mhurhangee/patent-ind-claim-en huggingface dataset:
An inverter-integrated electric compressor comprising: an inverter box provided on an outer periphery of a housing ; an inverter having a control circuit board and accommodated within the inverter box ; an electrical component mounted on a side of the control circuit board and being a constituent element of the inverter ; a heat-dissipating flat section provided on an inner wall of the inverter box , wherein the electrical component is disposed in abutment with the heat-dissipating flat section directly or via a heat conducting member so as to dissipate heat of the electrical component toward the housing ; and a spacer member interposed between the control circuit board and the electrical component so as to fill a space between the control circuit board and the electrical component , wherein the spacer member is of rigid construction such that the control circuit board and the electrical component are prevented from being displaced towards and away from each other, and wherein lead terminals of the electrical component extend through the spacer member and are inserted into lead-terminal insertion holes formed in the control circuit board so as to be connected to the control circuit board , characterized in that the control circuit board , the spacer member and the electrical component are fastened by a fastening member that extends through the control circuit board , the spacer member and the electrical component . an inverter box provided on an outer periphery of a housing ; an inverter having a control circuit board and accommodated within the inverter box ; an electrical component mounted on a side of the control circuit board and being a constituent element of the inverter ; a heat-dissipating flat section provided on an inner wall of the inverter box , wherein the electrical component is disposed in abutment with the heat-dissipating flat section directly or via a heat conducting member so as to dissipate heat of the electrical component toward the housing ; and a spacer member interposed between the control circuit board and the electrical component so as to fill a space between the control circuit board and the electrical component , wherein the spacer member is of rigid construction such that the control circuit board and the electrical component are prevented from being displaced towards and away from each other, and wherein lead terminals of the electrical component extend through the spacer member and are inserted into lead-terminal insertion holes formed in the control circuit board so as to be connected to the control circuit board , characterized in that the control circuit board , the spacer member and the electrical component are fastened by a fastening member that extends through the control circuit board , the spacer member and the electrical component .
A method for printing an object comprising the steps of: (a) printing a first layer of at least one ink, each of said at least one ink including: (i) a liquid carrier having a carrier boiling point temperature (T1); (ii) a dispersant having a dispersant boiling point temperature (T2); and (iii) particles having a particle sintering temperature (T3), (b) while maintaining a temperature of said first layer (TL) in a pre-defined range of temperatures via use of an electro-magnetic (EM) radiation source above the object, wherein said pre-defined range of temperatures is above a lower-bound ([T1]) of said carrier boiling point temperature and below an upper-bound ([T2]) of said dispersant boiling point temperature ([T1] < TL< [T2]), thus evaporating said carrier while said dispersant remains in said first layer, and wherein the first layer is flattened with a leveling apparatus after said carrier has evaporated, (c) printing a subsequent layer of said at least one ink on said first layer of at least one ink, (d) building the object by repeating steps (a) to (c), (e) after steps (a)-(d), heating the object in an oven to evaporate organic material, (f) after step (e), heating the object to a further elevated temperature where full sintering occurs. (a) printing a first layer of at least one ink, each of said at least one ink including: (i) a liquid carrier having a carrier boiling point temperature (T1); (ii) a dispersant having a dispersant boiling point temperature (T2); and (iii) particles having a particle sintering temperature (T3), (i) a liquid carrier having a carrier boiling point temperature (T1); (ii) a dispersant having a dispersant boiling point temperature (T2); and (iii) particles having a particle sintering temperature (T3), (b) while maintaining a temperature of said first layer (TL) in a pre-defined range of temperatures via use of an electro-magnetic (EM) radiation source above the object, wherein said pre-defined range of temperatures is above a lower-bound ([T1]) of said carrier boiling point temperature and below an upper-bound ([T2]) of said dispersant boiling point temperature ([T1] < TL< [T2]), thus evaporating said carrier while said dispersant remains in said first layer, and wherein the first layer is flattened with a leveling apparatus after said carrier has evaporated, (c) printing a subsequent layer of said at least one ink on said first layer of at least one ink, (d) building the object by repeating steps (a) to (c), (e) after steps (a)-(d), heating the object in an oven to evaporate organic material, (f) after step (e), heating the object to a further elevated temperature where full sintering occurs.
A vane arm assembly for a gas turbine engine comprising: a vane arm having a first end , a second end opposite the first end, and an aperture proximate the second end, the aperture being defined by an aperture wall ; a vane stem extending through the aperture of the vane arm; and a mechanical fastener retaining a position of the vane arm in a longitudinal direction of the vane stem, characterized by an impedance clip partially enclosing a portion of the second end of the vane arm to provide redundant position retention of the vane arm in the longitudinal direction of the vane stem. a vane arm having a first end , a second end opposite the first end, and an aperture proximate the second end, the aperture being defined by an aperture wall ; a vane stem extending through the aperture of the vane arm; and a mechanical fastener retaining a position of the vane arm in a longitudinal direction of the vane stem, characterized by an impedance clip partially enclosing a portion of the second end of the vane arm to provide redundant position retention of the vane arm in the longitudinal direction of the vane stem.
A clear, layered thermoplastic material for use in transparent, flame-resistant components, the layered thermoplastic material meeting Federal Aviation Administration FAR 25.853 requirements in terms of flammability resistance properties and heat release requirements, the layered material comprising: a transparent inner polymeric layer of polycarbonate material having a melt temperature between about 270 and 300 degrees Celsius which does not meeting the Federal Aviation Administration FAR 25.853 heat release requirements; and a first transparent outer polymeric layer coupled to a first side of said transparent inner polymeric layer and a second transparent outer polymeric layer coupled to a second side of said transparent inner polymeric layer , such that said transparent inner polymeric layer is contained between said first side and said second side, wherein said first and second transparent outer polymeric layers are a film material selected from the group consisting of polyetherketoneketone and polyetheretherketone meeting Federal Aviation Administration FAR 25.853 requirements in terms of flammability resistance properties and heat release requirements, wherein the thickness of the transparent inner polymeric layer is between about 0.76 mm and 5.1 mm (0.030 inches and 0.200 inches) and the thickness of the transparent outer polymeric layers do not exceed about 0.13 mm (5 mil). a transparent inner polymeric layer of polycarbonate material having a melt temperature between about 270 and 300 degrees Celsius which does not meeting the Federal Aviation Administration FAR 25.853 heat release requirements; and a first transparent outer polymeric layer coupled to a first side of said transparent inner polymeric layer and a second transparent outer polymeric layer coupled to a second side of said transparent inner polymeric layer , such that said transparent inner polymeric layer is contained between said first side and said second side, wherein said first and second transparent outer polymeric layers are a film material selected from the group consisting of polyetherketoneketone and polyetheretherketone meeting Federal Aviation Administration FAR 25.853 requirements in terms of flammability resistance properties and heat release requirements, wherein the thickness of the transparent inner polymeric layer is between about 0.76 mm and 5.1 mm (0.030 inches and 0.200 inches) and the thickness of the transparent outer polymeric layers do not exceed about 0.13 mm (5 mil).
A method for lubricating a driveline device, comprising supplying thereto a composition comprising: (a) an oil of lubricating viscosity; (b) 2 to 3.5 percent by weight on an active chemical basis of an oil-soluble quaternary ammonium compound comprising a hydrocarbyl-substituted imide or amide, further containing a quaternary nitrogen atom and a hydrocarbylsulfate anion; and (c) a thiadiazole compound. (a) an oil of lubricating viscosity; (b) 2 to 3.5 percent by weight on an active chemical basis of an oil-soluble quaternary ammonium compound comprising a hydrocarbyl-substituted imide or amide, further containing a quaternary nitrogen atom and a hydrocarbylsulfate anion; and (c) a thiadiazole compound.
An industrial process transmitter comprising: a sensor module in which a process sensor is located; a housing comprising: an electronics compartment having an internal space in which transmitter electronics are located; and a sensor compartment having an opening into which the sensor module is positioned; and a compression ring internal to the housing that applies a compressive force on the sensor module , wherein the compressive force arrests relative rotation of the housing and the sensor module . a sensor module in which a process sensor is located; a housing comprising: an electronics compartment having an internal space in which transmitter electronics are located; and a sensor compartment having an opening into which the sensor module is positioned; and a compression ring internal to the housing that applies a compressive force on the sensor module , wherein the compressive force arrests relative rotation of the housing and the sensor module . an electronics compartment having an internal space in which transmitter electronics are located; and a sensor compartment having an opening into which the sensor module is positioned; and a compression ring internal to the housing that applies a compressive force on the sensor module , wherein the compressive force arrests relative rotation of the housing and the sensor module .
Device for controlling an aircraft, comprising a yoke having a first and a second yoke portion , each of which are connected to a control system for controlling the aircraft, characterized in that the first and the second yoke portion can each be separately moved in a translational manner and moved in the same direction in a rotational manner and are provided for controlling the aircraft.
A method for signal detection, comprising: receiving , by a terminal, system configuration information of a second TP, from a first Transmission Point, TP, wherein the system configuration information comprises time synchronization information of the second TP, and the time synchronization information of the second TP comprises indication information for indicating whether the second TP is synchronous with the first TP; and performing , by the terminal, downlink signal detection of the second TP according to downlink timing of the first TP, when the indication information indicating that the second TP is synchronous with the first TP; wherein the first TP and the second TP are different cells. receiving , by a terminal, system configuration information of a second TP, from a first Transmission Point, TP, wherein the system configuration information comprises time synchronization information of the second TP, and the time synchronization information of the second TP comprises indication information for indicating whether the second TP is synchronous with the first TP; and performing , by the terminal, downlink signal detection of the second TP according to downlink timing of the first TP, when the indication information indicating that the second TP is synchronous with the first TP; wherein the first TP and the second TP are different cells.
Balloon catheter comprising: a balloon , wherein said balloon has a balloon membrane made of one or more expandable elastomers; a conventional catheter shaft which forms a wire lumen which is designed to guide a guide wire, and forms a fluid lumen via which a fluid can be supplied to the balloon ; wherein said balloon is attached to a first, proximal attachment site on a first catheter shaft member ; and the balloon is attached to a second, distal attachment site on a second catheter shaft member , wherein further the balloon surrounds a portion of the catheter shaft that extends between the first and second attachment sites ; and the portion of the catheter shaft which is surrounded by the balloon comprises varying regions of the catheter shaft according to the changing longitudinal extension of the balloon ; characterized in that the length of the balloon in the unextended state is ≥ 10 cm, or with a diameter of 3 mm is ≥ 30 mm. a balloon , wherein said balloon has a balloon membrane made of one or more expandable elastomers; a conventional catheter shaft which forms a wire lumen which is designed to guide a guide wire, and forms a fluid lumen via which a fluid can be supplied to the balloon ; wherein said balloon is attached to a first, proximal attachment site on a first catheter shaft member ; and the balloon is attached to a second, distal attachment site on a second catheter shaft member , wherein further the balloon surrounds a portion of the catheter shaft that extends between the first and second attachment sites ; and the portion of the catheter shaft which is surrounded by the balloon comprises varying regions of the catheter shaft according to the changing longitudinal extension of the balloon ; characterized in that the length of the balloon in the unextended state is ≥ 10 cm, or with a diameter of 3 mm is ≥ 30 mm.
Extinguishing agent container for use in a transport aircraft , wherein the extinguishing agent container comprises a lock and a reserve region , characterized in that a partition wall with a partition wall opening is arranged between the reserve region and the lock , wherein provision being made for the partition wall opening to be closable by means of a slide .
An image-processing device for performing processing of coloring a skin of an image of a person with a pattern in a certain color, comprising: a skin-identification unit configured to specify a degree of skin color of a color in the image of the person in each spot of a region in at least a part of the image of the person; and a coloring unit configured to color the image of the person with the color of the pattern at a depth corresponding to the degree of skin color of the color in said each spot. a skin-identification unit configured to specify a degree of skin color of a color in the image of the person in each spot of a region in at least a part of the image of the person; and a coloring unit configured to color the image of the person with the color of the pattern at a depth corresponding to the degree of skin color of the color in said each spot.
A method of wireless communication comprising: identifying a set of two or more available wireless communications channels for transmitting wireless communications; identifying at least one wireless communications channel of the set of available wireless communications channels that is available for transmission during a first time period; determining integrity check information, wherein the integrity check information is usable by a receiver to confirm correct channel activity detection based on a comparison of the integrity check information with an expected integrity check information for a detected channel activity at the receiver; and transmitting the integrity check information in the identified at least one wireless communications channel during the first time period. identifying a set of two or more available wireless communications channels for transmitting wireless communications; identifying at least one wireless communications channel of the set of available wireless communications channels that is available for transmission during a first time period; determining integrity check information, wherein the integrity check information is usable by a receiver to confirm correct channel activity detection based on a comparison of the integrity check information with an expected integrity check information for a detected channel activity at the receiver; and transmitting the integrity check information in the identified at least one wireless communications channel during the first time period.
Pressure-sensitive adhesive film strip which can be detached again, without leaving a residue and without causing damage, by expansive stretching substantially in the bonding plane, having a carrier which is provided on both sides with a respective adhesive composition layer, wherein • at least one of the adhesive composition layers comprises an outer adhesive composition layer which consists of an adhesive which is based on vinyl aromatic block copolymers and tackifier resins, wherein at least 75% (based on the total amount of resin) of the resin is chosen with a DACP (diacetone alcohol cloud point) of greater than -20°C, preferably greater than 0°C, wherein the DACP is determined in each case by cooling a heated solution of 5 g of resin, 5 g of xylene and 5 g of diacetone alcohol to the point at which the solution becomes cloudy, and wherein at least 75 wt.% of the tackifier resins are hydrocarbon resins or terpene resins or a mixture thereof, and • the carrier has at least one layer which consists of a polyurethane having an elongation at break of at least 100%, wherein the elongation at break is measured in a test atmosphere of 23°C and 50% relative humidity in accordance with DIN 53504 using shouldered test bars of size S3 at a rate of separation of 300 mm per minute, and a resilience of over 50%, as determined in the Test methods section of the description. • at least one of the adhesive composition layers comprises an outer adhesive composition layer which consists of an adhesive which is based on vinyl aromatic block copolymers and tackifier resins, wherein at least 75% (based on the total amount of resin) of the resin is chosen with a DACP (diacetone alcohol cloud point) of greater than -20°C, preferably greater than 0°C, wherein the DACP is determined in each case by cooling a heated solution of 5 g of resin, 5 g of xylene and 5 g of diacetone alcohol to the point at which the solution becomes cloudy, and wherein at least 75 wt.% of the tackifier resins are hydrocarbon resins or terpene resins or a mixture thereof, and • the carrier has at least one layer which consists of a polyurethane having an elongation at break of at least 100%, wherein the elongation at break is measured in a test atmosphere of 23°C and 50% relative humidity in accordance with DIN 53504 using shouldered test bars of size S3 at a rate of separation of 300 mm per minute, and a resilience of over 50%, as determined in the Test methods section of the description.
Process for the production of methanol from gaseous hydrocarbons, comprising the following steps: a. treating said gaseous hydrocarbons in a desulfurization unit producing a desulfurized hydrocarbon gas; b. reacting said desulfurized gas with an oxidising flow by means of a short contact time catalytic partial oxidation reaction to produce synthesis gas; c. producing hydrogen by electrolysis of water; d. mixing and compressing the synthesis gas and hydrogen; and e. sending said compressed mixture to a methanol synthesis unit to produce methanol. a. treating said gaseous hydrocarbons in a desulfurization unit producing a desulfurized hydrocarbon gas; b. reacting said desulfurized gas with an oxidising flow by means of a short contact time catalytic partial oxidation reaction to produce synthesis gas; c. producing hydrogen by electrolysis of water; d. mixing and compressing the synthesis gas and hydrogen; and e. sending said compressed mixture to a methanol synthesis unit to produce methanol.
Method for producing plastic granules , in which a process fluid is contained in a process chamber , underwater granulation is performed in the process chamber , the process fluid in the process chamber has a temperature which is in a temperature range of between 120°C and 160°C, a process pressure of at least 2.0 bar prevails in the process chamber , and the plastic strands are comminuted into plastic granules at this process pressure, a mixture of process fluid and plastic granules is discharged from the process chamber and supplied to a first cooling zone so as to cool the plastic granules , the plastic granules are separated from the process fluid in a first separating device at process pressure, characterized in that the process pressure is maintained in the first cooling zone , the pressure prevailing in the process chamber is higher than the pressure of the vapor pressure curve of the process fluid , and after separation of the plastic granules from the process fluid in the first separating device , the plastic granules are continuously fed in line to a dealdehydization vessel , in which the plastic granules are treated with a scavenging gas , in particular scavenging air so as to reduce the acetaldehyde content of the plastic granules .
A method for wireless communication at a transmitter, comprising: identifying a contention window comprising a first set of time-frequency resources; transmitting , to a receiver after the contention window expires, a request message to request initiation of a data transmission, the request message comprising an indication of a time of transmission from the receiver for a response message and a request threshold associated with the request message; receiving the response message from the receiver in response to the request message; measuring a signal quality metric associated with the received response message; and initiating the data transmission in a shared frequency spectrum band based at least in part on whether the signal quality metric measurement associated with the received response message exceeds a response threshold. identifying a contention window comprising a first set of time-frequency resources; transmitting , to a receiver after the contention window expires, a request message to request initiation of a data transmission, the request message comprising an indication of a time of transmission from the receiver for a response message and a request threshold associated with the request message; receiving the response message from the receiver in response to the request message; measuring a signal quality metric associated with the received response message; and initiating the data transmission in a shared frequency spectrum band based at least in part on whether the signal quality metric measurement associated with the received response message exceeds a response threshold.