Matches 1 - 17 out of 17


Match Document Document Title
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...
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...
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...
US20160167766 TRACK CONTAINER  
The present invention relates to a track container for receiving the track of a lift device actuator. The track container is elastically deformable from a rest position to a deflected position to...
US20090173827 METHOD AND APPARATUS FOR MONITORING THE INTEGRITY OF COMPONENTS AND STRUCTURES  
A method for monitoring the integrity of a permeable structure that is disposed in an environment containing a fluid at ambient pressure is provided. At least one cavity is formed in or on 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...
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...
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...
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...
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...
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....
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...
US20060071124 Reinforced structural assembly having a lap joint and method for forming the same  
Reinforced structural assemblies and methods for forming such assemblies are disclosed. In one embodiment, a reinforced structural assembly includes an engagement portion having at least one...
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...
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...
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...
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...

Matches 1 - 17 out of 17