mhurhangee/patent-ind-claim-en huggingface dataset:
Aircraft comprising: - a fuselage (F); - a set of electrical generators, comprising at least a first electrical generator (G1) and a second electrical generator (G2); - a set of electrical equipment items (40a ... 40j), distributed in the fuselage; and - an electrical power distribution network comprising: - a set of buses, comprising at least a first bus and a second bus ; and - a switching system , characterized in that : - each bus of the set of buses extends, at least partly, in a longitudinal direction of the fuselage (F); - the first bus and the second bus follow segregated paths in the fuselage; - the switching system is linked electrically to the first electrical generator (G1) and to the second electrical generator (G2), and to the first bus and to the second bus ; - the switching system comprises a so-called normal mode of operation, in which it is configured to electrically link the first electrical generator (G1) to the first bus and the second electrical generator (G2) to the second bus ; - each bus of the set of buses comprises connection points at different locations distributed along its length; and - each of the electrical equipment items of the set of electrical equipment items (40a ... 40j) is linked to a connection point of a single bus of the set of buses, via a local electrical power supply link . - a fuselage (F); - a set of electrical generators, comprising at least a first electrical generator (G1) and a second electrical generator (G2); - a set of electrical equipment items (40a ... 40j), distributed in the fuselage; and - an electrical power distribution network comprising: - a set of buses, comprising at least a first bus and a second bus ; and - a switching system , - a set of buses, comprising at least a first bus and a second bus ; and - a switching system , - each bus of the set of buses extends, at least partly, in a longitudinal direction of the fuselage (F); - the first bus and the second bus follow segregated paths in the fuselage; - the switching system is linked electrically to the first electrical generator (G1) and to the second electrical generator (G2), and to the first bus and to the second bus ; - the switching system comprises a so-called normal mode of operation, in which it is configured to electrically link the first electrical generator (G1) to the first bus and the second electrical generator (G2) to the second bus ; - each bus of the set of buses comprises connection points at different locations distributed along its length; and - each of the electrical equipment items of the set of electrical equipment items (40a ... 40j) is linked to a connection point of a single bus of the set of buses, via a local electrical power supply link .
An axle assembly which is designed and intended to be used in a heavy-duty vehicle , the axle assembly comprising: • a pivot bearing having a substantially vertically extending steering axis of rotation (X), • a bogie rotatably arranged about the steering axis of rotation (X), • a rocker mounted on the bogie so as to be pivotable about a substantially horizontally extending pivot axis (Y), • a wheel carrier operatively connected to the rocker having at least one wheel rotatably mounted thereon about a wheel axis of rotation (Z), the wheel axis of rotation (Z) extending substantially horizontally and, when driving straight ahead, substantially transversely to the direction of travel (V), and • a pneumatically actuatable power device , which is supported at one end on the bogie or on a part connected thereto and at the other end on the rocker or on a part connected thereto, wherein the wheel carrier is arranged on a portion of the rocker which is located between a free end of the rocker and the end thereof pivotably connected to the bogie, and in that the pneumatically actuatable power device is supported on the free end of the rocker or on the rocker adjacent to this free end, characterised in that the wheel carrier is pivotably attached to the rocker about a pivot axis (W) extending substantially parallel to the longitudinal extension direction of the rocker . • a pivot bearing having a substantially vertically extending steering axis of rotation (X), • a bogie rotatably arranged about the steering axis of rotation (X), • a rocker mounted on the bogie so as to be pivotable about a substantially horizontally extending pivot axis (Y), • a wheel carrier operatively connected to the rocker having at least one wheel rotatably mounted thereon about a wheel axis of rotation (Z), the wheel axis of rotation (Z) extending substantially horizontally and, when driving straight ahead, substantially transversely to the direction of travel (V), and • a pneumatically actuatable power device , which is supported at one end on the bogie or on a part connected thereto and at the other end on the rocker or on a part connected thereto, wherein the wheel carrier is arranged on a portion of the rocker which is located between a free end of the rocker and the end thereof pivotably connected to the bogie, and in that the pneumatically actuatable power device is supported on the free end of the rocker or on the rocker adjacent to this free end, characterised in that the wheel carrier is pivotably attached to the rocker about a pivot axis (W) extending substantially parallel to the longitudinal extension direction of the rocker . wherein the wheel carrier is arranged on a portion of the rocker which is located between a free end of the rocker and the end thereof pivotably connected to the bogie, and in that the pneumatically actuatable power device is supported on the free end of the rocker or on the rocker adjacent to this free end, characterised in that the wheel carrier is pivotably attached to the rocker about a pivot axis (W) extending substantially parallel to the longitudinal extension direction of the rocker .
System building block for constructing a splinter protection wall for a potentially explosive installation and/or a potentially explosive hazardous material, comprising a rectangular base surface provided with recesses, two opposing fluid-permeable rectangular side faces aligned perpendicularly to the base surface and a top surface provided with knobs , wherein the knobs are dimensioned and arranged corresponding to the recesses, so that a plurality of system building blocks can be stacked in an assembly to form a fluid-permeable wall and/or a fluid-permeable cage comprising interconnected walls.
A diffractive element comprising: a substrate a plurality of grating elements on the substrate each grating element having a u-shaped cross section comprising: a first ridge region ; a second ridge region ; and a saddle region extending between the first and second ridge regions, the saddle region having a first height, H 1 , lower than a second height, H 3 , of the first and second ridge regions; wherein the first ridge region comprises a first ridge body region with a first refractive index n 2 , and a first core element inside the first ridge body region, the first core element having a second refractive index, n 4 , greater than the first refractive index; and the second ridge region comprises a second ridge body region with the first refractive index n 2 , and a second core element inside the second ridge body region, the second core element having the second refractive index, n 4 . a substrate a plurality of grating elements on the substrate each grating element having a u-shaped cross section comprising: a first ridge region ; a second ridge region ; and a saddle region extending between the first and second ridge regions, the saddle region having a first height, H 1 , lower than a second height, H 3 , of the first and second ridge regions; a first ridge region ; a second ridge region ; and a saddle region extending between the first and second ridge regions, the saddle region having a first height, H 1 , lower than a second height, H 3 , of the first and second ridge regions; wherein the first ridge region comprises a first ridge body region with a first refractive index n 2 , and a first core element inside the first ridge body region, the first core element having a second refractive index, n 4 , greater than the first refractive index; and the second ridge region comprises a second ridge body region with the first refractive index n 2 , and a second core element inside the second ridge body region, the second core element having the second refractive index, n 4 .
A user equipment apparatus , configured to: store a core network element identifier; add said core network element identifier and a layer 3, L3, message to a Radio Resource Control, RRC, message for initiating a connection between the user equipment and a core network element ; and send said RRC message comprising said core network element identifier and said L3 message over a radio connection to a network element of a radio access network to establish a connection to one of a set of core network elements to which said apparatus will connect, the core network element identifier for selecting a core network element from a list of core network elements to connect to said user equipment. store a core network element identifier; add said core network element identifier and a layer 3, L3, message to a Radio Resource Control, RRC, message for initiating a connection between the user equipment and a core network element ; and send said RRC message comprising said core network element identifier and said L3 message over a radio connection to a network element of a radio access network to establish a connection to one of a set of core network elements to which said apparatus will connect, the core network element identifier for selecting a core network element from a list of core network elements to connect to said user equipment.
A method for assembling dopant molecules on the surface of a two-dimensional material formed on a substrate , the method comprises: - forming a spacer layer comprising at least one of an electrically insulating compound or a semiconductor compound on the surface of the two-dimensional material, the compound of the spacer layer is adapted to allow for the diffusion of dopant molecules through the compound during an annealing process, - depositing dopant molecules on the spacer layer, - annealing the substrate with spacer layer and the molecules at an elevated temperature above room temperature for an annealing time duration, wherein the elevated temperature and annealing time duration depend on the compound of the spacer layer and properties of the dopant molecules, and are such that at least a portion of the dopant molecules diffuse through the spacer layer towards the surface of the two-dimensional material during the annealing time duration to assemble on the surface of the two-dimensional material to thereby dope the two-dimensional material and cause an increase of the mobility of the two-dimensional material. - forming a spacer layer comprising at least one of an electrically insulating compound or a semiconductor compound on the surface of the two-dimensional material, the compound of the spacer layer is adapted to allow for the diffusion of dopant molecules through the compound during an annealing process, - depositing dopant molecules on the spacer layer, - annealing the substrate with spacer layer and the molecules at an elevated temperature above room temperature for an annealing time duration, wherein the elevated temperature and annealing time duration depend on the compound of the spacer layer and properties of the dopant molecules, and are such that at least a portion of the dopant molecules diffuse through the spacer layer towards the surface of the two-dimensional material during the annealing time duration to assemble on the surface of the two-dimensional material to thereby dope the two-dimensional material and cause an increase of the mobility of the two-dimensional material.
A method for displaying information to an aircraft pilot during actual or simulated flight, the method being performed by a computer system, the method comprising: causing a cockpit display to display an aircraft symbol representing a portion of an aircraft; receiving data representing a current angle of a throttle lever of the aircraft, a current altitude of the aircraft, a current aircraft weight of the aircraft, a current pitch attitude of the aircraft and a current flap setting of the aircraft; causing said cockpit display to display a horizon indicator having a position relative to said aircraft symbol which is a function of said current pitch attitude; determining a display mode of the cockpit display as a function of at least said current angle of said throttle lever and said current flap setting, wherein said determined display mode is one of Maximum Climb, Idle Descent, Level Flight and -3 Degree Glideslope; determining a target pitch attitude as a function of at least said determined display mode of the cockpit display, said current altitude and said current aircraft weight; and causing said cockpit display to display first symbology representing said target pitch attitude, said displayed first symbology having a position relative to said aircraft symbol which is a function of a difference between said current pitch attitude and said target pitch attitude, wherein said first symbology is displayed when primary air data is unavailable or unreliable. causing a cockpit display to display an aircraft symbol representing a portion of an aircraft; receiving data representing a current angle of a throttle lever of the aircraft, a current altitude of the aircraft, a current aircraft weight of the aircraft, a current pitch attitude of the aircraft and a current flap setting of the aircraft; causing said cockpit display to display a horizon indicator having a position relative to said aircraft symbol which is a function of said current pitch attitude; determining a display mode of the cockpit display as a function of at least said current angle of said throttle lever and said current flap setting, wherein said determined display mode is one of Maximum Climb, Idle Descent, Level Flight and -3 Degree Glideslope; determining a target pitch attitude as a function of at least said determined display mode of the cockpit display, said current altitude and said current aircraft weight; and causing said cockpit display to display first symbology representing said target pitch attitude, said displayed first symbology having a position relative to said aircraft symbol which is a function of a difference between said current pitch attitude and said target pitch attitude, wherein said first symbology is displayed when primary air data is unavailable or unreliable.
An implantable prosthetic valve comprising: an annular frame having a plurality of frame members; and a skirt assembly comprising a laminate having a fabric layer sandwiched between a first covering member and a second covering member , wherein the fabric layer is exposed at one or more windows in the second covering member ; wherein the skirt assembly is coupled to the annular frame by a suture extending through the fabric layer at the one or more windows and around at least one of the plurality of frame members. an annular frame having a plurality of frame members; and a skirt assembly comprising a laminate having a fabric layer sandwiched between a first covering member and a second covering member , wherein the fabric layer is exposed at one or more windows in the second covering member ; wherein the skirt assembly is coupled to the annular frame by a suture extending through the fabric layer at the one or more windows and around at least one of the plurality of frame members.
A shaving cartridge comprising: a housing having a top surface , a bottom surface , a front edge , a rear edge , and a pair of side edges extending between the front edge and the rear edge , the housing having at least one blade disposed between the front edge and the rear edge , the at least one blade having a cutting edge; and a pair of substantially c-shaped retainers each having a top portion , a bottom portion , a substantially convex portion connecting the top portion to the bottom portion , wherein the top portion of each of the retainers is substantially planar and the bottom portion of each of the retainers is curved, characterized in that the retainers are positioned on the pair of side edges and extend along the pair of side edges between the front edge of the housing and the rear edge of the housing and in that inner surfaces of the substantially convex portions of the pair of substantially c-shaped retainers are facing each other, when mounted to the shaving cartridge . a housing having a top surface , a bottom surface , a front edge , a rear edge , and a pair of side edges extending between the front edge and the rear edge , the housing having at least one blade disposed between the front edge and the rear edge , the at least one blade having a cutting edge; and a pair of substantially c-shaped retainers each having a top portion , a bottom portion , a substantially convex portion connecting the top portion to the bottom portion , wherein the top portion of each of the retainers is substantially planar and the bottom portion of each of the retainers is curved, characterized in that the retainers are positioned on the pair of side edges and extend along the pair of side edges between the front edge of the housing and the rear edge of the housing and in that inner surfaces of the substantially convex portions of the pair of substantially c-shaped retainers are facing each other, when mounted to the shaving cartridge .
A pierceable cap comprising: a shell ; an access port in the shell adapted to allow passage of at least part of a transfer device through the access port; a frangible seal , characterized in that the frangible seal comprises at least two intersecting ribs and a collar , wherein the intersecting ribs each extend from the collar to a bottom surface of the frangible seal having an intersecting openable or tearable portion and comprise end wall and sidewall portions ; and in that the end wall and sidewall portions extend simultaneously inward in a radial direction and downward in an axial direction, such that surfaces of the end wall and sidewall portions are not parallel to an inside surface of a sample vessel when such vessel has been disposed within the shell . a shell ; an access port in the shell adapted to allow passage of at least part of a transfer device through the access port; a frangible seal , characterized in that the frangible seal comprises at least two intersecting ribs and a collar , wherein the intersecting ribs each extend from the collar to a bottom surface of the frangible seal having an intersecting openable or tearable portion and comprise end wall and sidewall portions ; and in that the end wall and sidewall portions extend simultaneously inward in a radial direction and downward in an axial direction, such that surfaces of the end wall and sidewall portions are not parallel to an inside surface of a sample vessel when such vessel has been disposed within the shell .
A transport belt unit for a dynamic checkweigher, comprising a support frame , and a belt body connected to the support frame and adapted to transport an object, with with rollers arranged at the ends of the belt body located in the transport direction (T) and against the transport direction (T), and with a transport belt stretched over the rollers , wherein the transport belt is driven by means of a motor via one of the two rollers , wherein the transport belt unit further comprises a configuration change mechanism acting between the belt body and the support frame , which is adapted so that the conveyor belt unit is switched between a non-operational configuration and an operational configuration upon actuation of the configuration change mechanism, and wherein the configuration changing mechanism comprises at least one swivel joint element , characterized in that the swivel joint element consists of two joint legs which are connected to one another via a thin point , the thin point enabling a relative rotational movement of the joint legs with respect to one another about an axis of rotation defined by the thin point , and in that the swivel joint element is attached to the belt body by means of one joint leg and to the support frame by means of the other joint leg , thereby enabling the belt body to pivot relative to the support frame from the operational configuration to the non-operational configuration and back. a support frame , and a belt body connected to the support frame and adapted to transport an object, with with rollers arranged at the ends of the belt body located in the transport direction (T) and against the transport direction (T), and with a transport belt stretched over the rollers , wherein the transport belt is driven by means of a motor via one of the two rollers , wherein the transport belt unit further comprises a configuration change mechanism acting between the belt body and the support frame , which is adapted so that the conveyor belt unit is switched between a non-operational configuration and an operational configuration upon actuation of the configuration change mechanism, and wherein the configuration changing mechanism comprises at least one swivel joint element , characterized in that the swivel joint element consists of two joint legs which are connected to one another via a thin point , the thin point enabling a relative rotational movement of the joint legs with respect to one another about an axis of rotation defined by the thin point , and in that the swivel joint element is attached to the belt body by means of one joint leg and to the support frame by means of the other joint leg , thereby enabling the belt body to pivot relative to the support frame from the operational configuration to the non-operational configuration and back.