Abstract: A pivot arrangement for a thrust reverser door of a gas turbine engine, the pivot fitting having a base and a shaft projecting from a main side of the base. The shaft receives a preferably curved pivot arm of the door to provide a low profile arrangement which improves performance when the doors are stowed.

Abstract: A cargo container includes a cargo box affixed atop a hollow base, with the base including forklift tunnels extending therethrough with elongate bays disposed parallel thereto. Each bay includes a removable tray for receiving electrical batteries. And, a temperature control system is disposed on a sidewall adjoining the base.

Abstract: The thrust reverser comprises sections, such as arms and skins, which may be connected along joints to provide a thrust reverser body. A plurality of fittings may be integrally formed on a surface of each arm.

Abstract: A thrust reverser door provides in one aspect a separation of structural and aerodynamic functions through the provision of individual structures. In some embodiments, an aerodynamic element is adjustable in position, while in other embodiments, the relative positions are fixed. An exemplary aerodynamic element extends radially into the reverser flow to redirect the flow away from the door surface.

Abstract: A pair of laminated panels are simultaneously manufactured in a single panel press. A thermal band is stacked between two panel sets and then the two panel sets are simultaneously heated and compressed together in a common stack with the band, with the band being separately heated.

Abstract: The thrust reverser is used with an aircraft gas turbine engine and includes upper and lower doors pivotable between a stowed position and a deployed position. When deployed, the doors redirect a portion of the efflux to generate a nose-down pitching moment on an aircraft to improve handling during thrust reversing on a runway.

Abstract: A thrust reverser door is provided, in one configuration, with a plurality of peripherally-disposed frames circumferentially spaced apart from one another and projecting radially inwardly on an interior side of the door to thereby provide a channel for redirecting thrust.

Abstract: The thrust reverser includes, in one aspect, an interior flow deflector which defines a portion of a substantially continuous and uninterrupted nozzle interior surface with the interior of a jet pipe when the door is in a stowed position, thereby reducing aerodynamic losses and improving efficiency. In another aspect, improved sealing arrangement between the jet pipe and the door provides increased performance when the doors are stowed.

Abstract: The thrust reverser comprises a first reverser door and a second reverser door asymmetrically pivotable between a stowed position and a deployed position, one having a pivot axis closer to the central axis than the other.

Abstract: An erosion shield for an aircraft window includes an annular band having a radially outer brim and a radially inner clip. The shield is sized to cover a composite window frame having an outer rim and an inner sash around a central aperture in which is mounted a window pane. The clip is asymmetrical around the central aperture to protect the sash and permit assembly of the shield thereto.

Abstract: A label roll includes a web having front and back surfaces wound in a roll. The back surface includes adhesive patches aligned in a column along the running axis of the web. The front surface includes a release strip behind the column of patches and laminated thereto in successive layers in the roll.

Abstract: A slitting machine includes a stand for supporting a web which is slit into multiple ribbons by a plurality of blades, with the ribbons being wound on corresponding cores supported on an arbor. A common ink roller is mounted across the feedpath of the web and has a printing surface configured to print an end-of-roll warning stripe in a universal pattern bridging adjacent ribbons irrespective of individual width thereof.

Abstract: A postage sheet includes a face sheet adhesively bonded to a release liner. The face sheet includes a removable internet stamp having a diecut perimeter. A visible security indicium is disposed on the front side of the stamp and has a different color than the face sheet, and is not reproducible by photocopying.

Abstract: A thrust reverser includes reverser doors circumferentially spaced around a nacelle. An arcuate yoke is disposed coaxially around the nacelle. An actuator is mounted tangentially to the yoke for rotary movement thereof. Actuator rods join the doors to the yoke for simultaneous deployment of the doors as the yoke is rotated.

Abstract: A web is dispensed from a roll and includes first and second bands adjoining along a fold line. A pattern of release is applied to the front side of the web along the first band, and a pattern of adhesive is applied to the front side of the web along the second band. The web is folded along the fold line to bond together the first and second bands in a laminate, and exposing back sides of the bands on opposite sides of the laminate. The second band is cut to define a removable label therein.

Abstract: A stack of alternating sheets includes repeating diecuts offset among the sheets. The sheets may be made from a continuous web using a die to cut the repeating diecuts along the running axis of the web. Individual sheets are cut from the web and stacked with the diecuts offset from each other in turn. The stack of sheets may be loaded into a printer and fed individually therethrough, with the offset diecuts preventing interlocking therebetween.

Abstract: A thrust reverser includes reverser doors pivotally mounted in a nacelle. Each door includes a latch pin mounted at a distal end thereof. A complementary latch hook is pivotally mounted in the nacelle for engagement with the pin to latch closed the reverser door. A rotary retainer adjoins the hook for blocking rotation of the hook to latch closed the door, and selectively unblock rotation of the hook to permit the pin to disengage the hook.

Abstract: A turbofan nacelle includes forward and aft cowls adjoining at a joint, and including an exhaust duct having a main outlet for discharging exhaust. A variable nozzle surrounds the exhaust duct and includes a secondary outlet around the main outlet. A thrust reverser bridges the forward and aft cowls upstream from the variable nozzle. The variable nozzle is inductively powered and controlled across the closed joint, and is uncoupled inductively from the forward cowl when the joint is open.

Abstract: An exhaust nozzle includes an exhaust duct with an outlet and a row of radial apertures upstream therefrom. A radial frame surrounds the duct upstream from the apertures. A row of flaps are hinged to the frame to selectively cover and uncover the apertures for controlling exhaust flow discharged therethrough. An arcuate unison bar surrounds the duct adjacent to the frame and includes circumferentially spaced apart cam followers engaging corresponding cams affixed to the flaps. An actuator is joined to the bar for selective rotation thereof between opposite first and second directions to pivot open and closed the flaps atop the apertures.

Abstract: A pharmaceutical script includes a face sheet laminated to a liner by an adhesive therebetween. The face sheet includes a removable label defined by a perimeter diecut. The label includes an excisable tab spaced inboard from a surrounding rim. The tab includes a slit along one edge thereof. And, the label and tab are removable together from the liner to expose adhesive on the label rim, without adhesive being exposed on the tab.