mhurhangee/patent-ind-claim-en huggingface dataset:
Exhaust gas recirculation system for an internal combustion engine with - an exhaust gas channel of the internal combustion engine , - an inlet channel of the internal combustion engine , - an exhaust gas recirculation channel which branches off from the exhaust gas channel and leads into the inlet channel , - a heat exchanger which is arranged in the exhaust gas recirculation channel and comprises two separate paths , - an exhaust gas recirculation valve which is arranged at an outlet of the heat exchanger , - a flap valve which is arranged in the exhaust gas channel in such a way that the flap valve opens the exhaust gas channel in a first position, closes the exhaust gas channel in a second position in the flow direction downstream of the two paths , in a third position closes the exhaust gas channel in the region between the two paths and in a fourth position throttles the exhaust gas channel , characterised in that the heat exchanger can be bypassed via a bypass conduit , the flow cross-section of which can be controlled by means of a bypass valve and which branches off from the exhaust gas channel upstream of the flap valve . - an exhaust gas channel of the internal combustion engine , - an inlet channel of the internal combustion engine , - an exhaust gas recirculation channel which branches off from the exhaust gas channel and leads into the inlet channel , - a heat exchanger which is arranged in the exhaust gas recirculation channel and comprises two separate paths , - an exhaust gas recirculation valve which is arranged at an outlet of the heat exchanger , - a flap valve which is arranged in the exhaust gas channel in such a way that the flap valve opens the exhaust gas channel in a first position, closes the exhaust gas channel in a second position in the flow direction downstream of the two paths , in a third position closes the exhaust gas channel in the region between the two paths and in a fourth position throttles the exhaust gas channel ,
Method for operating an electrical machine , in particular an electric motor, which has a stator and a rotor and which comprises a first sensor for detecting a position of the rotor with respect to the stator or for detecting a change in a position of the rotor with respect to the stator and a second sensor for detecting an acceleration of the rotor with respect to the stator , in which method - a first sensor signal is detected by means of the first sensor , - a second sensor signal is detected by means of the second sensor , characterized in that - a speed is determined on the basis of the first and the second sensor signal , and - the speed is forwarded both to a speed control arrangement and also to a safety monitoring arrangement for executing a first safe function . - a first sensor signal is detected by means of the first sensor , - a second sensor signal is detected by means of the second sensor , characterized in that - a speed is determined on the basis of the first and the second sensor signal , and - the speed is forwarded both to a speed control arrangement and also to a safety monitoring arrangement for executing a first safe function .
A network address translation, NAT, entry management method, comprising: receiving and storing , by a NAT device , a connection parameter, wherein the connection parameter comprises an address of a controller; receiving , by the NAT device , a packet sent by a network device that is controlled by the controller, wherein a source address of the packet is a private address of the network device and a destination address of the packet is the address of the controller; performing , by the NAT device , NAT on the packet, wherein an after-NAT source address of the packet is a public address; and when a static entry condition is met, generating , by the NAT device , a target static NAT entry, wherein even if a duration in which the static NAT entry fails to be hit exceeds an aging time, the static NAT entry is not deleted, wherein the target static NAT entry comprises a correspondence between the private address of the network device, a before-NAT source port number of the packet, an after-NAT source port number of the packet, and the address of the controller, and the static entry condition comprises that the destination address of the packet is the address of the controller. receiving and storing , by a NAT device , a connection parameter, wherein the connection parameter comprises an address of a controller; receiving , by the NAT device , a packet sent by a network device that is controlled by the controller, wherein a source address of the packet is a private address of the network device and a destination address of the packet is the address of the controller; performing , by the NAT device , NAT on the packet, wherein an after-NAT source address of the packet is a public address; and when a static entry condition is met, generating , by the NAT device , a target static NAT entry, wherein even if a duration in which the static NAT entry fails to be hit exceeds an aging time, the static NAT entry is not deleted, wherein the target static NAT entry comprises a correspondence between the private address of the network device, a before-NAT source port number of the packet, an after-NAT source port number of the packet, and the address of the controller, and the static entry condition comprises that the destination address of the packet is the address of the controller.
A method characterised by comprising: transmitting (4-4), from a first apparatus to a second apparatus , over a first secure channel between the first apparatus and the second apparatus in a first access network, access information of a second network, which is required in the second access network to establish between the first apparatus and the second apparatus a parallel second secure connection over the second access network, the access information of the second network being not usable to establish a secure connection in the first access network.
A method for generating a synchronization channel by a transmitting node, comprising: determining a frequency band range for a carrier; configuring a synchronization channel information on the carrier according to the frequency band range, wherein the synchronization channel information comprises: a subcarrier spacing of the synchronization channel, and an orthogonal frequency division multiplexing, OFDM, symbol position of the synchronization channel, wherein, when the frequency band range is above 6 GHz, the configuring the synchronization channel information comprises configuring the synchronization channel to include four consecutive OFDM symbols on the carrier and the subcarrier spacing of 60 kHz; and transmitting the synchronization channel using the synchronization channel information; and transmitting data other than the synchronization channel using another subcarrier spacing when the frequency band range is less than 6 GHz, wherein the another subcarrier spacing comprises one of: 30 kHz or 60 kHz, wherein the configuring the synchronization channel information comprises configuring the synchronization channel to include two consecutive OFDM symbols on the carrier and the subcarrier spacing of 15 kHz when the frequency band range is less than 6 GHz. determining a frequency band range for a carrier; configuring a synchronization channel information on the carrier according to the frequency band range, wherein the synchronization channel information comprises: a subcarrier spacing of the synchronization channel, and an orthogonal frequency division multiplexing, OFDM, symbol position of the synchronization channel, wherein, when the frequency band range is above 6 GHz, the configuring the synchronization channel information comprises configuring the synchronization channel to include four consecutive OFDM symbols on the carrier and the subcarrier spacing of 60 kHz; and a subcarrier spacing of the synchronization channel, and an orthogonal frequency division multiplexing, OFDM, symbol position of the synchronization channel, wherein, when the frequency band range is above 6 GHz, the configuring the synchronization channel information comprises configuring the synchronization channel to include four consecutive OFDM symbols on the carrier and the subcarrier spacing of 60 kHz; and transmitting the synchronization channel using the synchronization channel information; and transmitting data other than the synchronization channel using another subcarrier spacing when the frequency band range is less than 6 GHz, wherein the another subcarrier spacing comprises one of: 30 kHz or 60 kHz, wherein the configuring the synchronization channel information comprises configuring the synchronization channel to include two consecutive OFDM symbols on the carrier and the subcarrier spacing of 15 kHz when the frequency band range is less than 6 GHz.
A method for enhancing fire-suppression for a class E cargo aircraft , comprising: receiving a fire-warning signal indicating presence of fire in a cargo compartment onboard a class E cargo aircraft at a first altitude (task 602); distributing an initial fire-suppression agent in the cargo compartment at the first altitude sufficient to suppress fire for an initial fire-suppression time interval during a depressurization phase during which the class E cargo aircraft flies to a second altitude below the first altitude (task 604) and during which airflow to the cargo compartment is shut off; distributing a re-enforcing fire-suppression agent in the cargo compartment (task 618) during a re-pressurization phase when a cabin altitude is below a predetermined cabin pressure level (PL) during which the class E cargo aircraft flies from the second altitude to a landing (task 616), after the initial fire-suppression time interval elapses; and maintaining distribution of the re-enforcing fire-suppression agent during a re-enforcing fire-suppression time interval . receiving a fire-warning signal indicating presence of fire in a cargo compartment onboard a class E cargo aircraft at a first altitude (task 602); distributing an initial fire-suppression agent in the cargo compartment at the first altitude sufficient to suppress fire for an initial fire-suppression time interval during a depressurization phase during which the class E cargo aircraft flies to a second altitude below the first altitude (task 604) and during which airflow to the cargo compartment is shut off; distributing a re-enforcing fire-suppression agent in the cargo compartment (task 618) during a re-pressurization phase when a cabin altitude is below a predetermined cabin pressure level (PL) during which the class E cargo aircraft flies from the second altitude to a landing (task 616), after the initial fire-suppression time interval elapses; and maintaining distribution of the re-enforcing fire-suppression agent during a re-enforcing fire-suppression time interval .
A general-purpose graphics processing unit including: a streaming multiprocessor having a single instruction, multiple thread, SIMT, architecture including hardware multithreading, wherein the streaming multiprocessor comprises: multiple sets of compute units (1411-1418), the compute units (1411-1418) each having a floating-point logic unit (1411B - 1418B) configured to perform floating-point operations and an integer logic unit (1411A - 1418A) configured to perform integer operations; and a memory coupled with the multiple sets of compute units, characterized in that in a compute unit the integer logic unit is enabled to execute a thread of a first instruction while the floating-point logic unit is enabled to execute a thread of a second instruction, the second instruction being different from the first instruction and the thread of the first instruction being executed concurrently with the thread of the second instruction. a streaming multiprocessor having a single instruction, multiple thread, SIMT, architecture including hardware multithreading, wherein the streaming multiprocessor comprises: multiple sets of compute units (1411-1418), the compute units (1411-1418) each having a floating-point logic unit (1411B - 1418B) configured to perform floating-point operations and an integer logic unit (1411A - 1418A) configured to perform integer operations; and a memory coupled with the multiple sets of compute units, multiple sets of compute units (1411-1418), the compute units (1411-1418) each having a floating-point logic unit (1411B - 1418B) configured to perform floating-point operations and an integer logic unit (1411A - 1418A) configured to perform integer operations; and a memory coupled with the multiple sets of compute units, characterized in that in a compute unit the integer logic unit is enabled to execute a thread of a first instruction while the floating-point logic unit is enabled to execute a thread of a second instruction, the second instruction being different from the first instruction and the thread of the first instruction being executed concurrently with the thread of the second instruction.
A device for displacing structures in a patient's body, the device comprising: an inner body having a first end and a second end ; an outer sleeve coaxial with the inner body, the outer sleeve movable relative to the inner body between a retracted position and an extended position; a strip of resilient material having a first end and a second end , the first end of the strip of resilient material fixed in position relative to the outer sleeve; and a handle with a trigger , the trigger mechanically connected to the outer sleeve such that operation of the trigger moves the outer sleeve relative to the handle and the inner body; wherein the second end of the inner body defines a cavity that is aligned with the strip of resilient material when the outer sleeve is in its retracted position, wherein the second end of the strip of resilient material is releasably engaged with the inner body when the outer sleeve is in its extended position, and wherein the second end of the strip of resilient material is disengaged from the inner body when the outer sleeve is in its retracted position such that strip of resilient material can move outward and inward with little or no contact with a portion of the second end of the inner body that defines the cavity. an inner body having a first end and a second end ; an outer sleeve coaxial with the inner body, the outer sleeve movable relative to the inner body between a retracted position and an extended position; a strip of resilient material having a first end and a second end , the first end of the strip of resilient material fixed in position relative to the outer sleeve; and a handle with a trigger , the trigger mechanically connected to the outer sleeve such that operation of the trigger moves the outer sleeve relative to the handle and the inner body; wherein the second end of the inner body defines a cavity that is aligned with the strip of resilient material when the outer sleeve is in its retracted position, wherein the second end of the strip of resilient material is releasably engaged with the inner body when the outer sleeve is in its extended position, and wherein the second end of the strip of resilient material is disengaged from the inner body when the outer sleeve is in its retracted position such that strip of resilient material can move outward and inward with little or no contact with a portion of the second end of the inner body that defines the cavity.
A system , comprising: a heat exchanger having a first passage and a second passage configured for exchange of heat therebetween, the first passage configured to receive at an inlet a boil-off gas stream of a first cryogenic fluid from a first tank , the second passage configured to receive at an inlet a liquid stream of a second cryogenic fluid from a second tank , wherein the second cryogenic fluid has a lower evaporation temperature than the first cryogenic fluid; a detection unit configured to detect a characteristic of the boil-off gas stream ; and a controller configured to acquire information from the detection unit corresponding to the characteristic and, responsive to the information acquired from the detection unit, to control the flow of the second cryogenic fluid from the second tank to provide sufficient exchange of heat from the boil-off gas stream via the heat exchanger to condense at least a portion of the boil-off gas stream, whereby a liquid stream of the first cryogenic fluid is output from the first passage and returned to the first tank, the controller being configured to control the flow of the second cryogenic fluid such that at least a portion of the second cryogenic fluid evaporates and is discharged as an exhaust gas stream from the second passage of the heat exchanger wherein the controller is configured to direct the exhaust gas stream proximate to a functional component of an aircraft system wherein the exhaust gas stream is used to inert and/or purge one or more aspects of the functional component. a heat exchanger having a first passage and a second passage configured for exchange of heat therebetween, the first passage configured to receive at an inlet a boil-off gas stream of a first cryogenic fluid from a first tank , the second passage configured to receive at an inlet a liquid stream of a second cryogenic fluid from a second tank , wherein the second cryogenic fluid has a lower evaporation temperature than the first cryogenic fluid; a detection unit configured to detect a characteristic of the boil-off gas stream ; and a controller configured to acquire information from the detection unit corresponding to the characteristic and, responsive to the information acquired from the detection unit, to control the flow of the second cryogenic fluid from the second tank to provide sufficient exchange of heat from the boil-off gas stream via the heat exchanger to condense at least a portion of the boil-off gas stream, whereby a liquid stream of the first cryogenic fluid is output from the first passage and returned to the first tank, the controller being configured to control the flow of the second cryogenic fluid such that at least a portion of the second cryogenic fluid evaporates and is discharged as an exhaust gas stream from the second passage of the heat exchanger wherein the controller is configured to direct the exhaust gas stream proximate to a functional component of an aircraft system wherein the exhaust gas stream is used to inert and/or purge one or more aspects of the functional component.
A composition comprising a compound (A) of general formula (I) comprising a compound (a) represented by the following general formula (II): wherein R 5 represents a hydrogen atom or a methyl group; and a polyfunctional compound (B) having two or more polymerizable functional groups in a molecule other than the compound (A) represented by the following general formula (I), wherein a mass ratio ((A)/ (B)) of the compound (A) to the polyfunctional compound (B) is 30 / 70 to 50 / 50: wherein, R 1 and R 2 each independently represent any one selected from the group consisting of a hydrogen atom, an alkyl group having 1 to 6 carbon atoms, an alkenyl group having 2 to 6 carbon atoms, an aryl group, and an aralkyl group; R 3 represents any one selected from the group consisting of an alkyl group having 1 to 6 carbon atoms, an alkenyl group having 2 to 6 carbon atoms, an aryl group, and an aralkyl group; R 4 represents any one selected from the group consisting of a (meth)acryloyl group, a styryl group, and an alkenyl group having 2 to 6 carbon atoms; and n represents any integer of 1 to 5. and a polyfunctional compound (B) having two or more polymerizable functional groups in a molecule other than the compound (A) represented by the following general formula (I), wherein a mass ratio ((A)/ (B)) of the compound (A) to the polyfunctional compound (B) is 30 / 70 to 50 / 50: wherein, R 1 and R 2 each independently represent any one selected from the group consisting of a hydrogen atom, an alkyl group having 1 to 6 carbon atoms, an alkenyl group having 2 to 6 carbon atoms, an aryl group, and an aralkyl group; R 3 represents any one selected from the group consisting of an alkyl group having 1 to 6 carbon atoms, an alkenyl group having 2 to 6 carbon atoms, an aryl group, and an aralkyl group; R 4 represents any one selected from the group consisting of a (meth)acryloyl group, a styryl group, and an alkenyl group having 2 to 6 carbon atoms; and n represents any integer of 1 to 5.
A plug connector comprising: a plug base (110, 110', 110", 210) with terminal contacts for external contacting of the plug connector and base-side connection contacts and a plug body with plug contacts , characterized in that the plug base (110, 110', 110", 210) further comprises a transformer unit for galvanic separation in at least a conductive path between the terminal contacts and the base-side connecting contacts , the plug base (110, 110', 110", 210) and the plug body enclose a contact element for connecting the base-side connecting contacts to the plug contacts and the contact element is planar in a plane perpendicular to a plug-in direction of the plug body . a plug base (110, 110', 110", 210) with terminal contacts for external contacting of the plug connector and base-side connection contacts and a plug body with plug contacts , characterized in that the plug base (110, 110', 110", 210) further comprises a transformer unit for galvanic separation in at least a conductive path between the terminal contacts and the base-side connecting contacts , the plug base (110, 110', 110", 210) and the plug body enclose a contact element for connecting the base-side connecting contacts to the plug contacts and the contact element is planar in a plane perpendicular to a plug-in direction of the plug body .
An eyeglasses frame comprising: - a front portion , - a first and a second temple band connected to the front portion and - an attachment member rotatably connected to the front portion to rotate in relation to the front portion around a first rotation axis (x1) of the attachment member , wherein the attachment member comprises two receiving portions arranged parallel to each other and opposite to each other in relation to the first rotation axis (x1) wherein each receiving portion is configured to receive a user unit to attach the user unit to the attachment member and to enable rotation of the user unit in relation to the attachment member around a second rotation axis (x2), wherein each receiving portion 6 comprises a groove arranged to receive an inserting portion (7.1, 7.1') of the user unit by inserting of the inserting portion (7.1, 7.1') into the grove, wherein a second user unit comprises two lenses fixedly connected to a frame of the second user unit , wherein the second axis (x2) is perpendicular to the first axis (x1) and wherein the attachment member is connected to the front portion at a middle position of the front portion between the first and the second temple band . - a front portion , - a first and a second temple band connected to the front portion and - an attachment member rotatably connected to the front portion to rotate in relation to the front portion around a first rotation axis (x1) of the attachment member , wherein