Matches 1 - 50 out of 127 1 2 3 >


Match Document Document Title
US20140367520 ATTITUDE CONTROL OF AN AIRCRAFT IN A DITCHING CONDITION  
Configurations provide rapid adjustment to an aircraft attitude in the water upon an emergency water landing. In one configuration, an aircraft fuselage has a forward compartment that includes a...
US20130009010 SYSTEM FOR DRAINING WATER CONDENSATION IN AN AIRCRAFT  
The invention relates to an aircraft comprising: a drainage system for condensation water formed in the aircraft between an upper zone thereof where the condensation water is formed and a lower...
US20140291449 DEVICE FOR HEATING A PORTION OF A CABIN FLOOR IN AN AIRCRAFT CABIN  
The invention relates to an arrangement for heating a portion of the cabin floor in an aircraft cabin, wherein the cabin floor has an upper side which can be walked on and a lower side opposite...
US20150191256 CONTAINMENT SYSTEM AND INCREASED STRENGTH RADOME ASSEMBLY  
A containment system for containing all or part of a radome and an external subassembly that is protected by the radome is disclosed. One embodiment of the containment system comprises a fabric...
US20110284690 Utility Device System For Releasing Or Capturing Disbursements For The Atmosphere By Means Of An Aircraft  
An aircraft carrying oxygen, gases, and/or fluid advancement tanks is flown to heights greater than ground level and released out to the atmosphere, or gathered in tanks contained in the fuselage....
US20070295862 Modular Wall Construction System for Aircraft Cabins  
The individual room units presently used in aircraft, e.g. crew rest rooms, are usually fixed installations so that quick on-demand changeover of passenger seats to such a room unit may only be...
US20090166472 FLOOR PLATE FOR COVERING A FLOOR FRAMEWORK IN AN AIRCRAFT  
The invention relates to a floor plate for bearing upon a floor framework in an aircraft. The floor framework is formed with a multiplicity of transverse beams which are arranged like a truss, and...
US20140361120 Flight Vehicle Fairing Having Vibration-Damping Blankets  
Vibration-damping blankets are attached to the back surfaces of fairing panels of a flight vehicle (e.g., an aircraft or spacecraft) to reduce vibration, fatigue, structure and airborne...
US20120325966 Flight Vehicle Fairing Having Vibration-Damping Blankets  
Vibration-damping blankets are attached to the back surfaces of fairing panels of a flight vehicle (e.g., an aircraft or spacecraft) to reduce vibration, fatigue, structure and airborne...
US20080302913 CARGO FLOOR, SYSTEM, AND METHOD  
Embodiments provide a cargo floor, a system, and a method adapted to be made integral with or complementary of the aircraft fuselage. Cargo floor members may be adapted to be coupled with a flat...
US20140008494 TIE DOWN AND JACK FITTING ASSEMBLY FOR HELICOPTER  
The present invention is an assembly (100) for use as a jack contact point and a secure tie-down location for a helicopter. The assembly includes a hollow waffled dome element (110) having support...
US20140117159 Flexible Truss Frame and Method of Making the Same  
A composite frame includes a plurality of truss elements covered by a cap. The truss elements are flexibly coupled with each other and with the cap. The frame flexes to conform to a contoured...
US20130020438 Flexible Truss Frame and Method of Making the Same  
A composite frame includes a plurality of truss elements covered by a cap. The truss elements are flexibly coupled with each other and with the cap. The frame flexes to conform to a contoured...
US20150151826 STRATOSPHERIC BALLOON HAVING IMPROVED COMPRESSIVE STRENGTH  
A three-dimensional structural framework has a plurality of inflatable rings, each having a T-shaped cross-section along a plane passing through an axis of revolution of the inflatable ring in an...
US20090212161 AIRCRAFT GRAYWATER EJECTION SYSTEM  
An aircraft (10) having a cabin (14) with a plurality of potable-water-using stations (22) that drain graywater to a transfer tank (24). The graywater ejection system pressurizes the transfer tank...
US20120104178 CANTILEVERED DIFFERENTIAL MOTION SENSOR AND ASSOCIATED FRAME  
The disclosed sensor includes a frame having a base and a plurality of arms integral with the base. The arms are biased to a relaxed position, which may be an extended position. A fuse is fastened...
US20120251092 Articulated Sensor Support Structure  
Embodiments include an assembly comprising: (a) a camera support structure comprising: a masthead disposed on the distal end of a mast wherein the masthead is configured to receive an imaging...
US20090026318 Installation system for an airplane  
An exemplary embodiment of the present invention indicates an installation system for an airplane for securing interior equipment, which exhibits longitudinal and transverse rails. The transverse...
US20060145003 Storage device for emergency equipment  
A storage device (50) for emergency equipment (2, 17, 19) for aircraft flight crew. The storage device (50) is adapted so that the emergency equipment (2, 17, 19) in the stored position presents...
US20120223183 AEROSPACE ARTICLES MADE FROM QUASI-ISOTROPIC CHOPPED PREPREG  
Quasi-isotropic chopped prepreg is used to make parts found in aerospace vehicles. Exemplary aerospace parts that are made using quasi-isotropic chopped prepreg include aircraft window frames,...
US20110011975 Aerospace articles made from quasi-isotropic chopped prepreg  
Quasi-isotropic chopped prepreg is used to make parts found in aerospace vehicles. Exemplary aerospace parts that are made using quasi-isotropic chopped prepreg include aircraft window frames,...
US20150069183 Arrangement For Guiding A Cable Between A Wing And An Aerodynamic Body Movably Supported Relative Thereto; Wing Of An Aircraft Having Such An Arrangement And Aircraft Having Such A Wing  
An assembly for guiding a cable between a structural part of an aircraft and a movable aerodynamic body includes a chain of pivotally connected links, a first coil device arranged between each...
US20080173755 Floor panel for forming a loading area in a cargo hold of an aircraft  
Disclosed is a floor panel, in particular for covering floors of cargo holds of aircraft. The floor panel is formed by a plurality of milled profiles, which are friction stir welded in each case...
US20140048649 UTILIZATION FOR AIRCRAFT AIRSTAIR SPACE AND FUEL CELL SYSTEM INTEGRATION  
Embodiments of the present invention provide improved space utilization concepts for aircraft, and particularly to using under floor space created by the envelope designed to house an airstair...
US20060138280 Arrangement and method for utilizing the heat of waste air for heating the bilge area of aircraft  
The present application describes an arrangement and a method for utilizing the heat of waste air for heating the bilge area of aircraft, wherein the bilge area is connected to a heat transfer...
US20080116094 RECEPTACLE FOR FASTENERS AND AN ASSOCIATED INSTALLATION METHOD  
A receptacle for a fastener is provided that may be relatively light weight and compact, may reduce the number of parts required for mounting an object to a surface, and may allow for greater...
US20100073899 BULKHEAD MOUNT EQUIPMENT SHELF RACK TRAY  
A Line Replaceable Unit (LRU) support system incorporates a unitary tray having a rear boss and an integral Air Cooling System (ACS) plenum and an ACS conduit through the rear boss communicating...
US20050236515 Internal link for aircraft  
The present invention relates to an internal link for aircraft having at least a first pylon which is intended for a load and provided with signal cabling, intended for e.g. countermeasure pods,...
US20100044512 Drainage Device, Aircraft, and Method for Letting Out a Fluid that is Present Between the Exterior Skin and the Interior Lining of an Aircraft  
A drainage device for letting out a fluid that is present between the exterior skin and the interior lining of an aircraft, wherein the drainage device comprises a collecting vessel and an outlet...
US20150197345 OBJECT DEFLECTION DEVICE AND PROTECTION UNIT  
An object deflection unit comprising a deflection unit having an adapting plate and a top surface, a plurality of doubler units affixed to an aircraft frame, where the deflection unit is secured...
US20080173759 APPARATUS WITH AN EXPANDING BAND DRIVE, AND ITS USE IN AIRCRAFT CONSTRUCTION  
In the case of apparatuses which are intended in particular for aircraft construction and have a movement device for objects such as films, cloths, lids or the like, expanding band drives are in...
US20070138341 Transformable skin  
A transformable skin. The transformable skin includes a first mechanism for enabling a first type of deformation of the skin. A second mechanism resists a second type of deformation that is...
US20090283633 INFILL PANEL OF A SUPPLY ARRANGEMENT IN A PASSENGER CABIN  
A supply device in a passenger cabin, such as an aircraft passenger cabin, includes a first panel or “function panel” having one or more comfort elements, operating elements, visual display...
US20110221626 HOUSING FOR AIRCRAFT MOUNTED COMPONENTS  
A traffic collision avoidance system device is provided. The device includes a radome having an antenna contained therein. A chassis is bonded to the radome by a layer of bonding material about...
US20090050742 DEVICE FOR GENERATING AERODYNAMIC DISTURBANCES SO AS TO PROTECT THE OUTER SURFACE OF AN AIRCRAFT AGAINST ELEVATED TEMPERATURES  
An aircraft with an outer surface from which flows an aerodynamic stream of cold air and includes at least one hot gas outlet, characterized in that it includes at least one device (16) for...
US20110253840 METHOD FOR INSTALLING AN INERTIAL REFERENCE UNIT IN AN AIRCRAFT, AND AIRCRAFT EQUIPPED IN THIS WAY  
The invention relates to a method for installing an inertial reference unit in an aircraft, in which: a reference unit support (1) is fixed to a structural element of the aircraft; support...
US20080210822 Very high frequency line of sight winglet antenna  
A line of sight antenna supported in an upturned terminal winglet or similar vertical member of an aircraft is disclosed. An aperture is formed in the conductive winglet or vertical member, and...
US20080067818 BIFURCATED LATCHING SYSTEM  
A bifurcated latching system for securing together first and second portions of an aircraft, the bifurcated latching system comprising a pin latch assembly and a pawl latch assembly. The pin latch...
US20060043238 Modular design with built-in upgradeability for aerospace applications  
An improved line replaceable unit (LRU) of modular design for aerospace applications that has a plurality of removable LRU modules to enhance manufacturability, serviceability, interchangeability...
US20120292446 Vertical Laminate Noodle for High Capacity Pull-Off for a Composite Stringer  
An apparatus comprises a composite elongate member, a channel, and a number of composite structures. The composite elongate member has a side configured for attachment to a surface of a structure....
US20100320320 AEROPSPACE STRUCTURE INCLUDING COMPOSITE BEAM CHORD CLAMPED BETWEEN REINFORCEMENT PLATES  
A structure for an aerospace vehicle includes a composite beam chord clamped between first and second metal plates. The beam chord is clamped at a force that precludes or reduces beam chord...
US20100219295 RETRACTABLE SYSTEM FOR AERONAUTICAL SENSORS  
The invention discloses a retractable optical sensor (1) composed of an EO/IR (Electro-Optical/Infrared Remote) sensor (2) which is fastened to an articulated structure (3) that is actuated by an...
US20050284984 Visual display provided with secured electronic architecture  
The invention relates to a display device with a secured electronic architecture for aeronautical applications. Each device comprises an electronic computer and an associated matrix-type display...
US20070235588 Deceleration device  
A deceleration device adapted for gradual dissipation of kinetic energy comprises a spool reel carrying a belt being wound up on the spool reel; an elevating spindle being driven by the spool reel...
US20080197236 LIGHTWEIGHT COMPOSITE MATERIAL AND METAL THRUST RECOVERY FLAPPER VALVE  
The present invention provides a thrust recovery valve that is less expensive and lighter weight while maintaining required system safety. It utilizes valve doors made partially of plastic...
US20120298801 AIRCRAFT WING AND SENSOR  
An apparatus is disclosed which includes an aircraft wing and a sensing unit. The sensing unit includes: a blister on an underside of the aircraft wing; a first and second sensor, at least part of...
US20080142633 HELICOPTER REDUCED VIBRATION ISOLATOR AXIAL SUPPORT STRUT  
Helicopter reduced vibration axial support struts and aircraft suspension system are disclosed with at least one vibration controlling fluid containing strut. The powered struts include an outer...
US20100090062 DRILL-ELASTIC AND FLEXURALLY RIGID ROD ELEMENT FOR THE SUPPORT AND GUIDANCE OF A MOVABLE FLAP RELATIVE TO A WING OF AN AIRCRAFT  
A drill-elastic and flexurally rigid rod element (10) for supporting and guiding a movable flap (24) relatively to a wing (26) of an aircraft, wherein the rod element encompasses a cross-shaped...
US20090084889 Aircraft having a reduced acoustic signature  
An aircraft the propulsive units of which include engines, and which is distinguished by reduced noise emissions, includes a wing structure fixed to an upper region of the fuselage, and a vertical...
US20100012767 LIGHT MULTIPURPOSE AIRCRAFT  
A light multi-purpose aircraft comprises a fuselage (1); a wing (2); a fin assembly (3); a landing gear (4); a main power plant (5); an auxiliary power plant (7); pylons (10); outboard suspension...

Matches 1 - 50 out of 127 1 2 3 >