Match Document Document Title
8205832 Floor structure for a fuselage  
The present invention provides a floor structure for a fuselage comprising a plurality of cross beams to which respectively at least one first strut and at least one second strut are associated...
8205824 Aircraft fuselage structure  
An aircraft fuselage structure is described for a flying-wing aircraft, having a central area of slight curvature and side areas of greater curvature, which forms a pressure body and has an outer...
8186621 Assembly between a front fitting and the traction coupling of the two lateral boxes of the horizontal stabilizer of an aircraft  
The invention relates to an assembly between a front fitting and the traction coupling of the two lateral boxes of the horizontal stabilizer of an aircraft comprising a front fitting (1, 1a and...
8181909 Pressure bulkhead for aircraft  
A pressure bulkhead assembly adapted for installation in an aircraft fuselage includes a bulkhead web and a reinforcing structure. The bulkhead web has a first side facing the pressurized...
8181421 Edge-wrapped panel and methods for edge-wrapping a panel  
An edge-wrapped panel and methods for edge-wrapping a panel. The panel comprises a substrate layer, a laminate layer, and at least one retainer. The laminate wraps around the substrate first edge...
8177166 Tail structure for an aircraft or spacecraft  
A tail structure for an aircraft or spacecraft, which adjoins a fuselage section of the aircraft or spacecraft, includes a support construction for supporting at least one craft component, and a...
8177167 Central section of aircraft with ventral or belly fairing capable of movement  
An aircraft center section includes a center part of an aircraft fuselage, a wing section, a center wing box installed at least partly in the fuselage and providing a junction between the wing...
8172181 Fuel range for an aircraft  
An apparatus and method for improving the fuel range of an aircraft are provided. The aircraft includes a fuselage with a front windshield, and an external skin providing a top cover for a cockpit...
8157212 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...
8146860 Aircraft fuselage with circular-arc-shaped exterior contour  
A fuselage section comprises an interior that forms a passenger cabin. In horizontal projection the fuselage section is geometrically defined by a first exterior skin region and a second exterior...
8142873 Rod for supporting components in a fuselage cell structure of an aircraft  
A rod for supporting components in a fuselage cell structure, in particular produced with fibre-reinforced composite materials, of an aircraft, in particular for supporting at least one floor...
8128029 Ventral fairing for an aircraft  
Ventral fairing for an aircraft provided between a left wing and a right wing, which comprises a lower central section of convex transverse cross-section located between the left lower surface of...
8127889 Noise reduction system for structures  
A method and apparatus are present for reducing noise. The apparatus comprises a core and a face sheet. The core is configured to reduce a speed of shear waves traveling through the core. The face...
8128028 Internally stiffened composite panels and methods for their manufacture  
Internally stiffened composite panels and associated manufacturing methods. An internally stiffened composite panel can include a first face sheet, a second face sheet offset from the first face...
8128030 Line system for an aircraft  
A line system for an aircraft, in particular an airplane, having multiple assemblies, in particular multiple fuselage sections of a fuselage cell and multiple wing shells, the line system...
8123166 Primary structure for aircraft of composite material with improved crash resistance and associated energy-absorbing structural element  
The disclosed embodiments relate essentially to a primary structure of an aircraft fuselage that has at least a first strut linked at one end to a crossbeam and at the other end to a reinforcing...
8124182 Application of insulating coating  
Systems and methods for discontinuously applying an insulating primer to a carbon fiber reinforced plastic (CFRP) component are disclosed. In one embodiment, a method for mitigating electrical...
8118259 Storage compartment for the nose gear of an aircraft  
A front landing gear storage compartment for an airplane, which includes a set of retractable landing gears including a front gear centered on a longitudinal median plane of the fuselage. The...
8118258 Separation element for attenuating the propagation of light in an aircraft  
The invention relates to a separation element for separating a first space from a second space in an aircraft. The separation element can be affixed between a ceiling region of the cabin, a...
8104715 Window arrangement for installing larger aircraft windows  
A window arrangement is provided for enlarging a window area in an aircraft. The window arrangement includes, but is not limited to at least one first installation element. The at least one first...
8104712 Aircraft fuselage element  
An aircraft fuselage element includes an outer shell and an inner shell that is disposed with clearance relative to the outer shell. An intermediate space between the outer shell and the inner...
8100360 Light rail system for powered introduction of large loads in a structure  
A device for securing installed equipment in an airplane, with one or more oblong attachment rails, one or more attachment means for securing the attachment rails to an airframe structure, and one...
8100361 Hull structure  
A hull structure is provided, for use in particular in an aircraft or spacecraft, the hull structure including an outer skin and structural components which are connected to said skin, as well as...
8100362 Cockpit and aircraft including such cockpit  
A cockpit and an aircraft including such cockpit. The cockpit includes a front section of an aircraft. Such cockpit includes a pressure bulkhead sealing the section and a pressurization system for...
8096503 Structuring construction for an aircraft fuselage  
A structuring construction for an aircraft fuselage is provided having an outer skin as well as a plurality of formers extending at a spacing side by side crosswise to the longitudinal direction...
8096504 Integrated aircraft structure in composite material  
Integrated aircraft structure in composite material that comprises a skin and stringers (1), with the skin comprising a string part (5) and a basic skin (3), which structure further comprises...
8087614 Stringer for an aircraft wing and a method of forming thereof  
The present invention relates to a stringer for an aircraft wing and a method of forming such a stringer in which the stringer is formed form a single piece of material and has differential...
8083182 Monolithic self-stiffened panels  
A composite panel having a first skin forming the outer wall of the panel, known as the lower face (1), and a second skin forming part of the inner wall of the panel. The second skin is formed...
8083175 Loading fitting having intersecting holes in the web side and end  
In one embodiment, a loading fitting includes at least one of an I, a T, and a J shaped cross-section having a flange attached to at least one supporting structure. In another embodiment, a method...
8083181 Airplane having a fuselage shell and a floor structure  
An airplane has a fuselage shell and a floor structure that includes cross members and floor plates. Rods are used exclusively to connect the fuselage shell to the floor structure.
8079549 Monolithic integrated structural panels especially useful for aircraft structures  
Structural panels for use in manufacturing fuselage bodies and other aircraft structures are disclosed herein. In one embodiment, a monolithic integrated structural panel is configured to include...
8074694 Stringer transition method  
A stringer comprises a base portion and first and second webs extending outwardly from the base portion. The orientation of at least one of the first and second webs may transition from a first...
8074928 Floor system for a fuselage airframe of an aircraft  
A floor system for a fuselage section of an aircraft is provided. The floor system has an essentially self-supporting design and is substantially mechanically separate from the fuselage section as...
8070098 Aircraft tail cone  
In a rear cone of a fuselage of an airplane a pressurized space is arranged in the rear cone and extends up to an impervious strong wall, placed on a rear portion of the length covered by a fin....
8066221 Aircraft ventral fairing partition wall and aircraft equipped with a ventral fairing  
The invention concerns a wall (10) of vertical partitioning for a ventral cowling of an aircraft including a plurality of vertical panels (11, 12, 12′, 13, 13′), each panel being linked to an...
8061655 Aircraft configuration utilizing fuselage, wing, empennage, and exhaust flow control devices  
Apparatus and methods provide for an aircraft configuration that utilize structural and engine exhaust flow control devices to enhance performance. Aspects of the disclosure provide a fuselage...
8061035 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...
8056850 Particle-filled wing-to-body fairing and method for reducing fairing vibrations  
A wing-to-body fairing for reducing noise due to wing-to-body fairing vibrations in an aircraft, spacecraft, or vehicle may include a honeycomb center having a cavity which is at least partially...
8057618 Method and apparatus for making structures of composite material, in particular airplane fuselage sections  
A method and a device for manufacturing hollow components out of a composite material, such as sections of an airplane fuselage, that include a skin and possibly strengthening elements. The method...
8047469 Airframe attachment fitting  
An airframe attachment fitting includes a fitting base having a base attachment surface and a flange attachment surface, at least one attachment post extending from the base attachment surface of...
8047465 Composite anti-crash structure with lateral retention, for an aircraft  
A structure for an aircraft comprises a first wall and a second wall. The first wall comprises two jackets of composite material disposed on either side of an intermediate arrangement and further...
8042315 Reinforced composite panel  
A reinforced panel, made of a composite material, includes a single base layer. A first plurality of mutually parallel ridges is affixed to the surface of the base layer. A second plurality of...
8042768 Systems and methods for reducing noise in aircraft fuselages and other structures  
Systems and methods for reducing noise in aircraft fuselages and other structures are described herein. A noise reduction system configured in accordance with one embodiment of the invention...
8038099 Bonded metal fuselage and method for making the same  
A bonded metal fuselage for aerospace vehicles includes a monocoque structure having an outer metal skin, metal tear straps bonded to the outer skin and metal stringers bonded to the outer skin...
8039115 Metallic aircraft component  
The invention relates to metallic aircraft components which can preferably be used for aircraft structures in the fuselage region. A damage-tolerant design is usual for aircraft components in the...
8033503 Pressure bulkhead for an aerospace fuselage  
A pressure bulkhead for an aerospace fuselage includes a bulkhead main portion having an approximately flat shape in unloaded state; and a frame supporting and connecting said bulkhead main...
8033502 Modular aircraft interior configuration and methods  
Modular configuration for an aircraft interior floor plan design is provided by an fuselage having starboard and port side attachment rails disposed longitudinally parallel to one another. Each of...
8025253 Commercial aircraft with a main deck and a lower deck  
In a commercial aircraft with a main deck (2) and a lower deck (5, 6), at least one passenger cabin (16, 16′) is also provided on the lower deck. The fuselage diameter lies on the order of a...
8021740 Radiation curable maskant and line sealer for protecting metal substrates  
The invention provides a coated metal substrate comprising a metal substrate having an outer surface, a maskant film adhered to at least a portion of the outer surface of the metal substrate, the...
8016236 Method and apparatus for attaching a wing to a body  
A method and apparatus for assembling an aircraft. A wing spar fitting is connected to a spar in a wing for the aircraft. A body frame fitting is connected to a frame in a body for the aircraft....