mhurhangee/ep-ind-claims huggingface dataset:
A wireless system operable to issue commands to a robotic device according to a typematic rate of interface, the system comprising: a processor operably coupled to the robotic device, wherein the robotic device further comprises a laser ultrasonic system operable to generate and detect ultrasonic surface displacements on a remote object (50,150); and a wireless communicator operably interfaced to the processor wherein the wireless communicator is operable to generate at least one command signal based on the typematic rate of interface; and the processor is operable to receive the at least one command signal and to operate the robotic device. a processor operably coupled to the robotic device, wherein the robotic device further comprises a laser ultrasonic system operable to generate and detect ultrasonic surface displacements on a remote object (50,150); and a wireless communicator operably interfaced to the processor wherein the wireless communicator is operable to generate at least one command signal based on the typematic rate of interface; and the processor is operable to receive the at least one command signal and to operate the robotic device.
A modified Cry1Ca toxin comprising residues 2 to 628 of SEQ ID NO:10 wherein amino acid residue 54 is selected from the group consisting of Gly and Ala, amino acid residue 57 is chosen from the group consisting of Leu and Met, amino acid residue 68 is chosen from the group consisting of Val, Phe, and Ile, amino acid residue 73 is chosen from the group consisting of Trp, Ala and Met, amino acid residue 596 is Met, and amino acid residue 620 is chosen from the group consisting of Leu and Phe.
A method of increasing speed of an electro-mechanical relay, the method comprising the steps of: providing an electro-mechanical relay having a coil and at least one contact, characterized by providing a first resistor and a second resistor, each in series with the coil, with the second resistor being in parallel with a first switch, providing a voltage to the first switch, with the first switch being ON, thereby shorting out the second resistor and providing a first constant current through the first resistor and to the coil, to move the contact to a closed position, thereby establishing a closing time of the contact to be about 1 mS, and after a certain amount of time, turning the first switch OFF, so that a second constant current is provided through the first and second resistors and to the coil, maintaining the contact in the closed position, thereby minimizing bouncing of the contact, wherein the electro-mechanical relay is provided as an output relay of a protective relay. providing an electro-mechanical relay having a coil and at least one contact, characterized by providing a first resistor and a second resistor, each in series with the coil, with the second resistor being in parallel with a first switch, providing a voltage to the first switch, with the first switch being ON, thereby shorting out the second resistor and providing a first constant current through the first resistor and to the coil, to move the contact to a closed position, thereby establishing a closing time of the contact to be about 1 mS, and after a certain amount of time, turning the first switch OFF, so that a second constant current is provided through the first and second resistors and to the coil, maintaining the contact in the closed position, thereby minimizing bouncing of the contact, wherein the electro-mechanical relay is provided as an output relay of a protective relay.
An UV-enhancer suitable for being arranged in an interspace of a high pressure gas discharge lamp comprising a discharge vessel and an outer envelope enclosing said discharge vessel and defining said interspace between the outer envelope and the discharge vessel, the UV-enhancer having a wall enclosing an electrode space with a filling gas and an internal electrode extending from the electrode space through the wall to the said interspace, said wall of the UV-enhancer being made of ceramic material,whereby the electrode is directly sintered on to the wall of the UV-enhancer, characterized in that the electrode is a closed metal tube.
An actuator system for a flight control surface of an aerial vehicle, comprising: a differential gear set having a first sun gear, a second sun gear and at least one planet gear (94a, 94b) configured to directly drive the flight control surface; a first electric servomotor configured to be coupled to the aerial vehicle, and the first electric servomotor drives the first sun gear to drive the at least one planet gear; and a second electric servomotor configured to be coupled to the aerial vehicle, and the second electric servomotor drives the second sun gear to drive the at least one planet gear such that the first electric servomotor and the second electric servomotor are configured to cooperate to rotate the flight control surface relative to the aerial vehicle by producing a single rotary output. a differential gear set having a first sun gear, a second sun gear and at least one planet gear (94a, 94b) configured to directly drive the flight control surface; a first electric servomotor configured to be coupled to the aerial vehicle, and the first electric servomotor drives the first sun gear to drive the at least one planet gear; and a second electric servomotor configured to be coupled to the aerial vehicle, and the second electric servomotor drives the second sun gear to drive the at least one planet gear such that the first electric servomotor and the second electric servomotor are configured to cooperate to rotate the flight control surface relative to the aerial vehicle by producing a single rotary output.
A lance for the combustion or flaring of combustible waste gases, comprising a waste gas channel annular in cross section and communicating with an outlet, wherein the waste gas channel is equipped with adjustment means for adjusting the flow cross section, said adjustment means comprising an adjustment body coaxially mounted in the interior of an external combustion tube and adjustable in the axial direction of the lance between a minimum position for the smallest flow cross section and a maximum position for the largest flow cross section, the conical lateral surface of which adjustment body, together with an associated, further conical surface, delimits the annular waste gas channel internally and externally, wherein the adjustment body is comprised of a body internally delimiting the waste gas channel and having a conical outer lateral surface, wherein the further conical surface constitutes a conical inner circumferential surface of the external combustion tube, whose diameter continuously increases in the direction to the outlet of the lance, and wherein the conical surfaces (9, 11) cover each other in the minimum position.
A telephoto lens system comprising: a first lens group having a positive refractive power and comprising a negative lens (111, 112, 113, 114) that is disposed closest to an object side and has a meniscus shape that is convex toward the object; a second lens group having a negative refractive power and consisting of a single negative lens (211, 212, 213, 214) that moves along an optical axis and performs focusing; and a third lens group having a positive refractive power, further comprising an aperture diaphragm interposed between the second lens group and the third lens group, wherein the first through third lens groups are disposed sequentially from the object side toward the image side, and the telephoto lens system satisfies the conditions: 0.5 < | f 2 / f | < 0.81, wherein f 2 denotes the focal length of the second lens group, and f denotes the focal length of the telephoto lens system; nd 3 > 1.78, wherein nd 3 denotes an average of refractive indexes of lenses constituting the third lens group; and vd 2 > 63, wherein vd 2 denotes an Abbe number of the second lens group.. a first lens group having a positive refractive power and comprising a negative lens (111, 112, 113, 114) that is disposed closest to an object side and has a meniscus shape that is convex toward the object; a second lens group having a negative refractive power and consisting of a single negative lens (211, 212, 213, 214) that moves along an optical axis and performs focusing; and a third lens group having a positive refractive power, further comprising an aperture diaphragm interposed between the second lens group and the third lens group, wherein the first through third lens groups are disposed sequentially from the object side toward the image side, and the telephoto lens system satisfies the conditions: 0.5 < | f 2 / f | < 0.81, wherein f 2 denotes the focal length of the second lens group, and f denotes the focal length of the telephoto lens system; nd 3 > 1.78, wherein nd 3 denotes an average of refractive indexes of lenses constituting the third lens group; and vd 2 > 63, wherein vd 2 denotes an Abbe number of the second lens group..
A humanized form of a murine anti-FGF19 antibody comprising: (i) a light chain comprising (a) hypervariable region -L1 sequences comprising sequence A1-A11, wherein A1-A11 is KASQDINSFLA (SEQ ID NO:11); (b) HVR-L2 comprising sequence B1-B7, wherein B1-B7 is RANRLVD (SEQ ID NO:2), RANRLVS (SEQ ID NO:13), or RANRLVE (SEQ ID NO:14); and (c) HVR-L3 comprising sequence C1-C9, wherein C1-C9 is LQYDEFPLT (SEQ ID NO:3); and (ii) a heavy chain comprising (a) HVR-H1 comprising sequence D1-D10, wherein D1-D10 is GFSLTTYGVH (SEQ ID NO:4); (b) HVR-H2 comprising sequence E1-E17, wherein E1-E17 is GVIWPGGGTDYNAAFIS (SEQ ID NO:7); and (c) HVR-H3 comprising sequence F1-F13, wherein F1-F13 is VRKEYANLYAMDY (SEQ ID NO:8); and (iii) light chain human K subgroup 1 consensus framework sequence, and (iv) heavy chain human subgroup III consensus framework sequence. (i) a light chain comprising (a) hypervariable region -L1 sequences comprising sequence A1-A11, wherein A1-A11 is KASQDINSFLA (SEQ ID NO:11); (b) HVR-L2 comprising sequence B1-B7, wherein B1-B7 is RANRLVD (SEQ ID NO:2), RANRLVS (SEQ ID NO:13), or RANRLVE (SEQ ID NO:14); and (c) HVR-L3 comprising sequence C1-C9, wherein C1-C9 is LQYDEFPLT (SEQ ID NO:3); and (ii) a heavy chain comprising (a) HVR-H1 comprising sequence D1-D10, wherein D1-D10 is GFSLTTYGVH (SEQ ID NO:4); (b) HVR-H2 comprising sequence E1-E17, wherein E1-E17 is GVIWPGGGTDYNAAFIS (SEQ ID NO:7); and (c) HVR-H3 comprising sequence F1-F13, wherein F1-F13 is VRKEYANLYAMDY (SEQ ID NO:8); and (iii) light chain human K subgroup 1 consensus framework sequence, and (iv) heavy chain human subgroup III consensus framework sequence.
System comprising a transducer, a hydrogen-containing fluid medium and a first space; which transducer determines the pressure of the hydrogen-containing fluid medium; wherein the hydrogen-containing fluid medium is arranged in the first space; wherein the transducer comprises a pressure side end facing the fluid medium; wherein the transducer comprises a housing which comprises a second space; wherein the transducer comprises a measuring arrangement; wherein the measuring arrangement is arranged in the second space; wherein at the pressure side end the transducer comprises a diaphragm for hermetically separating the first space containing the hydrogen-containing fluid medium from the second space; wherein the diaphragm comprises a metallic material; characterized in that the metallic material is made of a high-alloy martensite; wherein a high-alloy martensite is a martensite with an alloy content > 5 wt.%; wherein the alloy content is the content by mass of an alloying element; wherein alloying elements are understood to mean exclusively chromium, molybdenum or nickel.
A method for maneuvering an aircraft using an autopilot, a camera coupled to the aircraft, and a display configured to display an image captured by the camera, the method comprising: - detecting a first position (A, α, β) of the camera; - determining a first direction from the first position (A, α, β) of the camera directed towards a first target point, wherein the first target point corresponds to an image point within the image displayed by the display; - determining whether the aircraft is in a locked path flight mode or a camera tracking flight mode; characterized in that - if the aircraft is in the locked path flight mode, performing the steps of: -- maneuvering the aircraft according to a speed control signal and substantially along a locked flight path, wherein the locked flight path is defined, at least in part, by the detected first position (A, α, β) and the determined first direction, and -- allowing the camera to tilt and/or pan freely without affecting the maneuvering of the aircraft along the locked flight path; and - if the aircraft is in the camera tracking flight mode, performing the steps of: -- maneuvering the aircraft according to the speed control signal and substantially along a second flight path defined, at least in part, by the detected first position (A, α, β) and the determined first direction, wherein the second flight path is continuously and automatically updated every time the direction of the camera changes. - detecting a first position (A, α, β) of the camera; - determining a first direction from the first position (A, α, β) of the camera directed towards a first target point, wherein the first target point corresponds to an image point within the image displayed by the display; - determining whether the aircraft is in a locked path flight mode or a camera tracking flight mode; - if the aircraft is in the locked path flight mode, performing the steps of: -- maneuvering the aircraft according to a speed control signal and substantially along a locked flight path, wherein the locked flight path is defined, at least in part, by the detected first position (A, α, β) and the determined first direction, and -- allowing the camera to tilt and/or pan freely without affecting the maneuvering of the aircraft along the locked flight path; and -- maneuvering the aircraft according to a speed control signal and substantially along a locked flight path, wherein the locked flight path is defined, at least in part, by the detected first position (A, α, β) and the determined first direction, and -- allowing the camera to tilt and/or pan freely without affecting the maneuvering of the aircraft along the locked flight path; and - if the aircraft is in the camera tracking flight mode, performing the steps of: -- maneuvering the aircraft according to the speed control signal and substantially along a second flight path defined, at least in part, by the detected first position (A, α, β) and the determined first direction, wherein the second flight path is continuously and automatically updated every time the direction of the camera changes.
Nanostructure composed of one or multiple concentric layers around a carbon or vacuum core, comprising said one or multiple concentric layers at least one of the following components in crystalline or polycrystalline form: intrinsic silicon, intrinsic germanium, p or n doped silicon, p or n doped germanium, intrinsic silicon-germanium alloys, p or n doped silicon-germanium alloys, silicon oxide, germanium oxide, silicon nitride, germanium nitride or a combination thereof, characterized in that said nanostructure comprises metal particles attached by means of nanowires to at least one of said concentric layers or in that said nanostructure comprises holes in at least one of said concentric layers, which holes correspond to previously deposited metal particles which have been removed.
A method for detecting the presence of conductive objects, the method comprising: - determining (102, 104) a characteristic frequency function of an undisturbed magnetic tracking system; - measuring (108, 110) a disturbed real-time frequency function; - calculating real and imaginary components of the position indication signal using a chi-squared minimization of the disturbed frequency function to the undisturbed frequency function; - calculating a single chi-squared value based on the characteristic frequency function at multiple frequencies and the disturbed frequency function at equivalent multiple frequencies; and - monitoring the chi-squared value to detect changes indicating the presence of a conductive object. - determining (102, 104) a characteristic frequency function of an undisturbed magnetic tracking system; - measuring (108, 110) a disturbed real-time frequency function; - calculating real and imaginary components of the position indication signal using a chi-squared minimization of the disturbed frequency function to the undisturbed frequency function; - calculating a single chi-squared value based on the characteristic frequency function at multiple frequencies and the disturbed frequency function at equivalent multiple frequencies; and - monitoring the chi-squared value to detect changes indicating the presence of a conductive object.
Surface suction gripper for sucking and handling an object, with a gripper base part having a first vacuum chamber to be evacuated by means of a vacuum supply, and having a suction part facing the object and comprising a suction side, which can be connected with the gripper base part, wherein a quick exchange device is provided which is adapted for connecting the gripper base part and the suction part, characterized in that the quick exchange device is configured such that the suction part can be connected to the gripper base part unilaterally for reaching a pre-mounting position in such a way that the suction part can be folded into a final mounting position for a fluid-tight connection with the gripper base part, wherein the quick exchange device comprises a hook-up device which is configured in such a way that the suction part can be hooked unilaterally onto the gripper base part.
A method, comprising: sending a message to a user equipment having a variable rate vocoder, the message defining transport block sizes for the user equipment to select from in making uplink transmissions if the user equipment is permitted to vary a packet size during uplink transmission; and sending a scheduling grant to the user equipment, the scheduling grant including an indicator indicating whether the user equipment is permitted to vary the packet size during uplink transmissions by selecting a transport block size from among the defined transport block sizes; wherein, when the indicator indicates that the user equipment is permitted to vary the packet size, the indicator indicates that the user equipment is permitted to select a smallest of the defined transport block sizes that permits delivery of data in a buffer of the user equipment. sending a message to a user equipment having a variable rate vocoder, the message defining transport block sizes for the user equipment to select from in making uplink transmissions if the user equipment is permitted to vary a packet size during uplink transmission; and sending a scheduling grant to the user equipment, the scheduling grant including an indicator indicating whether the user equipment is permitted to vary the packet size during uplink transmissions by selecting a transport block size from among the defined transport block sizes; wherein, when the indicator indicates that the user equipment is permitted to vary the packet size, the indicator indicates that the user equipment is permitted to select a smallest of the defined transport block sizes that permits delivery of data in a buffer of the user equipment.
A straddled vehicle comprising: a right seat frame (4, 4A) extending in a vehicle longitudinal direction in a plan view of the vehicle; a left seat frame (5, 5A) disposed leftward of the right seat frame, and extending in the vehicle longitudinal direction in the plan view of the vehicle; a seat disposed above the right seat frame and the left seat frame; a first case disposed leftward of the right seat frame, rightward of the left seat frame, and below the seat; a second case (61, 61A) separate from the first case, and disposed leftward of the right seat frame, rightward of the left seat frame, below the seat, and a plurality of first electrical components stored in the first case; and a plurality of second electrical components stored in the second case; wherein the first electrical components comprise: a battery; and a hydraulic unit; and the second electrical components comprise: a first connector (91, 91A) for connecting wiring of a taillight; and the second case is smaller in volume than the first case, characterized in that the second case (61, 61A) is disposed behind the first case such that a length that is a distance in the longitudinal direction of the straddled vehicle from a front end of the first case to a rear end of the first case is smaller than a length (Lc) that is a distance in the longitudinal direction of the straddled vehicle from the front end of the first case to a rear end (61 r, 61rA) of the second case (61, 61A). a right seat frame (4, 4A) extending in a vehicle longitudinal direction in a plan view of the vehicle; a left seat frame (5, 5A) disposed leftward of the right seat frame, and extending in the vehicle longitudinal direction in the plan view of the vehicle; a seat disposed above the right seat frame and the left seat frame; a first case disposed leftward of the right seat frame, rightward of the left seat frame, and below the seat; a second case (61, 61A) separate from the first case, and disposed leftward of the right seat frame, rightward of the left seat frame, below the seat, and a plurality of first electrical components stored in the first case; and a plurality of second electrical components stored in the second case; wherein the first electrical components comprise: a battery; and a hydraulic unit; and a battery; and a hydraulic unit; and the second electrical components comprise: a first connector (91, 91A) for connecting wiring of a taillight; and the second case is smaller in volume than the first case, characterized in that the second case (61, 61A) is disposed behind the first case such that a length that is a distance in the longitudinal direction of the straddled vehicle from a front end of the first case to a rear end of the first case is smaller than a length (Lc) that is a distance in the longitudinal direction of the straddled vehicle from the front end of the first case to a rear end (61 r, 61rA) of the second case (61, 61A).
A method in a wireless device, comprising: transmitting a network request for voice service to a multi-channel wireless access point providing data and voice service; receiving a network reply from the wireless access point providing statistical information for a plurality of channels supported by the multi-channel wireless access point; wherein the statistical information includes latency statistics; comparing data derived from the statistical information to a threshold; and selecting one of the plurality of channels for voice traffic on the wireless device if the comparison indicates a channel can provide a performance level corresponding to the threshold. transmitting a network request for voice service to a multi-channel wireless access point providing data and voice service; receiving a network reply from the wireless access point providing statistical information for a plurality of channels supported by the multi-channel wireless access point; wherein the statistical information includes latency statistics; comparing data derived from the statistical information to a threshold; and selecting one of the plurality of channels for voice traffic on the wireless device if the comparison indicates a channel can provide a performance level corresponding to the threshold.