Match Document Document Title
8528862 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...
8528854 Self-righting frame and aeronautical vehicle  
An aeronautical vehicle that rights itself from an inverted state to an upright state has a self-righting frame assembly has a protrusion extending upwardly from a central vertical axis. The...
8523105 Aircraft provided with a fuel cell system  
According to the invention, a rear portion of a fuselage of an aircraft contains a fuel cell system, and the aircraft further includes a rear cone which is removably mounted relative to the rear...
8524352 Self-stabilised stiffener enabling element recovery  
A stiffener for a structure submitted to tensile and/or compression and/or shear stresses, that includes a shaped section including: a contact area with an element to be stiffened having a closed...
8523109 Airframe including crossmembers for fixing seats  
The invention relates to an airframe having a substantially circular cross section in a lateral direction (Y) and which extends in the longitudinal direction (X). The airframe comprises, a...
8523110 Door frame component of cast titanium and structural fuselage part  
A door frame component of cast titanium for a door opening in an outer skin of an aircraft or space vehicle and a structural fuselage part that includes the door frame component. The component...
8523112 Device for holding an insulating blanket and for fastening systems adapted to be mounted in an aircraft  
A device for holding an insulating blanket and for fastening systems for an aircraft including aircraft frames, a skin, and connecting pieces between the skin and the frames, the connecting pieces...
8517309 Integrally stiffened panel  
The integrally stiffened panel includes one or more stiffeners oriented in one direction, and one or more stiffeners oriented in a different direction. The stiffeners are integral with a sheet...
8519312 Missile with shroud that separates in flight  
A missile includes a separable shroud that covers a nose portion of the fuselage of the missile. The shroud covers and protects a seeker window and a seeker at the nose of the missile. The shroud...
8511601 Aircraft with tuned vibration absorber mounted on skin  
An apparatus and method for attenuating noise and vibration in a propeller aircraft comprises a tuned vibration absorber adapted to be mounted to the skin of a fuselage of a propeller aircraft....
8511609 Structural mode shape alignment  
Apparatus and method for controlling the orientation of a fundamental panel vibration mode shape of a structure, such as a skin panel of a fuselage of an aircraft, relative to the direction of a...
8505851 Profile comprising at least one hollow profile section  
A profiled part, for use, in particular, within an aircraft or spacecraft, the profiled part comprising at least one hollow profiled part portion and a T-shaped and/or L-shaped profiled part portion.
8507042 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...
8500066 Method and apparatus for wireless aircraft communications and power system using fuselage stringers  
A method and apparatus for transmitting wireless signals. An apparatus comprises a stringer having a channel and a waveguide located within the channel. The waveguide is capable of carrying a...
8496206 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...
8490920 Composite bulkhead and skin construction  
Aircraft fuselage structures have fuselage bulkheads in which the bulkhead outer caps are integrated with the skin, thereby reducing fastener count and weight. These outer caps and skin are...
8490921 Line system arrangement in an aircraft or spacecraft having a fuselage  
A line system arrangement in an aircraft or spacecraft having a fuselage includes at least one receiving region for receiving at least one component of a line system, wherein the at least one...
8490922 Lining for an aircraft  
A lining for an aircraft. The lining separates an intermediate space from an interior space of the aircraft in a pressuretight manner. The lining panels extend either substantially horizontally or...
8480030 Structural component and method for stiffening an external skin  
The present invention provides a structural component for an aircraft or a space craft having an outer skin and a first reinforcing element which runs on the outer skin along a first spatial...
8480027 Movable storage unit for an accommodation module of an aircraft  
According to an exemplary embodiment of the invention, a storage module is stated that is positioned in a region between two frame elements of an aircraft and that can be moved to a folded-out...
8479880 Multifunctional nano-skin articles and methods  
Methods for vibration and acoustic abatement. The methods comprise providing a substrate with a composite layer deposited thereon, the substrate receiving a vibration energy sufficient to provide...
8474758 Aircraft component assembly system  
An aircraft component assembly system for the assembly of an interior component, a pipe or an electric line in an aircraft includes at least one arc-shaped frame element, a connection element that...
8469311 Aircraft fuselage comprising a space for work and storage at the rear thereof  
This fuselage comprises a wall and side doors as well as a space arranged behind the side door the farthest to the rear of the aircraft. The space for work and storage is delimited by side walls...
8453973 Plug mounting  
A plug mounting (50) is provided as a combination of a plug (10) and a mount (30), for the detachable mounting of an equipment part, such as an inner panel, to a supporting frame, such as an...
8453975 Coupling device for coupling fuselage sections; combination of a coupling device and at least one fuselage section; and method for producing the coupling device  
A coupling device for connecting fuselage sections, in each case forming a transverse abutting region for creating an aircraft fuselage comprising fuselage sections with a fuselage skin, a...
8453971 Composite structure power distribution  
A particular method includes exposing a plurality of fibers of a composite skin of an aircraft component by providing an opening in a layer of a first resin overlaying the plurality of fibers at...
8453961 Supersonic aircraft with shockwave canceling aerodynamic configuration  
Disclosed is a supersonic aircraft design having a single structural component that simultaneously joins the wings to the aircraft fuselage, the engines to the aircraft fuselage, and the wings to...
8444089 Pressure bulkhead and method for subdivision of an aircraft or spacecraft  
The present invention provides a pressure bulkhead for subdivision of an aircraft or spacecraft into an internal and an external pressure region. The pressure bulkhead comprises a pressure plate...
8444088 Fuselage structure and method for the production of a fuselage structure  
The present invention provides a method for the production of a fuselage structure, and a fuselage structure, in particular of an aircraft or spacecraft, with an inner shell arrangement which has...
8444087 Composite skin and stringer structure and method for forming the same  
Composite stringer and skin structures and methods for forming the same are disclosed. In one embodiment, a composite stringer and skin structure includes a polymer-based elongated stringer...
8444090 Transverse butt connection between two fuselage sections  
A transverse butt connection between two fuselage sections, more particularly for creating a fuselage cell for an aircraft, can have a number of stringers arranged spaced out uniformly parallel to...
8439307 Structural component with rib and cross member element  
The present invention provides a fuselage structure for an aircraft or spacecraft with an outer skin. The fuselage structure comprises a rib element for stiffening the outer skin and ad cross...
8434716 Compliant crown panel for an aircraft  
An aircraft forward pressure bulkhead and an aircraft crown panel are described herein. The forward pressure bulkhead includes a malleable and deformable dome that is configured to “catch” foreign...
8424804 Attachment arrangement for attaching a component to the fuselage of an aircraft, aircraft and method for constructing an attachment arrangement  
An attachment arrangement for attaching a component to the fuselage of an aircraft. The attachment arrangement comprises an elongated stringer that can be connected to the aircraft fuselage, and a...
8418963 Aircraft load frame made of a composite material  
The present invention relates to an aircraft load frame (1) made of a composite material, characterized in that it comprises two side elements (2, 3) and a base element (7), the side elements (2,...
8408493 Composite stringer end trim  
A stringer having a stringer end trim that reduces pull-off forces in a stringer connection structure, including a stringer body; a stringer free edge provided on said stringer body; and a...
8408492 Floor panel for forming a loading area in a cargo hold of an aircraft  
A floor panel, in particular for covering floors of cargo holds of aircraft, is formed by a plurality of milled profiles, which are friction stir welded along their longitudinal edges, with...
8403263 Composite and structure, particularly in the aerospace sector  
The present invention provides a composite, in particular in the field of aviation and aerospace, comprising an omega-stringer that comprises a comb portion, and a connecting member that is...
8403256 Swept-wing powered-lift aircraft  
Apparatus and methods provide for a swept-wing powered-lift aircraft. Aspects of the disclosure provide a powered-lift aircraft that utilizes the engine exhaust flow over upper surface blown flaps...
8403261 Process for making an aircraft having a floor  
The method of fabricating an aircraft comprises the following steps: fastening two lateral floor portions, each firstly to a fuselage element and secondly to supports that are connected to the...
8398021 Compliant crown panel for an aircraft  
An aircraft forward pressure bulkhead and an aircraft crown panel are described herein. The forward pressure bulkhead includes a malleable and deformable dome that is configured to “catch” foreign...
8398022 Wide body aircraft architecture  
A large-capacity airplane principally includes a fuselage which has no region of constant width between the front and the rear and a wing fixed to the fuselage. As a preference, the engines are...
8398027 Method and apparatus for reinforcing composite structures  
A computer implemented method and apparatus for creating a structural joint for an aircraft. A first composite component and a second composite component are co-joined to form the structural joint...
8393575 Rib post  
A rib post (10) has a hollow substantially triangular cross-section comprising composite material. The rib post (10) can form a structural member to join two adjacently placed components together,...
8387917 Support structure for a cargo aircraft  
A method and apparatus for transporting containers in an aircraft. A number of containers is loaded into the aircraft. The aircraft is comprised of first and second outer planar structures, a...
8387918 Multi-directional support arm  
A compartment for a transportation device is provided. The compartment may include a one-piece basin, an inflatable wall member, and multi-directional support arms to attach the basin within the...
8382038 Device, in particular connection rod, for bracing a fuselage structure of an aircraft and/or for fastening a component  
The invention relates to a device, in particular a connection rod, for bracing a fuselage structure and/or for fastening components on the fuselage structure. In one embodiment, the joints are...
8382037 Composite barrel sections for aircraft fuselages and other structures  
Composite sections for aircraft fuselages and methods and systems for manufacturing such sections are herein. A composite aircraft panel manufacturing assembly comprises a skin, a stiffener, a...
8376275 Energy absorbing structure for aircraft  
Energy absorbing structure disposed beneath the cargo area of an aircraft provides maximum energy absorption and structural strength using carbon fiber reinforced epoxy composites. The energy...
8378233 Aircraft interior bushing  
An aircraft interior bushing assembly is disclosed comprising interoperating bushings, each bushing comprising a recessing portion, a radially inner surface operably configured to contact a...