Abstract: Optical reading system and methods having multiple modes of operation, for example: omnidirectional and single-code picking; fixed and handheld reading; 1D and 2D code reading. In one configuration, an image-based system obtains input data via an area sensor (e.g., a 2D CCD array) with only data corresponding to a pattern of virtual scan lines being stored and processed. A user may implement different operating modes such as a first mode reading codes in any location or orientation and a second mode reading only a code oriented along a particular virtual scan line or group thereof. Alternately, the data reader is operable to switch between handheld mode selecting a first pattern of virtual scan lines to process and/or decode and a fixed mode selecting a second pattern of virtual scan lines to process and/or decode. Virtual scan patterns in either mode can change within or between frames.

Abstract: An adapter system including an adapter unit is described herein. The adapter unit includes receptacles shaped for removably receiving at least a portion of a portable electronic device therewithin. The adapter unit further includes at least one of an image capture device and a data capture device controllable by operating at least one user interface of the portable electronic device.

Abstract: A case is provided which encloses a retractable ribbon, on which graphics or text may be added. A window may be provided in the case which reveals graphics or text that relate to the graphics or text extending from the case. A device may be included in the case which makes pre-recorded sounds related to the graphics or words.

Abstract: A tamper-proof identification device, includes: a flexible, and non-stretchable band configured, dimensioned and fastenable at regions of its opposing ends to enclose and fit a body part of a wearer to identify the wearer; a flexible, electrically-conductive pathway carried by the band to define, when regions at the opposing ends of the band are fastened together to enclose and fit the body part, an electrically-conductive loop having first and second gaps therein; an electronic identification device carried by the band and electrically connected to the loop across the first gap; and a pair of electrical terminals carried by the band and spaced by the second gap, the pair of electrical terminals being electrically connected to the loop at the second gap for connection to a data processor, such that electrical communication may be established between the electronic identification chip and the data processor via the electrically-conductive loop when the data processor is connected to the pair of electrical term

Abstract: It is described a transponder tagged object, comprising: a conductive structure (103, 105, 403, 405); an insulating region (109, 409) galvanically isolating a first portion (103, 403) of the conductive structure from a second portion (105, 405) of the conductive structure; and a transponder tag (111, 411, 611) comprising a first antenna pad (133, 333) and a second antenna pad (135, 335), wherein the transponder tag is fixed at the object such that the first portion of the conductive structure in particular capacitively couples to the first antenna pad and such that the second portion of the conductive structure in particular capacitively couples to the second antenna pad. Further, a method for manufacturing a transponder tagged object is described.

Abstract: A semiconductor device is provided with a power supply circuit having a function to generate a power supply voltage from a wireless signal and an A/D converter circuit having a function to detect the strength of the wireless signal by an A/D conversion of a voltage generated from the wireless signal. This enables to provide a semiconductor device which does not require replacement of batteries, has few limitations on its physical shape and mass, and has a function to detect a physical position. By formation of the semiconductor device with use of a thin film transistor formed over a plastic substrate, a lightweight semiconductor device, which has flexibility in physical shape and a function to detect a physical location, can be provided at low cost.

Abstract: In a method and an apparatus for personalizing card-shaped data carriers (10, 11, 12), for example chip cards in the formats ID000 to ID3 or other suitable formats, a card-shaped data carrier (10, 11, 12) to be personalized is transported by means of a transport device within the apparatus. During the transport motion, personalization data are transferred to an electronic storage device (13) of the card-shaped data carrier (10, 11, 12) by means of a personalization device (40). The transporting of the card-shaped data carrier (10, 11, 12) is effected by means of a band-shaped or tubular carrier (20, 21, 22, 23) on which a multiplicity of card-shaped data carriers (10, 11, 12) to be personalized are arranged one behind the other in the transport direction.

Abstract: A two-dimensional code having a rectangular region is provided. In the rectangular region, there are code blocks composed of a plurality of cells, a first specific pattern specifying the positions of the cells, and a second specific pattern separating the code blocks from a background of the code. The first specific pattern is located at a specified corner of the rectangular region. The second specific pattern is located along one or more of first borders along which the first specific pattern is located, the first borders being part of the borders of the rectangular region. The code blocks include error-correction code blocks, which are located along second borders which are different from a border of the borders along which the second specific pattern is located. The second borders are part of the borders. Compressed data code blocks are also arranged in the same way as the error-correction code blocks.

Abstract: A conveyer mechanism (110) may include one or more composition inspection units provided along the intended product transport path. The product's composition, e.g., it's ink composition, is compared with a predetermined standard, to determine whether the product is acceptable. A bar code (48, 45.1, 47.1, 85) may be provided to an external surface of the article for identification/traceability purposes.

Abstract: An apparatus for atomizing a precursor liquid for vapor generation and thin film deposition on a substrate. The precursor liquid is atomized by a carrier gas to form a droplet aerosol comprised of small precursor liquid droplets suspended in the carrier gas. The droplet aerosol is then heated to form vapor, producing a gas/vapor mixture that can be introduced into a deposition chamber to form thin films on a substrate. The liquid is introduced into the atomizing apparatus in such a manner as to avoid excessive heating that can occur or lead to the formation of undesirable by-products due to material degradation as result of thermal decomposition. The apparatus is particularly suited for vaporizing high molecular weight substances with a low vapor pressure that requires a high vaporization temperature for the liquid to vaporize. The apparatus can also be used to vaporize solid precursors dissolved in a solvent for vaporization.

Abstract: A pump fragrance device includes a pump spray, an inner housing connected to a spray head, and an outer housing on the inner housing. On the inner housing, a junction piece connected to the spray head has an opening thereon. The inner housing's surface has an assembling piece to fit with the outer housing, which has an assembling structure to fit with the inner housing. The inner and outer housings form a fixing structure. The fixing structure is filled with a volatile carrier agent, at least a part of which is located in the spray path of the pump spray. When used, the pump spray sprays content onto a surface of the volatile carrier agent, thereby reducing the quantity of the volatile aromatic agent used. This prolongs the diffusion time of the volatile aromatic agent, thereby relieving users from the danger of the fragrance device being under high temperature.

Abstract: According to various embodiments, a system includes a gasification fuel injector. The gasification fuel injector includes a tip portion, an annular coolant chamber disposed in the tip portion, a recessed surface for cooling control and a first structural support extending through the annular coolant chamber. The first structural support divides the annular coolant chamber into a first passage and a second passage.

Abstract: A rotary atomizer is disclosed, comprising an atomizer bell and a shaft carrying the same. The rotary atomizer may further include a retainer between the atomizer bell and the shaft, said retainer preventing, e.g., by the action of a centrifugal force, the atomizer bell from detaching itself from the shaft.

Abstract: A sprinkler includes a turbine, a gear drive, a nozzle turret, and a nozzle that is installed in the turret. The gear drive rotatably couples the turbine and the nozzle. The nozzle has an exit angle which is different from its entry angle to change the trajectory of the water as it passes through the nozzle. The nozzle can be installed in an orientation to increase the trajectory of the water leaving the sprinkler, or installed in an orientation to decrease the trajectory of the water leaving the sprinkler.

Abstract: An injector for vehicles improves utilization rate of air and mixing rate of air and fuel by disposing first and second nozzle holes having different K factors alternately. The injector for vehicles may include a housing of cylindrical shape, a plurality of nozzle holes communicating an inside of the housing with an outside thereof at a lower end of the housing, and a needle adapted to move reciprocally in the housing, and selectively opening or closing the nozzle hole, wherein the plurality of nozzle holes has a plurality of K factors.

Abstract: A multi-layer piezoelectric element includes a stacked body configured so that piezoelectric layers and internal electrode layers are alternately laminated, and an external electrode composed of a sintered material of both electrically conductive particles and a glass, the external electrode which is bonded to a side surface of the stacked body and makes electrical connection with the internal electrode layers. The external electrode has a stacked body-side layer region containing glass as secondary constituent at its stacked body-facing side, and an exterior-side layer region containing glass as minor constituent at its exterior side. The glass of the exterior-side layer region is distributed along grain boundary of the conductive particles on an outermost surface of the exterior-side layer region.

Abstract: A nozzle body may be provided. The nozzle body may comprise a flow path and a vent. The flow path may be configured to provide an open channel for a fluid between a lower portion of a pipe and at least one outlet. The vent may be configured to vent a gas in an upper portion of the pipe to the flow path.

Abstract: The invention relates to a method for reusing materials and/or products by pulsed power according to which a series of electrical discharges are generated between at least two electrodes in a reactor containing an ambient liquid as well as the materials and/or products to be reused, characterised in that the energy of said electric discharges, the voltage between the electrodes, the switching time and the frequency of the discharges are selected such that said discharges generate electric arcs that pass through the materials and/or products to be reused, and mechanical shock waves that propagate across the materials and/or products to be treated in the reactor. The result is fragmentation, pulverisation, dispersion and separation of the elements that make up the materials and/or products to be reused. The invention also relates to it device for implementing said method.

Abstract: The invention relates to a method for reusing materials and/or products according to which, in a first step, a series of electrical discharges are generated between at least two electrodes in a reactor containing an ambient liquid as well as the materials and/or products to be reused, in which the series of said electric discharges produces, due to the energy, the frequency of the electric discharges as well as the voltage between the electrodes and the switching time, a mechanical shock wave which propagates across the materials and/or products to be treated in the reactor, characterised in that after a first step of embrittlement by the mechanical shock wave thus produced, the products and/or materials are exposed to a series of electric discharges in which the energy, the voltage between the electrodes that generate said discharges, the switching time and the frequency of the discharges are selected so that said discharges perform selective fragmentation of the material by the effect of an electromagnetic

Abstract: A system and method of converting tires or other solid carbon based material is disclosed, including providing a chamber, feeding solid carbon based material into the chamber, rotating the chamber while heating and reducing the material in the chamber, collecting solid residue from the chamber, collecting vapor from the chamber, and converting vapor collected from the chamber to a liquid. The chamber has an interior surface and can include one or more ribs on the interior surface for rotating and tumbling the material in the chamber while heating the material. In an embodiment, the system and method includes rotating and heating tires in the chamber to a temperature from about 500° F. to about 1000° F. at least in part under vacuum causing the tires to collapse and liquefy, collecting solid carbon black, and collecting and re-pressurizing hot gasses from the chamber and using the re-pressurized hot gasses to heat the chamber.

Abstract: A flush system for processing waste slurry contains animal waste, comprising a primary separator, a primary digester, and a secondary digester. The primary separator separates the waste slurry into a first portion and a second portion. The primary digester digests the first portion. The secondary digester digests at least part of the second portion. A solids content of the first portion is higher than a solids content of the second portion.

Abstract: In order to detect a lack of coffee beans in a grinder unit of a coffee maker, a method is suggested in which the level and/or the spectrum of an oscillation generated by the grinder unit during its operation is measured. The level of the oscillation and/or the nature of the spectrum are used to decide whether or not coffee beans are present in the grinder unit. Preferably, the level of oscillation of the housing of the coffee grinder unit is monitored. If the level changes by more than a preset value and/or falls below a reference value, it is decided that coffee beans are lacking.

Abstract: A pulverizing grinder used in the industrial processing of partially processed, or raw, silicon ore to achieve finely powdered silicon or silicon compound. It involves several parts, primarily an electric motor and a disc and blade arrangement driven by the motor, to achieve a finely ground silicon powder material. The upper part of case contains the electric motor, which dives a shaft that extends to a lower part of the case. The revolving shaft of electric motor is connected with the main shaft inside the case. At least one tier of rotating disc is fastened to the bottom of the shaft. Each disc has an even number of blades, each of which is positioned by suitable anchor fixture. The grinding or pulverizing of the silicon material is achieved by the high speed rotation of the discs and the impact of the blades on the material.

Abstract: A retainer assembly for securing a bearing relative to a shaft in a first axial direction. The retainer assembly includes a collar, a lock ring, and a retaining nut. The collar includes a first portion, a second portion, and a bore extending through the first portion and the second portion. The first portion includes external threads, and the second portion includes an internal recess extending circumferentially around the bore. The lock ring is located within the internal recess such that the lock ring is positioned between the second portion of the collar and the shaft and is removably coupled to the shaft. The retaining nut includes internal threads that threadingly engage the external threads of the first portion.

Abstract: In one aspect of the invention, a system for exchanging a milling chamber comprises a vehicle comprising a milling chamber supported by the underside of the vehicle. The underside comprises a track that interfaces with a guide of the milling chamber. The track and guide are configured to accommodate lateral movement of the milling chamber with respect to a length of the vehicle.

Abstract: A moveable shaft assembly including a frame, a first shaft, and a first drive assembly. The frame includes a first support wall and a second support wall opposite the first support wall. The first shaft includes a drive end and a support end and defining a first axis therebetween. The first shaft extends between the first support wall and the second support wall. The first drive assembly rotates the first shaft about the first axis, and the first drive assembly is coupled to the drive end of the first shaft. The first shaft and first drive assembly are moveable relative to the frame in response to a reaction force acting on the first shaft in a direction oblique or transverse to the first axis.

Abstract: A pick holder for a roll sizer, the roll sizer including at least one roll drum defining a drum axis, the roll drum rotating about the drum axis. The pick holder includes a base and a shoulder. The base includes at least one hole for receiving a fastener for removably coupling the pick holder to the roll drum. The shoulder is coupled to the base.

Abstract: A buoyancy system (2) comprising at least one float (3) and deployment means (30) for deploying said float (3), said buoyancy system (2) having engagement means (5) for activating the deployment means (30) of said float (3), said buoyancy system (2) including at least two immersion sensors (20) for issuing an order for automatic deployment of said float (3) to the deployment means (30). Said engagement means (5) are activated only manually, said deployment means (30) are provided with a memory (31) containing a pre-established list of events, and said deployment means (30) deploy each float (3) when a predetermined event occurs.

Abstract: A torque link member for aircraft landing gear includes a first end for connecting to a lower portion or an upper portion of the aircraft landing gear and a second end for connecting to another torque link member. A locking pin is disposed on one of the upper portion, the lower portion, the first end or the second end. The locking pin is axially movable between an engaged position wherein the pin protrudes for interengagement with a cooperating aperture on the first end, the second end, the upper portion, the lower portion, or the second end of the other torque link member, and a disengaged position. The locking pin is biased toward the engaged position and movable against the biasing to the disengaged position.

Abstract: A mult-rib box-shaped aeronautical structure comprising upper and lower skins (19, 21) stiffened by span wise stringers (25, 25?, 25?), span wise front and rear spars (11, 13) and chord wise ribs (27, 27?, 27?), where at least one panel (31, 33) of any of said skins (19, 21) is non delimited by said ribs (27, 27?, 27?) and said stringers (25, 25?, 25?) and comprise an stiffening element (41, 43) arranged as a panel breaker to avoiding the need of increasing the panel thickness to withstand buckling loads.

Abstract: A lock is proposed for securing containers or similar freight on a cargo bay floor of an aircraft in a vertical direction perpendicular to the cargo bay floor and in a transverse direction perpendicular to a longitudinal direction of the aircraft. The locking element comprises at least one lock attached to a frame for securing containers or similar freight and with a claw in the transverse direction of the aircraft to surround and hold a part section of the container. At least one lock is arranged mobile and fixable in a guide of the frame in order to adapt the spacing of the locks to containers of different sizes.

Abstract: Disclosed is a support strut designed as a passive safety strut for the support of a floor structure of an aircraft, with a local instability formed by a strut section, for example for purposes of defining a design fracture point in the event of unusual compressive loading, for purposes of improving the safety of the occupants of the aircraft.

Abstract: An integrated user interface system being disposed at a chair and methods for manufacturing and using same. The user interface system comprises one or more interface elements that are disposed at an armrest or other suitable chair location and that are obscured from view or otherwise de-emphasized when a user is distal from the user interface system. At least one selected interface element becomes emphasized when a user hand becomes proximate to the user interface system. The selected interface element can become emphasized, for example, by becoming visible and/or by forming a raised projection. Upon becoming emphasized, the selected interface element is activated for use and can be manipulated to interact with available system resources. The chair advantageously can appear to be an ordinary chair when the user interface system is not in use and can present the user interface system when the user wishes to access the system resources.

Abstract: An assembly of longitudinal structural stiffeners for an aircraft including, in a front portion of the fuselage, a windscreen that is slightly recessed relative to the airplane nose, and a fuselage portion extending in alignment with the airplane nose up to the base of the windscreen. The stiffeners include a bending-resistance main plane and are arranged under the flap and connected to the fuselage along a force transfer line. For one or more of the stiffeners, the bending resistance main plane substantially coincides, at least a certain number of points of the fuselage force transfer line, with the plane predetermined by the local normal to the fuselage surface and the longitudinal axis of the airplane. A method is also provided for calculating the shape of the stiffeners.

Abstract: An aircraft structure 101 comprising a skin panel 111, having an outer surface forming an external face of the structure, and an inner surface internal to the structure, the aircraft structure 101 also comprising a plurality of stringers 150 extending along a length of the inner surface of the skin panel, and an inner panel 112 spaced apart from the inner surface of the skin panel 111, so as to form an internal cavity adjacent to the skin panel, and wherein the stringers 150 are located within the cavity.

Abstract: A tail-cone of an aircraft includes a skin provided with a movable fairing which, by a swing articulated mechanism, is supported on the skin in order to allow the opening/closing of the movable fairing and gain access to the inside of the tail-cone. The tail-cone includes actuators for operating the swing articulated mechanism in order to permit the automatic opening and closing of the movable fairing to be carried out.

Abstract: Disclosed is a method for the manufacture of an aircraft fuselage with at least two fuselage barrels wherein connecting segments are firstly prepared for the formation of a transverse joint region for a later transverse joint, and the fuselage barrels are then constructed around the connecting segments; also disclosed is an aircraft fuselage with ring-type connecting segments for the formation of such a transverse joint.

Abstract: An aerofoil structure (1) comprising at least two spars (2, 4) spaced apart in a fore and aft direction so as to define a fuel carrying volume between the spars, and at least one longitudinal corrugated reinforcing member (6, 7) disposed between the spars, each reinforcing member being corrugated in the longitudinal direction to form a series of forward ridges (9) on a forward side of the reinforcing member and a series of aft ridges (8) on an aft side of the reinforcing member, wherein each reinforcing member is directly attached by its forward ridges to one of the spars or to the aft ridges of an adjacent one of the reinforcing members, and wherein each reinforcing member is directly attached by its aft ridges to one of the spars or to the forward ridges of an adjacent one of the reinforcing members. Also, a method of manufacturing an aerofoil structure.

Abstract: Interface arrangement between a first component (11) and a second component (21) of an aircraft structure having an aerodynamic contour, such as a wing skin and a wing leading edge panel, the first component (11) having a joggle so that it includes a first area (13) which surface (15) belongs to the aircraft aerodynamic contour and a second area (17) where the joint with the second component (21) takes place, the second component (21) having a surface (23) belonging to the aircraft aerodynamic contour, in which a sealing part (31) suitable shaped to maintain the continuity of the aircraft aerodynamic contour in the interface area between said components (11, 13) as well as to fill the expected gap (25) between said components (11, 13) is joined to the second component (21).

Abstract: Interface arrangement between a first component (11) and a second component (21) of an aircraft structure having an aerodynamic contour, such as a wing skin and a wing leading edge panel, both components being made of composite material, the first component (11) having a joggle so that it includes a first area (13) which surface (15) belongs to the aircraft aerodynamic contour and a second area (17) where the joint with the second component (21) takes place, the second component (21) having a surface (23) belonging to the aircraft aerodynamic contour, in which an intermediate part (31) made of a composite material or a plastic material and suitable shaped for maintaining the continuity of the aircraft aerodynamic contour in the interface area between said components (11, 13) as well as to fill the expected gap (25) between said components (11, 13), is joined to the first component (21).

Abstract: Interface arrangement between a first component (11) and a second component (21) of an aircraft structure having an aerodynamic contour, such as a wing skin and a wing leading edge panel, the first component (11) having a joggle so that it includes a first area (13) which surface (15) belongs to the aircraft aerodynamic contour and a second area (17) where the joint with the second component (21) takes place, the second component (21) having a surface (23) belonging to the aircraft aerodynamic contour, in which the second component (21) includes a chamfer-shaped ending (29) that extends beyond the overlapping area (27) where the joint with the first component (11) takes place so that the gaps (26, 28) between the first component (11) and the second component (21) are minimized.

Abstract: An airframe structural element, such as an aircraft rib, is disclosed that comprises an integral pipe connector element for connecting pipes through the structural element. The pipe connection means provided by the pipe connector element may be aligned on a common axis with a pipe connection means provided by an adjacent airframe structural element.

Abstract: The invention concerns a shell segment for the purpose of manufacturing a fuselage cell section for a fuselage cell of an aeroplane, with at least one skin field and with a multiplicity of longitudinal stiffeners arranged thereon, in particular stringers, and also at least one transverse stiffening element running transverse to the longitudinal stiffeners, in particular at least one frame. In that the connection of the at least one transverse stiffening element to the at least one skin field is undertaken with at least one connecting bracket wherein the at least one connecting bracket has at least one corrugation, the supporting brackets for purposes of absorbing tilting moments of the frames, in forms of embodiment of shell segments of prior known art, can be omitted. By this means a considerable weight reduction is possible with, at the same time, a reduced production effort.

Abstract: An ejection system for ejecting a payload from a payload delivery vehicle is provided. The ejection system includes an airbag ejection system configured to eject the payload from the payload delivery vehicle, a payload separation system configured to selectively couple the payload to the airbag ejection system, and a controller configured to inflate the airbag ejection system and further configured to signal the payload separation system to release the payload from the airbag ejection system.

Abstract: A vital programmable logic device (VPD) is provided having at least two microprocessors. The VPD is configured to provide failsafe operation of a vital control system while operating in a closed circuit environment. In at least one embodiment of the present invention, railroad grade crossing signals are controlled by the VPD.

Abstract: The method includes the utilization of clips or hooks or other securing elements of any configuration or means of attachment that may be affixed to the body of a gutter guard for the purpose of receiving and securing heating cables and/or other cables or elements. Additionally, the method includes the use of openings or grommets within the body of a gutter guard through which cables or other elements may pass and be secured.

Abstract: A track type supporting mechanism for supporting at least one machine is disclosed in the present invention. The track type supporting mechanism includes a base, at least one linear guideway disposed on the base, at least one sliding block slidably disposed on the at least one linear guideway, and at least one supporting platform disposed on the at least one sliding block for supporting the at least one machine, so that the at least one machine slides relative to the base via the at least one linear guideway and the at least one sliding block.

Abstract: A cable mount 10 defines an aperture for receiving an electrical or fluid conduit, and has upstanding ribs 15 which define a circular track 14 for a cable tie. The ribs also define flat mounting planes to prevent rotation of the mount with respect to a substrate. An additional attachment member (41-46) is positioned to allow adaptation of a mould to different kinds of attachment member.

Abstract: A cable wedge assembly that can streamline installation of cabling assemblies upon trees and other structures is provided. For example, the cable wedge assembly need not require specialized tools for installation. Rather, the unique features and functions of the assembly attach to a cable merely by inserting a cable through the assembly, tightening a portion of the connector upon another and establishing tension in the cable. Once cable tension is established, the integral wedges seat causing attachment to and retention of the cable. This attachment and retention is effected by way of split conical inserts disposed within the housing of the assembly.

Abstract: An infant care organizational aid including a vertically extending and multi-sided body with a plurality of extending legs engaging a floor location. A plurality of clips extend from surface locations of the body and are configured to receive end extending portions associated with each of a plurality of individual holders in order to engage with specified clip locations associated with the body.