mhurhangee/ep-ind-claims huggingface dataset:
A method for provisioning subcarriers to users for Orthogonal Frequency Division Multiple Access, OFDMA, communications in a Wireless Local Area Network, WLAN, the method comprising the following steps executed by a network component: allocating subcarrier groups to a plurality of users; and signaling, to the plurality of users, a map of the subcarrier groups allocated to the plurality of users, wherein the subcarrier groups are in accordance with a pre-defined and deterministic grouping structure for an integer number of subcarriers in a channel of a certain bandwidth, wherein the map comprises an indication of a sequence of subcarrier groups and an indication of a sequence of scheduled users, wherein each one of the scheduled users in the sequence of scheduled users is mapped to one of the subcarrier groups in the sequence of subcarrier groups, wherein the map is signaled using an OFDMA physical layer, PHY, Protocol Data Unit, PPDU, comprising a first preamble portion, and a second preamble portion indicative of the map, and wherein the PPDU further comprises a data portion configured to carry data of the scheduled users in the channel, wherein data of each one of the scheduled users is carried on the one of the subcarrier groups to which said one of the scheduled users is mapped. allocating subcarrier groups to a plurality of users; and signaling, to the plurality of users, a map of the subcarrier groups allocated to the plurality of users, wherein the subcarrier groups are in accordance with a pre-defined and deterministic grouping structure for an integer number of subcarriers in a channel of a certain bandwidth, wherein the map comprises an indication of a sequence of subcarrier groups and an indication of a sequence of scheduled users, wherein each one of the scheduled users in the sequence of scheduled users is mapped to one of the subcarrier groups in the sequence of subcarrier groups, wherein the map is signaled using an OFDMA physical layer, PHY, Protocol Data Unit, PPDU, comprising a first preamble portion, and a second preamble portion indicative of the map, and wherein the PPDU further comprises a data portion configured to carry data of the scheduled users in the channel, wherein data of each one of the scheduled users is carried on the one of the subcarrier groups to which said one of the scheduled users is mapped.
A mobile terminal comprising: a body; a transparent display formed on a front surface of the body, and configured to display at least one text or image; a sensor configured to sense a color of an object positioned on a rear surface of the body, said object overlapping with the at least one text or image; and a controller configured to: select one or more regions on the transparent display, based on a determination that a color of the at least one text or image overlapping with the object and the sensed color of the object are similar; and display a background image on the selected one or more regions such that at least one text or image included in the selected region is overlapped with the background image. a body; a transparent display formed on a front surface of the body, and configured to display at least one text or image; a sensor configured to sense a color of an object positioned on a rear surface of the body, said object overlapping with the at least one text or image; and a controller configured to: select one or more regions on the transparent display, based on a determination that a color of the at least one text or image overlapping with the object and the sensed color of the object are similar; and display a background image on the selected one or more regions such that at least one text or image included in the selected region is overlapped with the background image. select one or more regions on the transparent display, based on a determination that a color of the at least one text or image overlapping with the object and the sensed color of the object are similar; and display a background image on the selected one or more regions such that at least one text or image included in the selected region is overlapped with the background image.
Method for coding a drilling device (7, 15) for an aircraft, wherein the method comprises: placing a drilling template with at least a drilling hole on a work piece; placing a drilling bushing in the drilling hole of the drilling template; placing the drilling device (7, 15) in the drilling hole of the drilling template; wherein the drilling bushing comprises a coding master device comprising a bushing edge comprising a first recess and a second recess; wherein the drilling device comprises a coding slave device comprising a coding sleeve edge comprising a first cading pin (10, 17) and a second coding pin (11, 18); and wherein the coding slave device engages with the coding master device when moving them axially towards each other such that the first coding pin engages with the first recess and the second coding pin engages with the second recess, wherein the second recess is spaced to the first recess along to the bushing edge in a predetermined angle (6, 14), and wherein the first and the second coding pin (10, 11) are spaced with the predetermined angle (6', 14'), characterised in that the bushing edge further comprises a first locking device and the coding sleeve edge further comprises a second locking device (19, 20), and in that the first locking device is connectable to the second locking device, if the first coding pin engages with the first recess and the second coding pin engages with the second recess. placing a drilling template with at least a drilling hole on a work piece; placing a drilling bushing in the drilling hole of the drilling template; placing the drilling device (7, 15) in the drilling hole of the drilling template; wherein the drilling bushing comprises a coding master device comprising a bushing edge comprising a first recess and a second recess; wherein the drilling device comprises a coding slave device comprising a coding sleeve edge comprising a first cading pin (10, 17) and a second coding pin (11, 18); and wherein the coding slave device engages with the coding master device when moving them axially towards each other such that the first coding pin engages with the first recess and the second coding pin engages with the second recess, wherein the second recess is spaced to the first recess along to the bushing edge in a predetermined angle (6, 14), and wherein the first and the second coding pin (10, 11) are spaced with the predetermined angle (6', 14'),
MEMS device having an interposer substrate, wherein the interposer substrate has: a front side and a rear side; a cavity (K1a; K1b), which proceeds from the rear side and extends to a first depth; a through-opening; and a depression region (ST1; ST2), which is arranged between the cavity (K1a; K1b) and the through-passage and, proceeding from the rear side, is depressed to a second depth in relation to the rear side; wherein the first depth is greater than the second depth, wherein the MEMs device additionally has: a MEMS substrate, which has a first movable structure (B1a; B1b) and a second movable structure (B2a; B2b); wherein the interposer substrate is bonded to the MEMS substrate in such a way that the first movable structure (B1a; B1b) is movable into the cavity (K1a; K1b), and in that the depression region (ST1; ST2) serves as a stop region for the second movable structure (B2a; B2b). a front side and a rear side; a cavity (K1a; K1b), which proceeds from the rear side and extends to a first depth; a through-opening; and a depression region (ST1; ST2), which is arranged between the cavity (K1a; K1b) and the through-passage and, proceeding from the rear side, is depressed to a second depth in relation to the rear side; wherein the first depth is greater than the second depth, wherein the MEMs device additionally has: a MEMS substrate, which has a first movable structure (B1a; B1b) and a second movable structure (B2a; B2b); wherein the interposer substrate is bonded to the MEMS substrate in such a way that the first movable structure (B1a; B1b) is movable into the cavity (K1a; K1b), and in that the depression region (ST1; ST2) serves as a stop region for the second movable structure (B2a; B2b). a MEMS substrate, which has a first movable structure (B1a; B1b) and a second movable structure (B2a; B2b); wherein the interposer substrate is bonded to the MEMS substrate in such a way that the first movable structure (B1a; B1b) is movable into the cavity (K1a; K1b), and in that the depression region (ST1; ST2) serves as a stop region for the second movable structure (B2a; B2b).
Orthopaedic brace comprising two rigid valves, each having a back portion; a rigid back plate extending in a longitudinal direction and partially overlapping the back portions of both valves; front closing devices, configured to tighten the valves at the front in an adjustable manner; back closing devices (9; 15; 21), configured to tighten the valves at the back in an adjustable manner; wherein each back closing device (9; 15; 21) is coupled to the back portion of a respective one of the valves and to the back plate; characterized in that each back closing device (9; 15; 21) comprises a retaining element (11; 16; 22) connected to the back portion of a respective one of the valves, and a belt (12; 17; 23) connected to the back plate and to the respective retaining element (11; 16; 22); the retaining elements (11; 16; 22) being configured to accommodate the respective belts (12; 17; 23) in a sliding manner in an adjustment position and to lock the respective belts (12; 17; 23) in a position of use. wherein each back closing device (9; 15; 21) is coupled to the back portion of a respective one of the valves and to the back plate; characterized in that each back closing device (9; 15; 21) comprises a retaining element (11; 16; 22) connected to the back portion of a respective one of the valves, and a belt (12; 17; 23) connected to the back plate and to the respective retaining element (11; 16; 22); the retaining elements (11; 16; 22) being configured to accommodate the respective belts (12; 17; 23) in a sliding manner in an adjustment position and to lock the respective belts (12; 17; 23) in a position of use.
A sensor comprising: a case having a through hole; a resistance substrate fixed within said case; a shaft member having a first end portion which is one end of the shaft member placed within said case and a second end portion which is other end of the shaft member exposed to an outside of said case from said through hole, said shaft member being placed at said through hole in a movable manner in an axial direction; and a sliding element receiver having a bearing end contacting with said first end portion of said shaft member, and attached with a brush sliding against said resistance substrate, said sliding element receiver being capable of moving relatively against said resistance substrate with said shaft member; wherein a hemispherical end face is formed at said first end portion, a hemispherical hole internally contacting with said hemispherical end face is formed at said bearing end and R > 1/D A is satisfied when a curvature of said hemispherical hole is defined as R, and when a distance between a center position of the axial direction of said through hole and the bottom portion of said hemispherical hole under the condition that said shaft member is most exposed to the outside of said case is defined as D A. a case having a through hole; a resistance substrate fixed within said case; a shaft member having a first end portion which is one end of the shaft member placed within said case and a second end portion which is other end of the shaft member exposed to an outside of said case from said through hole, said shaft member being placed at said through hole in a movable manner in an axial direction; and a sliding element receiver having a bearing end contacting with said first end portion of said shaft member, and attached with a brush sliding against said resistance substrate, said sliding element receiver being capable of moving relatively against said resistance substrate with said shaft member; wherein a hemispherical end face is formed at said first end portion, a hemispherical hole internally contacting with said hemispherical end face is formed at said bearing end and
A nacelle for a bypass turbojet engine, including a cascade thrust reverser, equipped with thrust reverser cascades disposed around an annular flow path of fresh air, under front cowls (6,8), these cascades moving back with movable rear cowls opening, in the annular flow path, lateral passages receiving these cascades to direct the fresh air flow forwards, the turbojet engine including fastening points, the nacelle comprising external hatches closing openings of the front cowls (6, 8) configured to be disposed radially outside these fastening points to access it, characterized in that each hatch opening includes a contour comprising edges of two front cowls (6, 8).
A library for the expression of all functional TCR types comprising 45 TCR constructs each encoding one of the 45 different TCR α chains and 47 TCR constructs each encoding one of the 47 different TCR β chains, wherein each of the 45 TCR constructs encoding one of 45 different TCR α chain comprises the following building blocks: - one of the variable AV segments coding for variable TCR α chain regions which are at least 80 % identical to the sequences set forth in SEQ ID No: 100 to SEQ ID No: 144, and - a constant AC segment; and wherein each of the 47 TCR constructs encoding one of 47 different TCR β chains comprises: - one of the variable BV segments coding for variable TCR β chain regions which are least 80 % identical to the sequences set forth in SEQ ID No: 145 to SEQ ID No: 191, and - a constant BC segment, wherein the building blocks contain at least one combination site at the 5'-end and at least one combination site at the 3'-end. - one of the variable AV segments coding for variable TCR α chain regions which are at least 80 % identical to the sequences set forth in SEQ ID No: 100 to SEQ ID No: 144, and - a constant AC segment; and - one of the variable BV segments coding for variable TCR β chain regions which are least 80 % identical to the sequences set forth in SEQ ID No: 145 to SEQ ID No: 191, and - a constant BC segment,
A coaxially tightening automatic lock, comprising: a hollow connecting rod, a top plate and a bottom plate respectively mounted on two ends of the connecting rod, a connecting lock device mounted on a lower end of the connecting rod and fixed on a surface of the bottom plate, the connecting lock device comprising: a flange connected to the bottom of the connecting rod, a lock cover sleeved on an outer wall of the flange, a lock core disposed in a cavity at an upper end of the flange, and a lock piece disposed between a lower end of the flange and an open slot in the surface of the bottom plate, a knock pin mounted in a hollow cavity at an upper end of the connecting rod, and a rotating handle sleeved on an outer wall at the upper end of the connecting rod.
A temperature adjusting apparatus comprising: a heat exchanger; a high-temperature radiator; a parent supply pipe arranged for being flowed through by a high-temperature fluid to be supplied to the high-temperature radiator; a high-temperature pipe which is branched from the parent supply pipe and is connected to the high-temperature radiator; a first supply pipe which is branched from the parent supply pipe and passes through the heat exchanger; a second supply pipe which is branched from the parent supply pipe; a mixed supply pipe arranged for being flowed through by a mixed fluid being a mixture of a first portion of the fluid which has flowed through the first supply pipe and a second portion of the fluid which has flowed through the second supply pipe, wherein the mixed supply pipe is to be connected, in use, to a low-temperature radiator; a return pipe arranged for being flowed through by the mixed fluid which has been supplied to the low-temperature radiator and from which heat has been radiated, the return pipe passing through the heat exchanger; a mixture adjusting valve that is configured to adjust a temperature of the mixed fluid by adjusting a mixture ratio of the first portion of the fluid and the second portion of the fluid in the mixed fluid; a temperature sensor provided at the mixed supply pipe; and a control unit that is configured to measure the temperature of the mixed fluid by using the temperature sensor provided at the mixed supply pipe, and to adjust the degree of opening of the mixture adjusting valve according to the measured temperature. a heat exchanger; a high-temperature radiator; a parent supply pipe arranged for being flowed through by a high-temperature fluid to be supplied to the high-temperature radiator; a high-temperature pipe which is branched from the parent supply pipe and is connected to the high-temperature radiator; a first supply pipe which is branched from the parent supply pipe and passes through the heat exchanger; a second supply pipe which is branched from the parent supply pipe; a mixed supply pipe arranged for being flowed through by a mixed fluid being a mixture of a first portion of the fluid which has flowed through the first supply pipe and a second portion of the fluid which has flowed through the second supply pipe, wherein the mixed supply pipe is to be connected, in use, to a low-temperature radiator; a return pipe arranged for being flowed through by the mixed fluid which has been supplied to the low-temperature radiator and from which heat has been radiated, the return pipe passing through the heat exchanger; a mixture adjusting valve that is configured to adjust a temperature of the mixed fluid by adjusting a mixture ratio of the first portion of the fluid and the second portion of the fluid in the mixed fluid; a temperature sensor provided at the mixed supply pipe; and a control unit that is configured to measure the temperature of the mixed fluid by using the temperature sensor provided at the mixed supply pipe, and to adjust the degree of opening of the mixture adjusting valve according to the measured temperature.
A system, comprising: an aircraft having a landing gear (12, 14, 16) comprising a wheel (13A, 13B, 15A, 15B, 17A, 17B); a friction brake having a brake material coupled to the wheel (13A, 13B, 15A, 15B, 17A, 17B); a regenerative brake comprising a reversible taxi motor coupled to the wheel (13A, 13B, 15A, 15B, 17A, 17B); a sensor configured to measure a wheel parameter of the landing gear and a friction brake temperature of the friction brake; and a tangible, non-transitory memory configured to communicate with a controller, the tangible, non-transitory memory having instructions stored thereon that, in response to execution by the controller, cause the controller to perform operations comprising: receiving, by the controller, a command signal, the wheel parameter, and the friction brake temperature; calculating, by the controller, a brake material temperature based on the wheel parameter, the friction brake temperature, and the command signal; and generating, by the controller, an allocated deceleration for the friction brake and the regenerative brake corresponding to the calculated brake material temperature and the command signal. an aircraft having a landing gear (12, 14, 16) comprising a wheel (13A, 13B, 15A, 15B, 17A, 17B); a friction brake having a brake material coupled to the wheel (13A, 13B, 15A, 15B, 17A, 17B); a regenerative brake comprising a reversible taxi motor coupled to the wheel (13A, 13B, 15A, 15B, 17A, 17B); a sensor configured to measure a wheel parameter of the landing gear and a friction brake temperature of the friction brake; and a tangible, non-transitory memory configured to communicate with a controller, the tangible, non-transitory memory having instructions stored thereon that, in response to execution by the controller, cause the controller to perform operations comprising: receiving, by the controller, a command signal, the wheel parameter, and the friction brake temperature; calculating, by the controller, a brake material temperature based on the wheel parameter, the friction brake temperature, and the command signal; and generating, by the controller, an allocated deceleration for the friction brake and the regenerative brake corresponding to the calculated brake material temperature and the command signal. receiving, by the controller, a command signal, the wheel parameter, and the friction brake temperature; calculating, by the controller, a brake material temperature based on the wheel parameter, the friction brake temperature, and the command signal; and generating, by the controller, an allocated deceleration for the friction brake and the regenerative brake corresponding to the calculated brake material temperature and the command signal.
A selective CO methanation catalyst comprising: a supported metal catalyst capable of methanizing CO, comprising: a carrier being an Al oxide containing a V oxide, and an active metal supported on the carrier, the active metal being Ni or an alloy or mixture of Ni and V; and a coating layer which covers a surface of the supported metal catalyst, the coating layer having pores, that are configured to reduce a CO concentration on the surface of the supported metal catalyst, the coating layer being made of mesoporous silica and at least one added metal selected from Ti, La, and Zr, and an atomic ratio of the added metal to Si of the mesoporous silica is 0.001 to 3. a supported metal catalyst capable of methanizing CO, comprising: a carrier being an Al oxide containing a V oxide, and an active metal supported on the carrier, the active metal being Ni or an alloy or mixture of Ni and V; and a carrier being an Al oxide containing a V oxide, and an active metal supported on the carrier, the active metal being Ni or an alloy or mixture of Ni and V; and a coating layer which covers a surface of the supported metal catalyst, the coating layer having pores, that are configured to reduce a CO concentration on the surface of the supported metal catalyst, the coating layer being made of mesoporous silica and at least one added metal selected from Ti, La, and Zr, and an atomic ratio of the added metal to Si of the mesoporous silica is 0.001 to 3. the coating layer having pores, that are configured to reduce a CO concentration on the surface of the supported metal catalyst, the coating layer being made of mesoporous silica and at least one added metal selected from Ti, La, and Zr, and an atomic ratio of the added metal to Si of the mesoporous silica is 0.001 to 3.