Match Document Document Title
9038953 Aircraft thermal insulation  
The invention provides an arrangement and methods for thermally insulating aircraft, particularly but not exclusively for when the aircraft is operating in extremely hot or cold conditions, and...
9038947 Floor for an aircraft cargo compartment and method for the assembly thereof  
In conventional aircraft cargo compartments panels or similar flat floor elements are fastened to floor beams or similar supporting elements that are installed in the body of the aircraft....
9034453 Reinforced aircraft fuselage panel and method of manufacture  
A fuselage panel made of composite material having a skin with an opening, at least part of the contour of which is reinforced by an integrated reinforcement made of composite material. The...
9027883 Aircraft fairing  
A shock control fairing for mounting a junction between adjoining aircraft surfaces. The fairing has a cross-sectional profile which varies along the length of the fairing. The cross-sectional...
9016628 Methods and apparatus for reducing noise in reinforced skin structures  
Assemblies, methods, and an apparatus for damping vibrational energy induced to a reinforced skin structure are disclosed. The reinforced skin structure includes an outer wall and at least one...
9018572 Rocket propelled payload with divert control system within nose cone  
A rocket is provided and includes booster stages at a rear of the nose cone, the booster stages being configured for propelling the nose cone in a propulsion direction and a divert control system...
9017510 Method and apparatus for fabricating large scale integrated airfoils  
An airfoil is fabricated by assembling cured skins with spars having cured spar webs and uncured spar chords. The skins are bonded to the spars by curing the spar chords.
9010688 Structural joint having continuous skin with inside and outside stringers  
Apparatus and methods provide for a structural joint utilizing overlapping blade stringers coupled to opposing sides of a continuous skin. According to embodiments described herein, a structural...
9010687 Insulating blanket for an aircraft and assembly integrating such a blanket  
This invention proposes an insulation blanket for an aircraft, the said blanket coming in the form of a strip of insulation material of elongated shape having two more or less parallel...
9010684 Automated inspection of soft-tooled hollow structure  
A system and method that allow inspection of hollow structures made of composite material, such as an integrally stiffened wing box of an aircraft. A wing box comprises top and bottom skins...
8991758 Unmanned aerial vehicle  
An unmanned aerial vehicle, comprising: a fuselage having a first side board and a second side board spaced apart and connected by at least one transverse board; the first side board, the second...
8991762 Wing/fuselage connection of an aircraft  
A wing-fuselage connection of an aircraft, in which a wing (2) that is arranged in the upper region of the fuselage (1) is connected to the fuselage (1) by means of a number of couplings (3, 4, 5,...
8991759 Rear fuselage of an aircraft  
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...
8991757 Self-supporting cabin structural segment  
A cabin structural segment is provided for an aircraft that includes, but is not limited to a fuselage structure and a floor structure. The fuselage structure defines an interior and separating it...
8979027 Wall installation system and method  
A system for attaching a wall panel includes a wall panel and a lock strip. The wall panel has a back and a tab extending from the back. The lock strip is moveably attached to a wall frame member,...
8974885 Structural element for reinforcing a fuselage of an aircraft  
A structural element for reinforcing a fuselage cell of an aircraft is provided. The structural element comprises a reinforcement profile which is made in one piece from a metallic material. The...
8968500 Method and device for adhesively joining large-surface components in vehicle construction  
A method for joining, by adhesive bonding, at least two large joining partners in vehicle construction, in particular in aircraft construction, comprises the following steps: detecting the...
8967526 Multi-role aircraft with interchangeable mission modules  
A flight-operable, truly modular aircraft has an aircraft core to which one or more of outer wings members, fuselage, cockpit, leading and trailing edge couplings, and empennage and tail sections...
8967540 Anti lateral-torsional buckling structural member of an aircraft fuselage  
A frame of an aircraft fuselage structure made from composite material, which includes a skin and several stringers fixed on the skin. The frame includes a profile elongated in a longitudinal...
8967539 Method for assembling a floor in a cockpit structure previously constructed from a section of aircraft fuselage  
A section of aircraft fuselage includes a body structure and a floor connected to the body structure. The body structure has an external skin and a framework including frames, positioned in...
8960603 Impact resistant and damage tolerant aircraft fuselage  
An aircraft fuselage part (31) located in a section of an aircraft (11) having a propulsion system (13) attached by upstream pylons (17), the fuselage part includes a skin (35); a plurality of...
8955804 Aircraft structure with air ducts integrated in structural elements  
An aircraft structure is provided with load-bearing hollow structural elements that form an aircraft fuselage. The cavities in the structural elements are designed as air ducts for an air...
8955802 Luggage storage compartment, aircraft with a luggage storage compartment, and method for operating the luggage storage compartment  
The present invention is directed to a luggage storage compartment for an aircraft having high ease of operation. Specifically, the luggage storage compartment comprises a housing and a housing...
8951375 Methods and systems for co-bonding or co-curing composite parts using a rigid/malleable SMP apparatus  
A method and apparatus for fabricating a composite part, such as a fuselage or internal stiffener, with a shape memory polymer (SMP) apparatus usable as both a rigid lay-up tool and a bladder. The...
8945325 Methods and systems for forming integral composite parts with a SMP apparatus  
A method and apparatus for fabricating a composite part, such as a fuselage or internal stiffener, with a shape memory polymer (SMP) apparatus usable as a rigid lay-up tool. The SMP apparatus may...
8939406 Joining composite fuselage sections along window belts  
A fuselage having a longitudinal window belt has a composite outer skin including upper and lower composite skin sections. The skin includes at least one window opening located at the window belt....
8939405 Aircraft fuselage element  
An aircraft fuselage element being a one-piece component, and including a closed wall defining an internal volume, an external surface of the wall forming the external skin of the fuselage. The...
8939404 Pressure fuselage of an aircraft with dome-shaped pressure bulkhead  
A pressure fuselage of an aircraft, which fuselage in longitudinal direction comprises several fuselage sections, wherein at least one rear dome-shaped pressure bulkhead is provided to form an...
8936215 Aircraft including floor support cross-members with bearings including a flexible material connecting the cross-member to the support  
An aircraft including: at least one floor cross-member; at least one support carrying the cross-member; and at least one bearing including at least one flexible material and connecting the...
8931592 Aircraft interior panel with acoustic materials  
A panel assembly that includes a first panel having an inner surface and an outer surface, and a second panel having an inner surface and an outer surface. The second panel includes a plurality of...
8931739 Aircraft having inflatable fuselage  
A method and apparatus for deploying an aircraft. An inflation system is activated to generate a gas. A fuselage of the aircraft is inflated with the gas. The fuselage comprises a frame for the...
8925862 Monument complex for an aircraft rear area  
A monument complex is provided for a rear area of a passenger cabin. The rear contour of the monument complex is adapted to the contour of the bulkhead so that an additional wash basin can be...
8925864 Component, in particular a shell component, which can be joined thermally and/or mechanically, for building a fuselage section of an aircraft  
A component for building a fuselage section of an aircraft includes a border area connectable to a corresponding further border area of a further component so as to form an electrically conductive...
8919696 Method and a device for the manufacture of a stiffening structure for an aircraft fuselage segment, and also a stiffening structure  
A method for stiffening a skin field of an aircraft fuselage includes providing a skin field for an aircraft fuselage, manufacturing an integral lattice-shaped stiffening structure including a...
8920594 Composite thermoplastic matrix airframe structure and method of manufacture therefore  
A thermoplastic matrix airframe structure section includes a multitude of thermoplastic matrix frame members and a multitude of thermoplastic matrix beam members which form a substructure, which...
8915469 System for draining water condensation in an aircraft  
The invention relates to an aircraft comprising: a drainage system for condensation water formed in the aircraft between an upper zone thereof where the condensation water is formed and a lower...
8915470 Aircraft nose and nose landing gear bay structure  
An aircraft nose structure includes a fuselage, a floor for a pressurized space and a nose landing gear bay arranged under the floor, on the opposite side to the space. The bay includes walls that...
8915468 Interior covering device for an aircraft cabin incorporating at least one system  
A device for interior covering of an aircraft cabin, intended to be fastened to a structure of an aircraft and to extend along a skin of the aircraft, the device comprising a covering panel. The...
8910908 Two-piece stiffening element  
The invention provides a stiffening element, in particular for a shell component of an aircraft or spacecraft, which has a stiffening profile part and a foot part. The stiffening profile part is...
8905352 Aircraft nose structure with landing gear compartment  
An aircraft nose structure includes a fuselage and a pressuretight bulkhead fixed at its periphery to the fuselage and transversely dividing the fuselage into a pressurized upper zone and an...
8905350 Structural panel with integrated stiffening  
A stiffened panel including at least one stiffener, known as a longitudinal stiffener, extending substantially from one extremity of the panel to another and whose trace on a surface of the panel...
8905351 Airframe  
The disclosure describes airframe systems. In one embodiment, an airframe system includes a first side wall and a second side wall. The airframe system further includes a drive train platform...
8905349 Structural element of an aircraft fuselage  
The structural element of an aircraft fuselage, with stringers running in the longitudinal direction of the aircraft fuselage and ribs running transversely to the stringers in the circumferential...
8899521 Aircraft floor of optimized compactness and housing utility members  
An aircraft floor portion includes crossmembers. Each crossmember comprises a top partial crossmember and a bottom crossmember, with at least one gap being left between the top partial crossmember...
8899520 Mid-wing airplane  
An airplane includes a wing mounted mid-level on a tubular fuselage. The wing includes carry-through that passes transversely through the fuselage and divides a cabin deck into fore and aft...
8899522 Aircraft fuselage with high strength frames  
A fuselage section of an aircraft includes a skin, a plurality of frames positioned transversely to a longitudinal axis of a fuselage of the aircraft, and a plurality of longitudinal stringers at...
8895908 Wing slot seal  
A low cost, lightweight frangible wing slot seal can be applied to a guidance wing slot of a folding fin aerial rocket or missile, providing a barrier against exposure of internal missile...
8894010 Aircraft fuselage frame element  
An aircraft fuselage frame assembly includes a first lower frame element having a cross member and a curved fuselage tub frame. A second upper frame element of the assembly has a cross member and...
8893865 Impact absorbing structure, method for producing impact absorbing structure, and movable body  
The impact absorbing structure of the present invention is an impact absorbing structure for absorbing an impact in a case where the impact absorbing structure is subjected to the impact in a...
8894011 Aircraft fuselage constructed of aircraft fuselage sections screwed together  
An aircraft fuselage is constructed of a plurality of cylindrical semi-monocoque fuselage sections that are each constructed with mirrored screw threads on either their interior or exterior...