mhurhangee/ep-ind-claims huggingface dataset:
A collapsible stereoscopic viewer comprising: a front viewing panel having apertures for lenses; a rear picture holding panel for placement of at least one stereogram; a first bracing side wall having a first diagonal folding crease, and a second bracing side wall having a second diagonal folding crease; a bottom panel; two ocular lenses; said bottom panel has a rear edge and a front edge, said rear edge being longer than said front edge, said rear edge of said bottom panel is integrally hinged to said rear picture holding panel, and said front edge of said bottom panel is integrally hinged to said front viewing panel; at a distance from said rear long edge of between 28% to 34% of the height of said rear picture holding panel, each of said first and second bracing side walls have a height of between 28% and 34% of the height of said picture holding panel; said first diagonal folding crease extends from a corner joining said picture holding panel and said first bracing side wall, and said second diagonal folding crease extends from a corner joining said rear picture holding panel and said second bracing side wall; said first bracing side wall is detachably secured to said front viewing panel, and said second bracing side wall is detachably secured to said front viewing panel when said stereoscope is in its assembled conformation, said first and said second diagonal folding creases (24, 26) cause said first and said bracing side wall (42, 44) to bend in toward each other; whereby said first and second bracing side walls support said stereogram against said rear picture holding panel. a front viewing panel having apertures for lenses; a rear picture holding panel for placement of at least one stereogram; a first bracing side wall having a first diagonal folding crease, and a second bracing side wall having a second diagonal folding crease; a bottom panel; two ocular lenses; said bottom panel has a rear edge and a front edge, said rear edge being longer than said front edge, said rear edge of said bottom panel is integrally hinged to said rear picture holding panel, and said front edge of said bottom panel is integrally hinged to said front viewing panel; at a distance from said rear long edge of between 28% to 34% of the height of said rear picture holding panel, each of said first and second bracing side walls have a height of between 28% and 34% of the height of said picture holding panel; said first diagonal folding crease extends from a corner joining said picture holding panel and said first bracing side wall, and said second diagonal folding crease extends from a corner joining said rear picture holding panel and said second bracing side wall; said first bracing side wall is detachably secured to said front viewing panel, and said second bracing side wall is detachably secured to said front viewing panel when said stereoscope is in its assembled conformation, said first and said second diagonal folding creases (24, 26) cause said first and said bracing side wall (42, 44) to bend in toward each other; whereby said first and second bracing side walls support said stereogram against said rear picture holding panel.
A passive electronic stacked component comprising: a stack of individual electronic capacitors (2 1 -2 N, 10 1 -10 N, 52 1 -52 N); a first lead (12, 54, 70, 182, 190, 194) attached to a first side of said stack; a second lead (12, 54, 70, 182, 190, 194) attached to a second side of said stack; a foot (20, 36, 40, 56, 60, 71, 180, 192, 195) attached to said first lead and extending inward towards said second lead; and a stability pin (22, 24, 42, 46, 48, 58, 181, 191, 193) attached to one of said foot or said first lead. a stack of individual electronic capacitors (2 1 -2 N, 10 1 -10 N, 52 1 -52 N); a first lead (12, 54, 70, 182, 190, 194) attached to a first side of said stack; a second lead (12, 54, 70, 182, 190, 194) attached to a second side of said stack; a foot (20, 36, 40, 56, 60, 71, 180, 192, 195) attached to said first lead and extending inward towards said second lead; and a stability pin (22, 24, 42, 46, 48, 58, 181, 191, 193) attached to one of said foot or said first lead.
A vacuum adiabatic body, comprising: a first plate having a first thickness; a second plate spaced apart from the first plate in an opposite manner, and having a second thickness, and the first thickness being greater than the second thickness; and sealing members arranged between the first plate and the second plate and configured to seal and fix the first plate and the second plate, a vacuum cavity being defined among the first plate, the second plate, and the sealing members, characterized in that the first plate is made of a stainless steel plate; the second plate is made of a stainless steel plate; and the sealing members are made of quartz glass, wherein the first thickness is 1.1 to 1.5 times the second thickness. a first plate having a first thickness; a second plate spaced apart from the first plate in an opposite manner, and having a second thickness, and the first thickness being greater than the second thickness; and sealing members arranged between the first plate and the second plate and configured to seal and fix the first plate and the second plate, a vacuum cavity being defined among the first plate, the second plate, and the sealing members, characterized in that the first plate is made of a stainless steel plate; the second plate is made of a stainless steel plate; and the sealing members are made of quartz glass, wherein the first thickness is 1.1 to 1.5 times the second thickness.
Cooking appliance with a cavity and an accessory part such as a turnspit which can be arranged within the cavity and which can be coupled by means of a coupling arrangement to a component which is arranged at least partially outside of the cavity, such as a driving component, wherein a coupling arrangement comprises a sleeve-like or tubular sealing element which provides a passage for a coupling section of the accessory part to a coupling section of the component, characterized in that the tubular sealing element is in substantially air tight contact to the component which is arranged completely outside of the cavity.
Use of a packaging unit with a receiving chamber for popcorn and the like and a pocket of rectangular shape in plan view, which is arranged externally on the receiving chamber and is dimensioned so that a conical beverage cup may be inserted into the pocket as a force fit, characterised in that at the lower end region of the pocket two strip-shaped wall sections are cut free from the side walls of the pocket by incisions, which extend parallel to the lower edge of the pocket, on both sides of two corners of the pocket situated next to one another and spaced from the receiving chamber, wherein the incisions extend at the same height on the pocket and wherein fold lines are formed at the two ends of the two strip-shaped wall sections extending perpendicular to them so that the two strip-shaped wall sections are foldable about the fold lines into the interior of the pocket for selectively receiving beverage cups of different size or a bottle in the receiving chamber, wherein either the beverage cup is inserted into the pocket as a force fit or a smaller beverage cup or the bottle is positioned on the upper edges of the two strip-shaped wall sections pressed inwardly into the interior of the pocket.
An abrasive article comprising: a base; an abrasive member comprising three distinct phases bonded to each other including abrasive particles, a metal matrix, and an infiltrant; and a backing region between the abrasive member and the base, wherein the backing region is a region distinct from the base and the abrasive member, wherein the backing region comprises a first phase and a second phase, characterised in that the first phase and the second phase are uniformly distributed within each other, and in that the first phase and the second phase are comprised of discrete regions, wherein the discrete regions of the first phase and the second phase have an average size within a range between 1 micron and 50 microns. a base; an abrasive member comprising three distinct phases bonded to each other including abrasive particles, a metal matrix, and an infiltrant; and a backing region between the abrasive member and the base, wherein the backing region is a region distinct from the base and the abrasive member, wherein the backing region comprises a first phase and a second phase, characterised in that the first phase and the second phase are uniformly distributed within each other, and in that the first phase and the second phase are comprised of discrete regions, wherein the discrete regions of the first phase and the second phase have an average size within a range between 1 micron and 50 microns.
A trigger pump dispenser comprising: a body; an outlet nozzle; a pump chamber; a dispensing passage; a piston for defining a variable volume in the pump chamber and thereby pumping liquid into and out of the pump chamber for dispensing through the outlet nozzle via the dispensing passage; a trigger coupled with the piston and movable to cause the piston to pump liquid; biasing means for biasing the trigger to a retracted position; and a shroud; in which the outlet nozzle is movable between a first 'on' position in which it is in fluid communication with the dispensing passage and a second 'off' position in which fluid communication with the dispensing passage is blocked; characterised by: the outlet nozzle having first and second indicator tabs (319B, 319A) projecting from the outlet nozzle and corresponding first and second indicator windows (322B, 322A) in the shroud wherein in the first 'on' position, the first indicator tab resides in the first indicator window and the second indicator tab is hidden by the shroud and in the second 'off' position, the second indicator tab resides in the second indicator window and the first indicator tab is hidden by the shroud. a body; an outlet nozzle; a pump chamber; a dispensing passage; a piston for defining a variable volume in the pump chamber and thereby pumping liquid into and out of the pump chamber for dispensing through the outlet nozzle via the dispensing passage; a trigger coupled with the piston and movable to cause the piston to pump liquid; biasing means for biasing the trigger to a retracted position; and a shroud; in which the outlet nozzle is movable between a first 'on' position in which it is in fluid communication with the dispensing passage and a second 'off' position in which fluid communication with the dispensing passage is blocked; characterised by: the outlet nozzle having first and second indicator tabs (319B, 319A) projecting from the outlet nozzle and corresponding first and second indicator windows (322B, 322A) in the shroud wherein in the first 'on' position, the first indicator tab resides in the first indicator window and the second indicator tab is hidden by the shroud and in the second 'off' position, the second indicator tab resides in the second indicator window and the first indicator tab is hidden by the shroud. the outlet nozzle having first and second indicator tabs (319B, 319A) projecting from the outlet nozzle and corresponding first and second indicator windows (322B, 322A) in the shroud wherein in the first 'on' position, the first indicator tab resides in the first indicator window and the second indicator tab is hidden by the shroud and in the second 'off' position, the second indicator tab resides in the second indicator window and the first indicator tab is hidden by the shroud.
Method for controlling fuel injection of a combustion engine having at least a first operating mode, being a standard default operating mode and a second operating mode, being a first economy mode, which method comprises the steps of: providing at least a first predetermined air-fuel mixture map, providing a constant air-fuel mixture map offset value for said second operating mode, and determining a first air-fuel ratio based on at least one engine operating parameter and said first predetermined air-fuel mixture map; adding said constant air-fuel mixture map offset value to the first air-fuel ratio to form a second air fuel ratio; determining if said first operating mode or said second operating mode is selected; controlling engine fuel injection according to said first air-fuel ratio when a currently requested fueling rate results in a smaller air-fuel ratio than said first air-fuel ratio and said first operating mode is selected; or alternatively controlling engine fuel injection according to said second air-fuel ratio when a currently requested fueling rate results in a smaller air-fuel ratio than said second air-fuel ratio and said second operating mode is selected. providing at least a first predetermined air-fuel mixture map, providing a constant air-fuel mixture map offset value for said second operating mode, and determining a first air-fuel ratio based on at least one engine operating parameter and said first predetermined air-fuel mixture map; adding said constant air-fuel mixture map offset value to the first air-fuel ratio to form a second air fuel ratio; determining if said first operating mode or said second operating mode is selected; controlling engine fuel injection according to said first air-fuel ratio when a currently requested fueling rate results in a smaller air-fuel ratio than said first air-fuel ratio and said first operating mode is selected; or alternatively controlling engine fuel injection according to said second air-fuel ratio when a currently requested fueling rate results in a smaller air-fuel ratio than said second air-fuel ratio and said second operating mode is selected.
A steering control apparatus for a steering system to which a motor torque that reciprocates a wheel turning shaft of a steering mechanism is applied by an actuator that uses a motor as a drive source, the steering control apparatus comprising a controller configured to: compute a torque command value that is a target value of the motor torque that the motor outputs; when an absolute value of a rotation angle of a rotary shaft exceeds a steering angle threshold for the steering system, compute a steering angle limit value that reduces with an increase in the absolute value of the rotation angle, the rotation angle of the rotary shaft being convertible to a wheel steering angle of a steered wheel coupled to the wheel turning shaft; set a limit value to less than or equal to the steering angle limit value, the limit value being an upper limit of an absolute value of the torque command value; control the motor such that the motor torque follows the torque command value whose absolute value is limited to less than or equal to the limit value; compute a basic command value based on a steering torque; when the absolute value of the rotation angle exceeds the steering angle threshold, compute a damping control amount such that the damping control amount increases with an increase in an excess of an angular velocity of the rotary shaft over a first upper limit angular velocity set according to the absolute value of the rotation angle; and compute the torque command value based on a value obtained by combining the basic command value and the damping control amount such that an absolute value of the basic command value is reduced. compute a torque command value that is a target value of the motor torque that the motor outputs; when an absolute value of a rotation angle of a rotary shaft exceeds a steering angle threshold for the steering system, compute a steering angle limit value that reduces with an increase in the absolute value of the rotation angle, the rotation angle of the rotary shaft being convertible to a wheel steering angle of a steered wheel coupled to the wheel turning shaft; set a limit value to less than or equal to the steering angle limit value, the limit value being an upper limit of an absolute value of the torque command value; control the motor such that the motor torque follows the torque command value whose absolute value is limited to less than or equal to the limit value; compute a basic command value based on a steering torque; when the absolute value of the rotation angle exceeds the steering angle threshold, compute a damping control amount such that the damping control amount increases with an increase in an excess of an angular velocity of the rotary shaft over a first upper limit angular velocity set according to the absolute value of the rotation angle; and compute the torque command value based on a value obtained by combining the basic command value and the damping control amount such that an absolute value of the basic command value is reduced.
Clip for fastening an article on a workpiece, having a basic body which is made of a relatively hard plastic material and has an accommodating portion, in which the article can be accommodated along a longitudinal axis, and a fastening portion, by means of which the basic body can be fastened on the workpiece, and having means for damping the transmission of vibrations between the article and the basic body, wherein the vibration-damping means have at least two first tongues which extend from the accommodating portion in a longitudinal direction, taper conically towards one another and are designed to be elastically deformable in the radial direction such that the accommodated article is retained by ends of the tongues wherein the accommodating portion has a radial opening for the radial introduction of the article, characterized in that at least one tongue (30a, 30e), adjacent to the radial opening, has an introduction slope.
A mirror comprising: a plate shaped mirror body; a heating section that is configured to heat a heated region in a plate face of the mirror body, characterized in that a heating density in the heated region of the mirror body is lower at an outer peripheral side of the mirror body than at a central side of the mirror body, and a heat generating body is provided at the heating section, the heat generating body generating heat so as to enable heating of the heated region of the mirror body on being supplied with cu rrent, an outer peripheral side of the heat generating body has a greater resistance than a central side of the heat generating body. a plate shaped mirror body; a heating section that is configured to heat a heated region in a plate face of the mirror body, characterized in that a heating density in the heated region of the mirror body is lower at an outer peripheral side of the mirror body than at a central side of the mirror body, and a heat generating body is provided at the heating section, the heat generating body generating heat so as to enable heating of the heated region of the mirror body on being supplied with cu rrent, an outer peripheral side of the heat generating body has a greater resistance than a central side of the heat generating body.
Method for controlling the operation of a burner which is used to heat feeder channels for molten glass originating from a glass furnace, said burner being supplied with a fuel gas, oxygen and an additional gas, characterised: - in that the power of the burner is varied by proportionally increasing or decreasing the fuel and oxygen flow rates so as to preserve a predefined constant stoichiometric ratio, and - in that the additional gas flow rate is injected in addition to the oxygen, said additional gas flow rate being controlled such that the sum of the additional gas flow rate, the oxygen flow rate and the fuel gas flow rate is greater than or equal to the minimum cooling flow rate of the burner D MIN. - in that the power of the burner is varied by proportionally increasing or decreasing the fuel and oxygen flow rates so as to preserve a predefined constant stoichiometric ratio, and - in that the additional gas flow rate is injected in addition to the oxygen, said additional gas flow rate being controlled such that the sum of the additional gas flow rate, the oxygen flow rate and the fuel gas flow rate is greater than or equal to the minimum cooling flow rate of the burner D MIN.
A method of manufacturing an aircraft, the method comprising: using a resilient vacuum cup to removably attach a tool-carrying rail to a rail-side surface of the aircraft, the tool-carrying rail including a longitudinal axis; and mounting a tool on the tool-carrying rail, wherein removably attaching the tool-carrying rail further comprises: removably sealing a perimeter of the vacuum cup to the rail-side surface of the aircraft against vacuum loss; rigidly positioning a point on the rail with respect to a point on the rail-side surface of the aircraft; coupling a vacuum source to a spatial volume occupying all of a space between the vacuum cup and the rail-side surface of the aircraft; and positioning the tool along the longitudinal axis of the tool-carrying rail; and characterized in that the method further comprises using a series of rigid stiffener elements (26, 28) to stiffen the resilient vacuum cup along a longer axis of each stiffener element (26, 28) perpendicular to the longitudinal axis of the tool-carrying rail and parallel to the rail-side surface of the aircraft and to stiffen the vacuum cup along a shorter axis of each stiffener element (26, 28) parallel to the longer axis of the tool-carrying rail and parallel to the rail-side surface of the aircraft. using a resilient vacuum cup to removably attach a tool-carrying rail to a rail-side surface of the aircraft, the tool-carrying rail including a longitudinal axis; and mounting a tool on the tool-carrying rail, wherein removably attaching the tool-carrying rail further comprises: removably sealing a perimeter of the vacuum cup to the rail-side surface of the aircraft against vacuum loss; rigidly positioning a point on the rail with respect to a point on the rail-side surface of the aircraft; coupling a vacuum source to a spatial volume occupying all of a space between the vacuum cup and the rail-side surface of the aircraft; and positioning the tool along the longitudinal axis of the tool-carrying rail; and removably sealing a perimeter of the vacuum cup to the rail-side surface of the aircraft against vacuum loss; rigidly positioning a point on the rail with respect to a point on the rail-side surface of the aircraft; coupling a vacuum source to a spatial volume occupying all of a space between the vacuum cup and the rail-side surface of the aircraft; and positioning the tool along the longitudinal axis of the tool-carrying rail; and