hollow shaft, of the electric motor,
A turbine rotor, comprising: a rotor body portion having turbine discs projecting radially outside over a circumferential direction in plural stages in a center axis direction of the turbine rotor; a plurality of axial passages, through which a cooling medium flows, formed at the rotor body portion radially outside than a center axis of the turbine rotor and radially inside than an outer peripheral surface of the rotor body portion in the center axis direction of the turbine rotor; an introduction passage introducing the cooling medium into each of the axial passages; and discharge passages that penetrate from each of the axial passages to the outer peripheral surface of the rotor body portion to discharge the cooling medium, characterized in that the turbine rotor is an integral-type forged product or a rotor formed by welding a plurality of turbine rotor components in the center axis direction. a rotor body portion having turbine discs projecting radially outside over a circumferential direction in plural stages in a center axis direction of the turbine rotor; a plurality of axial passages, through which a cooling medium flows, formed at the rotor body portion radially outside than a center axis of the turbine rotor and radially inside than an outer peripheral surface of the rotor body portion in the center axis direction of the turbine rotor; an introduction passage introducing the cooling medium into each of the axial passages; and discharge passages that penetrate from each of the axial passages to the outer peripheral surface of the rotor body portion to discharge the cooling medium, characterized in that the turbine rotor is an integral-type forged product or a rotor formed by welding a plurality of turbine rotor components in the center axis direction.
Exhaust gas liner for a gas turbine comprising an annular inner shell and an annular outer shell, which are arranged concentrically around a machine axis of said gas turbine and connected by means of a plurality of radial struts to define an annular exhaust gas channel in between, whereby said inner shell and/or said outer shell are composed of a plurality of liner segments (22, 23; 26, 27; 28), which are attached to a support structure (31, 38), said liner segments (22, 23; 26, 27; 28) are fixed to said support structure (31, 38) at fixation spots (29a-c; 30a-c), which are distributed over the area of said liner segments, such that said liner segments are clamped to that support structure through a whole engine thermal cycle without hindering thermal expansion, characterized in that all liner segments (22, 23; 26, 27; 28) comprise a central fixation spot (29b, 30b) for preventing movement in axial, radial and tangential direction, side fixation spots (29a, 30a) for preventing movement in radial direction but allowing thermal expansion in a combined axial and tangential direction, and an axially guiding fixation spot (29c, 30c) located on an axial centreline of said segments for preventing movement in tangential direction; wherein said liner segments (22, 23; 26, 27; 28) are fixed at said central fixation spot (29b, 30b) by means of a fixation bolt, which is screwed through a holder at the backside of said liner segments (22, 23; 26, 27; 28) into a fixation pin being fixed on said support structure (31, 38); said liner segments (22, 23; 26, 27; 28) are fixed at said side fixation spots (29a, 30a) by means of a fixation bolt, which is screwed through a holder at the backside facing the support structure (31, 38) of said liner segments (22, 23; 26, 27; 28) into a fixation pin being fixed on said support structure (31, 38), whereby said holder comprises an elongated hole orientated in the axial and tangential directions; said liner segments (22, 23; 26, 27; 28) are fixed at said axially guiding fixation spot (29c, 30c) by means of an axial guide pin, which is fixed to a holder at the backside of said liner segments (22, 23; 26, 27; 28) and engages in sliding radial and axial directions a fixation pin being fixed on said support structure (31, 38).
A method comprising: receiving a session setup request at a network entity (70, 31) via a network apparatus connected to the network entity (70, 31), wherein the session setup request originates from or is directed to a user device part of a closed subscriber group of an apparatus; and performing an enabling handshaking between the network entity (70, 31) and the apparatus if the apparatus is located in the coverage area of the network apparatus, wherein transmitting means and receiving means of said apparatus are enabled after successful completion of said enabling handshaking. receiving a session setup request at a network entity (70, 31) via a network apparatus connected to the network entity (70, 31), wherein the session setup request originates from or is directed to a user device part of a closed subscriber group of an apparatus; and performing an enabling handshaking between the network entity (70, 31) and the apparatus if the apparatus is located in the coverage area of the network apparatus, wherein transmitting means and receiving means of said apparatus are enabled after successful completion of said enabling handshaking.
A method of forming a wall (121, 122, 123, 124) of a floating caisson (100, 200, 300) comprising: providing a slab on a submersible platform; providing one or more base supports (130, 131) on top of the slab, the base supports (130, 131) having a first outer face and a second outer face; forming a first wall portion by spraying concrete on the first and the second outer faces; lowering the platform below a water level; and forming one or more subsequent wall portions on the first wall portion. providing a slab on a submersible platform; providing one or more base supports (130, 131) on top of the slab, the base supports (130, 131) having a first outer face and a second outer face; forming a first wall portion by spraying concrete on the first and the second outer faces; lowering the platform below a water level; and forming one or more subsequent wall portions on the first wall portion.