Match Document Document Title
7635105 Ejection device, ejectable hatch and aircraft having at least one ejectable hatch  
An ejection device for an aircraft hatch having at least one articulation hinge. The articulation hinge is provided with a lower element designed to be mounted in rotation on structure of the...
7631837 Electrical interlock and indication system for aircraft  
An electrical interlock and indication system for use with an aircraft having a hinged tail section is provided. The interlock and indication system prevents operation of a latch/lock actuation...
7621482 Weight optimized pressurizable aircraft fuselage structures having near elliptical cross sections  
An aircraft fuselage includes a tubular shell having a centerline axis, opposite ends, and a cross-section having a radius R(φ), where φ is the angular coordinate of a cylindrical coordinate...
7607614 Transition shim between structure for fastening a wing to a fuselage of an aircraft, and aircraft having such a shim  
A shim adapted for positioning on the upper surface of at least one wing of an aircraft. The shim restores an aerodynamic profile of the wing at the position of a zone of transition between...
7581697 Design methods and configurations for supersonic aircraft  
Methods for configuring aircraft that may be implemented to integrate aircraft sonic boom constraint requirements with the design process for a supersonic aircraft, for example, to reconcile a...
7581699 Stealth attack fighter bomber  
A fighter bomber aircraft having a rhomboid airframe with a dihedral bottom surface and a top surface designed as an airfoil. The rhomboid cross-sectional configuration gives it increased lift,...
7578473 Rib for aircraft wing and methods for the manufacture thereof  
There is provided a method of manufacturing a rib for an aircraft wing, the method comprising providing a billet of material for forming the rib, machining away material from all sides of the...
7578468 Acoustic absorption system for an aircraft airframe  
An airframe includes a mass barrier layer mounted to a multitude of frame members and adjacent to each of a multitude of foam portions to provide a contiguous layer to seal the foam portions...
7562845 Rudder unit connection to a fuselage without a bolt-fairing structure  
The connection of a rudder unit on the fuselage of an aircraft frequently leads to an inhomogeneous flow of forces in the connecting region between the rudder unit and the fuselage or even to an...
7556220 Seal for sealing a component opening in a component  
A seal for sealing component openings in components of a means of transport, in particular for sealing openings in aircraft airfoils and tail units, comprising an inner cover connected to an outer...
7552896 Aircraft window assembly  
A window assembly is provided to prevent the migration of the window seal. The window assembly includes an outer window pane, an inner window pane and a seal. The outer window pane having a...
7547865 Optical element mount and method thereof for a gun-launched projectile  
An optical element mount is effective in high G environments to protect brittle optical elements in which tensile stresses are generated on surface S2 without degrading optical performance. A...
7530530 Assembly for securing a stringer to a substrate  
Embodiments of an assembly for securing a stringer to a substrate are provided. The stringer assembly includes a stringer and a mandrel positioned within a channel defined in the stringer. A...
7530531 Apparatus and methods for installing an aircraft window panel  
A method of installing a window panel in an aircraft. The method includes connecting upper and lower ends of the window panel with upper and lower longerons of the aircraft, and connecting a side...
7527222 Composite barrel sections for aircraft fuselages and other structures, and methods and systems for manufacturing such barrel sections  
Composite sections for aircraft fuselages and methods and systems for manufacturing such sections are disclosed herein. A composite section configured in accordance with one embodiment of the...
7503524 Device for equipping a hole in a panel, and panel thus equipped  
A removable plate and a flange that occupies a hole in a panel. The flange has the particular feature of taking up compressive force to which the panel is subjected in its plane, perpendicularly...
7494092 Lightweight structural component in particular for aircraft and method for its production  
Lightweight structural component including at least one panel and at least one stiffening element oriented one of lengthwise and crosswise. The at least one stiffening element includes two side...
7481398 Intercostal for aircraft  
An intercostal for an aircraft for dissipating a load from a first frame onto a second frame and/or a skin of the aircraft, the intercostal having a framework.
7478780 Methods for manufacturing composite aircraft, parts and a family of composite aircraft  
The invention relates to systems and methods for manufacturing composite parts for aircraft. In one innovative aspect, a system and method for adjusting a location of a center of gravity of an...
7475850 Cockpit floor for aircraft  
The invention relates to an cockpit floor (4) for an aircraft comprising a plurality of spars (14) extending along a longitudinal direction (X) of the aircraft and a plurality of cross-beams (16)...
7461816 Internal arrangement of the walls of the fuselage of an aircraft  
An internal arrangement of aircraft fuselage walls supports two longitudinal auxiliary passage ducts at the upper part of the fuselage and on each side of its longitudinal plane of symmetry. The...
7429019 Auxiliary nose undercarriage, a force-transmission structure, and a rotary wing aircraft  
A steerable auxiliary nose undercarriage (2) for a rotary wing aircraft (1); the undercarriage (2) being retractable substantially rearwards. In the undercarriage (2), an oscillating system (13)...
7423245 Nose cover  
A nose cover (10) for a dome (12) through which radiation can pass, for a missile, the nose cover having an outer structure (22) through which radiation can pass and which is aerodynamically...
7416157 Apparatus and methods of attaching panels to support structures  
Apparatus and methods for attaching wall panels to support structures are disclosed. In one embodiment, an apparatus includes a first member and a second member. The first member is coupled to the...
7413140 Rotary wing aircraft with undercarriage structure  
A rotary wing aircraft (1) such as a helicopter comprises a force-transmission structure (5) for transmitting forces, in particular those coming from an undercarriage (2), and that, in...
7410126 Tunable acoustic absorption system for an aircraft cabin  
A tunable acoustic absorption system according to the present invention includes an airframe batting area; a primary soundproofing blanket area; an interior trim panel area; and a hard trim area,...
7407135 Aircraft provided with a belly fairing, and corresponding belly fairing  
In an aircraft comprising a fuselage and a belly fairing, the fairing is made of two independent parts. For example, a first part of the fairing comprises a front section, a central section and a...
7395989 Aircraft fuselage and corresponding aircraft  
An aircraft fuselage includes an outer skin and at least one main deck separating an interior space of the aircraft fuselage longitudinally into a first space and a second space. At least one...
7344108 Landing assist apparatus interface bulkhead and method of installation  
An aircraft landing assist apparatus is designed to be retrofit to existing aircraft having internal constructions that have been modified to support the apparatus. The apparatus is designed so...
7325771 Splice joints for composite aircraft fuselages and other structures  
Structures and methods for joining composite fuselage sections and other panel assemblies together are disclosed herein. In one embodiment, a shell structure configured in accordance with the...
7316372 Fuselage spar for aircraft and central sparbox provided with such a spar  
A fuselage spar for aircraft is vertically mounted between an upper surface panel and a lower surface panel of the fuselage at the junction between a first wing structure spar and a second wing...
7311287 Methods for incorporating area ruled surfaces in a supersonic aircraft  
A vertical stabilizer is configured to minimize the rate of change of cross-sectional area distribution of the vehicle or device to which the vertical stabilizer is mounted. One or more “waisted”...
7300693 Resin infused transparent skin panel and method of making same  
A transparent skin panel for use in a mobile platform having a plurality of metal sheets. A fiber reinforced resin at least partially surrounds the plurality of metal sheets. The fiber reinforced...
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...
7246772 Acoustic absorption system for an aircraft interior trim panel system  
An acoustic absorption trim panel includes a composite core, a decoupler layer, and a mass barrier layer. By ensuring that the mass barrier layer remains limp in a limp area but in contact with...
7240878 High wing monoplane aerospace plane based fighter  
The Hypersonic Orbital Fighter and the methods of flying it are disclosed. The Hypersonic Orbital Fighter is characterized by a winged, modified lifting body shape with the forward ventral section...
7237750 Autonomous, back-packable computer-controlled breakaway unmanned aerial vehicle (UAV)  
A modular unmanned aerial vehicle (UAV) having a fuselage, a nose cone, a left wing piece, a right wing piece, and a tail section. The tail section and nose cone each join to the fuselage through...
7228611 Method of transferring large uncured composite laminates  
A method of transferring an uncured composite laminate skin from a lay-up surface of a male mandrel tool to a female cure tool includes defining multiple vacuum zones on the lay-up surface, each...
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...
7198224 Energy absorbing airframe for a vertical lift vehicle  
An airframe includes an energy absorbing structure with a frame, a beam mounted to the frame at a rotational joint and a collapsible member. In response to reaching a predetermined threshold load...
7191982 Floor for aircraft  
The invention relates to an aircraft floor (4), preferably a cockpit floor, this floor comprising a plurality of spars (14) running along a longitudinal direction (X) of the aircraft and a...
7182291 Integrated aircraft structural floor  
A number of integrated floor structures made of lightweight composite materials for use in an aircraft are disclosed. Generally, each of such floors includes a top-layer skin, a bottom-layer skin...
7159822 Structural panels for use in aircraft fuselages and other structures  
Structural panels for use in manufacturing aircraft fuselages and other structures are disclosed herein. In one embodiment, a structural panel configured in accordance with the invention includes...
7134629 Structural panels for use in aircraft fuselages and other structures  
Structural panels for use in manufacturing aircraft fuselages and other structures are disclosed herein. In one embodiment, a structural panel configured in accordance with the invention includes...
7124982 Device for bracing a shell in an aircraft fuselage  
A device for bracing a shell surface in an aircraft fuselage against deformations and consisting of a continuous profile that is arranged so as, after conformation, to be mounted against the shell...
7121512 Drain particularly for engine support strut  
A drain, for example for an aircraft engine support strut, arranged on the trailing edge of the rear secondary structure of the strut. The drain includes a conduit with a substantially horizontal...
7118069 Integrated window belt system for aircraft cabins  
A system and a method is provided for fitting an aircraft cabin with modular sidewall panels, window reveals, and foam insulation blocks in an integrated manner. The system comprises a sidewall...
7108227 Insulation package and use thereof  
An insulation package to reduce the transmission of heat and/or noise between the outer skin and the cabin lining of an aircraft composed of an insulating material enclosed by an encapsulating...
7093799 Guided missile having a jettisoned protective cap  
A guided missile having a longitudinally extending airframe with a tip, a seeker head arranged in the tip and a window located in front of the seeker head for closing the airframe at the tip so as...
7087317 Composite laminated aluminum-glass fiber sandwich panels  
A Glare type composite laminated sandwich panel comprising (i) aluminum (ii) glass fibre with adhesive (iii) aluminum is disclosed. According to the present invention, at least one of the aluminum...