mhurhangee/ep-ind-claims huggingface dataset:
A rotor device for a gas hob control arrangement, comprising: a collar, that forms an opening and is configured to transfer a rotating and/or translating movement between the rotor device and a shaft device receivable in the opening, a ring body, that has a larger inner diameter than a width of the opening, and at least one arm comprising: an outer arm section, which extends radially inwards from the ring body, an inner arm section, which extends radially outwards from the collar, and a central arm section, which extends axially from a radially inner end of the outer arm section to a radially outer end of the inner arm section. a collar, that forms an opening and is configured to transfer a rotating and/or translating movement between the rotor device and a shaft device receivable in the opening, a ring body, that has a larger inner diameter than a width of the opening, and at least one arm comprising: an outer arm section, which extends radially inwards from the ring body, an inner arm section, which extends radially outwards from the collar, and a central arm section, which extends axially from a radially inner end of the outer arm section to a radially outer end of the inner arm section. an outer arm section, which extends radially inwards from the ring body, an inner arm section, which extends radially outwards from the collar, and a central arm section, which extends axially from a radially inner end of the outer arm section to a radially outer end of the inner arm section.
A rotary compressor comprising: - a hermetically-sealed upright cylindrical compressor casing having a refrigerant gas ejection portion disposed in an upper portion and a refrigerant gas suction portion (101, 102) disposed in a lower portion; - a compression unit provided in a lower portion of the compressor casing for sucking refrigerant gas from a low pressure side of a refrigerating cycle through the suction portion (101, 102) and ejecting the refrigerant gas from the ejection portion to a high pressure side of the refrigerating cycle through the inside of the compressor casing; - a motor provided in an upper portion of the compressor casing for driving the compression unit through a rotating shaft; - a gas hole formed in a rotor of the motor for causing refrigerant gas below the motor to pass upward; and - an oil separation plate (119; 219; 319; 419; 519) having a central cylindrical portion (119B; 219B; 319B; 419B; 519B), and an outer peripheral disk portion (119A; 219A; 319A; 419A; 519A) continuous to a curved portion (119C; 219C; 319C; 419C; 519C), characterized in that the curved portion (119C; 219C; 319C; 419C; 519C) of the oil separation plate (119; 219; 319; 419; 519) is continuous to the central cylindrical portion (119B; 219B; 319B; 419B; 519B) and curved in a radial direction, and the oil separation plate (119; 219; 319; 419; 519) is fixed on the rotor by a rivet so that a lower end portion of the central cylindrical portion (119B; 219B; 319B; 419B; 519B) comes into close contact with an upper end of the rotor or an upper end plate (113B; 513B) of the rotor at its entire periphery. - a hermetically-sealed upright cylindrical compressor casing having a refrigerant gas ejection portion disposed in an upper portion and a refrigerant gas suction portion (101, 102) disposed in a lower portion; - a compression unit provided in a lower portion of the compressor casing for sucking refrigerant gas from a low pressure side of a refrigerating cycle through the suction portion (101, 102) and ejecting the refrigerant gas from the ejection portion to a high pressure side of the refrigerating cycle through the inside of the compressor casing; - a motor provided in an upper portion of the compressor casing for driving the compression unit through a rotating shaft; - a gas hole formed in a rotor of the motor for causing refrigerant gas below the motor to pass upward; and - an oil separation plate (119; 219; 319; 419; 519) having a central cylindrical portion (119B; 219B; 319B; 419B; 519B), and an outer peripheral disk portion (119A; 219A; 319A; 419A; 519A) continuous to a curved portion (119C; 219C; 319C; 419C; 519C),
A gas turbine engine comprising: a plurality of rotatable components housed within a compressor section (24; 102) and a turbine section; a tap connected to a location upstream of a downstream most location in said compressor section, said tap connected to a heat exchanger, downstream of the heat exchanger is a shut off valve and downstream of said shut off valve is a cooling compressor, said cooling compressor being connected to deliver cooling air through a chamber (133; 144), and then to at least one of said plurality of rotatable components, and said chamber (133; 144) being provided with at least one check valve (134; 146) configured to selectively allow flow directly from a more downstream location in said compressor section than the location upstream, wherein said flow from said more downstream location has a higher pressure than a flow from the location upstream; a system for stopping operation of said cooling compressor; and a control for closing said shut off valve; wherein said cooling compressor is configured to compress air to a greater pressure than said higher pressure, such that when said cooling compressor is providing air, said at least one check valve (134; 146) is configured to maintain a closed position, but when said cooling compressor is not providing compressed air, said at least one check valve (134; 146) is configured to allow said higher pressure flow into said chamber (133; 144). a plurality of rotatable components housed within a compressor section (24; 102) and a turbine section; a tap connected to a location upstream of a downstream most location in said compressor section, said tap connected to a heat exchanger, downstream of the heat exchanger is a shut off valve and downstream of said shut off valve is a cooling compressor, said cooling compressor being connected to deliver cooling air through a chamber (133; 144), and then to at least one of said plurality of rotatable components, and said chamber (133; 144) being provided with at least one check valve (134; 146) configured to selectively allow flow directly from a more downstream location in said compressor section than the location upstream, wherein said flow from said more downstream location has a higher pressure than a flow from the location upstream; a system for stopping operation of said cooling compressor; and a control for closing said shut off valve; wherein said cooling compressor is configured to compress air to a greater pressure than said higher pressure, such that when said cooling compressor is providing air, said at least one check valve (134; 146) is configured to maintain a closed position, but when said cooling compressor is not providing compressed air, said at least one check valve (134; 146) is configured to allow said higher pressure flow into said chamber (133; 144).
An airfoil comprising: an airfoil body including: a leading edge and a trailing edge with an exterior surface therebetween, wherein the exterior surface includes a suction side, a pressure side and a recessed portion on the pressure side of the airfoil adjacent to the trailing edge, characterized in that: the pressure side further includes a flat non-recessed surface and a flat recessed surface with a continuously curved "S" shaped transition surface therebetween, wherein the trailing edge is an arcuate surface connecting between the suction side and the flat recessed surface of the pressure side, wherein both of the flat surfaces are proximate to the trailing edge, and wherein the flat recessed surface is part of the recessed portion; whereby the flat recessed surface is tangent to the arcuate surface of the trailing edge and is at an angle (α) with respect to the flat non-recessed surface. an airfoil body including: a leading edge and a trailing edge with an exterior surface therebetween, wherein the exterior surface includes a suction side, a pressure side and a recessed portion on the pressure side of the airfoil adjacent to the trailing edge, characterized in that: the pressure side further includes a flat non-recessed surface and a flat recessed surface with a continuously curved "S" shaped transition surface therebetween, wherein the trailing edge is an arcuate surface connecting between the suction side and the flat recessed surface of the pressure side, wherein both of the flat surfaces are proximate to the trailing edge, and wherein the flat recessed surface is part of the recessed portion; whereby the flat recessed surface is tangent to the arcuate surface of the trailing edge and is at an angle (α) with respect to the flat non-recessed surface. the pressure side further includes a flat non-recessed surface and a flat recessed surface with a continuously curved "S" shaped transition surface therebetween, wherein the trailing edge is an arcuate surface connecting between the suction side and the flat recessed surface of the pressure side, wherein both of the flat surfaces are proximate to the trailing edge, and wherein the flat recessed surface is part of the recessed portion; whereby the flat recessed surface is tangent to the arcuate surface of the trailing edge and is at an angle (α) with respect to the flat non-recessed surface.
A gas pressure welding process comprising: mixing a hydrocarbon gas and oxygen gas to form a a hydrocarbon-and-oxygen gas mixture, wherein the oxygen gas is supplied from an oxygen supply tank to a burner unit, and wherein the hydrocarbon gas is supplied from a gas supply tank to the burner unit; and igniting, by the burner unit, the hydrocarbon-and-oxygen mixture as a fuel source for a gas pressure welding apparatus to weld two parts (177,187) together, characterized in that the hydrocarbon gas is a propylene gas and in that a ratio of oxygen gas to propylene gas in the propylene-and-oxygen gas mixture is between about 2 and 3; and in that the total flow rate of oxygen-and-propylene mixture is between 650 and 850 standard cubic feet per hour (SCFH) (5.11x10 -3 and 6.33 x 10 -3 m 3 /s). mixing a hydrocarbon gas and oxygen gas to form a a hydrocarbon-and-oxygen gas mixture, wherein the oxygen gas is supplied from an oxygen supply tank to a burner unit, and wherein the hydrocarbon gas is supplied from a gas supply tank to the burner unit; and igniting, by the burner unit, the hydrocarbon-and-oxygen mixture as a fuel source for a gas pressure welding apparatus to weld two parts (177,187) together, characterized in that the hydrocarbon gas is a propylene gas and in that a ratio of oxygen gas to propylene gas in the propylene-and-oxygen gas mixture is between about 2 and 3; and in that the total flow rate of oxygen-and-propylene mixture is between 650 and 850 standard cubic feet per hour (SCFH) (5.11x10 -3 and 6.33 x 10 -3 m 3 /s).
A method for conducting a marine seismic survey using at least two marine seismic vibrators and a plurality of seismic receivers, the method comprising: activating a first marine seismic vibrator to produce a first time sequence of shots each corresponding to a sweep of seismic frequencies; activating a second marine seismic vibrator to produce a second time sequence of shots each corresponding to a sweep of seismic frequencies, the shots of the second time sequence being fired simultaneously with the shots of the first time sequence, wherein each of the second sequence of shots is phase shifted relative to the simultaneously fired shot of the first sequence of shots, wherein the phase in the first sequence of shots does not vary from shot to shot, and wherein the phase of the second sequence of shots is the same for all frequencies in each sweep and is randomly varied over the range 0-2π from shot to shot; recording earth responses with the plurality of seismic receivers; and using the earth responses to determine properties of a subterranean section of the earth. activating a first marine seismic vibrator to produce a first time sequence of shots each corresponding to a sweep of seismic frequencies; activating a second marine seismic vibrator to produce a second time sequence of shots each corresponding to a sweep of seismic frequencies, the shots of the second time sequence being fired simultaneously with the shots of the first time sequence, wherein each of the second sequence of shots is phase shifted relative to the simultaneously fired shot of the first sequence of shots, wherein the phase in the first sequence of shots does not vary from shot to shot, and wherein the phase of the second sequence of shots is the same for all frequencies in each sweep and is randomly varied over the range 0-2π from shot to shot; recording earth responses with the plurality of seismic receivers; and using the earth responses to determine properties of a subterranean section of the earth.
An arrangement comprising a valve for use in the supply or return of a water circuit for heating or cooling, comprising a housing (1, 16) forming a supply line and a discharge line, and an adjustment unit formed separately from the housing (1, 16) and penetrating the housing (1, 16) from the outside for adjusting a flow rate through the valve from the supply line to the discharge line, wherein the adjustment unit comprises a base body with which it is screwed into a receiving opening of the valve housing, and a valve tappet, a valve closing body (4, 4a) and a valve seat body, wherein the valve seat body is stationary with respect to the base body and wherein the valve tappet is mounted in the base body in an axially displaceable manner relative to the base body and is operatively connected to the valve closing body (4, 4a) in such a way that the valve closing body (4a, 4a) together with the valve seat body forms a valve gap which can be adjusted by axial displacement of the valve tappet, wherein the valve is designed in such a way that the valve gap is closed during intended operation with the valve tappet not actuated as a result of closing forces generated hydraulically, pneumatically and/or mechanically, and when the valve tappet is actuated to open the valve gap these closing forces need to be overcome, and wherein the arrangement further comprises an actuator by means of which, during the intended operation, the valve tappet can be displaced against the closing forces in order to open the valve gap, in particular in several steps or continuously, characterised in that the actuator comprises a pneumatically, hydraulically or electrically controllable or actuatable, respectively, drive element for providing the actuating forces for axially displacing the valve tappet in order to open the valve gap, wherein the drive element is arranged in axial extension of the valve tappet in the closing movement direction of the valve tappet, and in particular wherein the drive element can act directly on the end of the valve tappet pointing in the closing movement direction, for displacing the valve tappet against the closing movement direction and wherein the drive element is accommodated in the adjustment unit by means of a support structure designed in particular as a push button, and wherein this support structure is mounted in the adjustment unit so as to be axially displaceable along the axis of displacement of the valve tappet, in such a way that, when the valve gap is closed, it can be displaced from a basic position by manual pressure actuation from the outside together with the drive element accommodated therein in the opposite direction to the closing movement direction of the valve tappet, with a simultaneous displacement of the valve tappet in this direction over at least a part of the displacement path and a resulting opening of the valve gap resulting therefrom.
Containment enclosure comprising a wall made of a concrete material that delimits a space and at least one viewing module, said viewing module comprising at least one window arranged in an opening in the wall, said window having a frame in which at least one optical unit that provides protection from high-energy and/or neutron radiation is placed, said frame being fitted in the opening, the viewing module also having a protective element that comprises a sash bearing a pane and is arranged so as to close the opening at the level of the inside face of the enclosure, said viewing module therefore comprising at least one interface between two surfaces, characterized in that it further comprises at least one sealing system arranged at the level of at least one interface, said sealing system comprising at least one hermetic chamber on the periphery of the interface, said chamber being filled with a neutral gas, and in that said sealing system comprises a pressure measurement device for measuring pressure in the chamber and a gas injection device allowing an amount of neutral gas to be injected into the chamber depending on a value provided by the pressure measurement device.
Cooktop with a sensor device arranged therein for non-contact detection of a wall temperature of a cooking vessel radiating heat energy placed on the cooktop, which sensor device is able to be moved from a retracted rest position within the cooktop into an operating position projecting above the level of the cooktop, characterised in that display and/or control elements (23, 24) for the actuation or monitoring of the sensor device are part of the sensor device.
A process for preparing hydrogenated catmint oil comprising: (a) distilling crude catmint oil to produce (i) a distillate fraction comprising volatile components driven off from the beginning amount of crude catmint oil, and (ii) a pot fraction; and (b) contacting the pot fraction of step (a) with hydrogen and a hydrogenation catalyst to produce hydrogenated catmint oil; wherein the distillation of step (a) comprises steam distillation followed by solvent distillation. (a) distilling crude catmint oil to produce (i) a distillate fraction comprising volatile components driven off from the beginning amount of crude catmint oil, and (ii) a pot fraction; and (b) contacting the pot fraction of step (a) with hydrogen and a hydrogenation catalyst to produce hydrogenated catmint oil;
An automated method of control and evaluation of the operation of a lift installation, characterised in that the method comprises the steps of • Weighing of a load of at least one weight by means of a weighing machine; • Transmission via radio signals from a data emitter having a battery power supply, included in the weighing machine, of the load detected on site in the lift installation before introducing it to the lift cabin, to a portable control console; • Inserting the detected load in the lift cabin and weighing by means of a load weighing device; • Transmitting wirelessly to the portable control console, via a data emitter-receiver included in the load weighing device of data associated with the parameters measured by the load weighing device; • Supplying from the portable control console command signals converted from the data received from the load weighing device and the load weighing machine;and • Receiving via the data emitter-receiver, included in the load weighing device, of the command signals for correcting the operating parameters of the lift cabin. • Weighing of a load of at least one weight by means of a weighing machine; • Transmission via radio signals from a data emitter having a battery power supply, included in the weighing machine, of the load detected on site in the lift installation before introducing it to the lift cabin, to a portable control console; • Inserting the detected load in the lift cabin and weighing by means of a load weighing device; • Transmitting wirelessly to the portable control console, via a data emitter-receiver included in the load weighing device of data associated with the parameters measured by the load weighing device; • Supplying from the portable control console command signals converted from the data received from the load weighing device and the load weighing machine;and • Receiving via the data emitter-receiver, included in the load weighing device, of the command signals for correcting the operating parameters of the lift cabin.
A method for determining the amount of estradiol in a plasma or serum sample by tandem mass spectrometry in positive ion mode said method comprising: (a) acidifying the sample prior to purification with liquid chromatography with an agent in an amount sufficient to free estradiol from a protein that may be present in the sample; (b) purifying estradiol from said plasma or serum sample by liquid chromatography; (c) generating a precursor ion of said estradiol comprising a mass-to-charge ratio of 255.07±0.5; (d) generating one or more fragment ions of said precursor ion, wherein said one or more fragment ions comprise an ion with a m/z of 133.20 ±.5 or an ion with a m/z of 159.20 ±.5; and (e) detecting the amount of one or more of said ions generated in step (b) or (c) or both and relating the detected ions to the amount of said estradiol in said body fluid sample. (a) acidifying the sample prior to purification with liquid chromatography with an agent in an amount sufficient to free estradiol from a protein that may be present in the sample; (b) purifying estradiol from said plasma or serum sample by liquid chromatography; (c) generating a precursor ion of said estradiol comprising a mass-to-charge ratio of 255.07±0.5; (d) generating one or more fragment ions of said precursor ion, wherein said one or more fragment ions comprise an ion with a m/z of 133.20 ±.5 or an ion with a m/z of 159.20 ±.5; and (e) detecting the amount of one or more of said ions generated in step (b) or (c) or both and relating the detected ions to the amount of said estradiol in said body fluid sample.
A hot-stamping foil which is transferred to a transfer target by applying a transfer thermal pressure, comprising: a carrier that is a base film or a coated base film; and a laminated optical decoration, wherein the laminated optical decoration has a laminated optical structure formed on the carrier, a sinking control layer which contains a soft resin and a deformation limiting agent and is formed on the laminated optical structure, and an adhesive layer which is formed on the sinking control layer, wherein the adhesive layer contains a resin component which contains a thermoplastic resin having a glass transition temperature lower than room temperature and defines a thickness of the adhesive layer, and spacer particles which have a particle size larger than the thickness of the adhesive layer and a portion of which protrude from the resin component, and wherein the spacer particles sink into the sinking control layer after transfer thermal pressing. a carrier that is a base film or a coated base film; and a laminated optical decoration, wherein the laminated optical decoration has a laminated optical structure formed on the carrier, a sinking control layer which contains a soft resin and a deformation limiting agent and is formed on the laminated optical structure, and an adhesive layer which is formed on the sinking control layer, a laminated optical structure formed on the carrier, a sinking control layer which contains a soft resin and a deformation limiting agent and is formed on the laminated optical structure, and an adhesive layer which is formed on the sinking control layer, wherein the adhesive layer contains a resin component which contains a thermoplastic resin having a glass transition temperature lower than room temperature and defines a thickness of the adhesive layer, and spacer particles which have a particle size larger than the thickness of the adhesive layer and a portion of which protrude from the resin component, and a resin component which contains a thermoplastic resin having a glass transition temperature lower than room temperature and defines a thickness of the adhesive layer, and spacer particles which have a particle size larger than the thickness of the adhesive layer and a portion of which protrude from the resin component, and wherein the spacer particles sink into the sinking control layer after transfer thermal pressing.