mhurhangee/patent-ind-claim-en huggingface dataset:
Method for transmitting data in an IP network having a core network that has multiple network nodes (3 1 - 3 n ) and at least two independent network levels (A, B) of identical structure and whose network nodes (3 1 - 3 n ) are each connected among one another within the network levels (A, B) by cables forming network edges (4 1 - 4 n ), and having in each case multiple access networks (2 1 - 2 n ) that are interfaced to in each case all network levels (A, B) of the core network at the network nodes (3 1 - 3 n ) and whose data streams to be supplied to the core network are split, in terms of the data rate, over all network levels (A, B) of the core network , wherein the interaction of network elements of the IP network is controlled by a network management system and the function of the individual network elements is controlled by an element management system and wherein an error-affected network edge (4 1 - 4 n ) of the core network , following a restoration of data paths using this network edge (4 1 - 4 n ) for data transmission, continues to be useable at a decreased data transmission rate on account of network elements of at least the core network being equipped with interfaces having a flexible data transmission rate, characterized in that the error in the core network and the consequently decreased capacity, in respect of the available data transmission rate, of the affected network edge (4 1 - 4 n ) in the respective transition region between the core network and the access networks (2 1 - 2 n ) interfaced to the core network at the network nodes (3 1 - 3 n ) connected by the affected network edge (4 1 - 4 n ) are reacted to by means of a change in the load distribution by virtue of a) the network management system transmitting information about the error that has occurred at the network edge (4 1 - 4 n ) and the decreased capacity, in respect of the data transmission rate, of said network edge to the element management system in real time, and b) the element management system actuating network elements of the IP network on the physical level or on the IP level such that the data rate supplied to the network level (A, B) affected by the error is reduced, to the detriment of the at least one other network level (A, B), at least at each of the network nodes (3 1 - 3 n ) connected by the erroneous network edge (4 1 - 4 n ). a) the network management system transmitting information about the error that has occurred at the network edge (4 1 - 4 n ) and the decreased capacity, in respect of the data transmission rate, of said network edge to the element management system in real time, and b) the element management system actuating network elements of the IP network on the physical level or on the IP level such that the data rate supplied to the network level (A, B) affected by the error is reduced, to the detriment of the at least one other network level (A, B), at least at each of the network nodes (3 1 - 3 n ) connected by the erroneous network edge (4 1 - 4 n ).
A parking assistance device configured to assist a parking operation in which a vehicle is guided along a vehicle passage from a parking start position (Pa) via a reversing position (Pb) and perpendicularly parked in a parkable area (G), comprising: an attitude angle look-up circuit configured to look up attitude angles (θM) of the vehicle at the reversing position (Pb) with respect to a travel direction (Da) of the vehicle at the parking start position (Pa); a route generating circuit configured to generate a route along which the vehicle is to travel from the parking start position (Pa) to the parkable area (G) via the reversing position (Pb) according to the attitude angle set by use of the attitude angle look-up circuit ; a vehicle passage width obtaining circuit configured to obtain a width (WR) of a vehicle passage which the parkable area (G) faces; wherein the attitude look-up circuit determines whether the front portion of the vehicle will interfere with an obstacle (Ob1) adjacent to the vehicle passage in the width direction of the vehicle passage according to the width of the vehicle passage and the reversing position (Pb) on the route generated by the route generating circuit in response to the looked-up attitude angle, and characterized in that when it is determined that the front portion of the vehicle will interfere with the obstacle (Ob1), the attitude look-up circuit repeatedly looks up the attitude angle in a descending order starting from an attitude angle (θ F ) at a completion of parking until the generated route does not interfere with the obstacle (Ob1). an attitude angle look-up circuit configured to look up attitude angles (θM) of the vehicle at the reversing position (Pb) with respect to a travel direction (Da) of the vehicle at the parking start position (Pa); a route generating circuit configured to generate a route along which the vehicle is to travel from the parking start position (Pa) to the parkable area (G) via the reversing position (Pb) according to the attitude angle set by use of the attitude angle look-up circuit ; a vehicle passage width obtaining circuit configured to obtain a width (WR) of a vehicle passage which the parkable area (G) faces; wherein the attitude look-up circuit determines whether the front portion of the vehicle will interfere with an obstacle (Ob1) adjacent to the vehicle passage in the width direction of the vehicle passage according to the width of the vehicle passage and the reversing position (Pb) on the route generated by the route generating circuit in response to the looked-up attitude angle, and characterized in that when it is determined that the front portion of the vehicle will interfere with the obstacle (Ob1), the attitude look-up circuit repeatedly looks up the attitude angle in a descending order starting from an attitude angle (θ F ) at a completion of parking until the generated route does not interfere with the obstacle (Ob1).
A heavy truck tire tread having a longitudinal direction (LgD), a lateral direction (LtD), a tread depth direction (TdD), a ground contact surface (CS) and a pair of opposing tread shoulders spaced apart along the lateral direction, said tread consisting in : - a shoulder zone (SZ, SZ') adjacent each tread shoulder of said pair of opposing tread shoulders, said shoulder zones consisting of blocks , said blocks being adjacent to each other along the longitudinal direction and separated by lateral grooves ; and - a center zone (CZ) defined between said shoulder zones, said center zone consisting in a longitudinal center rib ; characterized in that the center zone is decoupled from both shoulder zones by at least one longitudinal sipe and wherein each lateral groove in a shoulder zone (SZ) is directly connected to an opposite lateral groove in the opposite shoulder zone (SZ') by a lateral sipe of the center rib. - a shoulder zone (SZ, SZ') adjacent each tread shoulder of said pair of opposing tread shoulders, said shoulder zones consisting of blocks , said blocks being adjacent to each other along the longitudinal direction and separated by lateral grooves ; and - a center zone (CZ) defined between said shoulder zones, said center zone consisting in a longitudinal center rib ;
Shaft lower part for a shaft system with a sealing, insertable and/or latchable connection to a shaft central part and/or shaft upper part, wherein the shaft lower part is configured with a first outer wall (3.4) and a second outer wall (3.5), wherein the first outer wall (3.4) is configured with stiffening elements, wherein on the stiffening elements of the first outer wall (3.4) lateral flanks are configured and wherein the second outer wall (3.5) is configured with stiffening elements , wherein the shaft lower part is configured with a first portion and a second portion , wherein the first portion forms the upper portion viewed in the installed position and the second portion forms the lower portion, wherein the two portions are integrally interconnected by a transition portion , and wherein the shaft lower part is configured with a support surface for placing on a substrate , said support surface having the shape of a circular or annular surface or approximately the shape of a circular or annular surface, wherein the second portion has a smaller cross-sectional area (F5), with respect to the outer wall (3.5), than the cross-sectional area (F4) of the first portion , with respect to the outer wall (3.4), wherein the cross-sectional area is the area obtained when the portion of the shaft lower part arranged in the installed position is projected vertically on to a horizontal plane (E) therebelow, and wherein reinforcement elements are configured as ribs on the transition portion , characterised in that at least two arrangement portions of the reinforcement elements configured as ribs are present, wherein in each portion at least two mutually adjacent ribs have lateral flanks arranged parallel to each other.
A razor cartridge , comprising: one or more shaving blades each having a cutting edge ; a blade housing configured to accommodate the one or more shaving blades in a longitudinal direction of the blade housing ; and one or more clips each configured to fix the one or more shaving blades to the blade housing and having a shape of a closed loop, wherein a clip of the one or more clips is configured to surround at least a portion of the blade housing about a first axis (ax1) parallel to the longitudinal direction, characterized in that the blade housing comprises: a recess formed at a region of the blade housing that is surrounded by the clip of the one or more clips, and the clip of the one or more clips comprises: a concave region formed toward the recess . one or more shaving blades each having a cutting edge ; a blade housing configured to accommodate the one or more shaving blades in a longitudinal direction of the blade housing ; and one or more clips each configured to fix the one or more shaving blades to the blade housing and having a shape of a closed loop, wherein a clip of the one or more clips is configured to surround at least a portion of the blade housing about a first axis (ax1) parallel to the longitudinal direction, characterized in that the blade housing comprises: a recess formed at a region of the blade housing that is surrounded by the clip of the one or more clips, and the clip of the one or more clips comprises: a concave region formed toward the recess . a recess formed at a region of the blade housing that is surrounded by the clip of the one or more clips, and the clip of the one or more clips comprises: a concave region formed toward the recess .
A supporting device for a gas turbine, comprising: a base frame ; and a fixing member installed on the base frame so as to support one end of a gas turbine; characterized in that the supporting device further comprises: an absorbing member installed on the base frame so as to support the other end of the gas turbine, and having lower stiffness than the fixing member so as to deform in first and second directions when the gas turbine thermally expands, wherein the first direction extends along a radial direction of the gas turbine, and the second direction extends along an axial direction of the gas turbine; and wherein the absorbing member comprises: a first moving part configured to fasten to a turbine housing of the gas turbine and deform along the first direction; and a second moving part configured to deform along the second direction. a base frame ; and a fixing member installed on the base frame so as to support one end of a gas turbine; a first moving part configured to fasten to a turbine housing of the gas turbine and deform along the first direction; and a second moving part configured to deform along the second direction.
A retrofit electric machine for a bicycle, comprising: a housing configured to be attached to a frame of a bicycle , a rotating electric machine attached to the housing ; an annular rotating member mounted on the housing in a rotatable manner and connected to the rotating electric machine in a torque transmitting relationship; and a torque transmitting member mounted on the rotating member and including a pair of parts configured to abut against either side of a crankarm for a pedal of the bicycle with respect to a rotational direction thereof characterized in that the retrofit electric machine comprises a connecting member configured to connect the torque transmitting member with a rotationally central part of the crankarm such that the rotating member is concentric to a rotational center line of the crankarm . a housing configured to be attached to a frame of a bicycle , a rotating electric machine attached to the housing ; an annular rotating member mounted on the housing in a rotatable manner and connected to the rotating electric machine in a torque transmitting relationship; and a torque transmitting member mounted on the rotating member and including a pair of parts configured to abut against either side of a crankarm for a pedal of the bicycle with respect to a rotational direction thereof characterized in that the retrofit electric machine comprises a connecting member configured to connect the torque transmitting member with a rotationally central part of the crankarm such that the rotating member is concentric to a rotational center line of the crankarm .
A tire pressure sensor assembly comprising: an over-inflation pressure relief valve engagable in a wheel of an aircraft wheel assembly; and a tire pressure sensor engaged with, and configured to be in fluid communication with, the over-inflation pressure relief valve and disengagable therefrom, the tire pressure sensor comprising: a sensor housing having a first engagement portion defining an opening ; and a pressure sensing element within the sensor housing and in fluid communication with the opening of the sensor housing , and characterized by the tire pressure sensor being configured to engage with the over-inflation pressure relief valve forming a tire pressure sensor assembly , wherein the over-inflation pressure relief valve comprises a frangible disk configured to rupture at a predetermined pressure within the tire pressure sensor assembly , and wherein the over-inflation pressure relief valve comprises a pressure relief housing comprising a stem defining a tire inflation gas entry opening and a second engagement portion defining a tire inflation gas outlet opening . an over-inflation pressure relief valve engagable in a wheel of an aircraft wheel assembly; and a tire pressure sensor engaged with, and configured to be in fluid communication with, the over-inflation pressure relief valve and disengagable therefrom, the tire pressure sensor comprising: a sensor housing having a first engagement portion defining an opening ; and a pressure sensing element within the sensor housing and in fluid communication with the opening of the sensor housing , and characterized by the tire pressure sensor being configured to engage with the over-inflation pressure relief valve forming a tire pressure sensor assembly , wherein the over-inflation pressure relief valve comprises a frangible disk configured to rupture at a predetermined pressure within the tire pressure sensor assembly , and wherein the over-inflation pressure relief valve comprises a pressure relief housing comprising a stem defining a tire inflation gas entry opening and a second engagement portion defining a tire inflation gas outlet opening . a sensor housing having a first engagement portion defining an opening ; and a pressure sensing element within the sensor housing and in fluid communication with the opening of the sensor housing , and characterized by the tire pressure sensor being configured to engage with the over-inflation pressure relief valve forming a tire pressure sensor assembly , wherein the over-inflation pressure relief valve comprises a frangible disk configured to rupture at a predetermined pressure within the tire pressure sensor assembly , and wherein the over-inflation pressure relief valve comprises a pressure relief housing comprising a stem defining a tire inflation gas entry opening and a second engagement portion defining a tire inflation gas outlet opening .
A fuel supply circuit for a combustion chamber of a turbomachine , in particular for an aircraft, comprising: - a fuel supply pump , said pump being configured to provide a fuel flow at a predetermined flow rate, - a plurality of fuel injectors , - a ramp for connecting the pump to the injectors , and - a device for the thermal treatment of the fuel comprising a chamber connected, on the one hand, to a fuel inlet connected to the pump and to a fuel outlet connected to the ramp , heating elements being located in this chamber and being configured to heat the flow of fuel provided by the pump up to a predetermined temperature so as to cause a coking of the fuel within the chamber , the supply circuit being characterised in that said heating elements comprise at least one perforated metal tube which comprises fuel passage orifices and which is associated with a heating electrode for heating the tube and thus the fuel passing through the tube . - a fuel supply pump , said pump being configured to provide a fuel flow at a predetermined flow rate, - a plurality of fuel injectors , - a ramp for connecting the pump to the injectors , and - a device for the thermal treatment of the fuel comprising a chamber connected, on the one hand, to a fuel inlet connected to the pump and to a fuel outlet connected to the ramp , heating elements being located in this chamber and being configured to heat the flow of fuel provided by the pump up to a predetermined temperature so as to cause a coking of the fuel within the chamber ,
Device for rinsing out a water-soluble solid cleaner, comprising a rinsing-out chamber , which has an outflow ; at least one rinsing-out nozzle arranged in the region of the rinsing-out chamber and comprising a receptacle for a storage container , arranged above the rinsing-out nozzle, for the solid cleaner, wherein the receptacle for the storage container is designed such that the water-soluble solid cleaner is arranged above a maximum attainable liquid level in the rinsing-out chamber during operation of the device; characterized in that a liquid sensor is arranged in a region spatially separated from the rinsing-out chamber and in liquid connection with the rinsing-out chamber , so that the same liquid level is set in the spatially separated region as in the rinsing-out chamber , wherein the liquid sensor is designed to interrupt a supply of liquid when a specified maximum liquid level is attained in the rinsing-out chamber , wherein a liquid passage between the rinsing-out chamber and the separated region is arranged below the detection level of the liquid sensor .
Method for the production and/or processing of a nonwoven glass fabric web (G), wherein the method comprises the following step: thermal drying of the nonwoven glass fabric web (G) by means of infrared radiation from an infrared radiation dryer , characterized in that a specific power density of at least 153 kW/m 2 is applied by the infrared radiation dryer to the surface of the nonwoven glass fabric web (G) facing toward the infrared radiation dryer , and in that after the irradiation by the infrared radiation dryer , the nonwoven glass fabric web (G) has a temperature of at least 40°C and at most 105°C on its surface facing toward the infrared radiation dryer .
Kit for making a luminaire comprising: - a flat casing integrating all the optical, electronic and electrical means of the luminaire , at least one face of which is at least partially glazed, housing at least one printed circuit board on which is mounted at least one light-emitting diode oriented towards the at least partially glazed face , - a support for hooking said casing above an area to be illuminated, and - a member for securing the casing to said support , comprising at least one housing designed able to house at least one part of the casing and an end-piece allowing the housing to be fixed to said support ; said support comprising within it means for controlling the printed circuit boards ; characterized in that - the casing comprises a bottom surmounted by a peripheral wall delimiting a space of shape and size adjusted according to the number of printed circuit boards hosted by said casing , said space being closed by said at least partially glazed face , and - the space is subdivided into at least two coplanar compartments by means of at least one V-shaped bar presenting two opposite flanks joined by a top and extending along the bottom of the casing in such a way that its top is oriented towards the at least partially glazed face of said casing , and - the at least partially glazed face rests and is fixed on a shoulder extending between the inner face and the free edge of the peripheral wall of the casing , and - the shoulder comprises a groove provided with a sealing joint. - a flat casing integrating all the optical, electronic and electrical means of the luminaire , at least one face of which is at least partially glazed, housing at least one printed circuit board on which is mounted at least one light-emitting diode oriented towards the at least partially glazed face , - a support for hooking said casing above an area to be illuminated, and - a member for securing the casing to said support , comprising at least one housing designed able to house at least one part of the casing and an end-piece allowing the housing to be fixed to said support ; said support comprising within it means for controlling the printed circuit boards ; - the casing comprises a bottom surmounted by a peripheral wall delimiting a space of shape and size adjusted according to the number of printed circuit boards hosted by said casing , said space being closed by said at least partially glazed face , and - the space is subdivided into at least two coplanar compartments by means of at least one V-shaped bar presenting two opposite flanks joined by a top and extending along the bottom of the casing in such a way that its top is oriented towards the at least partially glazed face of said casing , and - the at least partially glazed face rests and is fixed on a shoulder extending between the inner face and the free edge of the peripheral wall of the casing , and - the shoulder comprises a groove provided with a sealing joint.
An environmental control system of an aircraft, comprising a precooler ; an environmental control system duct, a high pressure bleed port and a low pressure bleed port ; a turbine installed in the environmental control system duct and in fluid communication with the at least one of the high pressure bleed port and the low pressure bleed port, wherein the turbine is arranged to discharge air to the precooler ; a generator coupled to the turbine and configured to produce power in response to rotation of the turbine ; and a power distribution system in electronic communication with the generator and an electrical distribution system of the aircraft; further comprising a valve coupled to the turbine , wherein the coupling between the valve and the turbine provides a variable output geometry to the turbine. a precooler ; an environmental control system duct, a high pressure bleed port and a low pressure bleed port ; a turbine installed in the environmental control system duct and in fluid communication with the at least one of the high pressure bleed port and the low pressure bleed port, wherein the turbine is arranged to discharge air to the precooler ; a generator coupled to the turbine and configured to produce power in response to rotation of the turbine ; and a power distribution system in electronic communication with the generator and an electrical distribution system of the aircraft;