Abstract: A reclosable package comprises a receptacle having first and second walls, respective mouth portions of the front and rear walls forming a mouth that communicates with an interior volume of the receptacle; a zipper having mutually interengageable zipper strips, one zipper strip being joined to the mouth portion of the front wall and the other zipper strip being joined to the mouth portion of the rear wall; a slider mounted to the zipper, the slider initially being parked in a position whereat the zipper is closed along a majority of its length; and a tack seal that resists movement of the slider in an opening direction from the initially parked position. The tack seal is designed to rupture and no longer resist slider movement when a predetermined threshold level of force is exerted by the slider.

Abstract: An assembly comprising: a tube made of resilient material, at least a portion of the tube forming a circumferential boundary of a chamber; first and second end cap assemblies supporting the tube at opposite ends thereof and forming respective end boundaries of the chamber, the chamber being filled with pressurized fluid; a hard roller that forms a nip with the tube; a fixed structure that supports the first and second end cap assemblies and the hard roller, the first and second end cap assemblies and the hard roller being respectively pivotably coupled to the fixed structure, and the fixed structure comprising a passageway that is in fluid communication with the chamber; and a slider-zipper-film assembly that is passed through the nip. The tube is deformed radially inward to allow passage of slider through the nip.

Abstract: A driving anvil washer retaining apparatus (12) for a rivet gun (14) includes a magnetized element (21). The magnetized element (21) is coupled to the rivet gun (14) and retains an anvil washer (52) during installation of a rivet (82). A method of installing a rivet (82) includes inserting a stem (46) of a rivet assembly (80) into a rivet gun nose (22) having at least one magnetized portion (21). A rivet (82) of the rivet assembly (80) is inserted into at least one object. The stem (46) is removed from the rivet assembly (80). A driving anvil washer (52) is retained via the magnetized portion (21).

Abstract: An attachment system for coupling together two airplane sections includes an attachment section securing one of the airplane sections and a mount section affixed to the other section. The attachment section includes a top, a bottom, a first end, and a second end. Coupled to the top are a two clamp sections, whereby at least one of the clamp sections is moveable. Coupled to the bottom is a pair of buttons. The mount section includes a top and a bottom, such that the mount bottom couples to the second airplane section. The mount section further includes a track coupled to the mount top, wherein the track includes an open end having outwardly tapered edges and a closed end. The one of the buttons slides into the track for coupling the attachment section to the mount section.

Abstract: A method of manufacturing flexible containers that are hermetically resealable. Each resealable container comprises a receptacle and a pair of plastic zipper strips. The zipper strips are flattened at the ends within the side seal regions and are joined to each other, without substantial deformation of the closure profiles, in respective transition areas substantially contiguous with the side seals. These transition areas of zipper strip joinder assist in providing a leakproof transition from the openable section of the zipper to the side seals, where the closure profiles are fused and flattened (i.e., crushed).

Abstract: An eccentric fastening device is provided. The eccentric fastening device includes a first threaded fastener, a base and a rotary lug providing a non-fastened pre-assembled position. The base includes a top, a bottom, a stem and a hole, where the stem axially extends from the bottom of the base, and the hole axially extends from the top through the stem of the base. The rotary lug is releasably retained in the hole of the base by the first threaded fastener. The rotary lug includes a cylindrical portion having a thread and a head, wherein the head is offset from the cylindrical portion. The cylindrical portion is substantially axially concentric with the hole of the base, allowing the head to be eccentrically rotated on or off of the stem, whereby a selective structure may be variably clamped and releasably retained between said head and said base. An aircraft having an eccentric fastening device is also provided. A method of installing the same is also provided.

Abstract: A security system for sea cargo containers wherein each container is provided with a container security device comprising a processor, a radio, a memory, a battery and one or more sensors. When the containers are within range of each other, the container security devices communicate to form an ad hoc wireless sensor network. That network communicates with a communications infrastructure, such as satellites or GSM communications means, via a gateway that aggregates data originating from the various container security devices.

Abstract: An architectural archway for an aircraft. The archways can be positioned individually, or in pairs or other sets along the length of an aircraft fuselage. The archways are used to run or connect various transport elements, such as electrical wiring, water lines, and environmental control system conduits, between the upper crown, lower bay and passenger cabin of the aircraft. The invention simplifies installation complexity and eliminates the installation and variability associated with running transport elements between the various sections of the aircraft.

Abstract: An optical fiber connector has a center component provided with opposite first and second ends into which first and second connector inserts holding ends of respective optical fiber bundles are to be inserted, an optical core element mounted in the center component having opposite ends against which the ends of the respective optical fiber bundles in the first and second connector inserts are to be abutted in alignment, and fastener elements provided with the first and second ends for securely holding the first and second connector inserts in abutting contact with the respective opposite ends of the optical core element.

Abstract: A method of manufacture comprising the following steps: (a) continuously advancing a web of bag making material at a first rate; (b) continuously joining portions of a downstream portion of a fastener tape to respective portions of the continuously advancing web of bag making material; (c) intermittently advancing an upstream portion of the fastener tape while the downstream portion is advancing continuously, the upstream portion of the fastener tape being stationary during a respective dwell time of each work cycle and advancing during the remainder of each work cycle at a second rate faster than the first rate; (d) accumulating a portion of the fastener tape disposed between the upstream and downstream portions to compensate for the difference in the first and second rates during the aforementioned remainder of each work cycle; and (e) deforming a respective section of the upstream portion of the fastener tape during each dwell time.

Abstract: In accordance with the present invention a method for the direct manufacture of aerospace duct elements is provided comprising executing a single build run on a build chamber using direct fabrication technology to generate at least one duct section. The at least one duct section is generated by forming a plurality of partial cylinder duct segments orientated within the build chamber in a nested arrangement during the single build run, and assembling at least two of the partial cylinder duct segments to form the duct section. The duct section has a duct cross-sectional profile larger than a build chamber profile.

Abstract: A reclosable package comprises a receptacle having a mouth, a header that encloses a space above the mouth, and a slider-zipper assembly disposed in the mouth, the slider-zipper assembly comprising a slider mounted to a zipper. The header has a tear-away portion and respective remaining portions that flank at least a portion of the slider. A pull tab is coupled to and rotatable relative to the slider and projects above the upper edges of the remaining portions of the header. This arrangement enables the user to move the slider by grasping the pull tab. The user need not reach into the space between the remaining portions of the header to grasp the slider itself. In one embodiment, the pull tab is coupled to the sidewalls of the slider.

Abstract: The invention provides a film holder for an advanced scanner having a notched and grooved frame surrounding a central support, preferably a glass plate. The frame contains grooves along the side edges of the frame that correspond with accepting gears of a scanner such as a 4,000-dpi scanner. The central support provides a mounting surface for a piece of film to be scanned, wherein the film is mounted on the central support with a mounting fluid. The mounting fluid smoothes over imperfections in the film and central support, and holds the film secure to the support over the entire surface area of the film, thereby improving scan quality.

Abstract: Nonwoven laminate products having improved wet peel strength after aging and ethylene oxide sterilization, and improved drape and softness, which are suitable for medical, surgical and hygienic applications, are produced by laminating one or more nonwoven substrates on one or both sides of a cast film. The cast film is produced using conventional extrusion processes, such as co-extrusion. Multiple extruders are used to process and melt different polymers and then specially designed selector plugs and feed-blocks are used to combine the different polymers into different layers to form a multiple layer structure such as A-B, A-B-A, A-B-C, A-B-B-A, etc.

Abstract: An apparatus and method for securing a plurality of stringers to a mandrel during lay-up is provided, the plurality of stringers and mandrel forming a lay-up surface. The apparatus includes a vacuum source and a first vacuum attachment assembly in communication with said vacuum source to tightly secure the first vacuum attachment assembly down against the lay-up surface. A second vacuum attachment assembly is provided in communication with the vacuum source to force it tightly down against the lay-up. A flexible spacer is in rigid communication with the second vacuum attachment assembly and includes an extended end in communication with the first vacuum attachment assembly such that the flexible spacer presses one of the stringers against the mandrel.

Abstract: A hybrid fluorescent-LED lighting system comprising a controller, LED elements, fluorescent lamp, and a color/brightness sensor, wherein the color/brightness sensor measures a combined light output of both the fluorescent lamp and the LED elements. A method for controlling the hybrid fluorescent LED lighting system includes receiving a request for brightness/color, setting a fluorescent lamp output to a particular brightness level, setting output of LEDs to a particular brightness level, measuring a combined output of the fluorescent lamp and LEDs; and adjusting the output of LEDs until the total output of the fluorescent lamp and LEDs matches the request for brightness/color. Adjusting the output of LEDs may include the step of driving a specific spectrum range of the LEDs as necessary in order to fill-in variances in a spectrum range of the fluorescent lamp. The method further allows modifying the color of light output.

Abstract: An object transport and stowage system for an aircraft (10) includes a transport unit (32) for the transport of an object (20) within the aircraft (10). A first transfer drive system (62) is attached to the transport unit (32) and includes object engagement devices (92) that are engagable with the object (20). A motor (120) is mechanically coupled to and rotates one or more of the object engagement devices (92). A controller (66) is electrically coupled to the motor (120) and translates the object (20) relative to the transport unit (32). Another object transport and stowage system for an aircraft (10) includes a housing (150) for the stowage of an object (20) on the aircraft (10). A transfer drive system (64?) is attached to the housing (150) and includes object engagement devices (168, 176), which are engagable with the object (20). A motor (162) is mechanically coupled to and rotates one or more of the object engagement devices (168, 176).

Abstract: A method for reducing force and position control tracking errors caused by changes in hydraulic pressure at the actuator ports of a hydraulic servo valve. The method may use either the force command signal or the load cell signal in conjunction with a mathematical algorithm to compensate for changes in the flow capacity in the servo valve caused by changes in pressure at its ports. Good performance can be attained using the load cell signal. Alternatively, the algorithm can use the force command signal. The performance of the control loop with proper velocity feed-forward compensation keeps the feedback signal largely in phase with the command. Pressure sensors for detecting pressure changes at the actuator ports of the servo valve are not required for load droop compensation.

Abstract: Interior lighting and illumination systems for aircraft, particularly commercial passenger airplanes. Opposing pairs of LED lamps are positioned in the ceiling panels above the aisles between sets of seats in the passenger cabins. One set of LED lights are directed to illuminate the ceiling panels and may be in a particular color. The other set of LED lights are positioned to shine their lights on storage/stowage bins positioned across the aisles, thus creating a cross-bin lighting system. This enhances the cabin architecture and provides cabin illumination. A reflector can be positioned to direct the light and reduce possible glare to the passengers. The reflector directs the light rays from the LED lights which emanate from the top of the reflector to shine on the lowest part of the bins. The light rays leaving the reflector cross in front of the reflector.