mhurhangee/patent-ind-claim-en huggingface dataset:
A method of determining a climb profile for an aircraft , the method comprising: receiving, by a controller module , an initial climb profile defining a portion of a flight plan for the aircraft between takeoff and a cruise profile , and an altitude climb constraint defining at least one altitude limitation of the aircraft ; determining, by the controller module , that the initial climb profile does not satisfy the altitude climb constraint ; selecting, by the controller module , a deviation point of the initial climb profile prior to the altitude climb constraint ; repeatedly calculating, by the controller module , a set of subsequent climb models starting from the deviation point based on successive aircraft energy levels; determining an updated climb profile based on the set of subsequent climb models ; determining the updated climb profile satisfies the altitude climb constraint ; and operating the aircraft in accordance with the updated climb profile ; and characterized in that : the repeatedly calculating the set of subsequent climb models is further based on successive aircraft energy levels increased by holding a thrust setting at a set thrust value. receiving, by a controller module , an initial climb profile defining a portion of a flight plan for the aircraft between takeoff and a cruise profile , and an altitude climb constraint defining at least one altitude limitation of the aircraft ; determining, by the controller module , that the initial climb profile does not satisfy the altitude climb constraint ; selecting, by the controller module , a deviation point of the initial climb profile prior to the altitude climb constraint ; repeatedly calculating, by the controller module , a set of subsequent climb models starting from the deviation point based on successive aircraft energy levels; determining an updated climb profile based on the set of subsequent climb models ; determining the updated climb profile satisfies the altitude climb constraint ; and operating the aircraft in accordance with the updated climb profile ; and characterized in that : the repeatedly calculating the set of subsequent climb models is further based on successive aircraft energy levels increased by holding a thrust setting at a set thrust value.
A linear compressor comprising: a linear motor having a mover reciprocating with respect to a stator ; a piston coupled to the mover to reciprocate; a cylinder into which the piston is slidingly inserted, the cylinder having an inner circumferential surface forming a bearing surface together with an external circumferential surface of the piston , the cylinder forming a compression space together with the piston , and the cylinder having at least one first hole formed through the inner circumferential surface of the cylinder and an outer circumferential surface of the cylinder to guide refrigerant discharged from the compression space to the bearing surface; a porous member coupled to the outer circumferential surface of the cylinder and configured to cover the first hole , the porous member having multiple micropores smaller than the first hole ; and a cover member surrounding the porous member and coupled to an outer circumferential surface of the porous member , characterized in that the cover member comprises at least one second hole formed on the cover member to communicate with the micropores of the porous member through an outer circumferential surface and an inner circumferential surface of the cover member , wherein the second hole has a larger inner diameter than the micropores. a linear motor having a mover reciprocating with respect to a stator ; a piston coupled to the mover to reciprocate; a cylinder into which the piston is slidingly inserted, the cylinder having an inner circumferential surface forming a bearing surface together with an external circumferential surface of the piston , the cylinder forming a compression space together with the piston , and the cylinder having at least one first hole formed through the inner circumferential surface of the cylinder and an outer circumferential surface of the cylinder to guide refrigerant discharged from the compression space to the bearing surface; a porous member coupled to the outer circumferential surface of the cylinder and configured to cover the first hole , the porous member having multiple micropores smaller than the first hole ; and a cover member surrounding the porous member and coupled to an outer circumferential surface of the porous member , characterized in that the cover member comprises at least one second hole formed on the cover member to communicate with the micropores of the porous member through an outer circumferential surface and an inner circumferential surface of the cover member , wherein the second hole has a larger inner diameter than the micropores.
A planar wave guide, PWG, amplifier having a first end for coupling to a light pump and a second end opposite to the first end comprising: a first cladding layer ; a second cladding layer ; and a uniformly doped core layer between the first cladding layer and the second cladding layer, wherein the core has a tapered configuration along its entire length, wherein the core layer is tapered having a smaller thickness at the first end and a larger thickness at the second end, and wherein a ratio of the core thickness to thickness of the cladding layers is smaller at the first end and larger at the second end, wherein the first cladding layer has a larger thickness than the second cladding layer, at any point along a length of the PWG amplifier, wherein the first cladding layer is proportionally tapered along the length of the PWG amplifier having a larger thickness at the first end and a smaller thickness at the second end oppositely proportional to the thickness of the core layer and the second cladding layer has a constant thickness along the length of the PWG amplifier to form the PWG amplifier with a uniform overall thickness along its length. a first cladding layer ; a second cladding layer ; and a uniformly doped core layer between the first cladding layer and the second cladding layer, wherein the core has a tapered configuration along its entire length, wherein the core layer is tapered having a smaller thickness at the first end and a larger thickness at the second end, and wherein a ratio of the core thickness to thickness of the cladding layers is smaller at the first end and larger at the second end, wherein the first cladding layer has a larger thickness than the second cladding layer, at any point along a length of the PWG amplifier, wherein the first cladding layer is proportionally tapered along the length of the PWG amplifier having a larger thickness at the first end and a smaller thickness at the second end oppositely proportional to the thickness of the core layer and the second cladding layer has a constant thickness along the length of the PWG amplifier to form the PWG amplifier with a uniform overall thickness along its length.
A holder for attachment to a medical appliance, preferably for attachment to a blood treatment device, comprising: an attachment portion which is formed to be attached to a rod of the medical appliance, a holding element by means of which a dialyzer can be fixed to the medical appliance, and a middle part which extends between the attachment portion and the holding element and is movable relative to the attachment portion and the holding element , wherein the middle part is rotatable relative to the attachment portion about a first axis of rotation (D1) and relative to the holding element about a second axis of rotation (D2), characterized in that the first axis of rotation (D1) and the second axis of rotation (D2) extend perpendicularly to each other. an attachment portion which is formed to be attached to a rod of the medical appliance, a holding element by means of which a dialyzer can be fixed to the medical appliance, and a middle part which extends between the attachment portion and the holding element and is movable relative to the attachment portion and the holding element , wherein the middle part is rotatable relative to the attachment portion about a first axis of rotation (D1) and relative to the holding element about a second axis of rotation (D2), characterized in that the first axis of rotation (D1) and the second axis of rotation (D2) extend perpendicularly to each other.
Method for operating a driver assistance system of a motor vehicle performing a driver assistance function, which driver assistance function can only be activated by the driver when at least one activation criterion is met and is automatically deactivated if at least one deactivation criterion is met, wherein if the driver assistance system can be activated, an activability information item indicating the activability is output to the driver and an expected activity period is determined before a deactivation criterion occurs and is output together with the activability information item, characterised in that a reliability value of the activity period is determined for the expected activity period and the output of the activability information item and/or the activation period is adjusted as a function of the reliability value.
A medical instrument which is capable of holding a guide wire (W) protruding from a first luminal organ (Bd) into a second luminal organ (D) via an opening portion (Dp), comprising: a sheath which has a center axis (O) extending in a longitudinal direction from a distal end thereof toward a proximal end thereof and which includes a first contact area (S1), which is formed on the most distal end side of a distal end surface of the sheath and which is capable of being in contact with the guide wire (W), and a second contact area (S2), which is formed on the most proximal end side of the distal end surface of the sheath and which is capable of coming into contact with the guide wire (W); and a holding portion which is advanceable and retractable in a lumen of the sheath and is retracted into the lumen of the sheath so that the guide wire (W) is pressed to the first and second contact areas (S1, S2) and the holding portion holds the guide wire (W), wherein the distal end surface , formed at the distal end of the sheath , is an inclined surface which is formed in an elliptical shape and is inclined with respect to the center axis (O); and wherein the guide wire (W) is held by the sheath at two places corresponding to the first contact area (S1) and the second contact area (S2), and characterized in that the holding portion has an annular portion having a slit portion in which the guide wire (W) is capable of being inserted, and a plate-shaped portion which extends in a direction of the center axis (O) and is connected to the annular portion . a sheath which has a center axis (O) extending in a longitudinal direction from a distal end thereof toward a proximal end thereof and which includes a first contact area (S1), which is formed on the most distal end side of a distal end surface of the sheath and which is capable of being in contact with the guide wire (W), and a second contact area (S2), which is formed on the most proximal end side of the distal end surface of the sheath and which is capable of coming into contact with the guide wire (W); and a holding portion which is advanceable and retractable in a lumen of the sheath and is retracted into the lumen of the sheath so that the guide wire (W) is pressed to the first and second contact areas (S1, S2) and the holding portion holds the guide wire (W), wherein the distal end surface , formed at the distal end of the sheath , is an inclined surface which is formed in an elliptical shape and is inclined with respect to the center axis (O); and wherein the guide wire (W) is held by the sheath at two places corresponding to the first contact area (S1) and the second contact area (S2), and characterized in that the holding portion has an annular portion having a slit portion in which the guide wire (W) is capable of being inserted, and a plate-shaped portion which extends in a direction of the center axis (O) and is connected to the annular portion .
A method for operating a turbomachine of a hybrid-electric propulsion system of an aircraft , the hybrid-electric propulsion system comprising an electric machine coupled to a rotating system of the turbomachine, the electric machine electrically coupled to an electric power source , the method comprising: rotating the electric machine with the turbomachine to generate electrical power during a flight operation mode of the turbomachine; rotating a propulsor of the hybrid electric propulsion system utilizing at least in part the electrical power generated from the rotating of the electric machine with the turbomachine to provide a propulsive benefit for the aircraft during the flight operation mode of the turbomachine; determining the turbomachine is in a post flight operation mode or in a pre-flight operation mode; and providing electrical power from the electric power source to the electric machine such that the electric machine rotates the rotating system of the turbomachine at a varying rotational speed to prevent or correct a bowed rotor condition. rotating the electric machine with the turbomachine to generate electrical power during a flight operation mode of the turbomachine; rotating a propulsor of the hybrid electric propulsion system utilizing at least in part the electrical power generated from the rotating of the electric machine with the turbomachine to provide a propulsive benefit for the aircraft during the flight operation mode of the turbomachine; determining the turbomachine is in a post flight operation mode or in a pre-flight operation mode; and providing electrical power from the electric power source to the electric machine such that the electric machine rotates the rotating system of the turbomachine at a varying rotational speed to prevent or correct a bowed rotor condition.
A semiconductor die , comprising: a power rail ; a first gate (420b, 420b-1); a second gate (420d, 420d-1); a first gate contact electrically coupled to the first gate, wherein the first gate contact is formed from a first middle of line, MOL, (CB) metal layer; a second gate contact electrically coupled to the second gate, wherein the second gate contact is formed from the first MOL metal layer (CB); and an interconnect formed from a second MOL metal layer (CA), wherein the interconnect is electrically coupled to the first and second gate contacts, and forms an electrical bridge between the first and the second gate contact, and at least a portion of the interconnect is underneath the power rail. a power rail ; a first gate (420b, 420b-1); a second gate (420d, 420d-1); a first gate contact electrically coupled to the first gate, wherein the first gate contact is formed from a first middle of line, MOL, (CB) metal layer; a second gate contact electrically coupled to the second gate, wherein the second gate contact is formed from the first MOL metal layer (CB); and an interconnect formed from a second MOL metal layer (CA), wherein the interconnect is electrically coupled to the first and second gate contacts, and forms an electrical bridge between the first and the second gate contact, and at least a portion of the interconnect is underneath the power rail.
A connection piece for connecting a post with either a frame member; a sash member or one or more other posts, the connection piece comprising: - a tubular body defining a through hole, the tubular body extending along an axis X-X and having a proximal end and a distal end ; - a shoulder portion provided at the proximal end of the tubular body configured to abut a sidewall of a first post or frame member , said shoulder portion defining an abutment extending in a plane askew from the X-X axis; - a pen or protrusion provided at or near the distal end of the tubular body and extending in a direction Y askew to the X-X axis; and - a screw extending through the tubular body , with a screw head seated next to the proximal end of the tubular body and a screw tip extending through the tubular body next to, yet askew in view of the pen or protrusion , characterized in that the shoulder portion at the proximal end of the tubular body extends in a plane parallel to a Y-direction under an angle ranging between 45° and 1° in view of the X-X axis. - a tubular body defining a through hole, the tubular body extending along an axis X-X and having a proximal end and a distal end ; - a shoulder portion provided at the proximal end of the tubular body configured to abut a sidewall of a first post or frame member , said shoulder portion defining an abutment extending in a plane askew from the X-X axis; - a pen or protrusion provided at or near the distal end of the tubular body and extending in a direction Y askew to the X-X axis; and - a screw extending through the tubular body , with a screw head seated next to the proximal end of the tubular body and a screw tip extending through the tubular body next to, yet askew in view of the pen or protrusion ,
A method comprising: receiving a plurality of images from a plurality of cameras , wherein the plurality of cameras comprise a first camera having a first orientation, a second camera having a second orientation, and a third camera having the first orientation, wherein the second camera is located between the first and third cameras, and wherein the plurality of images comprises a first image (I-L1) from the first camera, a second image (I-L2) from the second camera, and a third image (I-R1) from the third camera; detecting a plurality of feature points within the first (I-L1) and second images (I-L2); determining one or more pairs of corresponding feature points located within a region of overlap (210L 1-2 ) between the first (I-L1) and second images (I-L2), wherein the pairs of corresponding feature points comprise a respective one of the feature points from each of the first and second images (I-L1 and I-L2), and wherein the third image (I-R1) has a region corresponding to the region of overlap (210L 1-2 ) between the first and second images (I-L1 and I-L2); spatially adjusting the first or second image based on a calculated offset between each pair of corresponding feature points ; comparing the first and second images (I-L1 and I-L2) with the third image (I-R1) having the region corresponding to the region of overlap (210L 1-2 ) between the first and second images (I-L1 and I-L2); and combining the first and second images into a merged image based on the spatial adjustment and the comparison with the third image (I-R1). receiving a plurality of images from a plurality of cameras , wherein the plurality of cameras comprise a first camera having a first orientation, a second camera having a second orientation, and a third camera having the first orientation, wherein the second camera is located between the first and third cameras, and wherein the plurality of images comprises a first image (I-L1) from the first camera, a second image (I-L2) from the second camera, and a third image (I-R1) from the third camera; detecting a plurality of feature points within the first (I-L1) and second images (I-L2); determining one or more pairs of corresponding feature points located within a region of overlap (210L 1-2 ) between the first (I-L1) and second images (I-L2), wherein the pairs of corresponding feature points comprise a respective one of the feature points from each of the first and second images (I-L1 and I-L2), and wherein the third image (I-R1) has a region corresponding to the region of overlap (210L 1-2 ) between the first and second images (I-L1 and I-L2); spatially adjusting the first or second image based on a calculated offset between each pair of corresponding feature points ; comparing the first and second images (I-L1 and I-L2) with the third image (I-R1) having the region corresponding to the region of overlap (210L 1-2 ) between the first and second images (I-L1 and I-L2); and combining the first and second images into a merged image based on the spatial adjustment and the comparison with the third image (I-R1).
Sensing arrangement for indicating the depletion of a coreless roll of absorbent paper web material in a dispenser, the sensing arrangement comprising a roll support , configured for supporting an inner circumference of said coreless roll with said roll extending over a roll support length (L), said roll support extending along a longitudinal centre axis (X), the roll support comprising at least one roll expanding portion extending over a part of said roll support length (L) and having a maximum radial extension defining a first radius (r1) from said centre axis (X), and at least one sensing portion , extending longitudinally over another part of said roll support length (L) and having a maximum radial extension defining a second radius (r2) from said centre axis (X), wherein said first radius (r1) is greater than said second radius (r2) by a sensing offset length (I), and a sensing element arranged to sense at said sensing portion the amount of web material remaining on the roll when arranged over said roll support length (L), characterised in that said roll expanding portion(s) comprises at least one roll expanding member , providing said first radius (r1), wherein said roll expanding member(s) is/are resilient. a roll support , configured for supporting an inner circumference of said coreless roll with said roll extending over a roll support length (L), said roll support extending along a longitudinal centre axis (X), the roll support comprising at least one roll expanding portion extending over a part of said roll support length (L) and having a maximum radial extension defining a first radius (r1) from said centre axis (X), and at least one sensing portion , extending longitudinally over another part of said roll support length (L) and having a maximum radial extension defining a second radius (r2) from said centre axis (X), wherein said first radius (r1) is greater than said second radius (r2) by a sensing offset length (I), and a sensing element arranged to sense at said sensing portion the amount of web material remaining on the roll when arranged over said roll support length (L), characterised in that said roll expanding portion(s) comprises at least one roll expanding member , providing said first radius (r1), wherein said roll expanding member(s) is/are resilient.
A method for configuring special subframes in a wireless communication system, comprising: identifying a time period for an extended clear channel assessment "ECCA" operation; and determining a guard period portion included in a special subframe of a frame structure based on the identified time period. identifying a time period for an extended clear channel assessment "ECCA" operation; and determining a guard period portion included in a special subframe of a frame structure based on the identified time period.