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8882089 Dual radius isolator  
A vibration isolator includes a base plate having a first attachment feature that enables attachment of the isolator to a first surface, the isolator further including a second attachment feature...
8882039 Structural mode shape alignment  
A method is disclosed for reducing noise and vibration within a structure of a mobile platform, wherein the noise and vibration are at least in part caused by airflow over an outer skin of the...
8882038 Sealing device between a cross member and insulation blanket provided at an aircraft fuselage  
An insulation blanket to be connected at the inside surface (16) of an aircraft fuselage, includes at least one opening that allows a through element (20) to pass, at which is connected a sealing...
8876048 Fuselage of an aircraft or spacecraft and corresponding aircraft or spacecraft  
The invention relates to a fuselage of an air- or spacecraft. The fuselage comprises at least one shell element and one insulation element. The insulation element is configured as a passive,...
8869403 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...
8870117 Composite aircraft frame  
Composite aircraft frame (1) comprising two segments (10, 20), each of these segments (10, 20) being single unitary element made in composite material and comprising at least one web (2), a...
8864074 Composite panel stiffener  
A multi layer composite L-shaped stringer for use in an aerospace structure comprises a foot and a web extending from an edge of the foot. A first surface on the foot is shaped to abut a structure...
8864075 Elongate composite structural members and improvements therein  
A composite material elongate structural member, such as a spar, for use in an aerospace structure, comprises a web disposed between upper and lower flanges. The web may include a clockwise twist...
8864072 Structural component with improved conductivity and mechanical strength, and a method for its manufacture  
A structural component includes a fiber composite material structure having an outer surface and an electrically conductive metal profile disposed on the outer surface of the fiber composite...
8864076 Elongate composite structural member  
A composite material elongate structural member, such as a spar or stringer, for use in an aerospace structure, comprises a web having an angled portion, for example in the form of a chamfer,...
8857765 Method and apparatus for attaching an aircraft fuselage frame to a wing box  
The present disclosure is generally directed to an aircraft body including a fuselage skin on an outboard member of the aircraft body and a wing box extending through a member of the aircraft...
8857764 Fly away caul plate  
Techniques and apparatus for providing a fly away caul plate are disclosed. In an embodiment, a method for curing a composite structure includes placing a pre-cured caul plate proximate an uncured...
8857562 Standardised insulation device for an aircraft and processes of making and using thereof  
An insulation device for an aircraft, comprising a blanket comprising a layer of insulation filling enclosed in a cover and having provision areas for the passage of aircraft components, these...
8844871 Aircraft fuselage structural components and methods of making same  
Aircraft fuselage structures have reinforcement members in the vicinity of the stringer openings formed in frame members and are rigidly lap joined to a surface region of the frame members by a...
8844868 System and a method for fastening aircraft components in the case of a CFK-metal hybrid construction  
The present invention relates to the use of connecting elements for fastening CFK components and metal components in an aircraft or spacecraft, wherein a CFK component and a metal component can be...
8844874 Interchangeable joint concept for an aircraft rear fuselage cone  
Rear fuselage of an aircraft comprising a tail cone end and a rest of the real fuselage whereby the tail cone end is attached to the rest of the rear fuselage by means of an attachment system...
8844873 Stabilizer torque box assembly and method  
In an embodiment of the disclosure, there is provided an apparatus to provide a panel stiffening element. The apparatus has an outer braided thermoplastic tube and an inner braided thermoplastic...
8844869 Aircraft structural assembly and associated assembling method  
An assembly includes a structural wall and a composite wall extending in the extension of the structural wall and defining a second section positioned facing a first section of the wall. The...
8844870 Fuselage segment, and method for the production of a fuselage segment  
A fuselage segment of an aircraft fuselage is provided with an outer skin and an inner skin that are spaced apart from one another by a core, wherein conduits for system installations are...
8840066 Front part of an aircraft fuselage incorporating a bay for stowing landing gear  
A front part of an aircraft fuselage according to this invention comprises: frames (16) disposed transversely in relation to a longitudinal axis of the aircraft,an outer skin (14) fastened onto...
8840980 Stiffened structure integrating an opening  
A stiffened structure includes stiffeners (14.1, 14.2, 14.3) and nodes (12) at which three stiffeners (14.1, 14.2, 14.3) of different directions intersect, with the surfaces of the stiffeners...
8827057 Shock absorbing structure  
It is desired to make a shock absorbing structure small in size. The shock absorbing structure includes a beam-like structural member having a concave section; and a shock absorbing member, one...
8820682 High privacy passenger aircraft cabin arrangement  
An aircraft that includes a cabin that has a floor, side walls, a ceiling and an interior, a first class section positioned in the interior that includes a longitudinally extending first aisle...
8816916 Radome and device for attaching said radome to an aircraft  
The invention relates to a radome (1) for an aircraft, and more specifically to a device for connecting said radome to the structure of said aircraft. The radome that is the subject of the...
8813926 Impact-absorbing structure and method for producing the same  
An object is to provide an impact-absorbing structure superior in impact-absorbing capacity. An impact-absorbing structure includes a pair of flat, plate-like face plates arranged to oppose each...
8814083 Aircraft provided with a tail plane including means for combating flutter  
An aircraft (1) provided with a tail boom (4) including a tail plane (100) provided with an airfoil surface (5), the airfoil surface (5) being provided with at least one stabilizer portion (11,...
8814091 Floor made out of composite material and process for manufacturing such a floor  
A floor can be attached to a vertical frame structure of a vehicle and includes a horizontal boxed structure having a plurality of boxes positioned side by side to form a continuous, uniform upper...
8800922 Elements for signal and/or power transmission into or to cabin components  
The description covers cabin components for aircraft, which can be produced with a sandwich structure and may have the components 1003 for signal and/or power transmission. The cabin components in...
8800921 Structural component and fuselage of an aircraft or spacecraft  
A supporting component is provided for reinforcing the skin of an aircraft or spacecraft, for example a stringer or former, this component being configured as a closed profile (hollow profile),...
8783616 Loads interface, particularly a loads interface for a plug type aircraft door  
A loads interface (1), particularly a loads interface (1) of an aircraft door with an edge frame (13), an outer skin (15) and a beam (14). A loads transferring flange (11) is designed to transmit...
8783610 Transverse splicing plate for creating a fuselage, and a method for connecting two, in particular wound, CFP fuselage sections  
A transverse splicing plate for producing a fuselage of an aircraft by connecting several CFP fuselage sections that have in particular been produced in the winding method, in each case by forming...
8783615 Loads interface, particularly loads interface of an aircraft structure and application of said loads interface  
A loads interface (1) of an aircraft structure with an edge member (6) and a background structure both preferably made from fiber reinforced plastics. A loads transferring flange (2) is adapted...
8777160 Aircraft including an internal partition  
The aircraft includes a structural portion such as a fuselage, a wing, or a tail, the structural portion including a wall separating the inside from the outside of the portion and including...
8777158 Joint sealing system  
A method and apparatus comprises a first section, a second section, and a middle section. The first section is configured to be connected to a first structure. The second section is configured to...
8777159 Internal structure of aircraft made of composite material  
A reinforcement structure for an opening in the primary structure of an aircraft, the structure comprising a skin, frame members which are transverse with respect to the flying direction of the...
8770519 Structural component of an aircraft or spacecraft and a fuselage component arrangement of an aircraft or spacecraft  
In the case of a structural component of an aircraft or spacecraft comprising a fuselage portion connection region for connecting to an associated fuselage portion and having a thermal expansion...
8770520 Device for the mounting of connectors  
A device for mounting at least one connector in an aircraft fuselage includes a first and a second traverse configured to connect the device to a structural section of the aircraft fuselage at end...
8765042 Fuselage section of an aircraft and method for the production of the fuselage section  
In accordance with the method, an inside layer of a fuselage section skin made from first fibers is placed on a manufacturing surface, the first fibers being placed in one or more first fiber...
8757545 Segment of a fuselage of an aircraft  
According to an exemplary embodiment of the invention a fuselage segment of an aircraft fuselage is provided, which aircraft fuselage comprises four different radii of curvature, wherein two radii...
8752783 Wing-to-body faring 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.
8752791 Fuselage employing multifunctional crown and method of making the same  
A fuselage structure includes a fuselage body and framework for stiffening the body. The framework includes at least one frame member having a duct therein for routing a utility through the body.
8746616 Mid-wing multi-deck airplane  
An airplane comprises a twin-deck fuselage in which an upper deck support structure is utilized for carry-through of a mid-mount main wing box. The main landing gear of the airplane is mounted to...
8746621 Connector for stiffening frames between an aircraft fuselage and a wing box  
The stiffening frames (14) of an aircraft fuselage (2) remain continuous while passing through an upper panel (5) of the wing box and extend over the ribs (3) situated in that box. The overall...
8746618 Composite stringer with web transition  
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...
8740151 Adjustable splice fitting for shimless connection of structual members  
A fuselage section may include a structural member and a frame member having a stub frame extending over the structural member. The stub frame may have a web. The fuselage section may include an...
8740138 Aircraft engine supporting pylon  
An aircraft pylon support system for mounting and supporting aircraft propulsion systems to a fuselage section of an aircraft that includes an internal, central support box disposed within and...
8727279 Method and system for controlling swaying of an object  
A method of configuring a mount or of controlling sway in an object to be mounted includes configuring isolators of the mount to put a center of elasticity of the flexible mount at a desired...
8720823 Aircraft structural element located at the interface between a wing and the fuselage  
An aircraft structural element situated at an interface between a wing and the fuselage, and including a web and profiled elements flanking the web. At least one the profiled element includes a...
8722272 Modular fuel cell system module for connection to an aircraft fuselage  
A fuel cell system module for use in an aircraft includes at least one fuel cell system component. The fuel cell system module is connectable modularly to a fuselage section of the aircraft. A...
8720817 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...