Matches 1 - 50 out of 68 1 2 >


Match Document Document Title
US20120119030 REINFORCEMENT BEAM AS WELL AS METHOD AND FIBER LAMINATE FOR MANUFACTURING THE REINFORCEMENT BEAM  
Disclosed is a reinforcement blank, in particular a curved ring frame segment for fuselage cells of aircraft, comprising a synthetic material that is reinforced by at least one fiber laminate. The...
US20080302912 Bladderless Mold Line Conformal Hat Stringer  
Apparatus and techniques for providing a closed hat stringer are disclosed. In one embodiment, a closed hat stringer for stiffening a composite structure includes opposing cavity walls situated...
US20150259067 MODULE FOR AN AIRCRAFT  
A module for an aircraft has a fuselage structure and a floor element defining a floor plane. The module includes a frame device adapted for mounting a functional element and the frame device is...
US20110108667 Thermoplastic Composite Window Panel for Aircraft Applications  
An aircraft trim panel structure includes a thermoplastic resinated quadraxial fiberglass lay-up prepreg first open structure skin layer having at least a 28% open area. A thermoplastic resinated...
US20080237442 MULTI-RING SYSTEM FOR FUSELAGE BARREL FORMATION  
An aircraft fuselage barrel (10) includes a skin (12) and a shear tie (18). The shear tie (18) resides within and is integrally formed with the skin (12). The shear tie (18) is separate from and...
US20080099611 Tail cone for aircraft with movable fairing and support structure for auxiliary power unit and the ancillary elements thereof  
Tail cone (2) for aircraft (1) with a cover (8) housing an auxiliary power unit (3) and the ancillary systems thereof (6,7), and the cover (8) has a fixed forward section (11) by means of which...
US20110309187 NESTED CORE GAS TURBINE ENGINE  
An aircraft, with the ability to cruise at supersonic speeds, designed to increase cruise lift/drag ratio, reduce sonic boom and have greater downward visibility by having an ‘inverted’ nose...
US20070138695 STIFFENING ELEMENT AND A METHOD FOR MANUFACTURING OF A STIFFENING ELEMENT  
The present invention relates to a stiffening element (1) and a method for manufacturing of a stiffening element (1) of composite material, which stiffening element (1) is provided for attachment...
US20070210211 Airplane body and method for manufacturing it  
The invention refers to an airplane body, in particular the fuselage, the fuselage being manufactured from a synthetic structure. The fuselage consists of at least two parts which are connected at...
US20080248772 Integrated Aviation Rf Receiver Front End and Antenna Method and Apparatus  
An aviation radio frequency receiver front end (502) and a corresponding antenna (501) are coupled together. The antenna is configured and arranged to be disposed during use in a fixed position...
US20080029644 Process for manufacturing composite material structures with collapsible tooling  
A process for manufacturing stiffened structures (11) in composite materials formed by an outer skin (13) and a plurality of stiffeners or stringers (15) the cross-section of which has a closed...
US20050224630 SUPERSONIC AIRCRAFT WITH SPIKE FOR CONTROLLING AND REDUCING SONIC BOOM  
Method and arrangement for reducing the effects of a sonic boom created by an aerospace vehicle when said vehicle is flown at supersonic speed. The method includes providing the aerospace vehicle...
US20120001023 AIRCRAFT FUSELAGE MADE OUT WITH COMPOSITE MATERIAL AND MANUFACTURING PROCESSES  
Aircraft fuselage made out with composite material and manufacturing processes. The structure of the fuselage (11) comprises a skin (13), a plurality of frames (17) positioned transversely to the...
US20090266936 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...
US20130043344 HIGH-STRENGTH AIRCRAFT INTERIOR PANEL WITH EMBEDDED INSERT  
An aircraft interior panel for supporting high-weight loads including a core panel sandwiched between structural plies, a panel insert embedded in the panel and passing through and interrupting...
US20140175223 AIRCRAFT FRONT PORTION HAVING AN IMPROVED LANDING GEAR BAY  
An aircraft front portion in which the landing gear storage bay is arranged under a cockpit floor. The landing gear bay is mechanically connected to the fuselage frames of the aircraft front...
US20120325326 Method of Reducing Resistance of Streamlined Body of A Vehicle and Its Applications  
A method of reducing resistance of streamlined body of a vehicle and its applications is provided, wherein one or more raised structures are configured between the widest point and the caudal end...
US20070023571 Quiet airplane configuration  
A blended wing aircraft reduces forward, aft, and sideline flyover noise and heat energy by reflecting it upward using the wing and vertical stabilizers positioned just outboard of the engines....
US20120267472 AIR VEHICLE  
A sensor/emitter arrangement (M1-M3) is integrated into the fuselage (120) structure of a specially designed air vehicle (100), in which the air vehicle is configured for optimizing operation of...
US20100133380 SKIN PANEL FOR AN AIRCRAFT FUSELAGE  
The invention relates to a skin panel (11) of an aircraft (1), comprising a laminate of at least one first metal sheet (40) and preferably first fiber-reinforced polymer layers (41) connected...
US20160185437 TAIL CONE OF AN AIRCRAFT  
A tail cone of an aircraft, more specifically a tail cone made of composite materials comprising an internal skin, an external skin surrounding the internal skin, longitudinal structural members...
US20090145129 SPLIT-CYCLE AIRCRAFT ENGINE  
A split-cycle aircraft engine includes a crankshaft rotatable about a crankshaft axis. A power piston is slidably received within a power cylinder and is operatively connected to the crankshaft...
US20100243806 AIRCRAFT PRESSURE BULKHEAD ASSEMBLY STRUCTURE  
The structure comprises: a rim angle (22) with a front portion and a rear portion, the latter being slanted upward and backward and connected to the bulkhead (1); a simple frame (18), being...
US20080179459 Pressure bulkhead made of composite material for an aircraft  
The present invention relates to a curved rear pressure bulkhead (1) made of a composite material, comprising three layers: an outer layer (2) and an inner layer (3) symmetrical with one another,...
US20120119415 Improvements in Aircraft Seats and Related Components  
In one aspect, an aircraft seat assembly comprises a plurality of seat skeleton parts (22-26, 36,38) held in juxtaposition with one another by means of an over-moulded polymer material (42). In...
US20170129588 Truss-Reinforced Radome Crown Structure  
A truss-reinforced radome crown structure (TRRCS) that functions in combination with an aircraft and a communication radome or antenna. The TRRCS maintains and protects a radome and antenna...
US20160107753 SEAT FASTENING SYSTEM, SEAT OR SEAT GROUP, AIRCRAFT CABIN, AND METHOD FOR FASTENING A SEAT OR A SEAT GROUP  
In order to reduce weight, simplify the mounting of a seat or a seat group, and increase the flexibility in the cabin, a seat fastening system for a seat or a seat group of an aircraft comprises...
US20100163669 Super aircraft structrue  
An aircraft structure is provided. The aircraft structure for an aircraft includes a fuselage, front wings, rear small wings, vertical winglets, and four levels. The fuselage has a cross-section...
US20060237588 Composite structural member having an undulating web and method for forming the same  
Composite structural members and methods for forming the same are disclosed. In one embodiment, a composite structural member includes a central structural portion that extends in a first...
US20170043869 PROTECTION ELEMENT AND DEVICE FOR CAMERA DRONE  
A protection element and a protection device for a camera drone are disclosed herein. The protection element is installed between a landing gear and a propeller of the camera drone and comprises a...
US20100038487 FUSELAGE STRUCTURAL COMPONENT OF AN AIRCRAFT OR SPACECRAFT, WITH A FOAM LAYER AS THERMAL INSULATION  
The present invention creates a fuselage structural component of an aircraft or spacecraft, with a non-load-bearing outer skin and a load-bearing inner framework structure, wherein a foam layer...
US20080308676 Aircraft Fuselage  
The present invention provides an aircraft fuselage which comprises a bulletproof layer in at least partial areas, an aircraft fuselage being understood as both a primary fuselage structure of an...
US20080223986 Trussed Structure  
The invention provides a trussed structure comprising a frame and at least one strut, wherein the frame is of composite material and includes sockets which are integral with the frame. The...
US20160176085 METHOD AND SYSTEM FOR PRODUCING COMPOSITE STRUCTURES  
The subject matter disclosed herein relates to a method of producing a composite structure, such as an airframe or fuselage of an aircraft. The method comprises the steps of: arranging a first...
US20130264422 Aircraft frame and method for obtaining the same  
An aircraft frame and a method for obtaining an aircraft frame, which frame is made of composite material, and which frame comprises several partitions (20) that form, when joined, the...
US20150232165 AIRCRAFT PANEL FOR AN INTERIOR OF AN AIRCRAFT AND METHOD FOR MAKING THE AIRCRAFT PANEL  
Aircraft panel 1 for an interior of an aircraft, wherein the aircraft panel 1 has a sandwich structure 2, wherein the sandwich structure 2 comprises a core section 4 and a covering section 3 as...
US20170183081 Multi-Rotor Passenger-Carrying Aircraft with Foldable Aircraft Arm  
A multi-rotor passenger-carrying aircraft with foldable aircraft arm is disclosed, including an aircraft body, a fixing mechanism, a connector and an aircraft arm. The fixing mechanism is fastened...
US20160046392 Method For Assembling An Aircraft Fuselage  
A method for assembling an aircraft fuselage includes different steps. In a first step the secondary structural components and interior components are assembled to form a core structure. The core...
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...
US20140027573 AIRCRAFT FUSELAGE STRUCTURAL ELEMENT WITH VARIABLE CROSS-SECTION  
An aircraft fuselage structural element has the general form of an elongated profile and includes a web and at least one flange. The at least one flange has a curved cross-section tangent to the...
US20160244142 FLAT KINKED REAR PRESSURE BULKHEAD  
An aircraft fuselage comprising a pressurized cabin and an unpressurized rear section separated by a rear pressure bulkhead. The bulkhead comprises flat portions forming one or more kinks between...
US20160129985 AIRCRAFT STRUCTURE HAVING CABLES LOCATED IN STRINGERS  
An aircraft structure having cables located in stringers is disclosed. According to one embodiment, the aircraft structure includes a stringer having a hollow channel. Further, one or more cables...
US20120074261 FUSELAGE ARRANGEMENT, AIRCRAFT OR SPACECRAFT AND METHOD  
The present invention provides a fuselage arrangement for an aircraft or spacecraft, comprising: a skin portion which consists substantially of fibre composite material and/or of a...
US20080283664 Aircraft Fuselage Structure  
An aircraft fuselage shell section comprises a skin (11) defining a boundary between a first air pressure and a second air pressure, and a reinforcing structure (13) connected to the skin (11)....
US20050067531 Apparatus for positioning a cable behind a fixed structure  
An apparatus for positioning a cable in a recess behind a fixed structure, e.g. a storage bin, in an aircraft. A portion of the cable is enclosed in a conduit. Panels adjacent the structure are...
US20110155850 CROSS-BEAM AND AN AIRCRAFT WITH CROSS-BEAMS OF THIS TYPE  
A cross-beam for a floor structure of an aircraft includes a web having opposing end sections configured to connect to opposing structural sections of an aircraft fuselage and at least one stepped...
US20100230538 CLOSED STRUCTURE OF COMPOSITE MATERIAL  
The invention relates to a tubular-shaped closed structure (11) of composite material comprising a skin (21) and a plurality of omega-shaped reinforcing longitudinal stringers (23), such as a...
US20100090061 FUSELAGE OF AN AIRCRAFT OR SPACECRAFT OF CRP/METAL HYBRID CONSTRUCTION WITH A METAL FRAMEWORK  
The present invention provides an inherently rigid fuselage of an aircraft or spacecraft comprising shell elements or fuselage barrels of CRP construction, wherein the shell elements or fuselage...
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....
US20140054418 DOOR FRAME CONSTRUCTION, FUSELAGE PORTION AND AIRCRAFT OR SPACECRAFT  
The present invention provides a door frame construction in particular for an aircraft or spacecraft, including a former; a fibre metal laminate which is connected to the former; and an outer skin...

Matches 1 - 50 out of 68 1 2 >