mhurhangee/patent-ind-claim-en huggingface dataset:
A mounting aid for attaching a supplementary device to an injection device , wherein the injection device has an elongated housing extending in an axial direction , the mounting aid comprises: - a body extending in axial direction , configured to receive at least a portion of the housing - wherein the body comprises a side wall with an abutment face facing in a proximal direction , wherein the abutment face is defined on a plane that is inclined to the axial direction , characterized in that - the body has at least one radially extending engaging member to engage with a correspondingly shaped engaging member of the housing when in a specific position (M) relative to the housing , and - wherein the abutment face represents a symmetry-breaking feature and is configured to align and to abut with a complementary-shaped corresponding abutment face of the supplementary device when attached to the injection device . - a body extending in axial direction , configured to receive at least a portion of the housing - wherein the body comprises a side wall with an abutment face facing in a proximal direction , wherein the abutment face is defined on a plane that is inclined to the axial direction , characterized in that - the body has at least one radially extending engaging member to engage with a correspondingly shaped engaging member of the housing when in a specific position (M) relative to the housing , and - wherein the abutment face represents a symmetry-breaking feature and is configured to align and to abut with a complementary-shaped corresponding abutment face of the supplementary device when attached to the injection device .
A downhole tool comprising: a support structure with a longitudinal axis; an electromagnetic source mechanically coupled to the support structure and operable to generate electromagnetic radiation; an antenna communicatively coupled to the electromagnetic source and operable to transmit the electromagnetic radiation, the antenna capable of steering the electromagnetic radiation in at least one direction; an expandable casing within which the antenna is at least partially enclosed, wherein the expandable casing is mechanically coupled to the support structure and rotatable about the longitudinal axis of the support structure, the expandable casing can be caused to expand such that the casing comes into direct contact with the walls of a wellbore, at least a portion of the expandable casing comprising a ceramic material that is configured to absorb the electromagnetic radiation generated by the electromagnetic source and transmitted by the antenna and rapidly increase in temperature. a support structure with a longitudinal axis; an electromagnetic source mechanically coupled to the support structure and operable to generate electromagnetic radiation; an antenna communicatively coupled to the electromagnetic source and operable to transmit the electromagnetic radiation, the antenna capable of steering the electromagnetic radiation in at least one direction; an expandable casing within which the antenna is at least partially enclosed, wherein the expandable casing is mechanically coupled to the support structure and rotatable about the longitudinal axis of the support structure, the expandable casing can be caused to expand such that the casing comes into direct contact with the walls of a wellbore, at least a portion of the expandable casing comprising a ceramic material that is configured to absorb the electromagnetic radiation generated by the electromagnetic source and transmitted by the antenna and rapidly increase in temperature.
A deformable accumulator comprising: a. first and second deformable planar substrates , b. at least one first stretchable current collector (2a, 2b, ...) which is deposited on at least one portion of a face of the first substrate, in the vicinity and along at least one first portion of a curved line whose length is greater than the distance between the two ends thereof, c. at least one second stretchable current collector (2a', 2b', ...) deposited on at least one portion of a face of the second substrate, in the vicinity and on each side of at least one second curved line whose length is greater than the distance between the two ends thereof, d. an anode consisting of a first set of pillars deposited on the at least one first current collector (2a, 2b, ...), the pillars of the first set being spaced from each other on a surface of the first collector, the pillars of the first set of pillars having a height comprised between 1 μm and 1000 μm, and a width comprised between 1 μm and 100 μm, e. a cathode consisting of a second set of pillars , deposited on the at least one second current collector (2a', 2b', ...), the pillars of the second set being spaced from each other on a surface of the second collector, the pillars of the second set of pillars having a height comprised between 1 μm and 1000 μm, and a width comprised between 1 μm and 100 μm, f. an electrolyte allowing the transfer of the ionic species, the faces of the first and second substrates, on which the at least one first and at least one second current collectors are deposited respectively, being placed facing each other and delimiting a volume which is occupied by the electrolyte in which the pillars of the anode and the cathode are immersed. a. first and second deformable planar substrates , b. at least one first stretchable current collector (2a, 2b, ...) which is deposited on at least one portion of a face of the first substrate, in the vicinity and along at least one first portion of a curved line whose length is greater than the distance between the two ends thereof, c. at least one second stretchable current collector (2a', 2b', ...) deposited on at least one portion of a face of the second substrate, in the vicinity and on each side of at least one second curved line whose length is greater than the distance between the two ends thereof, d. an anode consisting of a first set of pillars deposited on the at least one first current collector (2a, 2b, ...), the pillars of the first set being spaced from each other on a surface of the first collector, the pillars of the first set of pillars having a height comprised between 1 μm and 1000 μm, and a width comprised between 1 μm and 100 μm, e. a cathode consisting of a second set of pillars , deposited on the at least one second current collector (2a', 2b', ...), the pillars of the second set being spaced from each other on a surface of the second collector, the pillars of the second set of pillars having a height comprised between 1 μm and 1000 μm, and a width comprised between 1 μm and 100 μm, f. an electrolyte allowing the transfer of the ionic species,
A microporous membrane suitable for dewatering acidic mixtures, comprising a bridged organosilica directly applied on a macroporous support comprising α-alumina, in the absence of an intermediate mesoporous layer, the bridged organosilica comprising divalent C 1 -C 9 organic groups A 2 and/or trivalent C 1 -C 9 organic groups A 3 directly bound to the silicon atoms of the organosilica, wherein "mesopores" means pores of between 2 nm and 50 nm, smaller pores are "micropores", and larger pores are "macropores".
Elevator system comprising at least one car , wherein at least two support means having different physical properties are arranged between the car and at least one counterweight of the car , wherein the elevator system is designed having two counterweights , wherein one of the support means is connected to one counterweight and the other support means is connected to the other counterweight , wherein the support means are designed to be redundant with regard to a maximum load-bearing capacity to be carried in the elevator system, characterized in that one of the support means has a greater safety reserve than the other support means .
An edge seal for preventing airflow through a space between a fan platform and an adjacent airfoil in a gas turbine engine , the edge seal comprising: a bonding segment being bondable to an inner surface of the fan platform ; a sealing flap converging with the bonding segment , the sealing flap being operatively contactable with the adjacent airfoil , wherein the sealing flap converges with the bonding segment at a crook so that the sealing flap is bendable with respect to the bonding segment ; and a bumper rib protruding from the bonding segment adjacent to where the sealing flap converges with the bonding segment , the bumper rib being bondable to a side edge of the fan platform ; wherein the crook is on the opposite side of the bumper rib with respect to a portion of the bonding segment that is configured to be bonded to an inner surface of the fan platform . a bonding segment being bondable to an inner surface of the fan platform ; a sealing flap converging with the bonding segment , the sealing flap being operatively contactable with the adjacent airfoil , wherein the sealing flap converges with the bonding segment at a crook so that the sealing flap is bendable with respect to the bonding segment ; and a bumper rib protruding from the bonding segment adjacent to where the sealing flap converges with the bonding segment , the bumper rib being bondable to a side edge of the fan platform ; wherein the crook is on the opposite side of the bumper rib with respect to a portion of the bonding segment that is configured to be bonded to an inner surface of the fan platform .
Container closure for closing the pouring opening of a container comprising - a screw cap with a free edge , a first cylindrical shell , a lid plate adjoining the shell and an inner thread configured on the inner side of the shell that can interact with an outer thread of a container neck of the container , - a safety ring that is connected to the free edge of the shell by desired-rupture legs and that includes engaging means that are configured for a positive-locking engagement into an abutment in the form of a retaining ring arranged in the area of the container neck , - a first arm with a first and a second arm end , wherein the first end is fixedly connected to the free edge of the screw cap and the second end is fixedly connected to the safety ring and - a second arm with a third and a fourth arm end , wherein the third end is fixedly connected to the free edge of the screw cap and the fourth end is fixedly connected to the safety ring , wherein the screw cap is collapsible from a closure position in which it closes the pouring opening into an open position in which it completely clears the pouring opening and vice-versa, characterized in that the safety ring is an open ring with a first and a second ring end , wherein the second arm end adjoins the first ring end and the fourth arm end adjoins the second ring end and a tab is configured between the first and the third arm end at the free end of the screw cap . - a screw cap with a free edge , a first cylindrical shell , a lid plate adjoining the shell and an inner thread configured on the inner side of the shell that can interact with an outer thread of a container neck of the container , - a safety ring that is connected to the free edge of the shell by desired-rupture legs and that includes engaging means that are configured for a positive-locking engagement into an abutment in the form of a retaining ring arranged in the area of the container neck , - a first arm with a first and a second arm end , wherein the first end is fixedly connected to the free edge of the screw cap and the second end is fixedly connected to the safety ring and - a second arm with a third and a fourth arm end , wherein the third end is fixedly connected to the free edge of the screw cap and the fourth end is fixedly connected to the safety ring , wherein the screw cap is collapsible from a closure position in which it closes the pouring opening into an open position in which it completely clears the pouring opening and vice-versa, characterized in that the safety ring is an open ring with a first and a second ring end , wherein the second arm end adjoins the first ring end and the fourth arm end adjoins the second ring end and a tab is configured between the first and the third arm end at the free end of the screw cap .
Thermal power plant , with a thermal energy storage device that is intrinsically in the power plant and is designed to supply energy during starting up of the thermal power plant for heating components and/or media of the thermal power plant , characterized by an additional electrical, chemical or mechanical energy storage device that is intrinsically in the power plant and is designed to supply energy during starting up of the thermal power plant for feeding into an electrical energy distribution network .
Use of a refractory material by self-expanding to have a maximum expansion rate of 250% or higher when the refractory material is brought close to a heat source or comes into contact with flame, the refractory material at least comprising: discontinuous reinforcing fibers having a thermal conductivity of 4 W/(m·K) or higher; and a flame-retardant thermoplastic resin having a limiting oxygen index of from 30 to 95, wherein the discontinuous reinforcing fibers are dispersed in the refractory material, the refractory material after expansion has a porosity of 30% or higher, wherein the maximum expansion rate is determined according to the measurement method disclosed in the description, wherein the thermal conductivity of fiber is determined according to the measurement method disclosed in the description, wherein the limiting oxygen index is determined in accordance with JIS K 7201-2 as disclosed in the description, and wherein the porosity of the refractory material after expansion is determined according to the measurement method in accordance with JIS K 7075. the refractory material after expansion has a porosity of 30% or higher, wherein the maximum expansion rate is determined according to the measurement method disclosed in the description, wherein the thermal conductivity of fiber is determined according to the measurement method disclosed in the description, wherein the limiting oxygen index is determined in accordance with JIS K 7201-2 as disclosed in the description, and wherein the porosity of the refractory material after expansion is determined according to the measurement method in accordance with JIS K 7075.
A peptide comprising a sequence having at least 90% of sequence identity with one of the sequences of the group consisting of: SEQ ID NO: 1; SEQ ID NO: 2; SEQ ID NO: 3; SEQ ID NO: 4; SEQ ID NO: 5; and SEQ ID NO: 6.
A flight control arrangement for a hybrid aircraft capable of horizontal fixed-wing flight, vertical takeoff and landing (VTOL) flight, and transitions therebetween, comprising: a fixed-wing flight control module configured and operative to control the horizontal fixed-wing flight, the fixed-wing flight control module being an integrated component having a respective first network interface connected to an aircraft data network via which the fixed-wing flight control module obtains sensory input and generates fixed-wing control output to network-connected fixed-wing flight components including one or more horizontal-thrust components ; and a VTOL flight control module configured and operative to control the VTOL flight, the VTOL flight control module also being an integrated component having a respective second network interface connected to the aircraft data network via which the VTOL flight control module observes flight status as reflected in network messages originated by the fixed-wing flight control module, and based on the observed flight status, generates VTOL control output to network-connected VTOL flight components including one or more vertical-thrust components, wherein the aircraft data network includes a plurality of controller area network (CAN) buses each carrying respective network messages originated by the fixed-wing flight control module and VTOL flight control module, and wherein the VTOL flight control module monitors and acts upon states, modes, and observable/sensors reporting of the fixed-wing flight control module as reflected in the network messages originated thereby. a fixed-wing flight control module configured and operative to control the horizontal fixed-wing flight, the fixed-wing flight control module being an integrated component having a respective first network interface connected to an aircraft data network via which the fixed-wing flight control module obtains sensory input and generates fixed-wing control output to network-connected fixed-wing flight components including one or more horizontal-thrust components ; and a VTOL flight control module configured and operative to control the VTOL flight, the VTOL flight control module also being an integrated component having a respective second network interface connected to the aircraft data network via which the VTOL flight control module observes flight status as reflected in network messages originated by the fixed-wing flight control module, and based on the observed flight status, generates VTOL control output to network-connected VTOL flight components including one or more vertical-thrust components, wherein the aircraft data network includes a plurality of controller area network (CAN) buses each carrying respective network messages originated by the fixed-wing flight control module and VTOL flight control module, and wherein the VTOL flight control module monitors and acts upon states, modes, and observable/sensors reporting of the fixed-wing flight control module as reflected in the network messages originated thereby.
A method of establishing an emergency call, comprising: triggering an emergency call in a vehicle comprising an in-vehicle system (IVS) for making an emergency call via a mobile network; generating an emergency setup message at the IVS to indicate that the IVS is only operable to place a call in emergency mode and the IVS is in an emergency for registration on a network; transmitting the emergency setup message from the IVS to the mobile network; receiving a high priority for registration of the IVS on the mobile network responsive to the emergency setup message being received at the mobile network; registering the IVS on the mobile network with the high priority pursuant to receiving the emergency setup message; and initiating an emergency call by the IVS, over the mobile network, after the IVS is registered on the mobile network, using the emergency setup message; wherein the emergency setup message comprises a service category information element having at least one bit used for an emergency call indicator wherein the at least one bit comprises a first bit indicating a high priority registration request and a second bit indicating an emergency call only IVS. triggering an emergency call in a vehicle comprising an in-vehicle system (IVS) for making an emergency call via a mobile network; generating an emergency setup message at the IVS to indicate that the IVS is only operable to place a call in emergency mode and the IVS is in an emergency for registration on a network; transmitting the emergency setup message from the IVS to the mobile network; receiving a high priority for registration of the IVS on the mobile network responsive to the emergency setup message being received at the mobile network; registering the IVS on the mobile network with the high priority pursuant to receiving the emergency setup message; and initiating an emergency call by the IVS, over the mobile network, after the IVS is registered on the mobile network, using the emergency setup message; wherein the emergency setup message comprises a service category information element having at least one bit used for an emergency call indicator wherein the at least one bit comprises a first bit indicating a high priority registration request and a second bit indicating an emergency call only IVS.
A process for the production of titania particles with a desired morphology, the process comprising: providing a titania sol; and then drying the sol to provide dried titania particles; characterised in that : the shape of the dried titania particles is controlled by applying the following criteria: the titania sol is dried by application of heat and spray drying is used and the temperature used during the spray drying step is controlled to be in the range of from 50 to 350°C, whereby the shape of the dried titania particles is controlled by using a higher spray drying temperature to obtain toroidal particles and by using a lower spray drying temperature to obtain more spherically shaped particles. providing a titania sol; and then drying the sol to provide dried titania particles;
A wind turbine blade , comprising: a plurality of electro-thermal heating panels disposed on or in a wind turbine blade structure; and one or more busbars electrically connected to each of the plurality of electro-thermal heating panels , wherein the one or more busbars extend along a chordwise and/or spanwise direction of the wind turbine blade , characterized in that adjacent busbars are substantially aligned in a vertical direction perpendicular to a surface of the wind turbine blade at the adjacent busbars to substantially prevent either a cold spot or hot spot in the wind turbine blade structure during heating of the wind turbine blade .
Primer for an adhesive comprising 1-60 wt.% reactive secondary amine (SA), 1-60 wt.% epoxy resin(ER), wherein the epoxy resin (ER) and the secondary amine (SA) are provided in a molar ratio of functional groups (epoxy groups and amine groups, respectively) (ER):(SA) of 0.5:1 to 10:1, 1-30 wt.% epoxy silane (ES) (R 8 -Si-(OR 6 ) (3-n) (OR 7 ) n ), wherein R 8 comprises an epoxide, and/or wherein R 6 and R 7 are each independently chosen from C 1 -C 15 alkyls, and/or wherein R 8 is independently chosen from a linear or branched C 1 -C 15 alkylene radical-epoxide, a (poly)oxy (C 1 -C 15 ) alkylene radical-epoxide, and glycidyl ether, and the remainder solvent, wherein the solvent is one or more of a carboxylate, an aromatic, a ketone, an ester, an ether, an alkane, and a hydrocarbon having a ring structure, wherein the secondary amine (SA) is one or more of H-N-{(R 1 ,R 2 )-Si-(OR 3 ) (3-n) (R 4 ) n } 2 and R 5 -NH-{(R 1 )-Si-(OR 3 ) (3-n) (R 4 ) n }, wherein n=0 or 1, R 1 , and R 2 are independently chosen of linear and branched C 1 -C 15 alkylene groups, R 3 , R 4 and R 5 are independently chosen from C 1 -C 15 alkyls, wherein all wt.% are based on a total weight of the primer. 1-60 wt.% reactive secondary amine (SA), 1-60 wt.% epoxy resin(ER), wherein the epoxy resin (ER) and the secondary amine (SA) are provided in a molar ratio of functional groups (epoxy groups and amine groups, respectively) (ER):(SA) of 0.5:1 to 10:1, 1-30 wt.% epoxy silane (ES) (R 8 -Si-(OR 6 ) (3-n) (OR 7 ) n ), wherein R 8 comprises an epoxide, and/or wherein R 6 and R 7 are each independently chosen from C 1 -C 15 alkyls, and/or wherein R 8 is independently chosen from a linear or branched C 1 -C 15 alkylene radical-epoxide, a (poly)oxy (C 1 -C 15 ) alkylene radical-epoxide, and glycidyl ether, and the remainder solvent, wherein the solvent is one or more of a carboxylate, an aromatic, a ketone, an ester, an ether, an alkane, and a hydrocarbon having a ring structure, wherein the secondary amine (SA) is one or more of H-N-{(R 1 ,R 2 )-Si-(OR 3 ) (3-n) (R 4 ) n } 2 and R 5 -NH-{(R 1 )-Si-(OR 3 ) (3-n) (R 4 ) n }, wherein n=0 or 1, R 1 , and R 2 are independently chosen of linear and branched C 1 -C 15 alkylene groups, R 3 , R 4 and R 5 are independently chosen from C 1 -C 15 alkyls, wherein all wt.% are based on a total weight of the primer.