| Patent application number | Description | Published |
|---|
| 20090008502 | Aircraft Fuselage Interior - An aircraft fuselage interior comprises a side wall that extends in a direction along the length of the fuselage and includes an upper section that slopes inwardly. In one embodiment, the side wall comprises a multiplicity of visible elongate features, such as sloping lines, arranged along the length of the side wall. Each elongate feature extends from a lower portion to an upper portion and slopes relative to a notional line defined by the intersection of the interior surface of the side wall and a plane whose normal axis is parallel to the length of the fuselage. When viewed by a seated passenger, the sloping elongate features may cause the side wall to appear to have a degree of inward sloping less than the actual degree of inward sloping. The fuselage interior may therefore appear larger than it is. | 01-08-2009 |
| 20090076668 | Method and apparatus for providing power in an aircraft to one or more aircraft systems - A method and apparatus is disclosed in which an aircraft system such as the landing gear system or braking system is operated at least partially under power provided by a generator driven by the wheels of the landing gear. | 03-19-2009 |
| 20090121077 | Method and apparatus for operating an aircraft landing system - A method and apparatus is disclosed in which an aircraft landing system is at least partly primarily powered by power provided by a ram air turbine (RAT). | 05-14-2009 |
| 20090308975 | APPARATUS FOR PROVIDING VARIABLE THERMAL INSULATION FOR AN AIRCRAFT - Apparatus is disclosed for providing variable thermal insulation for an aircraft. | 12-17-2009 |
| 20100155531 | AIRCRAFT TOILET FACILITY - The invention relates to an aircraft toilet facility, particularly an aircraft toilet facility on a single passenger-deck aircraft. The invention provides a first toilet unit ( | 06-24-2010 |
| 20110049173 | AIRCRAFT FUEL TANK SYSTEM - An aircraft fuel tank system is disclosed in which a vent tank is provided with a compact vent pipe comprising one or more built-in flame barrier elements providing high liquid fuel outflow rate. | 03-03-2011 |
| 20110056970 | AIRCRAFT FUEL TANK SYSTEM - An aircraft fuel tank system is disclosed in which a vent tank is provided with an ullage vent for use in combination with an eternal flamer barrier means during a refuelling process. | 03-10-2011 |
| 20110056971 | AIRCRAFT FUEL TANK SYSTEM - An aircraft fuel tank system is disclosed in which a vent tank is provided with an additional ullage vent for use, in combination with an eternal flame barrier means, when refuelling. | 03-10-2011 |
| 20110056972 | AIRCRAFT FUEL TANK SYSTEM - An aircraft fuel tank system is disclosed in which a vent tank is provided with an ullage vent for use in combination with an eternal flamer barrier means during a refuelling process. | 03-10-2011 |
| 20110056973 | VENT PIPE FOR AN AIRCRAFT FUEL SYSTEM VENT TANK - A vent pipe is disclosed for use in the vent tank of an aircraft fuel system. The vent pipe is arranged with guide vanes or corner cascades for assisting the flow of fluid around the corners. | 03-10-2011 |
| 20110056974 | AIRCRAFT FUEL TANK SYSTEM - An aircraft fuel tank system is disclosed in which a vent tank is provided with an additional ullage vent for use, in combination with an eternal flamer barrier means, when refuelling. | 03-10-2011 |
