Patent application number | Description | Published |
20090230247 | METHODS AND APPARATUS FOR INCORPORATING LUMINOPHORES INTO DECORATIVE LAMINATES - A process for incorporating light emitting materials into aircraft interiors is described. The method includes selecting at least one light emitting material, incorporating the selected at least one light emitting material into one or more of a laminate coating and an extruded component, and installing the one or more of a laminate coating and extruded component into an aircraft cabin configuration. | 09-17-2009 |
20100285264 | Heat Resistance Using Titanium Dioxide Nanofibers - A composite structure includes a resin and a plurality of titanium dioxide fibers provided in the resin. | 11-11-2010 |
20110259086 | Leak Detection In Vacuum Bags - A device indicates the location of an air leak in a vacuum bag used to process composite parts. The device includes a layer of material on the inner face of the bag that changes in appearance due to an oxidation-reduction reaction in areas of the layer exposed to oxygen caused by a leak in the bag. | 10-27-2011 |
20120076992 | METHODS AND APPARATUS FOR INCORPORATING LUMINOPHORES INTO DECORATIVE LAMINATES - A process for incorporating light emitting materials into aircraft interiors is described. The method includes selecting at least one light emitting material, incorporating the selected at least one light emitting material into one or more of a laminate coating and an extruded component, and installing the one or more of a laminate coating and extruded component into an aircraft cabin configuration. | 03-29-2012 |
20130122244 | Aircraft Interior Panels and Methods of Panel Fabrication - A multifunctional fully integral panel system design, a unique material configuration, and a process for fabricating a net shape (or nearly net shape) panel in one production cycle. The panel may comprise a base facing with an outer perimeter, a decorative film applied to the exterior of the base facing, an aft facing having an outer perimeter fused to the base facing, and a reinforcement core disposed between the unfused portions of the base and aft facings, which reinforcement core also acts as acoustic insulation (i.e., a noise attenuator). Alternatively or additionally, a foam core or blanket having thermal and/or acoustic insulation properties is attached to the external surface of the aft facing. The fabrication process involves the application of different heat treatments to panel components having different forming temperature or rubbery/elastic plateaus. | 05-16-2013 |
20130133202 | Fire Resistance For Optically Transparent Thermoplastics - A fire retardant, transparent panel and method of making the panel, that is especially well suited for use on mobile platforms, and particularly on aircrafts. The panel is a composite of a transparent matrix and a plurality of fire-retardant nanoparticles. The nanoparticles have a diameter less than the visible spectrum of light, and in one form between about 0.1 nm to about 400 nm in diameter. The nanoparticles may be arranged randomly or in predetermined patterns within the matrix during manufacturing of the panel. The panel is lightweight, transparent and yet highly fire retardant. | 05-30-2013 |
20130295809 | HEAT RESISTANCE USING TITANIUM DIOXIDE NANOFIBERS - A composite structure includes a resin and a plurality of titanium dioxide fibers provided in the resin. | 11-07-2013 |
20140199768 | LEAK DETECTION IN VACUUM BAGS - A device indicates the location of an air leak in a vacuum bag used to process composite parts. The device includes a layer of material on the inner face of the bag that changes in appearance due to an oxidation-reduction reaction in areas of the layer exposed to oxygen caused by a leak in the bag. | 07-17-2014 |
20140262358 | Fire Seal End Cap and Associated Multi-member Assembly and Method - A multi-member assembly including a first structural member, a second structural member opposed from the first structural member, a crossover seal positioned between the first and second structural members, wherein the crossover seal defines a bore, and an end cap including a cap portion and a plug portion protruding from the cap portion, wherein the plug portion is at least partially received in the bore such that the cap portion bridges the first and second structural members. | 09-18-2014 |
20150068691 | MULTILAYER AIRCRAFT SHADE MATERIAL - In one aspect, a multilayer material comprises a first layer formed from a thermoplastic elastomeric material, a second layer formed from a fabric and secured to a first side of the first layer, and a third layer formed from a fabric secured to a second side of the first layer. The multilayer material may be incorporated into a window shade for use in a vehicle, e.g., an aircraft or the like. | 03-12-2015 |