mhurhangee/ep-ind-claims huggingface dataset:
One or more computer storage media having computer-executable instructions embodied thereon that, when executed, cause a computing device to perform a method of distributing a scalable build service, the method comprising: determining a branch to build; identifying a first virtual machine of a pool of virtual machines for building at least a part of the branch, wherein a size of the pool of virtual machines is based on historical demand; identifying a plurality of source files to be transferred for the branch, wherein the first virtual machine processes at least a source file of the plurality of source files to generate a corresponding binary file; transferring the source file of the plurality of source files to the first virtual machine; deploying a build environment on the first virtual machine, wherein the build environment is distributed to the first virtual machine as needed; causing the first virtual machine to process at least the source file of the plurality of source files so as to generate a binary file; causing a digital signature for the binary file to be generated by a dedicated signing server, wherein signing keys are stored on the dedicated signing server and are not distributed to the virtual machines; transferring the digital signature to a second virtual machine; and causing at least the second virtual machine to generate a binary package from at least the binary file and the digital signature. determining a branch to build; identifying a first virtual machine of a pool of virtual machines for building at least a part of the branch, wherein a size of the pool of virtual machines is based on historical demand; identifying a plurality of source files to be transferred for the branch, wherein the first virtual machine processes at least a source file of the plurality of source files to generate a corresponding binary file; transferring the source file of the plurality of source files to the first virtual machine; deploying a build environment on the first virtual machine, wherein the build environment is distributed to the first virtual machine as needed; causing the first virtual machine to process at least the source file of the plurality of source files so as to generate a binary file; causing a digital signature for the binary file to be generated by a dedicated signing server, wherein signing keys are stored on the dedicated signing server and are not distributed to the virtual machines; transferring the digital signature to a second virtual machine; and causing at least the second virtual machine to generate a binary package from at least the binary file and the digital signature.
A rotary wing aircraft comprising: a fuselage including a plurality of surfaces; at least one engine mounted in the fuselage; a rotor assembly including a rotor shaft operatively connected to the at least one engine, and a plurality of rotor blades operatively connected to the at least one rotor shaft, the rotor assembly including a plurality of surface portions; an active air discharge opening (106; 110; 140) extends through one of the plurality of surfaces of the fuselage and one of the plurality of surfaces of the rotor assembly; and an active air generation system mounted in one of the fuselage and the rotor assembly, the active air generation system being configured and disposed to generate and direct a flow of air out through the active air discharge opening (106; 110; 140) to disrupt an airstream flowing over the one of the plurality of surfaces of the fuselage and the one of the plurality of surface portions of the rotor assembly, wherein the rotor assembly includes a rotor hub operatively connected to the plurality of rotor blades, characterized in that the at least one active air discharge opening is formed in the rotor hub and includes a plurality of active air discharge openings formed in an upper surface portion of the rotor hub. a fuselage including a plurality of surfaces; at least one engine mounted in the fuselage; a rotor assembly including a rotor shaft operatively connected to the at least one engine, and a plurality of rotor blades operatively connected to the at least one rotor shaft, the rotor assembly including a plurality of surface portions; an active air discharge opening (106; 110; 140) extends through one of the plurality of surfaces of the fuselage and one of the plurality of surfaces of the rotor assembly; and an active air generation system mounted in one of the fuselage and the rotor assembly, the active air generation system being configured and disposed to generate and direct a flow of air out through the active air discharge opening (106; 110; 140) to disrupt an airstream flowing over the one of the plurality of surfaces of the fuselage and the one of the plurality of surface portions of the rotor assembly, wherein the rotor assembly includes a rotor hub operatively connected to the plurality of rotor blades, characterized in that the at least one active air discharge opening is formed in the rotor hub and includes a plurality of active air discharge openings formed in an upper surface portion of the rotor hub.
Device for measuring the relative position of two objects which are able to be moved relative to each other along an axis or about an axis of rotation, said objects having a transmitter which provides unpolarised light, having a polariser and having at least two receivers arranged to be radially adjacent, said receivers measuring the light intensity passing through the polariser in order to generate a position-dependent signal, wherein a polarisation filter is arranged in front of the receivers and wherein the receivers and the polariser move relative to one another depending on the relative position of the two objects, wherein the polariser has at least two different polarisation directions, characterised in that the length of the receivers tangential to the direction of the relative movement is dependent on the speed with which the region of the polariser seen by the receiver moves relative to the receiver.
A system for providing wireless communication between a vehicle and a plurality of stationary communication systems (11A, 11C) located approximately along a track of the vehicle, the system comprising: antenna sets (A1, A2) each comprising a plurality of antennas (A11, A12 and A21, A22) mounted onto a convex-shaped vehicle roof, wherein an axis of antenna set is approximately perpendicular to an axis of antenna set, and wherein the antenna sets (A1, A2) are mounted below the top roof level of the convex-shaped vehicle roof; a switching device operable to switch between a first antenna configuration (MODE 1) and a second antenna configuration (MODE 2) of the antennas (A11, A12 and A21, A22) of the antenna sets (A1, A2), based on a measure of difference in signal power (P1, P2) received at the antenna sets (A1, A2); and wherein the first antenna configuration (MODE 1) is associated with a first stationary communication system of the plurality of stationary communication systems and a second antenna configuration (MODE 2) is associated with a second stationary communication system of the plurality of stationary communication systems, and wherein one of the sets of antennas is in operation physically closer to the transceiver antenna system of the second stationary communication system, whereas the other set of antennas are out of sight of the transceiver antenna system of the second stationary communication system and electromagnetically partially shielded by the presence of the vehicle roof. antenna sets (A1, A2) each comprising a plurality of antennas (A11, A12 and A21, A22) mounted onto a convex-shaped vehicle roof, wherein an axis of antenna set is approximately perpendicular to an axis of antenna set, and wherein the antenna sets (A1, A2) are mounted below the top roof level of the convex-shaped vehicle roof; a switching device operable to switch between a first antenna configuration (MODE 1) and a second antenna configuration (MODE 2) of the antennas (A11, A12 and A21, A22) of the antenna sets (A1, A2), based on a measure of difference in signal power (P1, P2) received at the antenna sets (A1, A2); and wherein the first antenna configuration (MODE 1) is associated with a first stationary communication system of the plurality of stationary communication systems and a second antenna configuration (MODE 2) is associated with a second stationary communication system of the plurality of stationary communication systems, and wherein one of the sets of antennas is in operation physically closer to the transceiver antenna system of the second stationary communication system, whereas the other set of antennas are out of sight of the transceiver antenna system of the second stationary communication system and electromagnetically partially shielded by the presence of the vehicle roof.
Outlet device of a roller shutter box for the passage of a rod through a board of the box, comprising: - said rod, intended to pass through the board of the box, - a support element intended to be fastened to the board of the box, exteriorly to said box and comprising a housing for a spherical element with a swivel connection with said support element, - said spherical element, having a through bore for the passage of the rod, characterised in that said device has: - a first seal, intended to be pinched between said support and the outer face of the board of the box in order to create the air seal between said support and said board, - a second seal, arranged between said rod and said spherical element in order to create the air seal on the inter-space between the rod and said spherical element. - said rod, intended to pass through the board of the box, - a support element intended to be fastened to the board of the box, exteriorly to said box and comprising a housing for a spherical element with a swivel connection with said support element, - said spherical element, having a through bore for the passage of the rod, - a first seal, intended to be pinched between said support and the outer face of the board of the box in order to create the air seal between said support and said board, - a second seal, arranged between said rod and said spherical element in order to create the air seal on the inter-space between the rod and said spherical element.
A wind turbine blade having an aerodynamic profile with a leading edge, a trailing edge and suction and pressure sides (17,19) between the leading edge and the trailing edge, wherein said profile comprises in at least a part of the wind turbine blade a trailing edge region TER which has a cross section increase in the direction of the trailing edge and the zone of the pressure side at the trailing edge region TER has a concave curved surface and characterized in that the angle B between an hypothetical tangent line to said zone and an hypothetical tangent line to the zone of the suction side at the trailing edge region TER is in the range of 0° to 45°.
A prosthetic implant (12, 14, 112, 114, 210, 310, 410, 510, 610, 710, 810, 910) comprising: a first end (313, 413, 513, 613, 713); a second end (314, 414, 514, 614, 714); an articular surface (22, 130, 222, 228, 311, 411, 511, 611, 711, 966); a bone contacting surface (24, 124, 218, 224, 312, 412, 512, 612, 712, 945) including a curved portion; the prosthetic implant being characterized in that it further comprises: a first element (26, 126, 220, 320, 420, 520, 620, 720) extending from the bone contacting surface and having a first curved surface; and a second element (28, 128, 226, 330, 430, 530, 630, 730) extending from the bone contacting surface and having a second curved surface, wherein the first and second curved surfaces are curved about a first pivot point (46, 160, 234, 322, 422, 522, 622, 722, 822). a first end (313, 413, 513, 613, 713); a second end (314, 414, 514, 614, 714); an articular surface (22, 130, 222, 228, 311, 411, 511, 611, 711, 966); a bone contacting surface (24, 124, 218, 224, 312, 412, 512, 612, 712, 945) including a curved portion; a first element (26, 126, 220, 320, 420, 520, 620, 720) extending from the bone contacting surface and having a first curved surface; and a second element (28, 128, 226, 330, 430, 530, 630, 730) extending from the bone contacting surface and having a second curved surface, wherein the first and second curved surfaces are curved about a first pivot point (46, 160, 234, 322, 422, 522, 622, 722, 822).
An integral fluid measurement system comprising: a hybrid interface unit for communicating with one or more sensors (60, 62) disposed in a fluid tank (20, 22), the hybrid interface unit comprising: a hybrid interface, the hybrid interface configured to communicate with a first sensor (60, 62) disposed in the fluid tank (20, 22) using a first communication technology, and with a second sensor (60, 62) disposed in the fluid tank (20, 22) using a second communication technology different from the first communication technology; a data bus interface; and a digital signal processor, the digital signal processor configured to exchange data between the hybrid interface and the data bus interface; a fluid tank (20, 22) configured to contain a fluid; and a calculating device configured to receive data from the data bus interface; wherein the data represents at least one parameter that is associated with the fluid; and the calculating device is configured to calculate at least one parameter that is associated with the fluid. a hybrid interface unit for communicating with one or more sensors (60, 62) disposed in a fluid tank (20, 22), the hybrid interface unit comprising: a hybrid interface, the hybrid interface configured to communicate with a first sensor (60, 62) disposed in the fluid tank (20, 22) using a first communication technology, and with a second sensor (60, 62) disposed in the fluid tank (20, 22) using a second communication technology different from the first communication technology; a data bus interface; and a digital signal processor, the digital signal processor configured to exchange data between the hybrid interface and the data bus interface; a hybrid interface, the hybrid interface configured to communicate with a first sensor (60, 62) disposed in the fluid tank (20, 22) using a first communication technology, and with a second sensor (60, 62) disposed in the fluid tank (20, 22) using a second communication technology different from the first communication technology; a data bus interface; and a digital signal processor, the digital signal processor configured to exchange data between the hybrid interface and the data bus interface; a fluid tank (20, 22) configured to contain a fluid; and a calculating device configured to receive data from the data bus interface; wherein the data represents at least one parameter that is associated with the fluid; and the calculating device is configured to calculate at least one parameter that is associated with the fluid. wherein the data represents at least one parameter that is associated with the fluid; and the calculating device is configured to calculate at least one parameter that is associated with the fluid.
A compressor (1, 101, 201, 301, 401) comprising: a first constituent element (23, 123, 125, 323, 325, 327, 327A, 327B) capable of being laser welded; and a first slider (24, 124, 224, 324, 324A, 326, 326A, 424) composed of cast iron capable of being laser welded and having a carbon content of from 2.0 wt% to 2.7 wt%, characterised in that the first slider being joined with the first constituent element by laser welding without using a filler; the first constituent element (23, 123, 125, 323, 325, 327, 327A, 327B) has a first joining surface; the first slider (24, 124, 224, 324, 324A, 326, 326A, 424) has a second joining surface; 50% or more of a contact portion between the first joining surface and the second joining surface is laser welded without using a filler; the first constituent element (23, 123, 125, 323, 325, 327, 327A, 327B) is subjected to chamfering in an end portion of the first joining surface on a side irradiated with laser light, the chamfering being greater than 0 mm and less than or equal to 1/4 of a spot diameter of the laser light; and the first slider (24, 124, 224, 324, 324A, 326, 326A, 424) is subjected to chamfering in an end portion of the second joining surface on the side irradiated with laser light, the chamfering being greater than 0 mm and less than or equal to 1/4 of a spot diameter of the laser light. a first constituent element (23, 123, 125, 323, 325, 327, 327A, 327B) capable of being laser welded; and a first slider (24, 124, 224, 324, 324A, 326, 326A, 424) composed of cast iron capable of being laser welded and having a carbon content of from 2.0 wt% to 2.7 wt%, characterised in that the first slider being joined with the first constituent element by laser welding without using a filler; the first constituent element (23, 123, 125, 323, 325, 327, 327A, 327B) has a first joining surface; the first slider (24, 124, 224, 324, 324A, 326, 326A, 424) has a second joining surface; 50% or more of a contact portion between the first joining surface and the second joining surface is laser welded without using a filler; the first constituent element (23, 123, 125, 323, 325, 327, 327A, 327B) is subjected to chamfering in an end portion of the first joining surface on a side irradiated with laser light, the chamfering being greater than 0 mm and less than or equal to 1/4 of a spot diameter of the laser light; and the first slider (24, 124, 224, 324, 324A, 326, 326A, 424) is subjected to chamfering in an end portion of the second joining surface on the side irradiated with laser light, the chamfering being greater than 0 mm and less than or equal to 1/4 of a spot diameter of the laser light.
Method for controlling the volume flow of a fan driven by a rotational speed variable drive motor, comprising the steps a. Determination of a volume flow (q V) conveyed by a fan, said volume flow (q V) being dependent on a fan wheel rotational speed (n V), wherein an impeller wheel driven by the volume flow of the fan is arranged in a blow-out section of the fan, wherein the rotational speed (n F) of said impeller wheel is detected and serves as a reference value of the volume flow (q V) of the fan, b. Detection of at least one fan parameter, wherein the at least one fan parameter is the fan wheel rotational speed (n V), c. Definition of a correction function (f) for the volume flow (q V) as a function of the rotational speed (n F) of the impeller wheel and the fan wheel rotational speed (n V), so that q V = f (n F, n V) applies, wherein a calculation of the volume flow (qV) using the correction function (f) is carried out for determining the volume flow (q V), d. Adjustment of the fan wheel rotational speed (n V) by the drive motor to adjust the calculated volume flow (q V) to a fixed target value of volume flow (q V -soll). a. Determination of a volume flow (q V) conveyed by a fan, said volume flow (q V) being dependent on a fan wheel rotational speed (n V), wherein an impeller wheel driven by the volume flow of the fan is arranged in a blow-out section of the fan, wherein the rotational speed (n F) of said impeller wheel is detected and serves as a reference value of the volume flow (q V) of the fan, b. Detection of at least one fan parameter, wherein the at least one fan parameter is the fan wheel rotational speed (n V), c. Definition of a correction function (f) for the volume flow (q V) as a function of the rotational speed (n F) of the impeller wheel and the fan wheel rotational speed (n V), so that q V = f (n F, n V) applies, wherein a calculation of the volume flow (qV) using the correction function (f) is carried out for determining the volume flow (q V), d. Adjustment of the fan wheel rotational speed (n V) by the drive motor to adjust the calculated volume flow (q V) to a fixed target value of volume flow (q V -soll).
A system, comprising: an insufflator for injecting a gas into a cavity of a patient; and a computed tomography imaging system including a console to control the operation of the imaging system, characterised in that the insufflator is adapted to receive control signals, insufflation parameters and/or other information from the console based on an imaging protocol selected by means of the console. an insufflator for injecting a gas into a cavity of a patient; and a computed tomography imaging system including a console to control the operation of the imaging system,
Elevator system comprising at least one autonomous unit (4, 5, 6) for controlling an elevator and a multichannel-edge-gateway being capable of building a communication between the autonomous unit (4, 5, 6) and data resources on an IoT network, the multichannel-edge-gateway comprises more than one communication channel, wherein these channels are capable of data communicating using the same protocol or different protocols either synchronously or asynchronously, characterized in that the multichannel-edge-gateway comprises a channel assignment means being capable of matching automatically one of the channels to one of the protocols according to data to be sent from the multichannel-edge-gateway, wherein a matching and/or an assigning by the said channel assignment means are executable by self-learning according to a data content, a data format and/or a data source. the multichannel-edge-gateway comprises more than one communication channel, wherein these channels are capable of data communicating using the same protocol or different protocols either synchronously or asynchronously, characterized in that the multichannel-edge-gateway comprises a channel assignment means being capable of matching automatically one of the channels to one of the protocols according to data to be sent from the multichannel-edge-gateway, wherein a matching and/or an assigning by the said channel assignment means are executable by self-learning according to a data content, a data format and/or a data source.
A method of generating a HEVC video file including coded video content, the method comprising: obtaining a plurality of slices of coded video content; obtaining a first plurality of parameter sets of a first type associated with the plurality of slices of video content and a second plurality of parameter sets of a second type associated with the plurality of slices of video content; encapsulating the plurality of slices of coded video content within a plurality of access units of a video stream; encapsulating the plurality of access units within a plurality of samples in a file track; encapsulating the first plurality of parameter sets; and encapsulating the second plurality of parameter sets; characterized by encapsulating the first plurality of parameter sets within the plurality of samples and encapsulating the second plurality of parameter sets within a sample description of the file track to support in-band transmission of the first plurality of parameter sets whilst supporting out-of-band transmission of the second plurality of parameter sets. obtaining a plurality of slices of coded video content; obtaining a first plurality of parameter sets of a first type associated with the plurality of slices of video content and a second plurality of parameter sets of a second type associated with the plurality of slices of video content; encapsulating the plurality of slices of coded video content within a plurality of access units of a video stream; encapsulating the plurality of access units within a plurality of samples in a file track; encapsulating the first plurality of parameter sets; and encapsulating the second plurality of parameter sets; characterized by encapsulating the first plurality of parameter sets within the plurality of samples and encapsulating the second plurality of parameter sets within a sample description of the file track to support in-band transmission of the first plurality of parameter sets whilst supporting out-of-band transmission of the second plurality of parameter sets.