mhurhangee/ep-ind-claims huggingface dataset:
A sensor for measuring the flex of a pole when exposed to one or more forces, the sensor including at least one magnet and Hall Effect sensor combination (212, 214), wherein the at least one magnet and Hall effect sensor (212, 214) are at a predetermined position relative to one another when there are no forces acting on the pole and which are movable relative to one another when forces act on the pole, such that a signal proportional to the relative movement is generated by the sensor, characterised in that the sensor is located internally inside of the pole; the sensor further comprises a cylindrical second end portion adapted to fit tightly within the pole and move therewith when the pole is acted upon by forces; and a protrusion that is not adapted to move with the pole and which has an end point in juxtaposing with an end surface of the cylindrical second end portion; wherein the sensor includes a plurality of flexible spiral elements connecting a cylindrical one end portion of the sensor with the second end portion and wherein the protrusion extends from the one end portion towards an internal surface of the second end portion; and the at least one magnet and Hall Effect sensor combination (212, 214) are located on the internal surface of the second end portion and the end point of the protrusion juxtaposed to the internal surface. the sensor is located internally inside of the pole; the sensor further comprises a cylindrical second end portion adapted to fit tightly within the pole and move therewith when the pole is acted upon by forces; and a protrusion that is not adapted to move with the pole and which has an end point in juxtaposing with an end surface of the cylindrical second end portion; wherein the sensor includes a plurality of flexible spiral elements connecting a cylindrical one end portion of the sensor with the second end portion and wherein the protrusion extends from the one end portion towards an internal surface of the second end portion; and the at least one magnet and Hall Effect sensor combination (212, 214) are located on the internal surface of the second end portion and the end point of the protrusion juxtaposed to the internal surface.
Capacitive detection device comprising: - at least one capacitive measurement electrode; - a current detector electrically referenced to a common ground and sensitive to an electric current flowing over a measurement input; - at least one alternating voltage excitation source electrically connected or coupled to the measurement input of the current detector and to the at least one capacitive measurement electrode; - guard elements electrically connected or coupled to the measurement input of the current detector; characterized in that it also comprises power supply generation means suitable for generating at least one secondary power supply source (Vf) referenced to the electrical potential of the guard elements, said power supply generation means also being arranged so as to have, within a frequency band extending from direct current, an impedance between the common ground and the guard elements with a reactive component of a capacitive or essentially capacitive type, or comparable to an open circuit. - at least one capacitive measurement electrode; - a current detector electrically referenced to a common ground and sensitive to an electric current flowing over a measurement input; - at least one alternating voltage excitation source electrically connected or coupled to the measurement input of the current detector and to the at least one capacitive measurement electrode; - guard elements electrically connected or coupled to the measurement input of the current detector;
An oil type release agent for die casting characterized by comprising: 0.2-1.2% by mass of water consisting of one or two kinds of water selected from distilled water, ion-exchange kinds of water, tap water and water comprising any one of aforementioned kinds of water and electrolyte(s) dissolved therein; and 0.8-4.8% by mass of a solubilizing agent.
A header for a combine harvester comprising a cutter bar and a rotatable reel, the reel comprising a central tube rotatable about a central axis and supported by two lateral supports, the reel comprising a first and second reel portion (10,11), each reel portion comprising two or more transverse members (13,14,20) mounted on the central tube and a plurality of tine bars (15,16) with tines attached thereto, the tine bars being coupled to the transverse members at regular intervals along the circumference of the members, the reel having an upper half above the central axis and a lower half below the central axis, characterized in that the central tube is further supported by at least one intermediate support, and that the first and second reel portion (10,11) are on either side of the intermediate support, and the two transverse members on either side of the intermediate support, belonging respectively to the first and second reel portion (10,11), are configured to be maintained in a slanted position with respect to the intermediate support during rotation of the reel, the slanted positions being such that the two slanted members are closer together in the lower half of the reel than in the upper half of the reel and wherein the tine bars (15,16) of both reel portions (10,11) are pivotably connected to the slanted members so that the rotation of the reel generates a reciprocating motion of at least a portion of the tine bars in the axial direction of the reel.
Clamping connection of a strut element for the coupling connection of assemblies or components, the clamping connection comprising an end region of a substantially tubular strut and a threaded bolt, characterized by a threaded sleeve which is arranged in the end region of the tubular strut in a radial annular gap between the threaded bolt and the inner cross section of the strut and has a conical external thread and an internal thread which corresponds to the threaded bolt, the strut end having a conical internal thread which corresponds to the external thread of the threaded sleeve, and the threaded sleeve being of radially elastic configuration at least in the region of its strut-side end.
A pressurized air system for an aircraft, the pressurized air system comprising: a compressor having a compressor inlet and a compressor outlet, the compressor inlet to receive air from a first air source and the compressor outlet to supply pressurized air to an environmental control system of the aircraft; a turbine having a turbine inlet to receive air from a second air source; a first overrunning clutch operatively coupled between an output shaft of an accessory gearbox and the compressor, the accessory gearbox operatively coupled to a drive shaft extending from an engine of the aircraft; and a second overrunning clutch operatively coupled between the compressor and the turbine, the first and second overrunning clutches (261, 265) to enable the accessory gearbox to drive the compressor during a first mode of operation and to enable the turbine to drive the compressor during a second mode of operation. a compressor having a compressor inlet and a compressor outlet, the compressor inlet to receive air from a first air source and the compressor outlet to supply pressurized air to an environmental control system of the aircraft; a turbine having a turbine inlet to receive air from a second air source; a first overrunning clutch operatively coupled between an output shaft of an accessory gearbox and the compressor, the accessory gearbox operatively coupled to a drive shaft extending from an engine of the aircraft; and a second overrunning clutch operatively coupled between the compressor and the turbine, the first and second overrunning clutches (261, 265) to enable the accessory gearbox to drive the compressor during a first mode of operation and to enable the turbine to drive the compressor during a second mode of operation.
A vehicle comprising a docking port and a selectively demountable switch having a body and a rotary knob on the body, and an interface between the switch and the docking port to enable commands entered by operation of the rotary knob to be communicated to the vehicle, wherein the docking port is configured to physically restrain the switch body when docked with the docking port, and the switch provides an input interface to a tow-assist system of the vehicle, which the vehicle has positive power-assisted steering, whereby operation of the rotary knob provides the tow-assist system with desired direction indications of a trailer connected to the vehicle during reversing of the vehicle and the tow-assist system controls steering of the vehicle.
Buried or semi-buried refuse collecting receptacle comprising a cylindrical containing (1, 10) whose transverse cross-section is at least partially confounded with an figure invariant by rotation, characterised in that the transverse cross-section of the container (1, 10) comprises a part (5, 10b) which is not confounded with the figure invariant by rotation.
An invisible bias generator, defined as an electronic device having at least two internal devices where the physical geometries of the internal devices cannot be used to determine the operating characteristics of the said electronic device, the invisible bias generator comprising: a first floating gate device as one of the at least two internal devices, the first floating gate device having a first geometry and a first characteristic; a second floating gate device as another one of the at least two internal devices, the second floating gate device having a second geometry and a second characteristic; and an output, wherein a level of the output is dependent upon a difference in the first characteristic and the second characteristic wherein either the first geometry and the second geometry are the same and the second characteristic is different than the first characteristic or the first geometry and the second geometry are different and the second characteristic is the same as the first characteristic. a first floating gate device as one of the at least two internal devices, the first floating gate device having a first geometry and a first characteristic; a second floating gate device as another one of the at least two internal devices, the second floating gate device having a second geometry and a second characteristic; and an output, wherein a level of the output is dependent upon a difference in the first characteristic and the second characteristic wherein either the first geometry and the second geometry are the same and the second characteristic is different than the first characteristic or the first geometry and the second geometry are different and the second characteristic is the same as the first characteristic.
A system for aiding airdrop computations, comprising in combination: a ground system that includes a first computer that receives data from a plurality of sensors; and an airborne system that includes a second computer that calculates a release point for an airdrop manoeuvre; wherein the ground system and the airborne system are configured for communication via a data link; wherein the first computer is configured to communicate the sensor data to the second computer via the data link in real-time, wherein the second computer is configured to calculate the release point based on the sensor data, characterised in that the second computer is configured to communicate status of the airdrop manoeuvre to the first computer via the data link in real-time, and wherein the first computer is configured to display, on an interface unit, (i) the status data of the airdrop manoeuvre, and (ii) an aircraft symbol overlaying a lateral track that the aircraft is expected to follow for the air drop manoeuvre, the lateral track including a stabilization point, at which the second computer finalises the calculation of the release point for use in the airdrop manoeuvre. a ground system that includes a first computer that receives data from a plurality of sensors; and an airborne system that includes a second computer that calculates a release point for an airdrop manoeuvre; wherein the ground system and the airborne system are configured for communication via a data link; wherein the first computer is configured to communicate the sensor data to the second computer via the data link in real-time, wherein the second computer is configured to calculate the release point based on the sensor data, characterised in that the second computer is configured to communicate status of the airdrop manoeuvre to the first computer via the data link in real-time, and wherein the first computer is configured to display, on an interface unit, (i) the status data of the airdrop manoeuvre, and (ii) an aircraft symbol overlaying a lateral track that the aircraft is expected to follow for the air drop manoeuvre, the lateral track including a stabilization point, at which the second computer finalises the calculation of the release point for use in the airdrop manoeuvre. (i) the status data of the airdrop manoeuvre, and (ii) an aircraft symbol overlaying a lateral track that the aircraft is expected to follow for the air drop manoeuvre, the lateral track including a stabilization point, at which the second computer finalises the calculation of the release point for use in the airdrop manoeuvre.
A bread making method, comprising steps 1 to 6: step 1, providing a bread ingredient box with a weak outer wall; step 2. putting a bread ingredient with flour and baking powder according to a proper formula into a first accommodating room of the bread ingredient box and packaging the bread ingredient; step 3. placing the bread ingredient box faced down in a hanging rack above a baking pan inside an automatic bread maker, operating the bread maker to make a sawtooth blade of the hanging rack pierce up the wall of the bread ingredient box and then dropping the bread ingredient inside down to different stock bins for temporary storage, controlling the covers of the stock bins to open at different times as required, making the bread ingredient drop to the baking pan, watering the baking pan at the same time; step 4. closing a housing of the automatic bread maker and turning on the baking pan of the automatic bread maker, processing the bread ingredient into a working dough by mixing, stirring and kneading so as to get a first dough from the baking pan; step 5. allowing the dough to rest and ferment in the baking pan, causing fermentation air to degas out of the dough; step 6. heating the dough in the baking pan and baking the dough until the bread is shaped well; getting the baking pan out, and removing the shaped bread. step 1, providing a bread ingredient box with a weak outer wall; step 2. putting a bread ingredient with flour and baking powder according to a proper formula into a first accommodating room of the bread ingredient box and packaging the bread ingredient; step 3. placing the bread ingredient box faced down in a hanging rack above a baking pan inside an automatic bread maker, operating the bread maker to make a sawtooth blade of the hanging rack pierce up the wall of the bread ingredient box and then dropping the bread ingredient inside down to different stock bins for temporary storage, controlling the covers of the stock bins to open at different times as required, making the bread ingredient drop to the baking pan, watering the baking pan at the same time; step 4. closing a housing of the automatic bread maker and turning on the baking pan of the automatic bread maker, processing the bread ingredient into a working dough by mixing, stirring and kneading so as to get a first dough from the baking pan; step 5. allowing the dough to rest and ferment in the baking pan, causing fermentation air to degas out of the dough; step 6. heating the dough in the baking pan and baking the dough until the bread is shaped well; getting the baking pan out, and removing the shaped bread.
Drive train for driving a wheel drive shaft or wheel set shaft coupled to at least one drive wheel; - having a chassis frame or bogie, on which the at least one drive wheel /the drive wheels are mounted; - having at least one electric drive machine; - having a transmission unit in the drive power flux between the drive machine and the drive wheels; - having a grounding device between chassis frame or bogie and the wheel drive shaft or wheel set shaft; wherein the transmission unit is formed with - a transmission housing; - an input shaft, which is mounted in the transmission housing via at least one bearing arrangement (L1, L2) and can be coupled to an electrical drive machine, and at least one output; - a grounding device, which is assigned to the input shaft and is connected at least indirectly to the transmission housing, for transmitting currents between the input shaft and the transmission housing; wherein the grounding device is arranged upstream of the first bearing arrangement on the input side of the input shaft into the transmission housing in the force flux direction, as viewed from the drive machine to the output of the transmission unit; wherein means are arranged on the transmission housing for connecting a device for the electrical coupling to a component spaced apart spatially from said transmission housing; and wherein the transmission housing is electrically coupled to the chassis frame or to the bogie to form at least one electrically conductive connection. - having a chassis frame or bogie, on which the at least one drive wheel /the drive wheels are mounted; - having at least one electric drive machine; - having a transmission unit in the drive power flux between the drive machine and the drive wheels; - having a grounding device between chassis frame or bogie and the wheel drive shaft or wheel set shaft; wherein the transmission unit is formed with - a transmission housing; - an input shaft, which is mounted in the transmission housing via at least one bearing arrangement (L1, L2) and can be coupled to an electrical drive machine, and at least one output; - a grounding device, which is assigned to the input shaft and is connected at least indirectly to the transmission housing, for transmitting currents between the input shaft and the transmission housing;
A method for lubricating a strain wave gearing using a powder of an ionic crystalline compound having a layered crystal structure, said method characterized in that: carrying out braking-in operation of the strain wave gearing using non-hydrophobized powder having been enclosed or packed as the powder of the ionic crystalline compound in an internal space of the strain wave gearing, the internal space being communicated with contact surfaces to be lubricated; transferring the non-hydrophobized powder to the contact surfaces to form a lubricating film on the contact surfaces by the breaking-in operation; after the breaking-in operation, removing any non-hydrophobized powder remaining in the internal space and enclosing or packing a hydrophobized powder in the internal space as a powder of the ionic crystalline compound; and during operation under load, maintaining a lubricated state of the contact surfaces by the lubricating film and the hydrophobized powder enclosed or packed in the internal space. carrying out braking-in operation of the strain wave gearing using non-hydrophobized powder having been enclosed or packed as the powder of the ionic crystalline compound in an internal space of the strain wave gearing, the internal space being communicated with contact surfaces to be lubricated; transferring the non-hydrophobized powder to the contact surfaces to form a lubricating film on the contact surfaces by the breaking-in operation; after the breaking-in operation, removing any non-hydrophobized powder remaining in the internal space and enclosing or packing a hydrophobized powder in the internal space as a powder of the ionic crystalline compound; and during operation under load, maintaining a lubricated state of the contact surfaces by the lubricating film and the hydrophobized powder enclosed or packed in the internal space.
A thermoplastic composition consisting of: from 49 wt. % to 98 wt. % of a polycarbonate component; from 1 wt. % to 50 wt. % of a filler; and from 0. 5 wt. % to 10 wt. % of an unmodified polyolefin elastomer, and optionally an additive selected from the group consisting of a plasticizer, a stabilizer, an anti-static agent, a colorant, an antioxidant, a mold release agent, an ultraviolet absorber, a lubricant, a blowing agent, or a combination thereof. wherein the thermoplastic composition exhibits an notched Izod impact strength of at least 150 J/m to 750 J/m at 23 °C according to ASTM D256, wherein the thermoplastic composition exhibits a modulus of at least 3300 MPa to 6100 MPa according to ASTM D638, wherein the thermoplastic composition exhibits a melt flow rate of at least 10 g/10 min to 25 g/10 min when measured at 300 °C under a load of 1.2 kg, or at 260 °C under a load of 5 kg according to ASTM D 1238, and wherein the combined weight percent value of all components does not exceed 100 wt. %, and wherein all weight percent values are based on the total weight of the composition. from 49 wt. % to 98 wt. % of a polycarbonate component; from 1 wt. % to 50 wt. % of a filler; and from 0. 5 wt. % to 10 wt. % of an unmodified polyolefin elastomer, and optionally an additive selected from the group consisting of a plasticizer, a stabilizer, an anti-static agent, a colorant, an antioxidant, a mold release agent, an ultraviolet absorber, a lubricant, a blowing agent, or a combination thereof. wherein the thermoplastic composition exhibits an notched Izod impact strength of at least 150 J/m to 750 J/m at 23 °C according to ASTM D256, wherein the thermoplastic composition exhibits a modulus of at least 3300 MPa to 6100 MPa according to ASTM D638, wherein the thermoplastic composition exhibits a melt flow rate of at least 10 g/10 min to 25 g/10 min when measured at 300 °C under a load of 1.2 kg, or at 260 °C under a load of 5 kg according to ASTM D 1238, and wherein the combined weight percent value of all components does not exceed 100 wt. %, and wherein all weight percent values are based on the total weight of the composition.