mhurhangee/patent-ind-claim-en huggingface dataset:
A digital camera comprising: a) a lens having a lens optical axis ; b) an image sensor ; c) a first optical path folding element (OPFE) for folding light arriving from an object in a first optical path to a second optical path substantially aligned with the lens optical axis; and d) a second OPFE for folding light from the second optical path to a third optical path toward the image sensor, wherein the third optical path is substantially parallel with the first optical path, wherein the first and third optical paths are substantially orthogonal to the second optical path, wherein the lens is operative to move in a first direction substantially parallel to the lens optical axis and in a second direction substantially perpendicular to both the first and second optical paths, wherein the second OPFE is operative to move in the first direction, and wherein the combined motion of the lens and of the second OPFE is operative to provide focus and to compensate for tilts of the camera around the first and second directions. a) a lens having a lens optical axis ; b) an image sensor ; c) a first optical path folding element (OPFE) for folding light arriving from an object in a first optical path to a second optical path substantially aligned with the lens optical axis; and d) a second OPFE for folding light from the second optical path to a third optical path toward the image sensor, wherein the third optical path is substantially parallel with the first optical path,
A two-wheeled vehicle , comprising: a chassis ; a first wheel carriage moveably coupled to, and longitudinally displaceable relative to the chassis ; at least a first wheel rotationally mounted on the first wheel carriage , the first wheel coupled to the chassis through the first wheel carriage ; a first linear actuator system coupled to the first wheel carriage , and configured to longitudinally displace the first wheel carriage relative to the chassis ; a first motor mounted to the first wheel and the first wheel carriage , configured to provide a drive energy to the first wheel , and to be displaced along with the first wheel carriage as the first wheel is displaced by the first linear actuator system ; a second wheel mounted on a second wheel carriage , the second wheel carriage disposed at a side of the two-wheeled vehicle opposite to the first wheel carriage ; a second linear actuator system coupled to the second wheel carriage at a side of the two-wheeled vehicle opposite to the first linear actuator system , and configured to longitudinally displace the second wheel carriage relative to the chassis ; and a second motor mounted to the second wheel and the second wheel carriage , configured to provide a drive energy to the second wheel , and to be displaced along with the second wheel carriage as the second wheel is displaced by second linear actuator system . a chassis ; a first wheel carriage moveably coupled to, and longitudinally displaceable relative to the chassis ; at least a first wheel rotationally mounted on the first wheel carriage , the first wheel coupled to the chassis through the first wheel carriage ; a first linear actuator system coupled to the first wheel carriage , and configured to longitudinally displace the first wheel carriage relative to the chassis ; a first motor mounted to the first wheel and the first wheel carriage , configured to provide a drive energy to the first wheel , and to be displaced along with the first wheel carriage as the first wheel is displaced by the first linear actuator system ; a second wheel mounted on a second wheel carriage , the second wheel carriage disposed at a side of the two-wheeled vehicle opposite to the first wheel carriage ; a second linear actuator system coupled to the second wheel carriage at a side of the two-wheeled vehicle opposite to the first linear actuator system , and configured to longitudinally displace the second wheel carriage relative to the chassis ; and a second motor mounted to the second wheel and the second wheel carriage , configured to provide a drive energy to the second wheel , and to be displaced along with the second wheel carriage as the second wheel is displaced by second linear actuator system .
A portable carrier bag for disposing pet waste, the portable carrier bag comprising: a pet waste storage space portion in which a fastener is installed along both lateral surfaces and a lower surface thereof to facilitate opening and closing, the pet waste storage space portion being configured to be opened toward the ground when the fastener is opened, and to dispose and store pet waste therein; a tissue storage space portion formed in front of the pet waste storage space portion as a separate space, wherein the tissue storage space portion comprises an opening and closing member , the tissue storage space portion being configured to store tissues or wet tissues therein; and a loop for connection with a pet leash, characterized in that the loop is formed in the center of a top surface of the pet waste storage space portion , wherein a material of the portable carrier bag is a hard synthetic resin, so as to allow for use of the portable carrier bag in rainy or snowy weather and also make it easy to clean the portable carrier bag, wherein the opening and closing member to open and close the tissue storage space portion is formed of a magnet, thereby making it easy to open and close the tissue storage portion, wherein a plurality of openings are formed on a rear surface of the pet waste storage space portion , thereby being capable of preventing permeation of smell into the portable carrier bag. a pet waste storage space portion in which a fastener is installed along both lateral surfaces and a lower surface thereof to facilitate opening and closing, the pet waste storage space portion being configured to be opened toward the ground when the fastener is opened, and to dispose and store pet waste therein; a tissue storage space portion formed in front of the pet waste storage space portion as a separate space, wherein the tissue storage space portion comprises an opening and closing member , the tissue storage space portion being configured to store tissues or wet tissues therein; and a loop for connection with a pet leash, characterized in that the loop is formed in the center of a top surface of the pet waste storage space portion , wherein a material of the portable carrier bag is a hard synthetic resin, so as to allow for use of the portable carrier bag in rainy or snowy weather and also make it easy to clean the portable carrier bag, wherein the opening and closing member to open and close the tissue storage space portion is formed of a magnet, thereby making it easy to open and close the tissue storage portion, wherein a plurality of openings are formed on a rear surface of the pet waste storage space portion , thereby being capable of preventing permeation of smell into the portable carrier bag.
A process for retreading a tire, the process comprising the steps of: (i) providing a tire casing; (ii) providing a cured rubber component having first and second planar surfaces; (iii) providing a cushion gum, wherein the cushion gum contains a cure system comprising at least one stable aryl dinitrile oxide compound, characterised in that said step of providing a cushion gum includes preparing the cushion gum at the same location in which the process for retreading a tire takes place; (iv) applying the cushion gum to the tire casing; and (v) forming a tire composite by applying the second planar surface of the cured rubber component to the cushion gum. (i) providing a tire casing; (ii) providing a cured rubber component having first and second planar surfaces; (iii) providing a cushion gum, wherein the cushion gum contains a cure system comprising at least one stable aryl dinitrile oxide compound, characterised in that said step of providing a cushion gum includes preparing the cushion gum at the same location in which the process for retreading a tire takes place; (iv) applying the cushion gum to the tire casing; and (v) forming a tire composite by applying the second planar surface of the cured rubber component to the cushion gum.
A gas turbine engine comprising a clearance control arrangement for a rotor , the arrangement comprising: • a rotor having an upstream side and a downstream side defined by airflow through the engine ; • a casing radially outside the rotor ; • a segment assembly spaced radially inwards from the casing and defining a radial clearance between the rotor and the segment assembly ; • a upstream carrier and a downstream carrier , the segment assembly supported by the carriers ; • a heat transfer cavity formed between the carriers , the segment assembly and the casing ; and • a settling chamber formed adjacent to the casing and upstream of the heat transfer cavity , wherein the clearance control arrangement is configured to receive air into the settling chamber and thence to deliver it to the heat transfer cavity ; characterised in that the settling chamber has an axial length (l SC ) of greater than or equal to half the axial distance (d FR ) between the upstream and downstream segment carriers to reduce turbulence in the air passing through it to below a threshold level. • a rotor having an upstream side and a downstream side defined by airflow through the engine ; • a casing radially outside the rotor ; • a segment assembly spaced radially inwards from the casing and defining a radial clearance between the rotor and the segment assembly ; • a upstream carrier and a downstream carrier , the segment assembly supported by the carriers ; • a heat transfer cavity formed between the carriers , the segment assembly and the casing ; and • a settling chamber formed adjacent to the casing and upstream of the heat transfer cavity , wherein the clearance control arrangement is configured to receive air into the settling chamber and thence to deliver it to the heat transfer cavity ;
A relay module structure comprising: a relay , comprising a main body and multiple pins connected to the main body ; a loading box , comprising a box body receiving the main body and a flexible latch portion connected to the box body , the box body comprising a force exerting portion and a relay seat , comprising a seat body , the seat body comprising a recess , a positioning portion and multiple terminal holes , the positioning portion and the terminal holes disposed in the recess , characterized in that the box body comprises multiple slots and in that the pins projecting from the main body of the relay extend through the slots and project from the slots ; wherein the loading box is inserted in the recess by engagement between the flexible latch portion and the positioning portion , the pins projecting from main body of the relay being inserted in the terminal holes ; and the flexible latch portion is configured to be separated from the positioning portion by exerting an external force on the force exerting portion of the box body to make the loading box receiving the relay separate from the relay seat . a relay , comprising a main body and multiple pins connected to the main body ; a loading box , comprising a box body receiving the main body and a flexible latch portion connected to the box body , the box body comprising a force exerting portion and a relay seat , comprising a seat body , the seat body comprising a recess , a positioning portion and multiple terminal holes , the positioning portion and the terminal holes disposed in the recess , characterized in that the box body comprises multiple slots and in that the pins projecting from the main body of the relay extend through the slots and project from the slots ; wherein the loading box is inserted in the recess by engagement between the flexible latch portion and the positioning portion , the pins projecting from main body of the relay being inserted in the terminal holes ; and the flexible latch portion is configured to be separated from the positioning portion by exerting an external force on the force exerting portion of the box body to make the loading box receiving the relay separate from the relay seat .
A 3-D printing method for manufacturing elements comprising hydraulic binder and aggregates, said method comprising: - mixing a dry mortar composition comprising hydraulic binder and aggregates with water, to form a wet mortar, - pumping and conveying said wet mortar towards the head of a computer-controlled printer, said printer head comprising a printing nozzle through which the wet mortar is extruded to form a layer, and - depositing a layer of wet mortar on a previous layer of mortar characterized in that, during said conveying at least two physical properties of the wet mortar are measured on-line, said physical properties including viscosity and at least one of flow and density. - mixing a dry mortar composition comprising hydraulic binder and aggregates with water, to form a wet mortar, - pumping and conveying said wet mortar towards the head of a computer-controlled printer, said printer head comprising a printing nozzle through which the wet mortar is extruded to form a layer, and - depositing a layer of wet mortar on a previous layer of mortar
A method of mounting or dismounting wind turbine components of energy generating units in a multirotor wind turbine , the multirotor wind turbine comprising a tower configured to support one or more load carrying structures each extending between a first end and a second end, wherein each load carrying structure is arranged for supporting at least two energy generating units arranged at or near the first and second ends of the load carrying structure and at opposite sides of the tower , and wherein the load carrying structure is attached to the tower via a yaw arrangement allowing the load carrying structure to yaw around the tower , the method comprising: - positioning or dispositioning a first wind turbine component of a first energy generating unit at or near the first end of the load carrying structure ; - yawing the load carrying structure approximately 180 degrees; - positioning or dispositioning a second wind turbine component of a second energy generating unit at or near the second end of the load carrying structure opposite the first end. - positioning or dispositioning a first wind turbine component of a first energy generating unit at or near the first end of the load carrying structure ; - yawing the load carrying structure approximately 180 degrees; - positioning or dispositioning a second wind turbine component of a second energy generating unit at or near the second end of the load carrying structure opposite the first end.
A semiconductor assembly comprising: a first semiconductor chip disposed on a substrate and comprising a first semiconductor body , a first chip electrode and a second chip electrode ; and a pedestal disposed on the substrate and comprising a first pedestal electrode and a second pedestal electrode , the second pedestal electrode being electrically connected to the second chip electrode ; a first bonding wire which is, at a first bonding location , bonded to the first chip electrode and, at a second bonding location , to the first pedestal electrode ; characterized in that the pedestal comprises a second semiconductor body ; for each polarity of an electrical voltage applied between the first chip electrode and the second chip electrode , the magnitude of a breakdown voltage of the second semiconductor body is greater than the magnitude of a breakdown voltage of the first semiconductor body . a first semiconductor chip disposed on a substrate and comprising a first semiconductor body , a first chip electrode and a second chip electrode ; and a pedestal disposed on the substrate and comprising a first pedestal electrode and a second pedestal electrode , the second pedestal electrode being electrically connected to the second chip electrode ; a first bonding wire which is, at a first bonding location , bonded to the first chip electrode and, at a second bonding location , to the first pedestal electrode ; the pedestal comprises a second semiconductor body ; for each polarity of an electrical voltage applied between the first chip electrode and the second chip electrode , the magnitude of a breakdown voltage of the second semiconductor body is greater than the magnitude of a breakdown voltage of the first semiconductor body .
Method for severing a solid body, wherein a high-energy beam travels along a contour on a surface of the solid body facing the high-energy beam and herein produces a cutting gap, wherein a control unit that controls the severing has a function for detecting contour breaches and a function for avoiding contour breaches, characterised in that at least one item of information relating to at least one feature of at least one defined contour is stored in the control unit (S10), the information is detected by the control unit (S12) and, when the information is detected, the contour breach avoidance is automatically deactivated (S13).
An inline heater system for use on board an aircraft comprising: a heater element positioned within a heated component ; at least one sensor configured to monitor the temperature within the heated component; an inline heater controller configured to receive information regarding the heater element via the at least one sensor ; wherein the inline heater controller is positioned at a location spaced away from the heater element and the heated component ; and wherein the inline heater controller is connected to an aircraft control system and transmits information regarding the heater element to the aircraft control system; characterized in that the at least one sensor is positioned within the heated component; and in that the inline heater controller comprises: a printed circuit board configured to receive the information regarding the heater element via the at least one sensor ; and an aerospace connector configured to transmit the information regarding the heater element from the at least one sensor to the aircraft control system; wherein the inline heater controller is mounted to the back of the aerospace connector . a heater element positioned within a heated component ; at least one sensor configured to monitor the temperature within the heated component; an inline heater controller configured to receive information regarding the heater element via the at least one sensor ; wherein the inline heater controller is positioned at a location spaced away from the heater element and the heated component ; and wherein the inline heater controller is connected to an aircraft control system and transmits information regarding the heater element to the aircraft control system; characterized in that the at least one sensor is positioned within the heated component; and in that the inline heater controller comprises: a printed circuit board configured to receive the information regarding the heater element via the at least one sensor ; and an aerospace connector configured to transmit the information regarding the heater element from the at least one sensor to the aircraft control system; wherein the inline heater controller is mounted to the back of the aerospace connector . a printed circuit board configured to receive the information regarding the heater element via the at least one sensor ; and an aerospace connector configured to transmit the information regarding the heater element from the at least one sensor to the aircraft control system; wherein the inline heater controller is mounted to the back of the aerospace connector .
A method of preparing a compound of Formula II, wherein R 8 is selected from hydrogen and C 1 -C 4 alkyl; and each of R 2 - R 7 is independently selected from hydrogen, halogen, C 1 -C 4 alkyl, and halogenated C 1 -C 4 alkyl, the method comprising I) forming a mixture comprising A) a first amount of a compound of Formula I, wherein R 1 is selected from hydrogen and C 1 -C 4 alkyl; and each of R 2 - R 7 is independently selected from hydrogen, halogen, Ci-C 4 alkyl, and halogenated C 1 -C 4 alkyl; B) an oxidizing agent; and C) an organic solvent; II) heating the mixture; III) adding an acid to the mixture; IV) adding a second amount of the compound of Formula I to the mixture; and V) completing the reaction of the mixture. R 8 is selected from hydrogen and C 1 -C 4 alkyl; and each of R 2 - R 7 is independently selected from hydrogen, halogen, C 1 -C 4 alkyl, and halogenated C 1 -C 4 alkyl, the method comprising I) forming a mixture comprising A) a first amount of a compound of Formula I, wherein R 1 is selected from hydrogen and C 1 -C 4 alkyl; and each of R 2 - R 7 is independently selected from hydrogen, halogen, Ci-C 4 alkyl, and halogenated C 1 -C 4 alkyl; B) an oxidizing agent; and C) an organic solvent; II) heating the mixture; III) adding an acid to the mixture; IV) adding a second amount of the compound of Formula I to the mixture; and V) completing the reaction of the mixture. I) forming a mixture comprising A) a first amount of a compound of Formula I, wherein R 1 is selected from hydrogen and C 1 -C 4 alkyl; and each of R 2 - R 7 is independently selected from hydrogen, halogen, Ci-C 4 alkyl, and halogenated C 1 -C 4 alkyl; B) an oxidizing agent; and C) an organic solvent; A) a first amount of a compound of Formula I, wherein R 1 is selected from hydrogen and C 1 -C 4 alkyl; and each of R 2 - R 7 is independently selected from hydrogen, halogen, Ci-C 4 alkyl, and halogenated C 1 -C 4 alkyl; R 1 is selected from hydrogen and C 1 -C 4 alkyl; and each of R 2 - R 7 is independently selected from hydrogen, halogen, Ci-C 4 alkyl, and halogenated C 1 -C 4 alkyl; B) an oxidizing agent; and C) an organic solvent; II) heating the mixture; III) adding an acid to the mixture; IV) adding a second amount of the compound of Formula I to the mixture; and V) completing the reaction of the mixture.
Magnet arrangement comprising a carrier sleeve made of metal featuring a flange with a front and a back to which flange a ring-shaped plastic-bonded permanent magnet is fixed directly on the back of the flange so as to make contact with the flange and is permanently attached to the flange, wherein the flange features recesses and the plastic-bonded permanent magnet features mouldings protruding through the recesses, each of which then overlap the front of the flange at the respective recesses and make direct contact to the front of the flange, wherein at least one of the recesses of the plastic-bonded permanent magnets is narrower in a radial direction R of the carrier sleeve than the associated recess of the flange in such a way that one area of the recess is exposed in a radial direction to the carrier sleeve, characterized in that the respective moulding overlaps the recess on both sides of the recess and wherein the area of the recess exposed in a radial direction is no bigger than 1.5 mm in a radial direction.
First double busbar having a contact device , wherein the first double busbar having a first busbar and a second busbar which are separated from one another by an insulation and are stacked on top of one another to form a stack, the contact device having an outer contact jack and an inner contact jack arranged coaxially in the outer contact jack , wherein an outer laminated band for contacting a mating jack of a counterpart to the contact device is arranged on an inner side of the outer contact jack and an inner laminated band for contacting a contact pin of the counterpart is arranged on an inner side of the inner contact jack , the outer contact jack being arranged on a flat side of the first busbar and being electrically conductive connected to the first busbar , the inner contact socket being electrically conductive connected to the second busbar and penetrating the first busbar .