mhurhangee/ep-ind-claims huggingface dataset:
A drive assembly for a drug delivery device, comprising: - a housing with a proximal end and a distal end, and a longitudinal axis extending between the proximal end and the distal end, - a rotation sleeve being rotatable relative to the housing, - a drive member being axially moveable relative to the housing, wherein the rotation sleeve is implemented to be in mechanical cooperation with the drive member to be rotatable relative to the housing when the drive member is displaced in axial direction relative to the rotation sleeve, wherein the rotation sleeve is implemented to rotate in a first direction relative to the housing when the drive member is displaced in the distal direction, and to rotate in a second direction when the drive member is displaced in the proximal direction, and - a piston rod being axially moveable relative to the housing, wherein the piston rod is implemented to be in mechanical cooperation with the rotation sleeve to be moveable in the distal direction relative to the housing when the rotation sleeve rotates in the first direction and to be stationary in axial direction relative to the housing when the rotation sleeve rotates in the second direction opposite to the first direction, and wherein the piston rod has an outer surface provided with at least one guide track arranged on the outer surface, and the rotation sleeve comprises a guide piece being disposed and being movable in the guide track. - a housing with a proximal end and a distal end, and a longitudinal axis extending between the proximal end and the distal end, - a rotation sleeve being rotatable relative to the housing, - a drive member being axially moveable relative to the housing, wherein the rotation sleeve is implemented to be in mechanical cooperation with the drive member to be rotatable relative to the housing when the drive member is displaced in axial direction relative to the rotation sleeve, wherein the rotation sleeve is implemented to rotate in a first direction relative to the housing when the drive member is displaced in the distal direction, and to rotate in a second direction when the drive member is displaced in the proximal direction, and - a piston rod being axially moveable relative to the housing, wherein the piston rod is implemented to be in mechanical cooperation with the rotation sleeve to be moveable in the distal direction relative to the housing when the rotation sleeve rotates in the first direction and to be stationary in axial direction relative to the housing when the rotation sleeve rotates in the second direction opposite to the first direction,
Protective clothing, in particular for firefighters, having a pair of trousers and a seat harness, wherein the seat harness is arranged inside the trousers, the seat harness comprises at least one hip strap and at least two leg loops (21a, 21b) connected in a force-transmitting manner to the hip strap, and wherein the protective clothing comprises a chest harness, the chest harness comprises at least one left and at least one right shoulder strap (31a, 31b), characterised in that the chest harness comprises at least one left and at least one right underarm strap (32a, 32b), wherein the shoulder straps (31a, 31b) and underarm straps (32a, 32b) are connected to one another, in that the chest harness is connected to the seat harness in a releasable or operationally non-releasable manner, and in that the chest harness is connected to the pair of trousers via at least one suspenders section.
A method, comprising: loading respective historic signatures of a plurality of links onto a receiver node, the historic signatures generated by a different device than the receiver node; receiving, at the receiver node, a packet over a link associated with a sender node of the packet; identifying the link associated with the sender node of the packet based on a pre-payload portion of the packet before decoding a MAC header of the packet, including: extracting current channel state information, CSI, from the pre-payload portion; determining a current signature of the current CSI; correlating the current signature against a historic signature of each of the plurality of links; selecting and loading one or more baseband receive parameters associated with the identified link at the receiver node; and receiving a payload of the packet at the receiver node using the one or more baseband receive parameters; wherein correlating the current signature against the historic signature of each of the plurality of links includes: calculating a distance metric between the current signature and the historic signature of each of the plurality of links; and selecting a link of the plurality of links with a historic signature that is closest to the current signature as the identified link. loading respective historic signatures of a plurality of links onto a receiver node, the historic signatures generated by a different device than the receiver node; receiving, at the receiver node, a packet over a link associated with a sender node of the packet; identifying the link associated with the sender node of the packet based on a pre-payload portion of the packet before decoding a MAC header of the packet, including: extracting current channel state information, CSI, from the pre-payload portion; determining a current signature of the current CSI; correlating the current signature against a historic signature of each of the plurality of links; extracting current channel state information, CSI, from the pre-payload portion; determining a current signature of the current CSI; correlating the current signature against a historic signature of each of the plurality of links; selecting and loading one or more baseband receive parameters associated with the identified link at the receiver node; and receiving a payload of the packet at the receiver node using the one or more baseband receive parameters; wherein correlating the current signature against the historic signature of each of the plurality of links includes: calculating a distance metric between the current signature and the historic signature of each of the plurality of links; and selecting a link of the plurality of links with a historic signature that is closest to the current signature as the identified link. calculating a distance metric between the current signature and the historic signature of each of the plurality of links; and selecting a link of the plurality of links with a historic signature that is closest to the current signature as the identified link.
Fluid product refill for filling a bottle provided with a threaded neck, the refill comprising: - a flexible pouch comprising an opening, - a dispensing assembly (D1; D2) comprising a sealing appendage (11; 11'), the dispensing assembly comprising a threaded connection sleeve (22; 22') forming an internal helical thread adapted to the screwing of the threaded neck of the bottle, characterised in that the dispensing assembly (D1; D2) comprises: - an insert (1; 1') forming the sealing appendage (11; 11'), a passage, and also a camway or an external thread, - a stopper (2; 2') forming the threaded connection sleeve (22; 22'), and also a cam profile or an internal thread engaging with the camway or the external thread, respectively, wherein the stopper (2; 2') is initially in sealed engagement with the insert (1; 1') so as to close off the passage, the cam profile or internal thread moving into the camway or external thread, following the screwing of the threaded neck of the bottle into the threaded connection sleeve (22; 22'), so as to open the passage. - a flexible pouch comprising an opening, - a dispensing assembly (D1; D2) comprising a sealing appendage (11; 11'), the dispensing assembly comprising a threaded connection sleeve (22; 22') forming an internal helical thread adapted to the screwing of the threaded neck of the bottle, - an insert (1; 1') forming the sealing appendage (11; 11'), a passage, and also a camway or an external thread, - a stopper (2; 2') forming the threaded connection sleeve (22; 22'), and also a cam profile or an internal thread engaging with the camway or the external thread, respectively,
A dispersion comprising crystalline, semi-crystalline or amorphous particles or a mixture thereof, which particles have a size range of 0.1 to 1 μm and are present in an amount of up to 50 wt.% based on the total weight of the dispersion, wherein the liquid outer phase of the dispersion comprises oil, selected from palm oil, coconut oil or sunflower oil, or melted fats selected from cocoa butter or hydrogenated palm kernel stearin, wherein the particles have a particle size distribution of more than 90 vol.% within a size range of 0.1 to 1 μm or of more than 50 vol.% within a size range of 0.1 to 0.3 μm, and which comprises an emulsifier or a mixture of emulsifiers in an amount of more than 1 wt.% up to 2 wt.%, wherein the plastic viscosity of the dispersion remains constant or increases at a lower rate than the increase in yield value.
A deployable wing structure (2, 3) for air-braking a satellite wherein, once deployed, the wing structure comprises at least one wing structure element that forms a three-dimensional structure and comprises at least two panels (2a, 2b, 3a, 3b) extending in secant planes and forming a dihedron, and deploys from at least one deployment mast, characterised in that the panels join along a common edge (6, 7) consisting of a deployment mast common to the two panels, at least one of the panels (2, 3) consisting of a flexible, flat membrane that is stretched, once deployed, on at least two sides by holding elements (5, 8, 9) and wherein the deployment mast consists of an additional holding element which stretches the membrane on a third side.
The tuning methods of the PI controller parameters in the closed loop control system of an object, which transfer function may be approximated as a first order filter with time constant T and dead time L, and known gain k, comprising the steps of: a. connecting in series the input of the controlled object with the output of the integral part of the controller which proportional part is disconnected, setting the lowest gain value and closing the control loop, b. increasing the controller gain up to stability limit with stable oscillations of the controlled variable and describing the period of the oscillations T osc and fixed value of the controller gain k U, c. calculating the first order lag T of the controlled system model using the following formula T = k U 2 k 2 − ω osc 2 ω osc 2 where ω osc = 2 πT osc and the coefficient θ = arcctg ω osc T / ω osc T = L T where L is the controlled system model dead time d. calculating the settings of the PI controller from the following formula k ° = 10 − 0.659 + 0.465 / θ τ = 0.88 + 0.37 θ and determine the physical settings of the real PI controller from the relations k pN = k o k T iN = τ ⋅ T where k pN is the proportional controller gain and T iN is the integral controller time constant. a. connecting in series the input of the controlled object with the output of the integral part of the controller which proportional part is disconnected, setting the lowest gain value and closing the control loop, b. increasing the controller gain up to stability limit with stable oscillations of the controlled variable and describing the period of the oscillations T osc and fixed value of the controller gain k U, c. calculating the first order lag T of the controlled system model using the following formula T = k U 2 k 2 − ω osc 2 ω osc 2 where ω osc = 2 πT osc and the coefficient θ = arcctg ω osc T / ω osc T = L T where L is the controlled system model dead time d. calculating the settings of the PI controller from the following formula k ° = 10 − 0.659 + 0.465 / θ τ = 0.88 + 0.37 θ and determine the physical settings of the real PI controller from the relations k pN = k o k T iN = τ ⋅ T where k pN is the proportional controller gain and T iN is the integral controller time constant.
An apparatus for the securing of a load at a load bed which has at least one longitudinal groove comprising at least one undercut; said apparatus having a clamping mechanism which comprises an adapter element having two engagement means which can be introduced into the longitudinal groove and an actuation element by which the engagement means of the adapter element can be brought into engagement with the undercut of the longitudinal groove in a shape-matched and force-transmitting manner, wherein the engagement means are movably supported in or at the adapter element and can be moved out of an insertion position, in which they can be inserted into the longitudinal groove, and into an engagement position, in which they engage behind the undercut of the longitudinal groove, by a rotation, a pivoting and/or a displacement, characterized in that the engagement means can be brought out of the insertion position and into the engagement position by a movement of a housing, at least partly surrounding the adapter element, relative to the adapter element, with the housing being configured such that it can be supported at a groove environment of the longitudinal groove and can clamp the load bed between the engagement means and the housing and thus fixes the securing apparatus to the load bed.
An airfoil for a gas turbine, comprises a compound fillet disposed between the airfoil and a platform, wherein the compound fillet consists of a first arc and a second arc, a first end of the first arc tangentially adjoining an outer surface of the airfoil, a second end of the first arc tangentially adjoining a first end of the second arc, and a second end of the second arc tangentially adjoining a top surface of the platform, characterized in that the following equation is satisfied: 0.15 ≤ R 1 / s ≤ 0.45, and 0.09 ≤ a / s ≤ 0.27, 0.024 ≤ R 2 / s ≤ 0.072 where R1 represents the radius of the first arc, s represent the chord length of the airfoil, and a represents the distance between the point where the first end of the first arc adjoins the outer surface of the airfoil and the top surface of the platform in the direction along the extension of the outer surface of the airfoil and R2 represents the radius of the second arc.
A separating element for separating oil aerosol particles from raw gas, wherein the separating element features - at least one coalescence filter medium folded several times, in particular zigzag-folded, - at least one spacer associated with a respective fold of the coalescence filter medium and designed for spacing the respective longitudinal surfaces of said fold, and - at least one frame for accommodating the coalescence filter medium with the spacers integrated in the folds of the coalescence filter medium, wherein - respectively, one longitudinal surface of the filter medium folds forms the raw side of the filter medium folds and the other longitudinal surface of the filter medium folds forms the clean side of the filter medium folds, characterized in that - the spacer comprises at least one porous material, namely a phenolic resin-impregnated paper containing cellulose fibers, - the porous material of the spacer is spatially shaped and - the porous material of the spacer extends respectively over a flat area in such a way between the longitudinal surfaces of the filter medium fold allocated to it that at least one channel through which the raw gas can flow is provided between the fold tip and the fold valley of this filter medium fold. - at least one coalescence filter medium folded several times, in particular zigzag-folded, - at least one spacer associated with a respective fold of the coalescence filter medium and designed for spacing the respective longitudinal surfaces of said fold, and - at least one frame for accommodating the coalescence filter medium with the spacers integrated in the folds of the coalescence filter medium, - respectively, one longitudinal surface of the filter medium folds forms the raw side of the filter medium folds and the other longitudinal surface of the filter medium folds forms the clean side of the filter medium folds, - the spacer comprises at least one porous material, namely a phenolic resin-impregnated paper containing cellulose fibers, - the porous material of the spacer is spatially shaped and - the porous material of the spacer extends respectively over a flat area in such a way between the longitudinal surfaces of the filter medium fold allocated to it that at least one channel through which the raw gas can flow is provided between the fold tip and the fold valley of this filter medium fold.
An oligonucleotide which targets a Sialidase 4 natural antisense transcript for use as a therapeutic compound, wherein the oligonucleotide increases the expression of Sialidase 4.
Aircraft with an attachment structure and an equipment unit, the attachment structure comprising: a first attachment device (22, 22') extending in a longitudinal direction of the aircraft, wherein the first attachment device (22, 22') is attached to a stringer and to a frame and wherein the first attachment device (22, 22') has a first engagement element (48, 48'); a second attachment device (24, 24') attached to the equipment unit, wherein the second attachment device (24, 24') has a second engagement element (62, 62') adapted for engaging into the first engagement element, such that a force from the equipment unit in the longitudinal direction on the second attachment device (24, 24') is transferred via the second engagement element to the first engagement element and via the first attachment device (22, 22') to the stringer and the frame; wherein the equipment unit comprises a movable bin that is movable with respect to an outer structure which is attached to the aircraft, wherein the movable bin is movable between a closed position and an opened position; wherein the second attachment device is attached to the movable bin, such that the second engagement element engages the first engagement element in the closed position. a first attachment device (22, 22') extending in a longitudinal direction of the aircraft, wherein the first attachment device (22, 22') is attached to a stringer and to a frame and wherein the first attachment device (22, 22') has a first engagement element (48, 48'); a second attachment device (24, 24') attached to the equipment unit, wherein the second attachment device (24, 24') has a second engagement element (62, 62') adapted for engaging into the first engagement element, such that a force from the equipment unit in the longitudinal direction on the second attachment device (24, 24') is transferred via the second engagement element to the first engagement element and via the first attachment device (22, 22') to the stringer and the frame; wherein the equipment unit comprises a movable bin that is movable with respect to an outer structure which is attached to the aircraft, wherein the movable bin is movable between a closed position and an opened position; wherein the second attachment device is attached to the movable bin, such that the second engagement element engages the first engagement element in the closed position.
An integrated circuit, comprising: a first plurality of ring oscillators configured to implement, in part, a physically unclonable function; a second plurality of ring oscillators configured to implement, in part, an age sensor circuit; and a ring oscillator selection circuit coupled to the first plurality of ring oscillators and the second plurality of ring oscillators, the ring oscillator selection circuit adapted to select at least two ring oscillator outputs (324a, 324b) from at least one of the first plurality of ring oscillators and from at least one of the second plurality of ring oscillators, wherein the ring oscillator selection circuit is commonly shared by the PUF and the age sensor circuit. a first plurality of ring oscillators configured to implement, in part, a physically unclonable function; a second plurality of ring oscillators configured to implement, in part, an age sensor circuit; and a ring oscillator selection circuit coupled to the first plurality of ring oscillators and the second plurality of ring oscillators, the ring oscillator selection circuit adapted to select at least two ring oscillator outputs (324a, 324b) from at least one of the first plurality of ring oscillators and from at least one of the second plurality of ring oscillators, wherein the ring oscillator selection circuit is commonly shared by the PUF and the age sensor circuit.
A method for the synthesis of trimethylamine, comprising the step of: a) hydrogenating CO 2 in the presence of ammonia and/or an ammonia salt and in the presence of a Ruthenium-Phosphine-complex, whereby when ammonia is used additionally a Lewis acid is present a) hydrogenating CO 2 in the presence of ammonia and/or an ammonia salt and in the presence of a Ruthenium-Phosphine-complex, whereby when ammonia is used additionally a Lewis acid is present
Method for using a food cooking appliance, such as a meat grill, comprising at least one heating plate (61, 63) for heating the food in contact therewith, the method comprising - memorisation by the appliance of different internal cooking temperatures of the food, - in order to attain a greater or lesser degree of cooking of the food, sought by a user, selection by the user of one of said temperatures and placing the food in contact with the heating plate(s) (61, 63), and - measurement of the thickness of the food arranged against said heating plate (61, 63) and/or estimation of the surface area occupied by this food on the heating plate (61, 63), the method being characterised in that it comprises - a calculation of the cooking time of the food according to the temperature selected and according to the thickness of the food, and/or of the surface area occupied by the food. - memorisation by the appliance of different internal cooking temperatures of the food, - in order to attain a greater or lesser degree of cooking of the food, sought by a user, selection by the user of one of said temperatures and placing the food in contact with the heating plate(s) (61, 63), and - measurement of the thickness of the food arranged against said heating plate (61, 63) and/or estimation of the surface area occupied by this food on the heating plate (61, 63), - a calculation of the cooking time of the food according to the temperature selected and according to the thickness of the food, and/or of the surface area occupied by the food.
A method, in a wireless environment that includes a first device and a second device, the method characterized by: calculating, with an Intercell Interference Coordination, ICIC, mechanism, expected interferences associated with a plurality of resources; determining, with the ICIC mechanism, one of the plurality of resources with a low expected interference; receiving a classification of data as one of a Radio Resource Control, RRC, message or a non-RRC message; and allocating data classified as a Radio Resource Control, RRC, message to the one of the plurality of resources with the low expected interference. calculating, with an Intercell Interference Coordination, ICIC, mechanism, expected interferences associated with a plurality of resources; determining, with the ICIC mechanism, one of the plurality of resources with a low expected interference; receiving a classification of data as one of a Radio Resource Control, RRC, message or a non-RRC message; and allocating data classified as a Radio Resource Control, RRC, message to the one of the plurality of resources with the low expected interference.