Did You Know...
...Chester Carlson was a patent agent who tired of having to make multiple copies of patent applications using the only duplication method available at the time: carbon paper. In 1959 he came up with a new copying system and took it to IBM for evaluation. The "experts" at IBM determined potential sales to be only 5,000 units because people wouldn't want to use a bulky machine when they had carbon paper. Carlson's invention was the xerography process, the company founded on the system is Xerox.
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| Number | Title | Issue Date |
| 8181422 | Energy-absorbing structural composite element A structural, energy absorbing composite element for aircraft structures includes a metallic or nonmetallic skin shell with a porous filler material insert positioned within the skin shell. The porous filler material is a material having ligaments that collapse resu... | 05/22/2012 |
| 7938365 | Line holder in an aircraft The invention relates to a holder module for affixing lines of various thicknesses in an aircraft, as well as to a holder system comprising two of the above-mentioned holder modules. Furthermore, the invention relates to a method that makes it possible to lead lines... | 05/10/2011 |
| 7883057 | Pivoting device and method for ceiling panels In one embodiment, a device for hanging a ceiling panel may include a clevis for attachment to a support structure, and a hinge for attachment to the ceiling panel. The clevis may include a pin and a first locking member. The hinge may include an elongated slot and ... | 02/08/2011 |
| 7784737 | Drag reduction fairing A vehicle including a body having an exterior surface and a protrusion extending outward from the surface. The vehicle further includes a fairing mounted on the surface directly adjacent and behind the protrusion. The fairing has a forward end, an aft end opposite t... | 08/31/2010 |
| 7708226 | Device for detecting synchronous errors of high-lift surfaces on aircraft A device for detecting synchronous errors of high-lift surfaces such as landing flaps or slats on aircraft, having an optical conductor which is laid over at least two adjacent high-lift surfaces, a light source and an optical receiver which are allocated to differe... | 05/04/2010 |
| 7690598 | Aircraft exhaust vent assembly An aircraft exhaust vent assembly for venting an exhaust gas through a window opening formed in an airplane fuselage. The aircraft exhaust vent assembly has an enclosure connected to the airplane fuselage and at least partially disposed within the window opening. An... | 04/06/2010 |
| 7686250 | Electronic display mount The invention is a mount for an electronic display device. The mount comprises a mount member that has a top face and a bottom face. Portions of the mount member are configured to engage portions of a mounting surface within the cockpit of an airplane. The mount als... | 03/30/2010 |
| 7681836 | Aircraft comprising a device for detection and/or measurement of atmospheric disturbances The invention relates to an aircraft comprising a device, for example an optical device, for detection and/or measurement of atmospheric disturbances in the path of the aircraft. This measurement device is placed in the pressurized zone between the aircraft nose and... | 03/23/2010 |
| 7422177 | Sealing device for a flap track in a belly fairing of an aircraft for a flap-actuating shaft Sealing device for the flap track for the flap-actuating shaft, in the belly fairing of an aircraft, with a top hollow body 1 and a bottom hollow body 7 which are flexibly compressible, each comprising at least one interior chamber 2, 8 with ope... | 09/09/2008 |
| 7422178 | Non-threaded structural insert for component attachment The present invention provides a non-threaded insert operable to transfer or couple a mechanical load to a structure. This non-threaded insert includes an upper insert having a noncircular cross section and a lower insert. The coupled upper and lower insert are rece... | 09/09/2008 |
| 7407136 | Static port skin applique apparatus and method A surface-mounted fuselage skin appliqué panel having an aperture to a reference static air input port is rugged, replaceable, and independently calibratable. The static port skin appliqué generally conforms to the fuselage surface, and is held in place either wit... | 08/05/2008 |
| 7387276 | Aerial sensor pod deployment system A roll-on/roll-off, aircraft-borne sensor pod deployment system having an operator station and a sensor pallet system and method of using same. The operator station has a base platform, a shelter box mounted on the base platform for accommodating a human operator, a... | 06/17/2008 |
| 7374132 | Insulation product and system suitable for use in an aircraft An acoustical and thermal insulation product suitable for use in an aircraft is provided, comprising an insulation layer formed from a sheet of insulation material, wherein the sheet of insulation material is arranged to form a series of undulations defining a serie... | 05/20/2008 |
| 7370831 | Power strip for seats A system for distributing signals between a first seat and a second seat of a platform. The system generally includes an elongated bus and a connector operable to provide a connection between the bus and the passenger seats. Signals can be transmitted between the bu... | 05/13/2008 |
| 7367527 | Reinforced insulation product and system suitable for use in an aircraft An acoustical and thermal insulation product suitable for use in an aircraft is provided, comprising: an insulation layer formed from a sheet of insulation material, wherein the sheet of insulation material is arranged to form a series of undulations defining a seri... | 05/06/2008 |
| 7360788 | Inflator and airbag apparatus An inflator is a hybrid inflator constructed by coupling a tank charged with a pressurized gas and a gas generator containing a gas-generating chemical. A coupling mechanism is provided in each of the tank and the gas generator, and the tank and the gas generator ar... | 04/22/2008 |
| 7350753 | RF shielding for aircraft windows Disclosed is an improved aircraft window having RF shielding. In one embodiment, a window shield comprises an electrically conductive, transparent, flexible film, which is applied by known processes to a window pane. This shield is grounded to the aircraft frame or ... | 04/01/2008 |
| 7350752 | Fairing and installation methodology for sensor pressure belts A fairing system developed to reduce the flow disturbance around sensor elements allowing accurate measurement of the pressure distribution on an airplane exterior surface. The fairing also protects the sensors and electronics of the pressure belt from direct exposu... | 04/01/2008 |
| 7338013 | Floor for aircraft This invention relates to a floor (4) for an aircraft, and preferably a cockpit floor, this floor comprising a plurality of spars (14) running along a longitudinal direction (X) of the aircraft and a plurality of cross-beams (16) assembled to th... | 03/04/2008 |
| 7334759 | Airplane surface protection film kits Described herein is a computer design-aided shield for exposed surfaces on aircraft, a method for manufacture, and kits derived from collections of shields, each kit appropriate for use on a single aircraft type. The shield is contemplated for first use on general a... | 02/26/2008 |
| 7327283 | System and apparatus for flight deck module integration An integrated communication system in an aircraft is provided. The system includes a plurality of solid state flight deck modules in an integrated flight deck panel, wherein the solid state flight deck modules include a microcontroller for interfacing with at least ... | 02/05/2008 |
| 7324747 | Aircraft fuselage element and method of taking a number of pictures An aircraft fuselage element (26) with a fuselage body (30) which forms an internal cavity (40) and which includes a viewing window (32, 34). To provide for taking substantially distortion-free high-resolution pictures in the infrared wav... | 01/29/2008 |
| 7317916 | Stratospheric-based communication system for mobile users using additional phased array elements for interference rejection A communication system has a stratospheric platform with a payload controller and a phased array antenna having a plurality of main array elements for generating a plurality of communication beams and a plurality of auxiliary elements for canceling interference betw... | 01/08/2008 |
| 7313888 | Device for and method of preventing rattling of door window glass for vehicles A device for preventing rattling of a door window glass for vehicles. In an activated condition, i.e. upon the upward and downward movement of the window glass, smoother upward and downward movement of the window glass is enabled, thereby eliminating noise due to fr... | 01/01/2008 |
| 7285753 | Heating system for use in on-board kitchens in means of transport and a method for heating food on board means of transport, in particular aircraft For use on board a mobile means of transport (eg. aircraft, bus, ship), a heating system and method are described which lead to a reduction of peak demand in the on-board kitchen energy supply system relating to the integrated heating appliances for the warming or h... | 10/23/2007 |
| 7281686 | Window assembly for aircraft fuselage A window assembly for an aircraft fuselage comprises an exterior transparent panel and an interior transparent panel positioned in an opening of the fuselage. At least one of the transparent panels may be relatively lightweight and the exterior transparent panel may... | 10/16/2007 |
| 7278608 | Reinforced insulation product and system suitable for use in an aircraft An acoustical and thermal insulation product suitable for use in an aircraft is provided, comprising: an insulation layer formed from at least one sheet of insulation material, and a plurality of elongated reinforcing members for reinforcing the insulation product, ... | 10/09/2007 |
| 7275710 | Aircrew restraint system A mobile aircrew restraint system includes a track system and a trolley which runs along the track and carries a retractor which releases a webbing strap attached to a harness. The track is preferably an extruded or sectioned track which follows contours of an aircr... | 10/02/2007 |
| 7275716 | Aircraft cabin module An aircraft cabin module of an elongated rectangular shape and that includes two large walls connected by two small walls, a service module arranged along a wall separating the module from an aisle, a door mounted in an opening implemented in a small wall, and at le... | 10/02/2007 |
| 7262957 | Modular communication fixture for installation on board of a passenger conveyance A modular communication fixture is installed in a passenger aircraft adjacent to an entrance and exit area adjoining a passenger boarding door. The fixture includes a housing, at least one access door that is selectively movable to an open position and a closed posi... | 08/28/2007 |
| 7261256 | Variable-duct support assembly One advantageous embodiment of the present invention is a variable-duct support assembly (14) for mounting one or more ducts (12a-12c) thereon. This variable-duct support assembly (14) includes one or more rails (18) ... | 08/28/2007 |
| 7258304 | Cushioned grounding clamp The present invention is directed toward clamping apparatus and methods for holding an item to an electrically conductive structure. In one embodiment, the clamp includes a strap, a fastener, a cushion, and a conductive material. The strap provides the structural st... | 08/21/2007 |
| 7258347 | Discrete active seal assemblies Active seal assemblies employing active materials that can be controlled and remotely changed to alter the seal effectiveness, wherein the active seal assemblies actively change modulus properties such as stiffness, shape orientation, and the like. In this manner, i... | 08/21/2007 |
| 7255376 | Pressure sensing dead bolt An apparatus, system and method including a latching device for displaceably retaining a panel relative to a frame. The latching device includes at least a bolt which is carried on the latching device and is operatively associated with the panel to prevent disengage... | 08/14/2007 |
| 7243881 | Multi-function trailing edge devices and associated methods Trailing edge devices configured to carry out multiple functions, and associated methods of use and manufacture are disclosed. An external fluid flow body (e.g., an airfoil) configured in accordance with an embodiment of the invention includes a first portion and a ... | 07/17/2007 |
| 7229046 | Servo mounting system for direct drive of an aircraft control surface This invention is a servo mounting system, which allows a servo with a rotating output shaft to directly power an aircraft control surface. A specially designed servo mount securely positions the servo with the central axis of its rotational output shaft on, and axi... | 06/12/2007 |
| 7222820 | Aircraft lavatory A lavatory complex for an aircraft. The lavatory complex includes a male lavatory facility and a female lavatory facility. The male lavatory facility includes stall units and may include urinals. The female lavatory facility includes stall units. Each stall unit sui... | 05/29/2007 |
| 7213409 | Reconfigurable hydrogen transfer heating/cooling system A reconfigurable system is provided for effecting temperature changes. A first thermally-conductive container stores a metal hydride while a second thermally-conductive container stores a metal alloy that is capable of absorbing hydrogen atoms at a pressure that is ... | 05/08/2007 |
| 7210655 | Reconfigurable interior sidewall A reconfigurable interior sidewall system includes one or more simply curved sidewall panels, each curved around the fuselage but longitudinally linear and providing a consistent mating surface for monuments. Panel openings are provided in each panel so that inner w... | 05/01/2007 |
| 7207524 | Device for warning of differential pressure during the opening of a pressurized closing device pertaining to an opening in the fuselage of an aeroplane An apparatus warns of differential pressure during the opening of a pressure-loaded door that closes an opening in an aircraft fuselage. An air guide passage extends from the side with higher pressure to the side with lower pressure. The air guide passage is closeab... | 04/24/2007 |
