Matches 1 - 50 out of 64 1 2 >


Match Document Document Title
US20120018580 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...
US20120305708 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...
US20110297785 AIRFRAME POSITION ADJUSTING STRUCTURE  
Provided is an airframe position adjusting structure capable of adjusting the position of an airframe (A) inclined in the left-and-right direction. In the airframe position adjusting structure...
US20130082138 VENTILATION SYSTEM, AIR BLOWING AND EXTRACTION CIRCUITS OF SUCH A SYSTEM, AS WELL AS AN AIRCRAFT AVIONICS BAY  
A ventilation system for an avionics bay has two strut assemblies for stiffening the floor of the cockpit, each strut assembly being arranged symmetrically regarding to the central plane of the...
US20070063099 Buoyancy-assisted air vehicle and system and method thereof  
A method and system for air flight is disclosed. The blended lifting body system is comprised of a lift module, a propulsion module, a payload module and a control system. The control system...
US20090032640 SELF SUPPORTING CELLULAR THERMAL ACOUSTIC INSULATION  
In one embodiment, a device includes first and second frame members, and a foam insulation member having first and second ends. At least one of the first and second ends is disposed at an angle...
US20130032660 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...
US20120267478 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...
US20090230235 Tambourine helicopter  
Disclosed is a profile of an end view of a base portion Vertical Take Off And Landing Craft, (VTLC) rotor-blade comprising a widened structure from leading to trailing edges. The profile further...
US20120012712 AIRCRAFT ASSEMBLY AND SPAR  
An aircraft assembly comprising: a pair of covers; a spar web extending between the covers in a thickness direction, the spar web having a length which extends in a span-wise direction; and a...
US20080210817 Energy-absorbing Square Tube Composite Stanchion  
An energy absorbing structural strut employs a composite tube bonded to an end fitting with the bond being slightly lower in strength than the crushing strength of the tube in axial compression....
US20120298800 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...
US20090320398 MONOLITHIC INTEGRATED STRUCTURAL PANELS ESPECIALLY USEFUL FOR AIRCRAFT STRUCTURES AND METHODS OF MAKING THE SAME  
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...
US20100308163 APPARATUS WITH DAMAGE INDICATION FEATURE  
A method of designing and manufacturing apparatus. The method comprises: creating a design space; analysing expected loads acting on the design space to calculate a first load path within the...
US20130026292 STIFF PANEL FOR AIRCRAFT, COMPRISING STIFFENERS WITH NOTCHED CORES  
A stiffened panel includes a panel at least one of whose surfaces is equipped with stiffeners each of which includes a base that is pressed against the surface of panel, as well as a core that is...
US20070246606 Imperative chute  
An aircraft emergency landing assist system comprised of a harness to cradle the major stress points of the aircraft. The harness made of lightweight high tension material attached to the aircraft...
US20110215201 STRUT SYSTEM FOR THE STABILIZATION OF THE SHELL OF AN AERODYNAMIC AIRCRAFT COMPONENT FOR A COMMERCIAL AIRCRAFT  
The invention relates to a strut system for the stabilisation of the shell (2) of an aerodynamic aircraft component in a commercial aircraft, comprising a pair of connection supports (4a, 4b)...
US20120006940 METHOD FOR REALIZATION OF AN AIRCRAFT STRUCTURE AND RESULTING STRUCTURE  
An aircraft structure includes a skin (28) that is reinforced in two directions: by a first family of stiffeners called stringers (30) that are arranged in the longitudinal direction of the...
US20090115088 Process for Producing a Substantially Shell-Shaped Component  
Disclosed is a process for producing a substantially shell-shaped component, from substantially carbon-fiber-reinforced synthetic material having at least one local reinforcing zone and at least...
US20090090813 Method of Dimensioning and Producing Stiffened Structural Components, Use of Structural Condition Sensors and an Aircraft  
The invention concerns a method of dimensioning and producing stiffened structural components (4) comprising at least one shell component (6) and at least one stiffening component (8) which can be...
US20140138489 Aircraft structure arrangement  
An aircraft structure arrangement which is in particular suitable to form a part of a secondary structure of an aircraft comprises a first longitudinal profile and a first frame profile. The...
US20090050737 Polysilazane coatings  
A composition and process for manufacturing a camouflaged aircraft component. The process includes providing an aircraft component; applying an uncured coating onto the aircraft component wherein...
US20080305000 ALUMINUM-MAGNESIUM-SILVER BASED ALLOYS  
Al—Mg—Ag wrought products and methods of making such products useful in aircraft applications. The Al—Mg—Ag wrought products have improved strength when compared to traditional AA5XXX alloys. The...
US20090283635 IMPACT RESISTANT COMPOSITE STRUCTURES  
An impact resistant composite sandwich structure includes least one laminate face sheet joined to a stiffening element. The stiffening element includes a plurality of fibers and a resin for...
US20090134275 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...
US20070018042 Insulation arrangement for the internal insulation of a vehicle  
The present invention relates to an insulation structure for the internal insulation of a vehicle. The insulation structure is improved in such a way that using it a fire incursion of the flames...
US20140021297 SEALING DEVICE FOR GALLEY HARD POINT  
A sealing device for mounting a monument on a structural element of an aircraft and for providing a seal between the sealing device and the floor of the aircraft is provided. The sealing device...
US20100012773 Aircrft Structure  
An aircraft structure is provided. The aircraft structure for an aircraft includes a fuselage, front wings, rear delta wings, vertical winglets, and three levels. The fuselage has a cross-section...
US20070114331 Helicopter collapsible deck  
A helicopter collapsible deck having at least one longitudinal member and at least one cross member, which extend respectively in a first and second direction intersecting at a point; the cross...
US20120286091 Composite Aircraft Joint  
A method and apparatus comprises a first number of layers of a composite material for a wing, a second number of layers of the composite material for the wing, and a metal layer located between...
US20100025529 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,...
US20130264421 Hat Stiffeners With Canted Webs and Method of Forming the Same  
In an embodiment of the disclosure, there is provided a hat stiffener. The hat stiffener has a cap. The hat stiffener further has a first web and a second web extending from opposite ends of the...
US20120286090 CONNECTION OF A FUSELAGE TO AN AIRCRAFT WING  
A wing box rib (13), joining an aircraft wing (3) to the wing box and to the rest of the structure, extends advantageously over an adjacent part of the fuselage (2), having in particular an upper...
US20110180663 METHOD AND A DEVICE FOR DRAINING A TANK, AND A TANK AND AN AIRCRAFT FITTED WITH SUCH A DEVICE  
The present invention relates to a method of draining a tank (2) having a plate (12) presenting an inside face (12′) and an outside face (12″) opposite from the inside face (12′), said plate (12)...
US20100127125 METAL SHEETS AND PLATES HAVING FRICTION-REDUCING TEXTURED SURFACES AND METHODS OF MANUFACTURING SAME  
Metal sheets and plates having friction-reducing textured surfaces and methods of manufacturing these metal sheets and plates are disclosed herein. In an embodiment, there is provided a...
US20130334366 FORMATION OF A SHAPED FIBER WITH SIMULTANEOUS MATRIX APPLICATION  
A coated fiber for a composite article may include a fiber body and a matrix layer. The fiber body may have at least one fiber surface. The matrix layer may at least partially coat the fiber...
US20100170985 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...
US20070152099 Onboard modular optronic system  
The present invention relates to a modular optronics system onboard a carrier, such as a combat aircraft, a helicopter or a drone. The system as claimed in the invention comprises at least one...
US20070120013 AIRCRAFT COMPONENT MANUFACTURING TOOL AND METHOD  
A creep forming tool modifies the shape of an aircraft component in the form of a wing skin portion. The tool includes a shaped surface defined by removable rib boards. The component is forced...
US20070029443 Cover for an aircraft structure  
The invention relates to nose parts of the fairing of vertical and horizontal tails and wings of an aircraft with a skin and a support structure, the skin (2) being disposed on the support...
US20120132743 AIRCRAFT LIFTING SURFACE SKIN  
A mult-rib box-shaped aeronautical structure comprising upper and lower skins (19, 21) stiffened by span wise stringers (25, 25′, 25″), span wise front and rear spars (11, 13) and chord wise ribs...
US20100264266 METAL-COATED FABRICS FOR FIBER-METAL LAMINATES  
Disclosed herein are laminates that include a layer containing a metal-coated fabric. The laminate may also include a layer or layers of an organic polymeric matrix composite. In accordance with...
US20120292448 METHOD FOR FORMING A STRUCTURAL COMPONENT OF AN AIRCRAFT OR SPACECRAFT, AND FORMING DEVICE  
In a method for forming a structural component of an aircraft or spacecraft a preform comprising at least one band is formed by means of braiding around a core. A severing cut is introduced at...
US20120126060 METHOD OF FABRICATING AN AIRCRAFT PART BY INFUSING RESIN  
The method of fabricating an aircraft part comprises the steps of placing in a stack comprising a preform at least one layer of a material that presents permeability to a predetermined resin that...
US20140001310 DAMPING MECHANICAL LINKAGE  
A mechanical linkage includes first and second end members and a pair of generally parallel arcuate beams, interconnecting the end members and defining a lateral space therebetween. A plurality of...
US20090294589 METHODS AND APPARATUS FOR AN INTEGRATED AERODYNAMIC PANEL  
An integrated aerodynamic panel—e.g., for a trailing edge or leading edge of an aircraft aerodynamic surface—includes a first panel region defining inner and outer mold lines, and a second panel...
US20100270429 EQUIPMENT ELEMENT WITH RETRACTABLE LINE  
An equipment element for transportation means, in particular an airplane, includes, but is not limited to a retractable line, the length of which can be set using a retraction mechanism.
US20110315820 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...
US20150191238 INTEGRATED HEAT EXCHANGER  
The invention relates to an integrated heat exchanger in a composite fibre reinforced polymer material, more preferably to a structural integrated heat exchanger which may be used for replacement...
US20100102168 OFFSET ATTACHMENT BOSS FOR RIBBED STRUCTURES  
An offset attachment boss for ribbed structure and aircraft components. The ribbed structure including a first plurality of rib members and a second plurality of rib members configured to define a...

Matches 1 - 50 out of 64 1 2 >