mhurhangee/patent-ind-claim-en huggingface dataset:
Kenter shackle for anchor chains, at least comprising two half-elements that are able to be coupled together and a coupling block element that is insertable between the half-elements , wherein the half-elements each have an L-shaped or J-shaped configuration, in which, at the end of a short connecting leg , an external toothing (12.1) having a plurality of parallel toothing planes is formed, and in which, at the end of a long connecting leg , a receiving chamber is formed, which has an internal toothing (16.1) with a plurality of parallel toothing planes, into which the external toothing (12.1) of the short connecting leg engages, and wherein the connecting legs are connected together via a curved clasp , characterized in that the receiving chamber in the long leg is widened above a central plane (M) by a cavity , wherein the central plane (M) extends along the end face of the external toothing (12.1) of the short leg and above the uppermost toothing plane, facing the clasp , of the internal toothing (16.1), and in that the lateral flank (17.1) of the cavity transitions by way of a rounded portion into a top region of the cavity . wherein the half-elements each have an L-shaped or J-shaped configuration, in which, at the end of a short connecting leg , an external toothing (12.1) having a plurality of parallel toothing planes is formed, and in which, at the end of a long connecting leg , a receiving chamber is formed, which has an internal toothing (16.1) with a plurality of parallel toothing planes, into which the external toothing (12.1) of the short connecting leg engages, and wherein the connecting legs are connected together via a curved clasp , characterized in that the receiving chamber in the long leg is widened above a central plane (M) by a cavity , wherein the central plane (M) extends along the end face of the external toothing (12.1) of the short leg and above the uppermost toothing plane, facing the clasp , of the internal toothing (16.1), and in that the lateral flank (17.1) of the cavity transitions by way of a rounded portion into a top region of the cavity .
A mobile device comprising: a communication interface ; a memory storing one or more instructions; and a processor configured to execute the one or more instructions stored in the memory to: connect, through the communication interface , to an electronic device that is to be wirelessly connected to an access point ,AP, obtain an AP list including one or more WLAN or WiFi APs with which the mobile device has a history of being connected, receive a list of scanned WLAN or WiFi APs including one or more scanned APs from the electronic device obtained by performing WLAN or WiFi channel scanning, compare the AP list including one or more APs having the history of being connected with the list of scanned APs including one or more scanned APs, identify one or more matched APs as candidate APs, and create a candidate AP list including information about the one or more selected APs identified as the candidate APs, and transmit, to the electronic device , the candidate AP list and information about a home AP to which the mobile device is currently connected. a communication interface ; a memory storing one or more instructions; and a processor configured to execute the one or more instructions stored in the memory to: connect, through the communication interface , to an electronic device that is to be wirelessly connected to an access point ,AP, obtain an AP list including one or more WLAN or WiFi APs with which the mobile device has a history of being connected, receive a list of scanned WLAN or WiFi APs including one or more scanned APs from the electronic device obtained by performing WLAN or WiFi channel scanning, compare the AP list including one or more APs having the history of being connected with the list of scanned APs including one or more scanned APs, identify one or more matched APs as candidate APs, and create a candidate AP list including information about the one or more selected APs identified as the candidate APs, and transmit, to the electronic device , the candidate AP list and information about a home AP to which the mobile device is currently connected. connect, through the communication interface , to an electronic device that is to be wirelessly connected to an access point ,AP, obtain an AP list including one or more WLAN or WiFi APs with which the mobile device has a history of being connected, receive a list of scanned WLAN or WiFi APs including one or more scanned APs from the electronic device obtained by performing WLAN or WiFi channel scanning, compare the AP list including one or more APs having the history of being connected with the list of scanned APs including one or more scanned APs, identify one or more matched APs as candidate APs, and create a candidate AP list including information about the one or more selected APs identified as the candidate APs, and transmit, to the electronic device , the candidate AP list and information about a home AP to which the mobile device is currently connected.
An elastic sensor patch comprising - an elastic and electrically isolating film layer with a stretchability of at least 100% in all directions in a plane of the film layer (X, Y), and - a plurality of elastic measurement strips attached to the elastic film layer , wherein each elastic measurement strip comprises an oblong capacitive strip with a dielectric electro-active polymer which has a stretchability of at least 50% in its length direction, characterized in that the sensor patch comprises a first number of at least two elastic measurement strips , which are oriented mutually parallel to each other in a first direction and lie at a distance from each other in the range of 3 mm to 100 mm, and a second number of at least two elastic measurement strips , which are oriented mutually parallel to each other in a second direction which intersects the first direction, wherein each elastic measurement strip comprises two electrically conductive metal film layers attached to opposite sides of the oblong capacitive strip with the dielectric electro-active polymer, wherein the two metal film layers have a geometric form which allows elastic elongation without breaking the metal film. - an elastic and electrically isolating film layer with a stretchability of at least 100% in all directions in a plane of the film layer (X, Y), and - a plurality of elastic measurement strips attached to the elastic film layer , wherein each elastic measurement strip comprises an oblong capacitive strip with a dielectric electro-active polymer which has a stretchability of at least 50% in its length direction, characterized in that the sensor patch comprises a first number of at least two elastic measurement strips , which are oriented mutually parallel to each other in a first direction and lie at a distance from each other in the range of 3 mm to 100 mm, and a second number of at least two elastic measurement strips , which are oriented mutually parallel to each other in a second direction which intersects the first direction, wherein each elastic measurement strip comprises two electrically conductive metal film layers attached to opposite sides of the oblong capacitive strip with the dielectric electro-active polymer, wherein the two metal film layers have a geometric form which allows elastic elongation without breaking the metal film.
An edge crack detection apparatus for detecting an edge crack of a metal plate (S) being conveyed, the edge crack detection apparatus comprising: a detection part including a plurality of elements arranged along a plate width direction of the metal plate (S), each of the plurality of elements being configured to be capable of detecting presence or absence of the metal plate (S) at a position of the element in the plate width direction; a plate edge position determination part configured to determine a plate edge position of the metal plate (S) in the plate width direction on the basis of a detection result of each of a plurality of first elements positioned within a first region (R1) in the plate width direction, from among the plurality of elements ; and an edge crack detection part configured to detect an edge crack of the metal plate (S) on the basis of a detection result of each of a plurality of second elements selected on the basis of the plate edge position and positioned within a second region (R2) which is narrower than the first region (R1) in the plate width direction, from among the plurality of elements , characterized in that the plate edge position determination part is configured to obtain the detection result by each of the plurality of first elements at intervals of a first cycle time (T1) and determine the plate edge position on the basis of the detection result, and the edge crack detection part is configured to obtain the detection result by each of the plurality of second elements at intervals of a second cycle time (T2) which is shorter than the first cycle time (T1). a detection part including a plurality of elements arranged along a plate width direction of the metal plate (S), each of the plurality of elements being configured to be capable of detecting presence or absence of the metal plate (S) at a position of the element in the plate width direction; a plate edge position determination part configured to determine a plate edge position of the metal plate (S) in the plate width direction on the basis of a detection result of each of a plurality of first elements positioned within a first region (R1) in the plate width direction, from among the plurality of elements ; and an edge crack detection part configured to detect an edge crack of the metal plate (S) on the basis of a detection result of each of a plurality of second elements selected on the basis of the plate edge position and positioned within a second region (R2) which is narrower than the first region (R1) in the plate width direction, from among the plurality of elements , characterized in that the plate edge position determination part is configured to obtain the detection result by each of the plurality of first elements at intervals of a first cycle time (T1) and determine the plate edge position on the basis of the detection result, and the edge crack detection part is configured to obtain the detection result by each of the plurality of second elements at intervals of a second cycle time (T2) which is shorter than the first cycle time (T1).
An aircraft engine comprising two concentric shafts extending in an engine axial direction, a bearing supporting a first of the shafts , and a support connecting the bearing to a second of the shafts , characterised in that the support comprises a mechanical decoupler, mainly consisting of a rigid body , in abutment through two opposite faces in an engine radial direction, perpendicular to the axial direction, on two abutting faces integral with the second shaft and the bearing respectively, the rigid body being able to be ruptured at a load threshold to be transmitted between the abutting faces, and a damper body housed in a cavity of the support delimited by the abutting faces.
A piezoelectric speaker-forming laminate comprising: a piezoelectric film ; a pressure-sensitive adhesive face ; an interposed layer being a porous body layer and/or a resin layer disposed between the piezoelectric film and the pressure-sensitive adhesive face; and a release layer joined to the pressure-sensitive adhesive face, wherein the pressure-sensitive adhesive face is disposed in such a manner that at least a portion of the piezoelectric film overlaps the pressure-sensitive adhesive face when the piezoelectric film is viewed in plan, and characterized in that the release layer includes a film and a release agent applied to a principal surface on the pressure-sensitive adhesive face side of the film, and in that the release layer is configured to be removed from the piezoelectric speaker-forming laminate to allow fixing of the piezoelectric film and the interposed layer to a support as a piezoelectric speaker or a portion of a piezoelectric speaker by sticking the pressure-sensitive adhesive face to the support. a piezoelectric film ; a pressure-sensitive adhesive face ; an interposed layer being a porous body layer and/or a resin layer disposed between the piezoelectric film and the pressure-sensitive adhesive face; and a release layer joined to the pressure-sensitive adhesive face, wherein the pressure-sensitive adhesive face is disposed in such a manner that at least a portion of the piezoelectric film overlaps the pressure-sensitive adhesive face when the piezoelectric film is viewed in plan, and characterized in that the release layer includes a film and a release agent applied to a principal surface on the pressure-sensitive adhesive face side of the film, and in that the release layer is configured to be removed from the piezoelectric speaker-forming laminate to allow fixing of the piezoelectric film and the interposed layer to a support as a piezoelectric speaker or a portion of a piezoelectric speaker by sticking the pressure-sensitive adhesive face to the support.
A fitting for windows, doors or the like, having a gear which comprises: a gear housing ; an input element which is rotatably supported about an axis of rotation (R) in the gear housing and which has a receiver for an actuation mechanism connection element such as a square pin; an output element which is coupled or couplable to a connecting rod and which can be driven to make a displacement movement by the rotation of the input element ; and a fixing element which, in a delivery state of the fitting, is held at the gear housing , on the one hand, and engages into a recess of the input element , on the other hand, in order to fix the input element in a predefined rotational position in this manner, wherein the fixing element projects into the receiver of the input element and, to establish an operating state of the fitting, said fixing element can be released from the gear housing by the action of an actuation mechanism connection element to be inserted into the receiver ; and wherein the fixing element can be released from the gear housing while tilting or pivoting, characterized in that , due to the action of the actuation mechanism connection element , the fixing element released from the gear housing can be moved into the receiver in a tilt movement or pivot movement about a tilt axis (S). a gear housing ; an input element which is rotatably supported about an axis of rotation (R) in the gear housing and which has a receiver for an actuation mechanism connection element such as a square pin; an output element which is coupled or couplable to a connecting rod and which can be driven to make a displacement movement by the rotation of the input element ; and a fixing element which, in a delivery state of the fitting, is held at the gear housing , on the one hand, and engages into a recess of the input element , on the other hand, in order to fix the input element in a predefined rotational position in this manner, wherein the fixing element projects into the receiver of the input element and, to establish an operating state of the fitting, said fixing element can be released from the gear housing by the action of an actuation mechanism connection element to be inserted into the receiver ; and wherein the fixing element can be released from the gear housing while tilting or pivoting, characterized in that , due to the action of the actuation mechanism connection element , the fixing element released from the gear housing can be moved into the receiver in a tilt movement or pivot movement about a tilt axis (S).
Computer-implemented method for computing a transition parameter of a liquefied gas storage medium, the storage medium comprising at least one sealed and unrefrigerated tank (2, 4, 5, 6, 7 or 11) equipped with a safety valve , the transition parameter characterizing an evolution of a two-phase mixture contained in the sealed and unrefrigerated tank between an initial state and a final state , the two-phase mixture including a liquid phase and a vapour phase, wherein said transition parameter is selected in a group consisting of a duration of the transition τ , a liquid bleeding rate ṁ l or a vapour bleeding rate ṁ v , the method comprising the steps of: - determining, for the liquid phase and the vapour phase in the initial state , initial mass densities ρ l,i and ρ v,j , and initial internal mass energies U l,i and U v,i on the basis of an initial liquid phase temperature T l,i , an initial vapour phase temperature T v,i , an initial vapour phase pressure P i , an initial liquid phase volume V l,i and an initial liquid phase composition x l,i ; - determining, for the liquid phase and the vapour phase in the final state , final mass densities ρ l,f and ρ v,f , final internal mass energies U l,f and U v,f , and final mass enthalpies H l,f and H v,f on the basis of an equation of state and a final vapour phase pressure P f , the final pressure of the vapour phase P f being less than or equal to the setting pressure of the safety valve and greater than or equal to the initial pressure of the vapour phase P i ; - computing the transition parameter using the following equation: τ Q ̇ + m ̇ v H v , f − U ̅ + m ̇ l H l , f − U ̅ = ρ l , i V l , i U ̅ − U l , i + ρ v , i V t − V l , i U ̅ − U v , i + ρ v , f V t U v , f − U ̅ in which Q̇ corresponds to an energy contribution by heat ingress through the walls of a tank per unit of time, V t corresponds to a total volume of the tank and with U ̅ = ρ l , f U l , f − ρ v , f U v , f ρ l , f − ρ v , f . - determining, for the liquid phase and the vapour phase in the initial state , initial mass densities ρ l,i and ρ v,j , and initial internal mass energies U l,i and U v,i on the basis of an initial liquid phase temperature T l,i , an initial vapour phase temperature T v,i , an initial vapour phase pressure P i , an initial liquid phase volume V l,i and an initial liquid phase composition x l,i ; - determining, for the liquid phase and the vapour phase in the final state , final mass densities ρ l,f and ρ v,f , final internal mass energies U l,f and U v,f , and final mass enthalpies H l,f and H v,f on the basis of an equation of state and a final vapour phase pressure P f , the final pressure of the vapour phase P f being less than or equal to the setting pressure of the safety valve and greater than or equal to the initial pressure of the vapour phase P i ; - computing the transition parameter using the following equation: τ Q ̇ + m ̇ v H v , f − U ̅ + m ̇ l H l , f − U ̅ = ρ l , i V l , i U ̅ − U l , i + ρ v , i V t − V l , i U ̅ − U v , i + ρ v , f V t U v , f − U ̅
A method for landing site localization, the method comprising: receiving an image capturing a landing site from a field of view of an aircraft, the image having an associated time stamp; determining a reference position of a reference object associated with the landing site; from the reference position, generating an image-estimated pose of the aircraft; matching the image-estimated pose with a first inertial measurement unit, IMU, output having a time stamp nearest to the time stamp associated with the image; updating a pose trajectory of the aircraft by forward propagating components of the image-estimated pose to a set of IMU outputs generated subsequently to the first IMU output; and based upon the updated pose trajectory, generating a set of computer-readable instructions for flight control of the aircraft toward a flight path to the landing site. receiving an image capturing a landing site from a field of view of an aircraft, the image having an associated time stamp; determining a reference position of a reference object associated with the landing site; from the reference position, generating an image-estimated pose of the aircraft; matching the image-estimated pose with a first inertial measurement unit, IMU, output having a time stamp nearest to the time stamp associated with the image; updating a pose trajectory of the aircraft by forward propagating components of the image-estimated pose to a set of IMU outputs generated subsequently to the first IMU output; and based upon the updated pose trajectory, generating a set of computer-readable instructions for flight control of the aircraft toward a flight path to the landing site.
A soundproof structure , comprising: a sheet member having a plurality of through-holes passing therethrough in a thickness direction; and a sound absorbing body disposed in contact with one main surface of the sheet member, wherein an average opening diameter of the through-holes is 0.1 μm or more and less than 100 μm, a parameter A expressed by A = σ × φ 2 is 92 or less assuming that the average opening diameter of the through-holes is φ μm and an average opening ratio of the through-holes is σ, the soundproof structure characterised in that a shape of at least some of the through-holes is a shape in which a hole diameter increases not at the outermost surface of the through-hole but inside the through-hole so as to have a maximum diameter inside the through-hole, and a surface roughness Ra of the inner wall surface of the through-hole is 0.1 μm to 10.0 μm. a sheet member having a plurality of through-holes passing therethrough in a thickness direction; and a sound absorbing body disposed in contact with one main surface of the sheet member, wherein an average opening diameter of the through-holes is 0.1 μm or more and less than 100 μm, a parameter A expressed by A = σ × φ 2 is 92 or less assuming that the average opening diameter of the through-holes is φ μm and an average opening ratio of the through-holes is σ, the soundproof structure characterised in that a shape of at least some of the through-holes is a shape in which a hole diameter increases not at the outermost surface of the through-hole but inside the through-hole so as to have a maximum diameter inside the through-hole, and a surface roughness Ra of the inner wall surface of the through-hole is 0.1 μm to 10.0 μm.
A method for displaying a graphical user interface, GUI, on a touch screen comprising a display unit in an apparatus further comprising a tactile sensor unit different from a touch sensor unit included in the touch screen , the tactile sensor unit being located on a lateral side of the apparatus , the method comprising: detecting (S210) a contact of the tactile sensor unit ; determining (S220) a contact pattern from the detected contact; displaying (S240) the GUI based on the contact pattern; and characterised in detecting, after displaying (S240) the GUI based on the contact pattern, an increase of contact pressure of the tactile sensor unit , and changing a location or display size of the GUI elements according to the pressure of the detected contact and execute a specific application when the pressure increases beyond a predetermined threshold. detecting (S210) a contact of the tactile sensor unit ; determining (S220) a contact pattern from the detected contact; displaying (S240) the GUI based on the contact pattern; and characterised in detecting, after displaying (S240) the GUI based on the contact pattern, an increase of contact pressure of the tactile sensor unit , and changing a location or display size of the GUI elements according to the pressure of the detected contact and execute a specific application when the pressure increases beyond a predetermined threshold.