mhurhangee/patent-ind-claim-en huggingface dataset:
An insert measurement system for measuring a parameter of a muscular-skeletal system, the insert measurement system comprising: an articular surface ; and a load -bearing surface ; a first support structure having the articular surface ; a second support structure having the load-bearing surface ; at least one interior cavity housing electronic circuitry operatively coupled to at least one sensor ; wherein the first support structure and the second support structure are coupled together to form the at least one interior cavity; characterized in that the insert measurement system further comprises: a sterilization gas within the at least one interior cavity ; and a port ; wherein the port is configured to be externally accessed when the first support structure and the second support structure are coupled together, to deliver the sterilization gas to sterilize the at least one interior cavity . an articular surface ; and a load -bearing surface ; a first support structure having the articular surface ; a second support structure having the load-bearing surface ; at least one interior cavity housing electronic circuitry operatively coupled to at least one sensor ; wherein the first support structure and the second support structure are coupled together to form the at least one interior cavity; characterized in that the insert measurement system further comprises: a sterilization gas within the at least one interior cavity ; and a port ; wherein the port is configured to be externally accessed when the first support structure and the second support structure are coupled together, to deliver the sterilization gas to sterilize the at least one interior cavity . a sterilization gas within the at least one interior cavity ; and a port ; wherein the port is configured to be externally accessed when the first support structure and the second support structure are coupled together, to deliver the sterilization gas to sterilize the at least one interior cavity .
A garment care device comprising: - a housing ; - a chamber within the housing to receive at least one garment, the chamber having an air inlet and an air outlet ; - an air channel linking the air inlet and the air outlet ; - a first fan for circulating an air flow between the chamber , the air outlet , the air channel , and the air inlet , - a heater for heating the air flow, wherein the air inlet is configured such that air entering the chamber flows along a first direction (A1, A2), and wherein the air outlet is configured to draw the air in the chamber along a second direction (B) transverse to the first direction (A1, A2), characterised in that the garment care device comprises further - an extraction channel which vents to atmosphere, - a second fan , the extraction channel linking the chamber with the second fan , wherein the second fan is operable such as to selectively draw a further air flow out of the chamber , into and through the extraction channel to vent to the atmosphere when the second fan is being operated, and - a controller configured to control the heater and the first fan such that for a first predetermined time period the air in the garment care device is at above a first temperature level, and is circulated at above a first flow rate, and for a second predetermined time period the air is below the first temperature level and is circulated at above the first flow rate. - a housing ; - a chamber within the housing to receive at least one garment, the chamber having an air inlet and an air outlet ; - an air channel linking the air inlet and the air outlet ; - a first fan for circulating an air flow between the chamber , the air outlet , the air channel , and the air inlet , - a heater for heating the air flow, - an extraction channel which vents to atmosphere, - a second fan , the extraction channel linking the chamber with the second fan , wherein the second fan is operable such as to selectively draw a further air flow out of the chamber , into and through the extraction channel to vent to the atmosphere when the second fan is being operated, and - a controller configured to control the heater and the first fan such that for a first predetermined time period the air in the garment care device is at above a first temperature level, and is circulated at above a first flow rate, and for a second predetermined time period the air is below the first temperature level and is circulated at above the first flow rate.
Arrangement comprising a frequency converter and an electric motor on which the frequency converter is mounted in a joining direction (F), and at least one fastening element for the detachable fastening of the frequency converter on the electric motor , in which the fastening element is a locking element lying between the frequency converter and the electric motor with at least two physically separate locking sections , in which the locking element along with the locking sections is moveable in a plane transverse to the joining direction (F) from a release position to a locking position where the locking sections hold the frequency converter on the electric motor , characterised by the locking element being moveable via at least two guide screws respectively extending through an elongated opening in the locking element , the heads of which hold the locking element on the frequency converter or electric motor so that it is only moveable in the plane transverse to the joining direction (F).
LED light unit for an aircraft, comprising: a support portion , a light source having at least one LED, the light source being arranged on the support portion , and a refractive optical element having an inner surface and an outer surface , the refractive optical element being attached to the support portion and being arranged over the light source , wherein the refractive optical element has a chamfer portion adjacent the support portion , wherein at least one of the inner surface and the outer surface has at least one chamfer surface (92; 94; 96; 98) in the chamfer portion , characterised in that the LED light unit is an air plane rear navigation light unit having an air plane rear navigation light intensity distribution, and in that the at least one chamfer surface (92; 94; 96; 98) refracts light away from an ambient light emission direction of the air plane rear navigation light intensity distribution, wherein the ambient light emission direction is an angular region of between 70° and 90° with respect to a principal light emission direction of the LED light unit . a support portion , a light source having at least one LED, the light source being arranged on the support portion , and a refractive optical element having an inner surface and an outer surface , the refractive optical element being attached to the support portion and being arranged over the light source , wherein the refractive optical element has a chamfer portion adjacent the support portion , wherein at least one of the inner surface and the outer surface has at least one chamfer surface (92; 94; 96; 98) in the chamfer portion , characterised in that the LED light unit is an air plane rear navigation light unit having an air plane rear navigation light intensity distribution, and in that the at least one chamfer surface (92; 94; 96; 98) refracts light away from an ambient light emission direction of the air plane rear navigation light intensity distribution, wherein the ambient light emission direction is an angular region of between 70° and 90° with respect to a principal light emission direction of the LED light unit .
A seat for a vehicle, comprising: a seat pan , having a seat pan front edge and a seat pan rear edge; a backrest , having a backrest top edge and a backrest bottom edge, wherein the backrest bottom edge is articulately disposed adjacent to the seat pan rear edge, and at least one of the seat pan and the backrest is configurable into a plurality of positions; an undercarriage supporting the seat pan , the undercarriage comprising spaced-apart left and right lateral brackets; and a back support lattice disposed adjacent to the backrest for providing back support, a control operable by a passenger of the seat for setting an initial degree of back support provided by the back support lattice ; wherein the back support lattice is operatively connected to at least one of the seat pan and the backrest , and wherein the back support provided by the back support lattice is automatically adjustable from the initial degree of back support depending on the plurality of positions, characterized in that the seat further comprises a tilt link operably connected, at a tilt link top end, to at least one of the backrest and the seat pan and, at a tilt link bottom end, to the undercarriage , wherein the tilt link is a S-shaped plate from a side view between the tilt link top end and the tilt link bottom end. a seat pan , having a seat pan front edge and a seat pan rear edge; a backrest , having a backrest top edge and a backrest bottom edge, wherein the backrest bottom edge is articulately disposed adjacent to the seat pan rear edge, and at least one of the seat pan and the backrest is configurable into a plurality of positions; an undercarriage supporting the seat pan , the undercarriage comprising spaced-apart left and right lateral brackets; and a back support lattice disposed adjacent to the backrest for providing back support, a control operable by a passenger of the seat for setting an initial degree of back support provided by the back support lattice ; wherein the back support lattice is operatively connected to at least one of the seat pan and the backrest , and wherein the back support provided by the back support lattice is automatically adjustable from the initial degree of back support depending on the plurality of positions, characterized in that the seat further comprises a tilt link operably connected, at a tilt link top end, to at least one of the backrest and the seat pan and, at a tilt link bottom end, to the undercarriage , wherein the tilt link is a S-shaped plate from a side view between the tilt link top end and the tilt link bottom end.
An image-capturing device comprising: a band-pass filter that is divided into a plurality of areas, each of which transmits incident light in a different wavelength band; a mask that is divided corresponding to the plurality of areas, and modulates the incident light in the different wavelength bands that are each transmitted through a corresponding one of the plurality of areas of the band-pass filter ; a solid-state image-capturing device that has an image-capturing plane that is divided corresponding to the plurality of areas, and captures, as a two-dimensional pixel signal, the incident light modulated by the mask in each of the plurality of areas, wherein a distance from the mask to the image-capturing plane of the solid-state image-capturing device differs for each of the plurality of areas. a band-pass filter that is divided into a plurality of areas, each of which transmits incident light in a different wavelength band; a mask that is divided corresponding to the plurality of areas, and modulates the incident light in the different wavelength bands that are each transmitted through a corresponding one of the plurality of areas of the band-pass filter ; a solid-state image-capturing device that has an image-capturing plane that is divided corresponding to the plurality of areas, and captures, as a two-dimensional pixel signal, the incident light modulated by the mask in each of the plurality of areas, wherein a distance from the mask to the image-capturing plane of the solid-state image-capturing device differs for each of the plurality of areas.
A nutritional composition comprising 10 to 50 wt.% vegetable lipids based on dry weight of the composition, and 0.5 to 20 wt.% phospholipids based on total lipid, wherein the phospholipids are derived from milk lipids, and said composition comprising lipid globules with a core comprising said vegetable lipids and a coating comprising said phospholipids, and wherein the lipid globules of the composition have i) a volume-weighted mode diameter above 1.0 μm, preferably between 1.0 and 10 μm, and/or ii) a diameter of 2 to 12 μm in an amount of at least 45, more preferably at least 55 volume % based on total lipid for use in prevention of obesity and/or reducing the risk of obesity , and wherein volume and size distribution of the lipid globules is determined by the method described in Michalski et al, 2001, Lait 81: 787-796, using a Mastersizer, Malvern Instruments, Malvern, UK, as particle size analyzer, and wherein the composition is for feeding a human subject with an age between 0 and 36 months and is for preventing obesity later in life and/or reducing the risk of obesity later in life of a human subject when said human subject has reached an age above 18 years. i) a volume-weighted mode diameter above 1.0 μm, preferably between 1.0 and 10 μm, and/or ii) a diameter of 2 to 12 μm in an amount of at least 45, more preferably at least 55 volume % based on total lipid
A calibration device comprising: a measurement housing accommodating a filling vessel to which a high pressure fuel gas is fed from outside from a hydrogen filling apparatus to be calibrated; a scale for measuring a weight of a fuel gas fed to the filling vessel ; and a main body housing accommodating the measurement housing and the scale , characterized in that the filling vessel , a filling gas supply pipe arranged between a receptacle and the filling vessel , and a filling gas release pipe are fixed or disposed to the measurement housing through supporting members (8, 14A-14C, 15), said filling vessel being mounted on a bottom face of the measurement housing through a supporting member , said filling gas supply pipe being fixed to a bottom face portion of the measurement housing by the supporting members (14A-14C) and said filling gas release pipe being fixed to the upper face portion of the measurement housing by a supporting member , said supporting members (8, 14A-14C, 15) having a heat insulating property, a portion of which is a member with low heat conductivity such as rubber and resin. a measurement housing accommodating a filling vessel to which a high pressure fuel gas is fed from outside from a hydrogen filling apparatus to be calibrated; a scale for measuring a weight of a fuel gas fed to the filling vessel ; and a main body housing accommodating the measurement housing and the scale , characterized in that the filling vessel , a filling gas supply pipe arranged between a receptacle and the filling vessel , and a filling gas release pipe are fixed or disposed to the measurement housing through supporting members (8, 14A-14C, 15), said filling vessel being mounted on a bottom face of the measurement housing through a supporting member , said filling gas supply pipe being fixed to a bottom face portion of the measurement housing by the supporting members (14A-14C) and said filling gas release pipe being fixed to the upper face portion of the measurement housing by a supporting member , said supporting members (8, 14A-14C, 15) having a heat insulating property, a portion of which is a member with low heat conductivity such as rubber and resin.
A cable strain relief with a crimp sleeve for the mechanical operative connection of a cable with a crimp collar , wherein in the crimped state the crimp sleeve serves to clamp a fibre braid of the cable , provided for strain relief, between the crimp sleeve and the crimp collar , characterised in that at its cable-side end the crimp sleeve has a deformable plastic sleeve , which is inserted into the crimp sleeve , and, in the crimped state, produces a mechanical operative connection between an outer sheath of the cable and the crimp sleeve , wherein the crimp sleeve is cylindrical, and in the same crimping operation the fibre braid can be clamped under the crimp sleeve , and the deformable plastic sleeve can be crimped onto the cable sheath.
System for detecting and monitoring a speed of a rotor , in particular of a rotor of a wind turbine , having at least three sensor units , wherein each sensor unit has an acceleration sensor and a gyroscope and is configured to determine the speed and position of the rotor independently of the other sensor units , wherein each sensor unit further has a communication component for communication with the other sensor units , characterised in that the system is configured to monitor a speed of the rotor in a fail-safe manner by comparing the speeds and positions determined by the sensor units , wherein the system is further configured in the event of a failure of one of the sensor units to initiate a normal shutdown of the monitored rotor , in particular of the wind turbine , and in the event of a failure of a plurality of the sensor units , in particular in the event of a failure of at least 50% of the sensor units, to initiate an emergency shutdown of the monitored rotor, in particular of the wind turbine. each sensor unit has an acceleration sensor and a gyroscope and is configured to determine the speed and position of the rotor independently of the other sensor units , wherein each sensor unit further has a communication component for communication with the other sensor units , characterised in that the system is configured to monitor a speed of the rotor in a fail-safe manner by comparing the speeds and positions determined by the sensor units , wherein the system is further configured in the event of a failure of one of the sensor units to initiate a normal shutdown of the monitored rotor , in particular of the wind turbine , and in the event of a failure of a plurality of the sensor units , in particular in the event of a failure of at least 50% of the sensor units, to initiate an emergency shutdown of the monitored rotor, in particular of the wind turbine.
Shock absorbing apparatus comprising: a flexible housing substantially formed from at least one fluid-impermeable elastomeric section and defining an interior, a plate disposed within the interior of the housing and having at least one orifice , the plate creating adjacent chambers containing a hydraulic fluid that are fluidically connected by the at least one orifice ; at least one mounting plate for connecting the housing to a structure that is under load in which transmitted loads acting on the flexible housing from the structure cause a pressurized hydraulic fluid to move between the adjacent chambers through the at least one orifice to provide shock absorption; in which the shock absorbing apparatus is characterized by two pin members disposed in axial relation on opposite sides of the plate and movable disposed in relation to the at least one orifice , in which transmitted loads acting on the flexible housing on either side of the plate cause movement of the two pin members relative to the at least one orifice to create a variable orifice diameter. a flexible housing substantially formed from at least one fluid-impermeable elastomeric section and defining an interior, a plate disposed within the interior of the housing and having at least one orifice , the plate creating adjacent chambers containing a hydraulic fluid that are fluidically connected by the at least one orifice ; at least one mounting plate for connecting the housing to a structure that is under load in which transmitted loads acting on the flexible housing from the structure cause a pressurized hydraulic fluid to move between the adjacent chambers through the at least one orifice to provide shock absorption; in which the shock absorbing apparatus is characterized by two pin members disposed in axial relation on opposite sides of the plate and movable disposed in relation to the at least one orifice , in which transmitted loads acting on the flexible housing on either side of the plate cause movement of the two pin members relative to the at least one orifice to create a variable orifice diameter.
A sustained release capsule comprising a hollow tubular body sealed at a first end, a movable piston within the body, a spring biasing the piston towards a second end of the body, an apertured cover at the second end to define a first chamber between the movable piston and the apertured cover capable of containing a first dose of material within the hollow tubular body for subsequent sustained release through the apertured cover into the rumen of an animal, wherein the movable piston has an end face facing towards the first dose, characterised in that the capsule comprises a hollow central sleeve extending rearwardly from the end face to assist in locating a spring, an aperture in the end face into the hollow interior of the central sleeve, the central sleeve having a closed portion distal from the end face to create a void capable of containing an exit dose of material.
Luminescent lanthanide complexes including a chelating agent, formed with a macrocycle with a 1,4,7-triazacyclononane structure complexing a lanthanide ion Ln 3+ chosen among Eu 3+ , Sm 3+ , Tb 3+ or Dy 3+ , characterized in that the chelating agent is formed with a macrocycle substituted with at least two betaine groups.
An aeroengine having a compressor inlet system comprising: a main inlet duct for directing a first air flow from a main intake opening to a compressor , the main intake opening being defined at a forward end of the inlet system with respect to a flight direction ; a secondary inlet duct for directing a second air flow from a secondary intake opening to the compressor ; and an inertial particle separator (IPS) duct connected in fluid communication with the main inlet duct , and extending from the main inlet duct rearward and terminating at a rear opening of the IPS duct , characterised in that the compressor inlet system further comprises: a control apparatus configured to select which of the first and second air flows to provide to the compressor , wherein in use the IPS duct directs a portion of the first air flow to bypass the compressor and to be discharged from the rear opening when the first airflow is selected to enter the compressor , and the control apparatus comprises a main valve configured to selectively close the main inlet duct to discontinue the first air flow and to thereby cause the IPS duct to draw air from the rear opening , functioning as the secondary inlet duct and the secondary intake opening for directing the second air flow to the compressor . a main inlet duct for directing a first air flow from a main intake opening to a compressor , the main intake opening being defined at a forward end of the inlet system with respect to a flight direction ; a secondary inlet duct for directing a second air flow from a secondary intake opening to the compressor ; and an inertial particle separator (IPS) duct connected in fluid communication with the main inlet duct , and extending from the main inlet duct rearward and terminating at a rear opening of the IPS duct , characterised in that the compressor inlet system further comprises: a control apparatus configured to select which of the first and second air flows to provide to the compressor , wherein in use the IPS duct directs a portion of the first air flow to bypass the compressor and to be discharged from the rear opening when the first airflow is selected to enter the compressor , and the control apparatus comprises a main valve configured to selectively close the main inlet duct to discontinue the first air flow and to thereby cause the IPS duct to draw air from the rear opening , functioning as the secondary inlet duct and the secondary intake opening for directing the second air flow to the compressor .