Matches 1 - 50 out of 69 1 2 >


Match Document Document Title
US20140117149 Tetra-Propeller Aircraft  
Described herein is a vertical take-off and landing aircraft comprising: an upper enclosure comprising a first upper arm and a second upper arm; a lower enclosure comprising a first lower arm and...
US20140001311 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....
US20140175226 Avionics cargo hold module having an upper integrated floor  
An integral avionics bay module. The module has a structure that has an integral cabin floor on top that closes the structure. Installing such an integral avionics bay structure in a single...
US20140175225 AIRCRAFT COCKPIT HAVING A LOWERED FLOOR FOR WALKING ON  
A cockpit for an aircraft nose, the cockpit having a floor that acts solely as a floor for the crew to walk on and that is lower than the height of the cabin floor situated behind the cockpit. The...
US20110036946 AIRCRAFT FLOOR MODULE, STRUCTURE AND METHOD FOR ATTACHING SUCH A MODULE AND AIRCRAFT COMPRISING THEM  
A method of fitting-out of an aircraft by laying of a floor, particularly in a cockpit of an aircraft, and such a fitted-out aircraft. The aircraft includes a fuselage part defining an interior...
US20120074260 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...
US20140117157 Circumference Splice for Joining Shell Structures  
The disclosed shell structure splice and method may include a first panel having a first edge, a second panel having a second edge, the second edge being positioned in edgewise alignment with the...
US20110180665 AIRCRAFT FUSELAGE ELEMENT  
The invention relates to an aircraft fuselage element. According to the invention, -said fuselage element being a one-piece component, it comprises a closed wall (1) defining an internal volume,...
US20140175224 AIRCRAFT NOSE WITH COCKPIT AND AVIONICS BAY MODULES INTEGRATED THEREIN  
An aircraft nose comprising a primary fuselage structure, and housed inside said structure, a cockpit, and an avionics bay containing a plurality of avionics racks designed to receive electrical...
US20150108273 MODULAR AIRCRAFT FLOOR TRACK ADAPTER SYSTEM  
A modular floor track adapter system including a plurality of adapter plates laterally sized to span existing aircraft floor beams, each of the plurality of adapter plates shaped to interlock with...
US20070194175 Airplane floor assembly  
The invention relates to airplane floor assemblies and to methods for their assembly. In one embodiment, an airplane comprises at least one fuselage section and at least one floor section. At...
US20120223187 DIAMOND SHAPED WINDOW FOR COMPOSITE AND/OR METALLIC AIRFRAME  
An aircraft fuselage may include a barrel section having a side region. The fuselage may include a first cutout and a second cutout formed in the side region in side-by-side relation to one...
US20140151504 Aircraft fuselage structure and method  
An aircraft fuselage structure having a first fuselage barrel section and a second fuselage section barrel which are joined by tension fasteners extending through frame holes. A shank diameter of...
US20090250554 SELF-SUPPORTING CABIN STRUCTURE  
A cabin structural unit for attaching cabin installation elements is provided for an aircraft. The cabin structural unit is set up in such a way that a cabin installation element is attachable....
US20100320322 TRANSVERSE BUTT CONNECTION BETWEEN TWO FUSELAGE SECTIONS  
The invention relates to a transverse butt connection (1, 24) between two fuselage sections (2, 3, 25, 26), more particularly for creating a fuselage cell for an aircraft, with a number of...
US20120104167 FUSELAGE ELEMENT COMPRISING A FUSELAGE SEGMENT AND JUNCTION MEANS, FUSELAGE PORTION, FUSELAGE AND AIRCRAFT  
The invention relates to a fuselage element (1) comprising a first fuselage segment (2a) comprising a skin (3a), and junction means (4) for connecting the first segment (2a) to a second adjacent...
US20150034765 REAR FUSELAGE SECTION OF AN AIRCRAFT  
A rear fuselage section of an aircraft comprises at least one closed frame constructed as a unitary body, and a horizontal tail plane comprising a box-type central element and two lateral torsion...
US20080105785 OPTIMIZED FUSELAGE STRUCTURE  
A fuselage structure including an upper fuselage portion defined by a first cross-section including at least three different radii of curvature. The fuselage structure may also include a lower...
US20080210819 Stringers assembled at a circumferential join of an airplane fuselage  
The disclosed embodiments relates to an airplane fuselage produced by assembly, at a circumferential join, at least two sections including a skin and at least one stringer split into two elements...
US20090236473 PROVIDING SKINS FOR AIRCRAFT FUSELAGES  
An aircraft including a space frame fuselage structure. A plurality of panels are connected with the structure and configured to form a skin over the structure. The panels are movable relative to...
US20140061384 MODULAR MINIATURE UNMANNED AIRCRAFT WITH VECTORED-THRUST CONTROL  
An aircraft for unmanned aviation is described. The aircraft includes an airframe, a pair of fins attached to a rear portion of the airframe, a pair of dihedral braces attached to a bottom portion...
US20110024563 PRESSURE FUSELAGE OF AN AIRCRAFT OR SPACECRAFT WITH PRESSURE CALOTTE  
A pressure fuselage of an aircraft or a spacecraft includes at least two fuselage sections disposed longitudinally along the fuselage; at least one pressure calotte disposed in the fuselage so as...
US20080210820 AIRCRAFT FLOOR AND METHOD OF ASSEMBLY  
The invention relates to aircraft floor assemblies and to methods for their assembly. In one embodiment, an aircraft comprises at least one fuselage section and at least one floor section. At...
US20090272846 BONDED METAL FUSELAGE AND METHOD FOR MAKING THE SAME  
A bonded metal fuselage for aerospace vehicles includes a monocoque structure having an outer metal skin, metal tear straps bonded to the outer skin and metal stringers bonded to the outer skin...
US20100025531 Aircraft-fuselage assembly concept  
An aircraft fuselage section includes a first interior tube as well as a second interior tube that are produced in an upstream production step, which interior tubes are subsequently enclosed by an...
US20110168840 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...
US20100032523 AIRCRAFT FUSELAGE MADE FROM LONGITUDINAL PANELS AND METHOD OF PRODUCING SUCH A FUSELAGE  
The invention relates to an aircraft fuselage comprising a nose cone, a tail section and a central section, the central section comprising longitudinal panels assembled directly with one another,...
US20090014587 AIRCRAFT SAFETY SYSTEM  
An aircraft (10) comprising a fuselage (12) having an upper pilotable fuselage portion (10A) and a lower jettisonable fuselage portion (10B), the lower jettisonable fuselage portion (10B) being...
US20080296432 METHOD OF EXTENDING LENGTH OF AIRCRAFT TO INCREASE INTERIOR SPACE  
A method of modifying an aircraft, increasing its length, to increase interior of the aircraft fuselage to accommodate more passenger rows or more freight. The typical aircraft such as the Boeing...
US20100025532 SHELL ELEMENT AS PART OF AN AIRCRFAFT FUSELAGE  
The present invention provides a shell element as part of an aircraft fuselage, wherein the shell element is formed as a curved sheet-like element and is at least partially or completely of CRP...
US20120292435 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...
US20120132750 METHOD FOR PRODUCING AN AIRCRAFT FUSELAGE AND AIRCRAFT FUSELAGE  
Disclosed is a method for the manufacture of an aircraft fuselage with at least two fuselage barrels wherein connecting segments are firstly prepared for the formation of a transverse joint region...
US20140209743 AIRCRAFT FRAME  
An aircraft frame comprising a first partial aircraft frame configured to be attached to a first aircraft fuselage segment and a second partial aircraft frame configured to be attached to a second...
US20140077471 TRANSPORT AND ASSEMBLY SYSTEM AND METHOD FOR COMPOSITE BARREL SEGMENTS  
A barrel assembly for a composite structure includes a barrel of composite material, a first end ring, and a mid support. The barrel of composite material has a first end, an interior surface and...
US20110303791 Fuselage Section of an Aircraft and Method for the Production of the Fuselage Section  
In accordance with the method, an inside layer of a fuselage section skin made from first fibers is placed on a manufacturing surface, the first fibers being placed in one or more first fiber...
US20110089291 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...
US20120153082 SPLICE AND ASSOCIATED METHOD FOR JOINING FUSELAGE SECTIONS  
A splice and an associated method are provided in order to efficiently join structures, such as adjacent fuselage sections. A splice for joining fuselage sections may include a strap configured to...
US20080142635 Aircraft safety system  
A system for enabling the safe landing of an aircraft during an in-flight emergency is provided. The system includes a plurality of onboard devices for releasably securing a plurality of wings to...
US20100282905 SPLICING OF OMEGA-SHAPED STIFFENERS AT A CIRCUMFERENTIAL JOINT IN AN AIRCRAFT FUSELAGE  
An aircraft fuselage produced by assembling, at a circumferential joint, at least two sections, each section including a coating and at least one element of at least one stiffener, the...
US20090020646 ASSEMBLY OF PANELS OF AN AIRPLANE FUSELAGE  
An aircraft fuselage including at least two sections kept assembled at a circumferential join, each section having at least one panel. The circumferential join includes at least one inner ring,...
US20090184202 STRUCTRUAL ELEMENT MADE OF AN ALUMINUM ALLOY INCLUDING AN OPTICAL SENSOR  
Provided herein is a method for manufacturing a worked product comprising a fiber sensor therein. Also provided is a wrought product comprising a fiber sensor as well as structural elements and...
US20120318919 AIR VEHICLE MOUNTED TRANSMITTING OR RECEIVING EQUIPMENT  
Disclosed is an air vehicle mounted or mountable transmitting and/or receiving equipment including a transmitting and/or receiving turret allowing at least a forward field of view, the device...
US20100170988 SECTION OF AIRCRAFT FUSELAGE IN COMPOSITE MATERIAL WITH A CONSTANT INTERIOR PROFILE  
The disclosed embodiments concern an aircraft fuselage section made of composite material with an internal skeleton having frames that form the radial structure of the fuselage and stringers that...
US20110084166 ARRANGEMENT FOR DIVIDING A SPACE INTO A PLURALITY OF AREAS  
The invention relates to an arrangement for dividing a space into a plurality of areas, said arrangement comprising at least one frame with at least one fixing means for holding the frame in...
US20100012782 Aircraft With Modular Structure  
An aircraft includes a module carrier for accommodating a plurality of module elements in which in each case at least one system element is integrated. The module elements and system elements are...
US20150253116 LONG FIBER THERMOPLASTIC THIN-WALLED AEROSHELLS FOR MISSILE APPLICATIONS AND METHODS OF MANUFACTURE  
Aeroshells and methods for manufacturing aeroshells are provided. In this regard, a representative aeroshell for a missile formed of a long fiber thermoplastic composite exhibits a wall thickness...
US20100320321 METHOD FOR JOINING TWO FUSELAGE SECTIONS BY CREATING A TRANSVERSE BUTT JOINT AS WELL AS TRANSVERSE BUTT JOINT CONNECTION  
The invention relates to a method of connecting two fuselage sections (1, 2, 21, 22) formed by a fibre-reinforced plastics material, in particular wound fuselage sections (1, 2, 21, 22) for...
US20130292514 METHOD AND SYSTEMS FOR USE IN ASSEMBLING A FUSELAGE  
A fuselage assembly is provided. The fuselage assembly includes a first barrel section including a body that extends from a first end to a second end and a second barrel section coupled to said...
US20130256457 FUSELAGE SEGMENT AND METHOD FOR MANUFACTURING A FUSELAGE SEGMENT  
The invention pertains to a fuselage segment (2) that extends in a longitudinal fuselage segment axis (A) and is closed in a circumferential direction (U) around this longitudinal fuselage segment...
US20090026804 Floor Panel And Installation For Fixing Layout Elements Comprising Such Panels  
The disclosed embodiments concerns a floor panel for a transport vehicle such as an aircraft and an installation for fixing cabin layout elements including such panels. The disclosed embodiments...

Matches 1 - 50 out of 69 1 2 >