Match Document Document Title
8376276 Load introduction structure, in particular a lining frame, for an aircraft  
The invention relates to a load introduction structure for an aircraft, comprising two lateral frames which are arranged opposite one another in the two lateral regions of a fuselage airframe...
8376281 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...
8371550 Equipment holder with optional grid function  
An equipment holder is provided with an optional grid function for positioning a first cabin component of an aircraft relative to a second cabin component of the aircraft and for attaching the two...
8371530 Aircraft with a rear fuselage protection shield  
The invention relates to an aircraft with a protection shield for the rear composite material, fuselage 25) for conducting tail impact tests, in addition to a tail absorber, the shield (11) being...
8371529 Interconnection and aircraft or spacecraft having such an interconnection  
The invention relates to an interconnection, including: a T-stringer which has a web portion and two foot portions; a Ω-stringer which has a comb portion and two foot portions; and a connection...
8371528 Intercostal for an aircraft or spacecraft  
The present invention relates to an intercostals for an aircraft or space craft for diverting a load from a first rib to a second rib and/or a skin of the aircraft and/or space craft, with at...
8366043 Structure, especially a fuselage structure of an aircraft or a spacecraft  
The present invention provides a fuselage structure (1; 1′) of an aircraft comprising an annular skin segment (2; 2′) which has a cross-sectional opening (3; 3′), a pressure cap (4; 4′) for a...
8366050 Blended wing body cargo airplane  
A blended wing body cargo aircraft is disclosed. A body section defines a cargo volume, where an outer surface of the body section is shaped to provide an aerodynamic lifting surface. A cargo door...
8366042 Arrangement for installing electric cables in the floor region of an aircraft  
An arrangement for installing electric cables in the floor region of an aircraft includes longitudinal guide elements that form cable channels and essentially extend in the longitudinal direction...
8366041 Aircraft floor, use of said floor and aircraft section fitted with said floor  
An aircraft floor, and aircraft section provided with such a floor, and the utilization of such a floor in an aircraft section. The aircraft floor generally includes at least one central rail...
8360355 Wing-to-body fairing with spray-on foam and noise reduction method  
A fairing includes a fairing body having a fairing interior and an interior surface and a spray-on insulation foam layer provided on the interior surface of the fairing body.
8360362 Aircraft floor and method of assembly  
The invention relates to aircraft floor assemblies and to methods for their assembly. In one embodiment, an aircraft comprises at least one fuselage section and at least one floor section. At...
8356771 Coupling for joining two frame segments  
The invention relates to a coupling for joining two frame segments within a fuselage cabin structure of an aircraft. The frame segments may comprise a Z-shaped or I-shaped cross-sectional...
8356772 Lightweight structure  
A lightweight structure is disclosed, in particular a lightweight structure for an aircraft which is formed from a large number of components which can be joined together by weld joining...
8356773 Structural wing-fuselage component for connecting two wings to a fuselage section of an aircraft  
A structural wing-fuselage component for connecting two aerofoils to a fuselage section of an aircraft includes: a first wing shell component for the first wing and a second wing shell component...
8353479 Arrangement of two fuselage sections of an aircraft and a connecting structure for connecting fuselage skins  
A coupling element for connecting stringers in the process of joining two fuselage sections by means of at least one transverse splicing plate, wherein in each case the fuselage sections on the...
8353478 Blended wing aircraft  
Apparatus and methods provide for a blended wing passenger or cargo aircraft. Aspects of the disclosure provide an aircraft having wings with spars having a thickness at the wing root...
8342449 Vertically movable passageway for rest rooms in ceiling region  
A vertically movable passageway for a space in the ceiling region in an aircraft cabin. The passageway comprises a passageway floor and a displacement device, wherein the displacement device is...
8336823 Aircraft fuselage  
An aircraft fuselage including a front part including a cockpit, a central part, and a rear part. The central part of the fuselage includes a first zone located at the front part and that...
8336822 Apparatus for providing variable thermal insulation for an aircraft  
An aircraft insulation apparatus is disclosed having a variable thermal insulating member adjacent the inner fuselage wall and adjacent an aircraft heat source. The variable thermal insulating...
8327976 Insulation design for thermal and acoustic insulation of an aircraft  
The invention pertains to an insulation structure for thermally and acoustically insulating an aircraft that features at least one heavy layer, wherein the insulation structure according to the...
8322656 Wing-fuselage section of an aircraft  
A wing-fuselage section of an aircraft, which wing-fuselage section comprises a wing root at which the wing of the aircraft is connected to the fuselage, a fuselage region with fuselage frame...
8322655 Twin-boom empennage  
Apparatus and methods provide for an aircraft empennage that utilizes two torque tube members to create opposing sides of the empennage. The torque tube members are connected using a bridging...
8317134 Stiffened casing for an aircraft or spacecraft with a laminate stringer of high rigidity and corresponding laminate stringer  
The present invention provides a casing structure of low weight provided with a laminate stringer of high rigidity. The stringer has the form of a laminate with a plurality of metallic layers and...
8317133 Aircraft floor and fuselage supplied with said floor  
An aircraft floor including two lengthwise external beams and at least one pair of cross beams extending between the lengthwise beams, an external end of each cross beam being interlocked to the...
8308108 Fuselage arrangement for airplane  
An aircraft fuselage with a shape elongated along a longitudinal axis X along a longitudinal axis of the aircraft that determines a direction toward the front along a direction of motion of the...
8302909 Splicing of omega-shaped stiffeners at a circumferential joint in an aircraft fuselage  
An aircraft fuselage produced by assembling, at a circumferential joint, at least two sections, each section including a coating and at least one element of at least one stiffener, the...
8302908 Blended wing aircraft  
Apparatus and methods provide for a blended wing passenger or cargo aircraft. Aspects of the disclosure provide an aircraft having wings with spars having a thickness at the wing root...
8302486 Reinforced panel  
A reinforced panel (1) comprising: a composite skin (2); a plurality of stringers (3, 4) bonded to the skin; and one or more strain actuators (5), each positioned between an adjacent pair of...
8297555 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...
8294020 Energy harvesting devices  
Energy harvesting devices, wherein one illustrative embodiment includes a crease beam, a thermoelectric element disposed in thermally-conductive contact with the crease beam and a heat exchanger...
8291671 Joint arrangement for composite-material structural members  
A joint arrangement for composite-material structural members in components including a skin and a plurality of structural members, applicable to pairs of first and second intersecting structural...
8292226 Weight-optimizing internally pressurized composite-body aircraft fuselages having near-elliptical cross sections  
A method for minimizing the weight of an internally pressurized aircraft fuselage of a type that includes an elongated tubular shell having a near-elliptical cross-section with a radius R(φ)- and...
8292214 Vibration damping for wing-to-body aircraft fairing  
A wing-to-body fairing for aircraft is formed from a sandwich structure having integrated vibration damping.
8292225 Airplane with flat rear fuselage said queue-de-morue empennage  
An airplane includes a fuselage having a shape elongated along a longitudinal axis X of the airplane and at least one wing fixed to the fuselage between the front end and the rear end of the...
8282041 Fastening element for insulation packages  
A fastening element includes, but is not limited to at least one first body, at least one second body, and at least one locking device. The first body and the second body in each case on one end...
8282036 Multi wing aircraft  
A multi-wing, airfoil fuselage aircraft that is capable of flying in a ground-effect mode includes a main airfoil fuselage wing, a fin that extends vertically from this wing, a pivot mount that is...
8267352 Structure of the load introduction zone in the rear end of an aircraft  
Load introduction zone in the rear end of an aircraft comprising receiving elements (3, 4) of the loads of the horizontal and vertical tail stabilizers connected to structural elements (2, 8, 9)...
8262024 Aircraft frames  
The invention relates to a reinforcing frame (1) of the fuselage (2) of an aircraft, said fuselage (2) comprising a skin (3) and stringers (20), the mentioned frame (1) comprising a structural...
8262020 Casing and front landing gear assembly for an aircraft  
A casing including a wall defining an internal housing which allows retraction of a corresponding landing gear into the interior of the housing. The wall separates the non-pressurized internal...
8262023 Aircraft frame element connected to an air-conditioning system  
A frame element for use in an aircraft air-conditioning system is attachable to an aircraft structure and includes at least one strut which is formed to at least in sections as a hollow cylinder,...
8256713 Aircraft fuselage section  
The invention relates to an aircraft fuselage section comprising several longitudinal strengthening beams attached to the fuselage section lower panel and several longitudinal rails intended for...
8245974 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...
8240606 Integrated aircraft floor with longitudinal beams  
An integrated floor for an aircraft fuselage includes a composite panel forming a floor surface and composite beams bonded to the floor panel. The beams extend longitudinally within the fuselage...
8231080 Distributing power in systems having a composite structure  
Systems and methods to distribute power in a system having a composite structure are provided. A particular aircraft includes a fuselage having a composite skin. The composite skin includes a...
8226035 ***WITHDRAWN PATENT AS PER THE LATEST USPTO WITHDRAWN LIST***
Blended wing aircraft
 
Apparatus and methods provide for a blended wing passenger or cargo aircraft. Aspects of the disclosure provide an aircraft having wings with spars having a thickness at the wing root...
8226034 Cargo deck and a method for assembling said deck  
An aircraft cargo deck is provided to receive loads stored in the cargo compartment. The aircraft comprises an outer skin to which longitudinal beams are secured, preferably via ribs attached to...
8215584 Aircraft structure including stiffener edge junctions  
An aircraft structure including stiffened panels assembled at the junction, without continuity of the stiffeners. Multiple panels are used to form the fuselage, tail units and wings of an...
8210477 Vibrations damper for fastenings elements in aircrafts  
Means for attaching installed parts (14) are cell-side attachment points (15) in a vehicle cell (11) of a vehicle, in particular of an aircraft (10), for conveying goods and passengers....
8210472 Method for improving the performance of an aircraft  
Disclosed is a method for improving the performance of transport aircraft. In particular, the aircraft is provided with a rounded nose cone in front of a center of gravity of the aircraft. The...