mhurhangee/patent-ind-claim-en huggingface dataset:
An image forming apparatus comprising: a body frame ; a door to open or close the body frame, the door rotatable, relative to the body frame, about a first rotation axis; a roller frame rotatably provided at the body frame, the roller frame rotatable relative to the body frame about a second rotation axis (C1); and a link member to link the door and the roller frame to each other, wherein the link member restricts rotation of the roller frame when the door is closed, and allows the roller frame to be rotated about the second rotation axis when the door is opened; wherein: one side of the link member is coupled to the roller frame so as to be rotatable about a third rotation axis (C2) relative to the roller frame by a predetermined angle and the other side of the link member is coupled to the door, wherein the link member is movable along the third rotation axis when the door is open or closed by a predetermined angle about the first rotation axis; and wherein: the link member includes a plurality of rotating-direction guide bars extending toward the roller frame; and the roller frame includes a plurality of rotating-direction guide slots to accommodate the plurality of rotating-direction guide bars so as to guide rotation of the link member about the third rotation axis. a body frame ; a door to open or close the body frame, the door rotatable, relative to the body frame, about a first rotation axis; a roller frame rotatably provided at the body frame, the roller frame rotatable relative to the body frame about a second rotation axis (C1); and a link member to link the door and the roller frame to each other, wherein the link member restricts rotation of the roller frame when the door is closed, and allows the roller frame to be rotated about the second rotation axis when the door is opened; wherein: one side of the link member is coupled to the roller frame so as to be rotatable about a third rotation axis (C2) relative to the roller frame by a predetermined angle and the other side of the link member is coupled to the door, wherein the link member is movable along the third rotation axis when the door is open or closed by a predetermined angle about the first rotation axis; and wherein: the link member includes a plurality of rotating-direction guide bars extending toward the roller frame; and the roller frame includes a plurality of rotating-direction guide slots to accommodate the plurality of rotating-direction guide bars so as to guide rotation of the link member about the third rotation axis. the link member includes a plurality of rotating-direction guide bars extending toward the roller frame; and the roller frame includes a plurality of rotating-direction guide slots to accommodate the plurality of rotating-direction guide bars so as to guide rotation of the link member about the third rotation axis.
An apparatus comprising: a housing , wherein the housing is configured to be received by a receiving device adapted to be coupled to an unmanned aerial vehicle ; a first swing arm coupled to the housing proximate to a first end of the first swing arm, wherein the first swing arm is operable to toggle between a first open position and a first closed position, wherein the first closed position locates a second end of the first swing arm within the housing, wherein the first open position exposes the second end of the first swing arm outside the housing at an acute angle with respect to a first sidewall of the housing such that the first swing arm is positioned to secure a payload to the housing; a second swing arm coupled to the housing proximate to a first end of the second swing arm, wherein the second swing arm is operable to toggle between a second open position and a second closed position, wherein the second closed position locates a second end of the second swing arm within the housing, wherein the second open position exposes the second end of the second swing arm outside the housing at an acute angle with respect to a second sidewall of the housing such that the second swing arm is positioned to secure the payload to the housing; and a mechanism coupled between the first and second swing arms, wherein a cam of one of the first or second swing arms is configured, when contacted by the receiving device when the receiving device receives the housing , to cause, via the mechanism, the other of the first or second swing arms to be arranged in its respective open position. a housing , wherein the housing is configured to be received by a receiving device adapted to be coupled to an unmanned aerial vehicle ; a first swing arm coupled to the housing proximate to a first end of the first swing arm, wherein the first swing arm is operable to toggle between a first open position and a first closed position, wherein the first closed position locates a second end of the first swing arm within the housing, wherein the first open position exposes the second end of the first swing arm outside the housing at an acute angle with respect to a first sidewall of the housing such that the first swing arm is positioned to secure a payload to the housing; a second swing arm coupled to the housing proximate to a first end of the second swing arm, wherein the second swing arm is operable to toggle between a second open position and a second closed position, wherein the second closed position locates a second end of the second swing arm within the housing, wherein the second open position exposes the second end of the second swing arm outside the housing at an acute angle with respect to a second sidewall of the housing such that the second swing arm is positioned to secure the payload to the housing; and a mechanism coupled between the first and second swing arms, wherein a cam of one of the first or second swing arms is configured, when contacted by the receiving device when the receiving device receives the housing , to cause, via the mechanism, the other of the first or second swing arms to be arranged in its respective open position.
A robotic vehicle for movable operation in a work area , the movable operation comprising a soil cultivation, the work area being represented by a set of discretized coordinate grid points , the vehicle comprising a Global Navigation Satellite System, GNSS, receiver and a controller , the controller comprising a memory and a processor, the memory comprising instructions , wherein execution of the instructions by the processor causes the vehicle for each grid point of a subset of the grid points at different first points in time performing an initialization process, the initialization process comprising : - receiving at a first point in time of the different first points in time a first set of GNSS signals from a fixed vehicle base , said vehicle base being spaced apart from the vehicle and comprising a GNSS receiver for receiving the first set of GNSS signals, - receiving at said first point in time a second set of GNSS signals from the GNSS receiver of the vehicle, - determining an accuracy of a location determination, the location determination being based on the second set of GNSS signals , the determination of the accuracy being based on a comparison of the signal qualities of the first set of GNSS signals and the second set of GNSS signals , wherein execution of the instructions by the processor further causes the vehicle for planning the movable operation for future points in time based on results of the initialization process, the results of the initialization process comprising at least some of the grid points for which an accuracy of the location determination is available and the accuracy of the location determination at each one of said least some of the grid points . - receiving at a first point in time of the different first points in time a first set of GNSS signals from a fixed vehicle base , said vehicle base being spaced apart from the vehicle and comprising a GNSS receiver for receiving the first set of GNSS signals, - receiving at said first point in time a second set of GNSS signals from the GNSS receiver of the vehicle, - determining an accuracy of a location determination, the location determination being based on the second set of GNSS signals , the determination of the accuracy being based on a comparison of the signal qualities of the first set of GNSS signals and the second set of GNSS signals ,
A bush for isolating vibrations, the bush comprising: a first anchor part defining a longitudinal axis; a second anchor part disposed coaxially with respect to the first anchor part ; a first resilient body operably engaged with the first anchor part ; a second resilient body operably engaged with the second anchor part ; and an inertial mass element disposed between the first anchor part and the second anchor part , wherein the inertial mass element is independently connected to the first resilient body and the second resilient body , wherein the first resilient body , second resilient body and inertial mass element are arranged to isolate vibrations between the first anchor part and the second anchor part within a predetermined operational frequency range, and wherein the inertial mass element is arranged to isolate the first anchor part and second anchor part from dynamic stiffness increases associated with eigenmodes of the first resilient body and the second resilient body in the predetermined operational frequency range, characterized in that the bush includes one or more snubber portions to physically limit an extent of relative radial movement between the first and second anchor parts, and wherein at least one of the first and second anchor parts includes the one or more snubber portions . a first anchor part defining a longitudinal axis; a second anchor part disposed coaxially with respect to the first anchor part ; a first resilient body operably engaged with the first anchor part ; a second resilient body operably engaged with the second anchor part ; and an inertial mass element disposed between the first anchor part and the second anchor part , wherein the inertial mass element is independently connected to the first resilient body and the second resilient body , wherein the first resilient body , second resilient body and inertial mass element are arranged to isolate vibrations between the first anchor part and the second anchor part within a predetermined operational frequency range, and wherein the inertial mass element is arranged to isolate the first anchor part and second anchor part from dynamic stiffness increases associated with eigenmodes of the first resilient body and the second resilient body in the predetermined operational frequency range, characterized in that the bush includes one or more snubber portions to physically limit an extent of relative radial movement between the first and second anchor parts, and wherein at least one of the first and second anchor parts includes the one or more snubber portions .
A computer program for prediction of fluid responsiveness of a subject connected to a breathing apparatus providing mechanical ventilation to said subject , the breathing apparatus comprising a PEEP regulating arrangement configured to regulate a positive end-expiratory pressure, PEEP, applied to said subject , and a control unit for controlling said PEEP regulating arrangement and for monitoring at least one parameter indicative of a degree of carbon dioxide elimination of the subject, characterized in that the computer program comprises computer-readable code which, when executed by a processing unit of the control unit , causes the control unit to perform the steps of: - monitoring (S1) a carbon dioxide elimination (VCO 2 ) of the subject as said at least one parameter indicative of a degree of carbon dioxide elimination; - applying (S2) a PEEP maneuver in which a positive end-expiratory pressure (PEEP) applied to the subject is changed from a first PEEP level to a second PEEP level; - predicting (S3) the fluid responsiveness of the subject based on a change in said at least one monitored parameter following said change in PEEP, and - visually and/or audibly signalling to an operator of the breathing apparatus whether or not the subject is deemed to be fluid responsive based on a result of said prediction. - monitoring (S1) a carbon dioxide elimination (VCO 2 ) of the subject as said at least one parameter indicative of a degree of carbon dioxide elimination; - applying (S2) a PEEP maneuver in which a positive end-expiratory pressure (PEEP) applied to the subject is changed from a first PEEP level to a second PEEP level; - predicting (S3) the fluid responsiveness of the subject based on a change in said at least one monitored parameter following said change in PEEP, and - visually and/or audibly signalling to an operator of the breathing apparatus whether or not the subject is deemed to be fluid responsive based on a result of said prediction.
An anode for an X-ray generating tube , comprising: a transmission target including: a target layer for generating an X-ray through irradiation of an electron beam ; and a transmitting substrate for supporting the target layer and for transmitting the X-ray generated by the target layer ; and a tubular anode member for supporting the transmitting substrate at a tube inner circumference thereof, wherein a side surface of the transmitting substrate and the tube inner circumference of the tubular anode member are bonded together by a bonding material , wherein the bonding material has a thickness that varies in a direction along a tube axis (P) of the tubular anode member , wherein the transmitting substrate includes a support surface for supporting the target layer , characterized in that the tubular anode member includes a ring-shaped protruding portion that protrudes inward from the tube inner circumference for supporting the transmitting substrate , the ring-shaped protruding portion including a bearing surface opposed to a periphery of the support surface , and wherein the bonding material extends from a gap in a tube axial direction between the side surface and the tube inner circumference to a gap in a tube radial direction between the bearing surface and the periphery of the support surface . a transmission target including: a target layer for generating an X-ray through irradiation of an electron beam ; and a transmitting substrate for supporting the target layer and for transmitting the X-ray generated by the target layer ; and a target layer for generating an X-ray through irradiation of an electron beam ; and a transmitting substrate for supporting the target layer and for transmitting the X-ray generated by the target layer ; and a tubular anode member for supporting the transmitting substrate at a tube inner circumference thereof, wherein a side surface of the transmitting substrate and the tube inner circumference of the tubular anode member are bonded together by a bonding material , wherein the bonding material has a thickness that varies in a direction along a tube axis (P) of the tubular anode member , wherein the transmitting substrate includes a support surface for supporting the target layer , characterized in that the tubular anode member includes a ring-shaped protruding portion that protrudes inward from the tube inner circumference for supporting the transmitting substrate , the ring-shaped protruding portion including a bearing surface opposed to a periphery of the support surface , and wherein the bonding material extends from a gap in a tube axial direction between the side surface and the tube inner circumference to a gap in a tube radial direction between the bearing surface and the periphery of the support surface .
Functional device (DF) adapted to be secured to a wall (PF) inclined with respect to a horizontal plane and provided with at least two screws (Vj), said device (DF) having a center of gravity (CG) located in a front part (PV1) and comprising in a rear part (PR1) a base (ED) provided with at least one upper bushing (DS) and a lower bushing (DI) suitable for the said screws (Vj) to pass through, at least one upper sleeve (DS) comprising a screw passage (PA) delimited by an internal face (FI) comprising in an upper front zone (ZVS) at least one rigid claw (G) adapted to be housed between two neighboring portions of a thread of a screw (V1) to pre-hold said base (ED) with respect to the latter (V1), said screw passage (PA) of the upper sleeve (DS) having in a lower zone a radius decreasing from a lower front zone (ZVI) towards a lower rear zone (ZRI) to facilitate the crossing of said screw (V1) participating in the pre-maintenance audit.
A lithium battery comprising: an anode, a cathode, wherein the cathode comprises one or more transition metals, an electrolyte, and a separator interposed between the cathode and anode, wherein the separator comprises a boehmite and an anionic compound comprising sulfonate groups, and wherein the anionic compound is an anthraquinone. an anode, a cathode, wherein the cathode comprises one or more transition metals, an electrolyte, and a separator interposed between the cathode and anode, wherein the separator comprises a boehmite and an anionic compound comprising sulfonate groups, and wherein the anionic compound is an anthraquinone.
An optical device, having an optical axis and comprising: an objective having a first focal length, which is positive, and comprising a first group of one or more first lenses; an eyepiece having a second focal length, which is positive, and comprising a second group of one or more second lenses having a characteristic aberration; and a power corrector having a third focal length and comprising a third group of one or more third lenses located on the optical axis between the objective and the eyepiece, wherein the optical device has an input focal length defined jointly by the first and third focal lengths and a magnification equal to a ratio of the input focal length to the second focal length, and wherein the input focal length is such that an intermediate image of a scene is formed jointly by the objective and the power corrector, and the power corrector is located on the optical axis between the intermediate image and the objective, and the intermediate image is located between the power corrector and the eyepiece, and wherein the eyepiece and the power corrector together have a combined aberration that is less than the characteristic aberration of the eyepiece, and wherein the objective, the eyepiece, and the power corrector together define an exit pupil of the optical device of a given pupil diameter, and wherein the eyepiece has an eye relief defined by a location of the exit pupil. an objective having a first focal length, which is positive, and comprising a first group of one or more first lenses; an eyepiece having a second focal length, which is positive, and comprising a second group of one or more second lenses having a characteristic aberration; and a power corrector having a third focal length and comprising a third group of one or more third lenses located on the optical axis between the objective and the eyepiece, wherein the optical device has an input focal length defined jointly by the first and third focal lengths and a magnification equal to a ratio of the input focal length to the second focal length, and wherein the input focal length is such that an intermediate image of a scene is formed jointly by the objective and the power corrector, and the power corrector is located on the optical axis between the intermediate image and the objective, and the intermediate image is located between the power corrector and the eyepiece, and wherein the eyepiece and the power corrector together have a combined aberration that is less than the characteristic aberration of the eyepiece, and wherein the objective, the eyepiece, and the power corrector together define an exit pupil of the optical device of a given pupil diameter, and wherein the eyepiece has an eye relief defined by a location of the exit pupil.
A lithium secondary battery comprising a positive electrode, a negative electrode and an electrolyte for lithium secondary batteries interposed between the positive electrode and the negative electrode, wherein the electrolyte for lithium secondary batteries comprises a compound having a lithium-rich antiperovskite (LiRAP) crystal structure represented by the following Formula 2 or 3: [Formula 2] Li 3-y-x M y O 1-x Hal,Cl wherein M is Na, K, Rb, or Cs, Hal is F, Cl, Br, or I, and x and y are 0 < x < 1 and 0 < y < 2; [Formula 3] Li 3-2y-x M y O 1-x Hal x Cl wherein M is Mg, Ca, Sr, or Ba, Hal is F, Cl, Br, or I, and x and y are 0 < x < 1 and 0 < y < 1.
Planet-carrier for a mechanical reduction gear of a turbine engine, in particular of an aircraft, said planet-carrier comprising a cage defining an internal housing intended to receive a central sun gear with an axis of rotation X, and an annular row of planet gears arranged around the sun gear, said cage comprising two annular radial walls with respect to said axis X, and connected to one another at their outer periphery by a cylindrical wall of axis X, at least one of these radial walls comprising a mounting orifices of the axes of said planet gears, and the cylindrical wall comprising through-holes of the passage of the gearings of the planet gears so that they may engage with a gearing of the ring gear , which is intended to extend around the planet gears and the cage, characterised in that it comprises first and second independent lubrication circuits , the first circuit comprising a first oil inlet connected by a first annular oil chamber extending around the axis X to ducts supplying oil to said axes of the planet gears, and the second circuit comprising an second oil inlet connected by a second annular oil chamber extending around the axis X to channels supplying oil to the gearings of the planet gears with the ring gear, and in that said cage , first and second inlets, said ducts , said channels and at least a portion of said first and second chambers are formed of a single part.