Matches 1 - 18 out of 18


Match Document Document Title
US20150175253 LEADING EDGE FOR AN AIRCRAFT LIFTING SURFACE  
An optimized leading edge for an aircraft lifting or supporting surfaces, such as wings and stabilizers, wherein the leading edge includes inboard and outboard leading edge sections that are...
US20150053818 UPPER JOINTS BETWEEN OUTBOARD WING BOXES AND WING CENTER SECTIONS OF AIRCRAFT WING ASSEMBLIES  
An upper joint of a wing assembly of an aircraft includes an outboard upper wing panel, a center upper wing panel, a rib, and an upper joint assembly operatively interconnecting the outboard upper...
US20110147521 METHOD OF CONSTRUCTING A FIXED-WING AIRCRAFT  
The following steps are performed in the method of constructing an aircraft: taking a subassembly comprising two wings that are rigidly fastened together, and fitting it to a fuselage wall; and...
US20090072088 FLYAWAY KABOBS  
An aircraft wing made of a composite material, and its method of manufacture, require a plurality of kabobs (i.e. substantially rectangular shaped hollow tubes having an open end and a closed...
US20090001218 Stifffened multispar torsion box  
The invention relates to an integrated structure of a composite material multispar torsion box (1) for aircraft, comprising a lower skin (12), an upper skin (11), several spars (9) defining cells...
US20080308669 COMPOSITE AIRCRAFT COMPONENT  
This invention relates to improving the tolerance of composite laminate structures to damage and/or delamination, resulting in weakening of the structure and/or to reducing the possibility of such...
US20070018049 Integrated wingtip extensions for jet transport aircraft and other types of aircraft  
Methods and systems for efficiently increasing the wing area of an aircraft are disclosed herein. An integrated wingtip extension configured in accordance with one embodiment of the invention...
US20130099063 Segmented Aircraft Wing Having Solar Arrays  
An aircraft wing has a plurality of wing segments mounted on a wing spar by joints that allow relative movement between the spar and the wing segments. Tuning of coefficients of thermal expansion...
US20080042011 COVER PANEL FOR AN AIRCRAFT WING AND A METHOD OF FORMING THEREOF  
The present invention relates to a wing cover panel for an aircraft wing and a method of forming such a wing cover panel, which is formed as a plurality of sections each carrying stringer sections...
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...
US20150014482 UNMANNED AERIAL VEHICLE (UAV) WITH INTER-CONNECTING WING SECTIONS  
An unmanned aerial vehicle (UAV) is described. The UAV may include a fuselage assembly and a plurality of inter-connecting wing sections. The inter-connecting wing section may include a connecting...
US20090302159 Aircraft Wing Including a Plurality of Dismountable Members  
The invention relates to an aircraft wing including two members removably connected end to end by a coupling means including: a male coupling part with spaced opposed upper and lower faces, a...
US20070023573 Aircraft wing  
An aircraft wing that may be used in large transport aircraft comprising a first wing portion that, in use, forms an inner portion of an aircraft wing, and is attached to a readily replaceable...
US20130068888 AIRFOIL STRUCTURE  
An airfoil structure including a plurality of molded monolithic members that extend in a side-by-side manner along the spanwise direction of the airfoil structure. Each molded monolithic member is...
US20130099050 AIRCRAFT WING WITH KNUCKLED RIB STRUCTURE  
An aircraft wing has hinged ribs, and a skin covering the ribs. The ribs each include plural rib sections, array from the leading edge of the wing, to the trailing edge of the wing, and a lock to...
US20130037655 METHOD OF SEALING A GAP  
A method of sealing a gap between first and second aerodynamic surfaces. The width of the gap between the two surfaces is measured to obtain a gap measurement. The width of a seal member is...
US20170043859 TRAILING EDGE COMPONENTS, AIRCRAFT STRUCTURES INCLUDING TRAILING EDGE COMPONENTS AND METHODS FOR MANUFACTURING TRAILING EDGE COMPONENTS  
Trailing edge components of aircraft structures, aircraft structures comprising such trialing edge components, and methods of manufacturing such trailing edge components are provided. In an...
US20170001707 UPPER JOINTS BETWEEN OUTBOARD WING BOXES AND WING CENTER SECTIONS OF AIRCRAFT WING ASSEMBLIES  
An upper joint of a wing assembly of an aircraft includes an outboard upper wing panel, a center upper wing panel, a rib, and an upper joint assembly operatively interconnecting the outboard upper...

Matches 1 - 18 out of 18