mhurhangee/patent-ind-claim-en huggingface dataset:
A method for preparing pathogen-inactivated cryo-poor plasma, the method comprising: a) photochemically inactivating one or more units of plasma in the presence of a psoralen, wherein the photochemical inactivation is performed under sterile conditions in a first container containing the one or more units of plasma; b) transferring under sterile conditions the one or more units of plasma from the first container to a compound absorption device (CAD) coupled to the first container; c) transferring under sterile conditions the one or more units of plasma from the CAD to two or more second containers coupled to the CAD to provide pathogen-inactivated plasma; d) transferring under sterile conditions the pathogen-inactivated plasma from the two or more second containers to a third container coupled to the two or more second containers; e) freezing the pathogen-inactivated plasma followed by thawing of the pathogen-inactivated plasma under conditions that provide for the formation of a cryoprecipitate and pathogen-inactivated cryo-poor plasma; f) transferring the pathogen-inactivated cryo-poor plasma to at least a first of the two or more second containers; and g) transferring the cryoprecipitate to a second of the two or more second containers. a) photochemically inactivating one or more units of plasma in the presence of a psoralen, wherein the photochemical inactivation is performed under sterile conditions in a first container containing the one or more units of plasma; b) transferring under sterile conditions the one or more units of plasma from the first container to a compound absorption device (CAD) coupled to the first container; c) transferring under sterile conditions the one or more units of plasma from the CAD to two or more second containers coupled to the CAD to provide pathogen-inactivated plasma; d) transferring under sterile conditions the pathogen-inactivated plasma from the two or more second containers to a third container coupled to the two or more second containers; e) freezing the pathogen-inactivated plasma followed by thawing of the pathogen-inactivated plasma under conditions that provide for the formation of a cryoprecipitate and pathogen-inactivated cryo-poor plasma; f) transferring the pathogen-inactivated cryo-poor plasma to at least a first of the two or more second containers; and g) transferring the cryoprecipitate to a second of the two or more second containers.
External vehicle trim with an external strip and a support strip , wherein the external strip in its intended installed condition forms one part of the external vehicle surface with a surface of an external strip part which surface is facing towards the outside of the vehicle, and onto which the support strip , which in its intended installed condition is connected with the vehicle chassis structure , is placed on, characterised in that the external strip and the support strip together form a guide channel for a guide profile arranged on a lowerable window pane .
Motor vehicle door latch, comprising a locking mechanism substantially consisting of a catch and pawl , further comprising a pawl spring for acting on the pawl in the closing direction, and comprising an operation lever for opening the locking mechanism , the operation lever additionally being designed to act on the pawl spring and being equipped with a projection which interacts with the pawl spring , characterized in that the projection acts on the pawl spring only when the pawl is lifted from its engagement with the catch .
Method for controlling an unmanned aerial vehicle (UAV) used for recording and surveying objects in a specified region, wherein - a largely obstacle-free flyover zone (UZ) is defined for the region (BER) to be recorded and surveyed, in which zone the unmanned aerial vehicle (UAV) performs overview measurements of the region using suitable sensors and acquisition techniques, characterised in that - a three-dimensional digital surface model (DOM) of the region (BER) including the objects located therein is determined on the basis of the overview measurements, and - on the basis of the digital surface model (DOM) is determined a sequence of positions for detailed measurements and an obstacle-free flight route (FR) for an unmanned aerial vehicle (UAV) for adopting the sequence of positions, which route is taken as a basis for controlling the unmanned aerial vehicle (UAV). - a largely obstacle-free flyover zone (UZ) is defined for the region (BER) to be recorded and surveyed, in which zone the unmanned aerial vehicle (UAV) performs overview measurements of the region using suitable sensors and acquisition techniques, characterised in that - a three-dimensional digital surface model (DOM) of the region (BER) including the objects located therein is determined on the basis of the overview measurements, and - on the basis of the digital surface model (DOM) is determined a sequence of positions for detailed measurements and an obstacle-free flight route (FR) for an unmanned aerial vehicle (UAV) for adopting the sequence of positions, which route is taken as a basis for controlling the unmanned aerial vehicle (UAV).
Transport container for bottles, jars or the like, comprising a bottom from which corner columns extend which are interconnected by side walls forming end faces and longitudinal sides, and which is provided with a placement rim , a compartment being provided on the bottom , wherein the bottom is arranged at a distance from the placement rim , characterized in that two ribs extending diagonally along the bottom are provided on the underside of the bottom , the height of which ribs corresponds substantially to the distance of the bottom from the placement rim and which ribs cross in the middle of the bottom .
A system for powering a tethered aircraft, the system comprising: an aircraft comprising: a connection point for a tether ; an electrical power connection for receiving electrical power through an electrical cable associated with the tether; a power-receiving unit configured to receive electric power, via the electrical cable, from a pulsed electrical delivery system connected through the electrical power connection; a monitoring unit configured to detect electrical pulses received by the receiving unit, a communications transmitter configured to transmitt an acknowledgement signal in response to the monitoring unit detecting an electrical pulse received by the receiving unit; wherein the aircraft is configured to enter a controlled descent mode if the monitoring unit detects no electrical pulses within a predetermined period; and a ground station located remotely from the aircraft, and comprising: the pulsed electrical delivery system , a control unit configured to receive the acknowledgement signal, and to cause transmission of a further electrical pulse only upon receiving the acknowledgement signal; and suspension of transmission of a further electrical pulse if no acknowledgement signal is received. a connection point for a tether ; an electrical power connection for receiving electrical power through an electrical cable associated with the tether; a power-receiving unit configured to receive electric power, via the electrical cable, from a pulsed electrical delivery system connected through the electrical power connection; a monitoring unit configured to detect electrical pulses received by the receiving unit, a communications transmitter configured to transmitt an acknowledgement signal in response to the monitoring unit detecting an electrical pulse received by the receiving unit; the pulsed electrical delivery system , a control unit configured to receive the acknowledgement signal, and to cause transmission of a further electrical pulse only upon receiving the acknowledgement signal; and suspension of transmission of a further electrical pulse if no acknowledgement signal is received. a control unit configured to receive the acknowledgement signal, and to cause transmission of a further electrical pulse only upon receiving the acknowledgement signal; and suspension of transmission of a further electrical pulse if no acknowledgement signal is received.
Apparatus comprising: a headset for a wearer, the headset including a left earcup for providing sound to the wearer's left ear and a right earcup for providing sound to the wearer's right ear; and a headset controller and a push to talk unit configured to be electrically connected with the headset and configured for receiving multiple incoming radio signals, the headset controller including: a first radio signal input connection configured for receiving a first radio signal from a first radio ; a second radio signal input connection configured for receiving a second radio signal from a second radio different from the first radio ; and an electrical switching mechanism; the switching mechanism being operative to sense the presence of a first radio signal at the first radio signal input connection; the switching mechanism being operative to sense the presence of a second radio signal at the second radio signal input connection; the electrical switching mechanism being operative, when a first radio signal is present and a second radio signal is not present, to direct the first radio signal to both the left earcup and the right earcup ; the electrical switching mechanism being operative, when a second radio signal is present and a first radio signal is not present, to direct the second radio signal to both the left earcup and the right earcup ; and the electrical switching mechanism being operative, when both a first radio signal and a second radio signal are present, to direct the first radio signal to only the left earcup and the second radio signal to only the right earcup . a headset for a wearer, the headset including a left earcup for providing sound to the wearer's left ear and a right earcup for providing sound to the wearer's right ear; and a headset controller and a push to talk unit configured to be electrically connected with the headset and configured for receiving multiple incoming radio signals, the headset controller including: a first radio signal input connection configured for receiving a first radio signal from a first radio ; a second radio signal input connection configured for receiving a second radio signal from a second radio different from the first radio ; and an electrical switching mechanism; the switching mechanism being operative to sense the presence of a first radio signal at the first radio signal input connection; the switching mechanism being operative to sense the presence of a second radio signal at the second radio signal input connection; the electrical switching mechanism being operative, when a first radio signal is present and a second radio signal is not present, to direct the first radio signal to both the left earcup and the right earcup ; the electrical switching mechanism being operative, when a second radio signal is present and a first radio signal is not present, to direct the second radio signal to both the left earcup and the right earcup ; and the electrical switching mechanism being operative, when both a first radio signal and a second radio signal are present, to direct the first radio signal to only the left earcup and the second radio signal to only the right earcup .
A brake disc release device for elevators, comprising: an actuating mechanism having a first end and a second end ; characterized in that the brake disc release device further comprises: a gear connected to the first end of the actuating mechanism ; a first slider capable of sliding along a first guide piece and comprising a rack portion for engagement with the gear and a first wedge portion ; a second slider capable of sliding along a second guide piece and comprising a second wedge portion for engagement with the first wedge portion of the first slider ; and a pulling cable having a first end connected to the second slider and a second end connected to the brake disc ; wherein the actuating mechanism is rotated to drive the gear to rotate, drive the first slider to move in a first direction by means of the engagement between the gear and the rack portion of the first slider, drive the second slider to move in a second direction by means of the engagement between the first wedge portion of the first slider and the second wedge portion of the second slider , and thus drive the pulling cable to pull the brake disc . an actuating mechanism having a first end and a second end ; a gear connected to the first end of the actuating mechanism ; a first slider capable of sliding along a first guide piece and comprising a rack portion for engagement with the gear and a first wedge portion ; a second slider capable of sliding along a second guide piece and comprising a second wedge portion for engagement with the first wedge portion of the first slider ; and a pulling cable having a first end connected to the second slider and a second end connected to the brake disc ; wherein the actuating mechanism is rotated to drive the gear to rotate, drive the first slider to move in a first direction by means of the engagement between the gear and the rack portion of the first slider, drive the second slider to move in a second direction by means of the engagement between the first wedge portion of the first slider and the second wedge portion of the second slider , and thus drive the pulling cable to pull the brake disc .
A deflector element for a solar panel module mounting system, the deflector element comprising: a tray ; a first side wall coupled to a first edge of the tray and extending away from an upper surface of the tray ; and a second side wall coupled to a second edge of the tray opposing the first edge of the tray , the second side wall extending away from the upper surface of the tray , such that the tray , the first sidewall, and the second sidewall together define a channel for receiving a ballast weight , wherein: the first sidewall and the second sidewall are arranged at angles of less than 90 degrees with the respect to the upper surface of the tray such that the first sidewall and the second sidewall exert a clamping force on the ballast weight when the ballast weight is positioned on the upper surface of the tray within the channel , wherein the tray further comprises: a first security tab positioned at a first end of the tray and a second security tab positioned at a second end of the tray , the first security tab and the second security tab configured to be moved into positions protruding into the channel to prevent the ballast weight from sliding laterally within the channel . a tray ; a first side wall coupled to a first edge of the tray and extending away from an upper surface of the tray ; and a second side wall coupled to a second edge of the tray opposing the first edge of the tray , the second side wall extending away from the upper surface of the tray , such that the tray , the first sidewall, and the second sidewall together define a channel for receiving a ballast weight , wherein: the first sidewall and the second sidewall are arranged at angles of less than 90 degrees with the respect to the upper surface of the tray such that the first sidewall and the second sidewall exert a clamping force on the ballast weight when the ballast weight is positioned on the upper surface of the tray within the channel , wherein the tray further comprises: a first security tab positioned at a first end of the tray and a second security tab positioned at a second end of the tray , the first security tab and the second security tab configured to be moved into positions protruding into the channel to prevent the ballast weight from sliding laterally within the channel .
A power drive unit, PDU, for an aircraft cargo hold floor system, comprising: a first motorized roller comprising an outer rotor having a first magnetic member disposed on a radially inner surface of the outer rotor, the first motorized roller configured to rotate about an axis further comprising a second motorized roller comprising a cylindrical member coupled to a shaft , the cylindrical member configured to rotate with the shaft about the axis; an inner rotor having a second magnetic member disposed on a radially outer surface of the inner rotor, the inner rotor configured to drive the shaft; and a stator located between the outer rotor and the inner rotor, the stator having at least one winding in electromagnetic communication with the first magnetic member and the second magnetic member. a first motorized roller comprising an outer rotor having a first magnetic member disposed on a radially inner surface of the outer rotor, the first motorized roller configured to rotate about an axis further comprising a second motorized roller comprising a cylindrical member coupled to a shaft , the cylindrical member configured to rotate with the shaft about the axis; an inner rotor having a second magnetic member disposed on a radially outer surface of the inner rotor, the inner rotor configured to drive the shaft; and a stator located between the outer rotor and the inner rotor, the stator having at least one winding in electromagnetic communication with the first magnetic member and the second magnetic member.
A plug-in coupling device for receiving a first RJ connector at a first end, and a second RJ connector at a second end, comprising: a data coupling apparatus for connecting a plurality of data conductors of the first RJ connector to a plurality of data conductors of the second RJ connector; and a power coupling apparatus for connecting a plurality of power conductors of the first RJ connector to a plurality of power conductors of the second RJ connector, characterized in that the plug-in coupling device comprises a first printed circuit board and a second printed circuit board, and the power coupling apparatus cross-connects the plurality of power conductors of the first RJ connector to the plurality of power conductors of the second RJ connector, wherein the power coupling apparatus cross-connects, power contact elements at the first end for producing an electrical contact with the first RJ connector to power contact elements at the second end for producing an electrical contact with the second RJ connector, wherein the data coupling apparatus and the power coupling apparatus are designed to be electrically separate from each other, wherein the data coupling apparatus is at least partially formed on the first printed circuit board, and wherein the power coupling apparatus is at least partially formed on the second printed circuit board. a data coupling apparatus for connecting a plurality of data conductors of the first RJ connector to a plurality of data conductors of the second RJ connector; and a power coupling apparatus for connecting a plurality of power conductors of the first RJ connector to a plurality of power conductors of the second RJ connector, characterized in that the plug-in coupling device comprises a first printed circuit board and a second printed circuit board, and the power coupling apparatus cross-connects the plurality of power conductors of the first RJ connector to the plurality of power conductors of the second RJ connector, wherein the power coupling apparatus cross-connects, power contact elements at the first end for producing an electrical contact with the first RJ connector to power contact elements at the second end for producing an electrical contact with the second RJ connector, wherein the data coupling apparatus and the power coupling apparatus are designed to be electrically separate from each other, wherein the data coupling apparatus is at least partially formed on the first printed circuit board, and wherein the power coupling apparatus is at least partially formed on the second printed circuit board.
A sensor device removably attachable to a drug delivery device , the sensor device comprising: a sensing arrangement arranged within the sensor device; and circuitry configured to process signals provided by the sensor arrangement, wherein the sensing arrangement is configured such that, when the sensor device is attached to the drug delivery device, the sensing arrangement is operable to read encoded information present on a rotatable component that is internal to the drug delivery device and that is able to be sensed through a window or aperture of the drug delivery device, and is operable to sense through the window or aperture the presence or absence of at least a part of a drive mechanism of the drug delivery device, wherein the circuitry is configured: to determine, based on the encoded information, information relating to a set dose, and to determine, based on sensing the presence or absence of the part of the drive mechanism, information relating to whether the drug delivery device is in a dose setting mode or whether the device is in a dose delivery mode. a sensing arrangement arranged within the sensor device; and circuitry configured to process signals provided by the sensor arrangement, wherein the sensing arrangement is configured such that, when the sensor device is attached to the drug delivery device, the sensing arrangement is operable to read encoded information present on a rotatable component that is internal to the drug delivery device and that is able to be sensed through a window or aperture of the drug delivery device, and is operable to sense through the window or aperture the presence or absence of at least a part of a drive mechanism of the drug delivery device, wherein the circuitry is configured: to determine, based on the encoded information, information relating to a set dose, and to determine, based on sensing the presence or absence of the part of the drive mechanism, information relating to whether the drug delivery device is in a dose setting mode or whether the device is in a dose delivery mode. to determine, based on the encoded information, information relating to a set dose, and to determine, based on sensing the presence or absence of the part of the drive mechanism, information relating to whether the drug delivery device is in a dose setting mode or whether the device is in a dose delivery mode.
A weapon launch system for a submersible vessel, comprising : - at least one electrical actuator capable of exerting a sequence of mechanical actions on a weapon launch tube; - a power module capable of providing electrical power; - a control module capable of controlling the operation of the electric actuator ; - a first security module electrically connecting the power module to the control module and capable of monitoring the operation of the power module by implementing a first monitoring logic ; - a second security module electrically connecting the control module to the actuator and capable of monitoring the operation of the control module by implementing a second monitoring logic, the second monitoring logic being different and dissimilar to the first monitoring logic. - at least one electrical actuator capable of exerting a sequence of mechanical actions on a weapon launch tube; - a power module capable of providing electrical power; - a control module capable of controlling the operation of the electric actuator ; - a first security module electrically connecting the power module to the control module and capable of monitoring the operation of the power module by implementing a first monitoring logic ; - a second security module electrically connecting the control module to the actuator and capable of monitoring the operation of the control module by implementing a second monitoring logic, the second monitoring logic being different and dissimilar to the first monitoring logic.