mhurhangee/ep-ind-claims huggingface dataset:
An assembly for a gas turbine engine, comprising: a wall comprising a shell, a heat shield and a cooling cavity; the heat shield including a first panel and a second panel; the first panel extending longitudinally between a first panel first end and a first panel second end, and the first panel including a first panel base and a first panel rail; the second panel extending longitudinally between a second panel first end and a second panel second end, the second panel at the second panel first end arranged between and displaced from the shell and the first panel at the first panel second end, the second panel including a second panel base and a second panel rail, and the second panel base comprising an uninterrupted surface that extends longitudinally from the second panel rail to the second panel first end, the second panel rail disposed a longitudinal first distance from the second panel first end and a longitudinal second distance from the second panel second end, wherein the cooling cavity is longitudinally bounded by the first panel rail and the second panel rail, characterized in that the longitudinal first distance is greater than the longitudinal second distance. a wall comprising a shell, a heat shield and a cooling cavity; the heat shield including a first panel and a second panel; the first panel extending longitudinally between a first panel first end and a first panel second end, and the first panel including a first panel base and a first panel rail; the second panel extending longitudinally between a second panel first end and a second panel second end, the second panel at the second panel first end arranged between and displaced from the shell and the first panel at the first panel second end, the second panel including a second panel base and a second panel rail, and the second panel base comprising an uninterrupted surface that extends longitudinally from the second panel rail to the second panel first end, the second panel rail disposed a longitudinal first distance from the second panel first end and a longitudinal second distance from the second panel second end, wherein the cooling cavity is longitudinally bounded by the first panel rail and the second panel rail, characterized in that the longitudinal first distance is greater than the longitudinal second distance.
Silica, characterized in that it has: - a CTAB specific surface area (S CTAB) of between 95 and 525 m 2 /g, - a BET specific surface area (S BET) of between 45 and 550 m 2 /g, - a pore distribution width ldp of greater than 0.70, in particular greater than 0.80, said silica being obtained by a preparation process of the type comprising the reaction of a silicate with an acidifying agent, by means of which a silica suspension is obtained, then the separation and drying of this suspension, characterized in that the reaction of the silicate with the acidifying agent is carried out according to the following successive steps: (i) an aqueous feedstock is formed, having a pH of between 2 and 5, preferably between 2.5 and 5, (ii) silicate and acidifying agent are added simultaneously to said feedstock, such that the pH of the reaction medium is kept between 2 and 5, preferably between 2.5 and 5, (iii) the addition of the acidifying agent is stopped while continuing the addition of the silicate into the reaction medium until a pH value of the reaction medium of between 7 and 10, preferably between 7.5 and 9.5, is obtained, (iv) silicate and acidifying agent are added simultaneously to the reaction medium such that the pH of the reaction medium is kept between 7 and 10, preferably between 7.5 and 9.5, (v) the addition of the silicate is stopped while continuing the addition of the acidifying agent into the reaction medium until a pH value of the reaction medium of less than 6 is obtained. - a CTAB specific surface area (S CTAB) of between 95 and 525 m 2 /g, - a BET specific surface area (S BET) of between 45 and 550 m 2 /g, - a pore distribution width ldp of greater than 0.70, in particular greater than 0.80, (i) an aqueous feedstock is formed, having a pH of between 2 and 5, preferably between 2.5 and 5, (ii) silicate and acidifying agent are added simultaneously to said feedstock, such that the pH of the reaction medium is kept between 2 and 5, preferably between 2.5 and 5, (iii) the addition of the acidifying agent is stopped while continuing the addition of the silicate into the reaction medium until a pH value of the reaction medium of between 7 and 10, preferably between 7.5 and 9.5, is obtained, (iv) silicate and acidifying agent are added simultaneously to the reaction medium such that the pH of the reaction medium is kept between 7 and 10, preferably between 7.5 and 9.5, (v) the addition of the silicate is stopped while continuing the addition of the acidifying agent into the reaction medium until a pH value of the reaction medium of less than 6 is obtained.
A mixing device for mixing a spray from an injector into a gas flowing through a substantially tubular chamber from an upstream side to a downstream side, said mixing device comprising: - a partially open wall on a side upstream of said spray; and - a closed wall on a side downstream of said spray; said closed wall and said partially open wall together forming a surface closed onto itself defining a mixing cavity, said mixing cavity comprising: - a spray inlet opening for receiving a conical spray from said injector; and - an outlet opening in a plane intersecting an axis of said injector; characterized in that a downstream side of said mixing device is shaped so as to define a helicoidal groove for circumferentially guiding said gas from said outlet opening in a downstream direction. - a partially open wall on a side upstream of said spray; and - a closed wall on a side downstream of said spray; - a spray inlet opening for receiving a conical spray from said injector; and - an outlet opening in a plane intersecting an axis of said injector;
Sensor arrangement having - a housing, - a movement sensor, wherein the movement sensor is mounted on a bearing element that is connected to the housing, - a position sensor, and - a position transducer, wherein the position sensor and the position transducer are mutually disposed in such a manner that the movement of the movement sensor is measurable, wherein the bearing element is configured so as to project from the housing, - furthermore having a housing module for receiving the position sensor or the position transducer, wherein the housing module is attachable to the housing so as to be aligned on an axis, in particular a rotation axis, of the bearing element, characterized in that the housing module is configured such that said housing module intersects the at least one rotation axis of the bearing element so close to the movement sensor that an axial removal of the movement sensor from the bearing element is prevented. - a housing, - a movement sensor, wherein the movement sensor is mounted on a bearing element that is connected to the housing, - a position sensor, and - a position transducer, wherein the position sensor and the position transducer are mutually disposed in such a manner that the movement of the movement sensor is measurable, wherein the bearing element is configured so as to project from the housing, - furthermore having a housing module for receiving the position sensor or the position transducer, wherein the housing module is attachable to the housing so as to be aligned on an axis, in particular a rotation axis, of the bearing element, characterized in that the housing module is configured such that said housing module intersects the at least one rotation axis of the bearing element so close to the movement sensor that an axial removal of the movement sensor from the bearing element is prevented.
A method to fabricate a composite product, where an intermediate product is formed from raw material including fibre containing material and polymer based material with the help of extrusion and a composite product is shaped from the intermediate product with at least one shaping tool, characterised in that the cross sectional profile of the intermediate product is shaped with at least one extrusion tool during the extrusion and the temperature of the intermediate product is controlled after the extrusion tool so that in different parts of the cross sectional profile of the intermediate product different temperature zones are arranged according to the predetermined target values of the temperature ranges and the temperature of the intermediate product is adjusted in different parts of the cross sectional profile, between 50 - 250 degrees Celsius, and the composite product is shaped from the intermediate product with the shaping tool which is based on pressing.
Measuring device for the determination of gas concentrations of several gas components of a measuring gas by means of filter correlation and/or gas filter correlation - with a light source which emits light in a wavelength range and - whose light beams are guided along a beam path through a measuring section, - with a receiving arrangement (30; 130) which receives the light of the light source after passing through the measuring section and provides receiving signals depending on the light intensity incident on the receiving arrangement (30; 130), - with an optical filter unit having a filter wheel (52; 152), with which optionally different optical filters (F1, F2, F3, F4, GF) can be introduced into the beam path, - with an evaluation unit for evaluating the received signals and determining a gas concentration therefrom and - with a beam deflection unit (60; 160), characterized in that, - the beam deflecting unit (60; 160) deflects the beam path (14; 14-1 and 14-2) in such a way that the beam path (14; 14-1 and 14-2) passes through the filter wheel (52; 152) twice and two of the filters (GF and F1) are passed through by the beam path in at least one position of the filter wheel (52; 152). - with a light source which emits light in a wavelength range and - whose light beams are guided along a beam path through a measuring section, - with a receiving arrangement (30; 130) which receives the light of the light source after passing through the measuring section and provides receiving signals depending on the light intensity incident on the receiving arrangement (30; 130), - with an optical filter unit having a filter wheel (52; 152), with which optionally different optical filters (F1, F2, F3, F4, GF) can be introduced into the beam path, - with an evaluation unit for evaluating the received signals and determining a gas concentration therefrom and - with a beam deflection unit (60; 160), - the beam deflecting unit (60; 160) deflects the beam path (14; 14-1 and 14-2) in such a way that the beam path (14; 14-1 and 14-2) passes through the filter wheel (52; 152) twice and two of the filters (GF and F1) are passed through by the beam path in at least one position of the filter wheel (52; 152).
A fluid control valve for mixing hot and cold water has an inlet for cold water, an inlet for hot water and at least one outlet for temperature controlled water, wherein the valve further has a temperature control device for mixing hot and cold water to provide a source of temperature controlled water comprising a cartridge having inlet ports (27, 25) in communication with the inlets (17, 15) for hot and cold water and an outlet port in communication with the at least one outlet for temperature controlled water, and wherein the valve further has an inner sleeve that defines with the cartridge a first passageway, and an outer sleeve that defines with the inner sleeve and cartridge a second passageway, the first and second passageways configured to deliver hot and cold water to the inlet ports (25, 27) of the cartridge.
A carbon catalyst, comprising two kinds of transition metals, and a carbon structure having an interplanar spacing d 002 of 0.374 nm or more, the interplanar spacing d 002 being determined from a Bragg angle of a diffraction peak f broad which is one of three diffraction peaks f broad, f middle, and f narrow obtained by separating a diffraction peak around a diffraction angle (2θ) of 26° in an X-ray diffraction pattern of powder X-ray diffraction with a CuKα ray, wherein the area ratios of the three peaks f broad, f middle and f narrow are determined as set out in the description. two kinds of transition metals, and a carbon structure having an interplanar spacing d 002 of 0.374 nm or more, the interplanar spacing d 002 being determined from a Bragg angle of a diffraction peak f broad which is one of three diffraction peaks f broad, f middle, and f narrow obtained by separating a diffraction peak around a diffraction angle (2θ) of 26° in an X-ray diffraction pattern of powder X-ray diffraction with a CuKα ray, wherein the area ratios of the three peaks f broad, f middle and f narrow are determined as set out in the description.
A tubular device for a catheter or sheath comprising a proximal end and a distal end sized for introduction into a patient's body, the device comprising: a primary lumen (18a, 518) extending between the proximal and distal ends; one or more elongate conducting elements extending at least partially between the proximal and distal ends adjacent the primary lumen, wherein the one or more conducting elements extend substantially parallel to a longitudinal axis of the tubular device at least partially between the proximal and distal ends; a plurality of reinforcement members (43, 542) braided around the primary lumen and comprising windings extending helically around the primary lumen between the proximal and distal ends, at least some of the windings passing between the primary lumen and the one or more conducting elements and at least some of the windings surrounding both the primary lumen and the one or more conducting elements; one or more layers (44, 544) surrounding the one or more reinforcement members; and one or more sensing elements (550a, 530b, 500c) on a distal portion of the tubular device coupled to the one or more conducting elements. a primary lumen (18a, 518) extending between the proximal and distal ends; one or more elongate conducting elements extending at least partially between the proximal and distal ends adjacent the primary lumen, wherein the one or more conducting elements extend substantially parallel to a longitudinal axis of the tubular device at least partially between the proximal and distal ends; a plurality of reinforcement members (43, 542) braided around the primary lumen and comprising windings extending helically around the primary lumen between the proximal and distal ends, at least some of the windings passing between the primary lumen and the one or more conducting elements and at least some of the windings surrounding both the primary lumen and the one or more conducting elements; one or more layers (44, 544) surrounding the one or more reinforcement members; and one or more sensing elements (550a, 530b, 500c) on a distal portion of the tubular device coupled to the one or more conducting elements.
Aircraft seat comprising a seat base, wherein - a first side of the seat base can be fastened to a seat unit of the aircraft seat, and - a second side of the seat base can be fastened to a floor attachment assembly in order to fasten it to the aircraft, wherein - the seat base is formed by at least one flexurally rigid shell component, wherein - the shell component comprises a cavity for receiving at least one functional element (7, 13), wherein - the cavity is closed, wherein - a first heat-transfer element comprising an inner and an outer portion (9, 10) is provided, wherein - the inner portion is assigned to the cavity and is in contact with the functional element (7, 13) in order to absorb thermal energy generated by the functional element (7, 13), wherein - the outer portion is assigned to an external environment of the shell component in order to dissipate the thermal energy, characterised in that - the functional element (7, 13) is suspended in the cavity, wherein - the functional element (7, 13) is fastened to the bottom of the first heat-transfer element. - a first side of the seat base can be fastened to a seat unit of the aircraft seat, and - a second side of the seat base can be fastened to a floor attachment assembly in order to fasten it to the aircraft, wherein - the seat base is formed by at least one flexurally rigid shell component, wherein - the shell component comprises a cavity for receiving at least one functional element (7, 13), wherein - the cavity is closed, wherein - a first heat-transfer element comprising an inner and an outer portion (9, 10) is provided, wherein - the inner portion is assigned to the cavity and is in contact with the functional element (7, 13) in order to absorb thermal energy generated by the functional element (7, 13), wherein - the outer portion is assigned to an external environment of the shell component in order to dissipate the thermal energy, - the functional element (7, 13) is suspended in the cavity, wherein - the functional element (7, 13) is fastened to the bottom of the first heat-transfer element.
A deagglomerator (400; 500; 701) for a breath-actuated dry powder inhaler, the deagglomerator (400; 500; 701) comprising: an inner wall (412; 512) defining a swirl chamber (414; 514) extending along a longitudinal axis (A, B) from a first end (418; 518) to a second end (420; 520); at least one inlet port (424; 425; 524; 525) in the inner wall (412; 512) of the swirl chamber (414; 514) adjacent to the first end of the swirl chamber (414; 514) providing fluid communication between a region exterior to the deagglomerator (400; 500; 701) and the first end (418; 518) ofthe swirl chamber (414; 514), and directing airflow into the swirl chamber in a transverse direction; an outlet port (432; 530); an airflow adaptor (100; 200; 300; 501; 601; 702); wherein the airflow adaptor (100; 200; 300; 501; 601; 702) provides fluid communication between the outlet port (432; 530) and a region exterior to the deagglomerator (400; 500; 701) and the outlet port (432; 530) provides fluid communication between the second end (420; 520) and the airflow adaptor (100; 200; 300; 501; 601; 702); and wherein the airflow adaptor (100; 200; 300; 501; 601; 702) comprises at least one swirl chamber by-pass port (102-105; 204-206; 304-306; 502-505; 603-606) for allowing air to flow from a proximal end of the airflow adaptor (100; 200; 300; 501; 601; 702) to a distal end of the airflow adaptor (100; 200; 300; 501; 601; 702) independently of the swirl-chamber (414; 514) when a breath-induced low pressure is applied to the distal end of the airflow adaptor (100; 200; 300; 501; 601; 702); and characterised in that the deagglomerator further comprises a dry powder supply port (422; 522) in the first end (418; 518) of the swirl chamber (414; 514) for providing fluid communication between a dry powder delivery passageway of an inhaler and the first end (418; 518) of the swirl chamber (414; 514) and directing airflow and entrained powder into the swirl chamber in a longitudinal direction. an inner wall (412; 512) defining a swirl chamber (414; 514) extending along a longitudinal axis (A, B) from a first end (418; 518) to a second end (420; 520); at least one inlet port (424; 425; 524; 525) in the inner wall (412; 512) of the swirl chamber (414; 514) adjacent to the first end of the swirl chamber (414; 514) providing fluid communication between a region exterior to the deagglomerator (400; 500; 701) and the first end (418; 518) ofthe swirl chamber (414; 514), and directing airflow into the swirl chamber in a transverse direction; an outlet port (432; 530); an airflow adaptor (100; 200; 300; 501; 601; 702);
A stabilization system for a wind power generation system including a wind power generator, the stabilization system comprising: a deadband limiter configured for detecting when a signal is outside of a respective signal range, wherein the signal comprises a frequency; an input frequency washout configured for calculating a frequency deviation, wherein the deadband limiter is configured to use the frequency deviation to set the respective signal range; a power shaper configured for providing a transient power generation adjustment signal for a turbine control to transiently boost power in response to the signal being outside of the respective signal range; and a limit controller to configured to prevent the adjustment signal from causing the wind power generator to operate outside of at least one operating constraint. a deadband limiter configured for detecting when a signal is outside of a respective signal range, wherein the signal comprises a frequency; an input frequency washout configured for calculating a frequency deviation, wherein the deadband limiter is configured to use the frequency deviation to set the respective signal range; a power shaper configured for providing a transient power generation adjustment signal for a turbine control to transiently boost power in response to the signal being outside of the respective signal range; and a limit controller to configured to prevent the adjustment signal from causing the wind power generator to operate outside of at least one operating constraint.
A polarization modulation method of photonic pulses, for generating quantum cryptographic keys, comprising the steps of: • generating a stream of photonic pulses, each one comprising a given polarization state obtained by the superposition of both the horizontal and the vertical polarization modes thereof, and by routing them in a first fiber; • splitting, inside said first fiber, said horizontal and vertical polarization modes, and routing them through respective terminals of a second fiber forming a ring, whereby they travel such ring clockwise and counter-clockwise respectively, or vice versa. wherein said first and second fibers are both polarization-maintaining fibers whereby, inducing a respective phase modulation, Φ e and Φ 1, of both said polarization modes, in one point of said ring which is spaced from said terminals by optical paths having different lengths along said ring, a polarization-maintaining fiber delay line is determined; the polarization modulation method further comprising the step of: • recombining said polarization modes in one single photonic pulse beam, and routing the resulting beam through said first fiber, by obtaining, at the output thereof, a polarization state of the pulses depending upon the difference between said phase modulations, Φe and Φ1. • generating a stream of photonic pulses, each one comprising a given polarization state obtained by the superposition of both the horizontal and the vertical polarization modes thereof, and by routing them in a first fiber; • splitting, inside said first fiber, said horizontal and vertical polarization modes, and routing them through respective terminals of a second fiber forming a ring, whereby they travel such ring clockwise and counter-clockwise respectively, or vice versa. • recombining said polarization modes in one single photonic pulse beam, and routing the resulting beam through said first fiber, by obtaining, at the output thereof, a polarization state of the pulses depending upon the difference between said phase modulations, Φe and Φ1.