Abstract: An interior aircraft lighting assembly comprises: at least one infrared lighting device for emitting infrared light; at least one further lighting device for emitting visible light; a lighting assembly controller for controlling an operation of the at least one infrared lighting device and of the at least one further lighting device; a supplementary infrared lighting device controller; and a power supply network, which is configured for supplying electric power from the lighting assembly controller to the at least one further lighting device. The supplementary infrared lighting device controller is tapped into the power supply network. The lighting assembly controller is configured to provide an electric trigger pulse on the power supply network for activating the at least one infrared lighting device.

Abstract: An interior aircraft lighting assembly comprises: at least one infrared lighting device for emitting infrared light; at least one further lighting device for emitting visible light; a lighting assembly controller for controlling an operation of the at least one infrared lighting device and of the at least one further lighting device; a supplementary infrared lighting device controller; and a power supply network, which is configured for supplying electric power from the lighting assembly controller to the at least one further lighting device. The supplementary infrared lighting device controller is tapped into the power supply network. The lighting assembly controller is configured to provide an electric trigger pulse on the power supply network for activating the at least one infrared lighting device.

Abstract: An interior aircraft lighting assembly comprises: at least one infrared lighting device for emitting infrared light; at least one further lighting device for emitting visible light; a lighting assembly controller for controlling an operation of the at least one infrared lighting device and of the at least one further lighting device; a supplementary infrared lighting device controller; and a power supply network, which is configured for supplying electric power from the lighting assembly controller to the at least one further lighting device. The supplementary infrared lighting device controller is tapped into the power supply network. The lighting assembly controller is configured to provide an electric trigger pulse on the power supply network for activating the at least one infrared lighting device.

Abstract: The present invention relates to an adeno-associated virus (AAV), comprising an insertion of at least 6-8 amino acids between the positions corresponding to position 587 and 588 of SEQ ID NO: 1. Also envisioned are AAVs of the present invention for use as a medicament and pharmaceutical compositions comprising the AAV of the present invention. Further, the present invention relates to an in vitro use of AAV of the present invention for transduction of the nucleus of retinal cells. Also concerned is a method for screening an insertion sequence as well as a peptide obtainable by the method for screening. Also contemplated are kits comprising the AAV of the present invention.

Abstract: A protective cover for a fuselage-mounted exterior aircraft light includes a fuselage-facing mounting side for mounting the protective cover to an exterior aircraft light housing or to an exterior skin of an aircraft; a light transmissive forward facing light emission surface; and an air deflection zone, which is shaped to direct a portion of an impinging air stream (A) along and over the forward facing light emission surface for shielding the forward facing light emission surface from the impinging air stream (A).

Abstract: The present invention relates to an adeno-associated virus (AAV), comprising an insertion of at least 6-8 amino acids between the positions corresponding to position 587 and 588 of SEQ ID NO: 1. Also envisioned are AAVs of the present invention for use as a medicament and pharmaceutical compositions comprising the AAV of the present invention. Further, the present invention relates to an in vitro use of AAV of the present invention for transduction of the nucleus of retinal cells. Also concerned is a method for screening an insertion sequence as well as a peptide obtainable by the method for screening. Also contemplated are kits comprising the AAV of the present invention.

Abstract: A protective cover for a fuselage-mounted exterior aircraft light includes a fuselage-facing mounting side for mounting the protective cover to an exterior aircraft light housing or to an exterior skin of an aircraft; a light transmissive forward facing light emission surface; and an air deflection zone, which is shaped to direct a portion of an impinging air stream (A) along and over the forward facing light emission surface for shielding the forward facing light emission surface from the impinging air stream (A).

Abstract: An apparatus and a method for embossing micro- and/or nanostructures include the embossing of the micro- and/or nanostructures in an embossing material.

Abstract: An apparatus and a method for embossing micro- and/or nanostructures in an embossing material.

Abstract: A structure stamp has a flexible stamp which has a microstructured or nanostructured stamp surface for embossing of an embossing structure which corresponds to the stamp surface on an embossing surface, and a frame for clamping the stamp. Moreover, the invention relates to a device for embossing an embossing pattern on an embossing surface with the following features: a stamp receiver for accommodating and moving a structure stamp, an embossing material receiver for accommodating and placing an embossing material opposite the structure stamp, and an embossing element drive for moving an embossing element along the structure stamp.

Abstract: A structure stamp has a flexible stamp which has a microstructured or nanostructured stamp surface for embossing of an embossing structure which corresponds to the stamp surface on an embossing surface, and a frame for clamping the stamp. Moreover, the invention relates to a device for embossing an embossing pattern on an embossing surface with the following features: a stamp receiver for accommodating and moving a structure stamp, an embossing material receiver for accommodating and placing an embossing material opposite the structure stamp, and an embossing element drive for moving an embossing element along the structure stamp.

Abstract: A structure stamp has a flexible stamp which has a microstructured or nanostructured stamp surface for embossing of an embossing structure which corresponds to the stamp surface on an embossing surface, and a frame for clamping the stamp. Moreover, the invention relates to a device for embossing an embossing pattern on an embossing surface with the following features: a stamp receiver for accommodating and moving a structure stamp, an embossing material receiver for accommodating and placing an embossing material opposite the structure stamp, and an embossing element drive for moving an embossing element along the structure stamp.

Abstract: An apparatus and a method for embossing micro- and/or nanostructures in an embossing material.

Abstract: A structure stamp has a flexible stamp which has a microstructured or nanostructured stamp surface for embossing of an embossing structure which corresponds to the stamp surface on an embossing surface, and a frame for clamping the stamp. Moreover, the invention relates to a device for embossing an embossing pattern on an embossing surface with the following features: a stamp receiver for accommodating and moving a structure stamp, an embossing material receiver for accommodating and placing an embossing material opposite the structure stamp, and an embossing element drive for moving an embossing element along the structure stamp.

Abstract: A structure stamp with a flexible stamp which has a microstructured or nanostructured stamp surface for embossing of an embossing structure which corresponds to the stamp surface on an embossing surface, and a frame for clamping the stamp. Moreover, the invention relates to a device for embossing an embossing pattern on an embossing surface with the following features: a stamp receiver for accommodating and moving a structure stamp, an embossing material receiver for accommodating and placing an embossing material opposite the structure stamp, an embossing element drive for moving an embossing element along the structure stamp.

Abstract: A structure stamp with a flexible stamp which has a microstructured or nanostructured stamp surface for embossing of an embossing structure which corresponds to the stamp surface on an embossing surface, and a frame for clamping the stamp. Moreover, the invention relates to a device for embossing an embossing pattern on an embossing surface with the following features: a stamp receiver for accommodating and moving a structure stamp, an embossing material receiver for accommodating and placing an embossing material opposite the structure stamp, an embossing element drive for moving an embossing element along the structure stamp.

Abstract: An integrated aircraft landing and taxi light includes upper and lower reflector regions in the shape of substantially circular segments and a central longitudinal third reflector region extending between the upper and lower reflector regions. Landing light LEDs are arranged within the upper and lower reflector regions and the outer portions of the central longitudinal reflector region with the diagonals of the LED dies oriented substantially along radial lines extending outward from the center of the light. Taxi light LEDs are arranged within the central and outer portions of the central longitudinal reflector region such that the sides of the LED dies are oriented substantially horizontally and vertically with respect to the aircraft.

Abstract: The present invention relates to devices for efficient transport, transfer and movement of fluids. In particular, the invention provides fluidic micro-structures for controlled transport and movement of liquids in devices for analytical and other purposes. Devices of the invention include one or more features that can enhance performance of the fluid transfer, referred to as a pre-shooter stop, a butterfly structure, a cascade structure, a waste chamber inlet, a capillary driven sample inlet chamber, a capillary stop structure, a bifurcation flow-through structure, and a hydrophobic vent.

Abstract: The present invention relates to devices for efficient transport, transfer and movement of fluids. In particular, the invention provides fluidic micro-structures for controlled transport and movement of liquids in devices for analytical and other purposes. Devices of the invention include one or more features that can enhance performance of the fluid transfer, referred to as a pre-shooter stop, a butterfly structure, a cascade structure, a waste chamber inlet, a capillary driven sample inlet chamber, a capillary stop structure, a bifurcation flow-through structure, and a hydrophobic vent.

Abstract: The present invention relates to devices for efficient transport, transfer and movement of fluids. In particular, the invention provides fluidic micro-structures for controlled transport and movement of liquids in devices for analytical and other purposes. Devices of the invention include one or more features that can enhance performance of the fluid transfer, referred to as a pre-shooter stop, a butterfly structure, a cascade structure, a waste chamber inlet, a capillary driven sample inlet chamber, a capillary stop structure, a bifurcation flow-through structure, and a hydrophobic vent.