71819 ⎘
Fuselages; Constructional features common to fuselages, wings, stabilising surfaces and the like; Frames; Stringers; Longerons ; Fuselage sections Spars
Vibration isolation systems for compound helicopters
#2AIRCRAFT WING ASSEMBLY
#3System, apparatus, and method of manufacture for a rib structure
#4Method of manufacturing an assembly having a nominal thickness skin panel
#5Convertible aircraft system
#6Aircraft empennage with a horizontal stabilizer interfacing at the vertical stabilizer root
#7Aircraft keel beam assembly
#8Aircraft with rear spar integration assemblies and methods of manufacturing thereof
#9Freighter configuration for aircraft with composite wings
#10Fabrication of multi-segment spars
#11VTOL tilting fuselage winged frame multirotor aircraft
#12METHOD FOR PRODUCING A TORSION BOX FOR A STRUCTURE OF AN AIRPLANE AND A TORSION BOX FOR A STRUCTURE OF AN AIRPLANE
#13Aircraft panel assembly
#14Vibration isolation systems for compound helicopters
#15Aerial vehicle airframe design and manufacturing
#16COMPOSITE MATERIAL AND METHOD OF SHAPING COMPOSITE MATERIAL
#17Modular tooling for multi-spar torsion box
#18Arched horizontal pressure deck to rear spar gutter
#19Method and system for joining structures
#20Composite structural elements
#21FRAME ASSEMBLY FOR A REAR SECTION OF AN AIRCRAFT AND REAR SECTION OF AN AIRCRAFT COMPRISING SAID FRAME ASSEMBLY
#22AIRCRAFT COMPONENT
#23Methods for manufacturing elongated structural elements of composite material
#24Aerofoil body with integral curved spar-cover
#25Stiffened beam assembly
#26Energy dispersion plug for UAV
#27Aircraft framework assembly, aircraft structural framework and aircraft with an aircraft structural framework
#28Box structural arrangement for an aircraft and manufacturing method thereof
#29FORMERS FOR AIRCRAFT FUSELAGE
#30Method and system for joining structures
#31AIRCRAFT STABILIZER LEADING EDGE INTEGRATION WITH TORSION BOX AND FUSELAGE
#32Particulate prepreg forming aid
#33Aerofoil body with integral curved spar-cover
#34Tandem rigid rotor system and method
#35Stiffened beam assembly
#36Aircraft fuselage section incorporating a dynamic harness
#37Systems for shape memory alloy structures
#38Fuselage structure and method for manufacturing a fuselage structure
#39Apparatuses and methods for flexurally controlling elongated structures
#40Apparatuses and methods for creating layered tape composite structures
#41Methods and systems for shape memory alloy structures
#42Methods for manufacturing elongated structural elements of composite material
#43Multi-role aircraft with interchangeable mission modules
#44Aircraft structure
#45Part of a fuselage of an aircraft and aircraft comprising a keel beam and an aft lower shell
#46Aircraft structure
#47Propulsion system for aircraft, in particular lightweight aircraft
#48Method and device for compacting and consolidating a thick composite panel having a thermoplastic matrix
#49Methods for treating aircraft structures
#50Aircraft wing
#51Multi-role aircraft with interchangeable mission modules
#52High-wing-aircraft fuselage support structure
#53Aircraft support structure
#54Aircraft front landing gear and method of operating the same
#55Aircraft main landing gear and method of operating the same
#56Aircraft fuselage
#57Aircraft wing flap device and method of operating the same
#58Vertically integrated stringers
#59Laminated composite bending and stiffening members with reinforcement by inter-laminar metal sheets
#60Reinforced stiffeners and method for making the same
#61Keel beam of an aircraft
#62Beam
#63Reducing risk of disbonding in areas of differing strain
#64Boron fiber reinforced structural components
#65Floor for an aircraft cargo compartment and method for the assembly thereof
#66REINFORCEMENT BEAM AS WELL AS METHOD AND FIBER LAMINATE FOR MANUFACTURING THE REINFORCEMENT BEAM
#67Fuselage cell structure for an aircraft in hybrid design
#68Attachment system of aircraft components
#69Structural component of an aircraft or spacecraft and a fuselage component arrangement of an aircraft or spacecraft
#70Structural element for reinforcing a fuselage of an aircraft
#71Impact resistant and damage tolerant aircraft fuselage
#72Method of manufacturing spars, longerons and fuselage beams having a variable H cross-section
#73Composite laminate structure
#74CROSS-BEAM AND AN AIRCRAFT WITH CROSS-BEAMS OF THIS TYPE
#75Energy absorbing impact band
#76JOINING OF STRUCTURAL AIRCRAFT ELEMENTS
#77Multi-functional aircraft structures
#78Aeropspace structure including composite beam chord clamped between reinforcement plates
#79Joint arrangement for composite-material structural members
#80Profile comprising at least one hollow profile section
#81Elongate composite structural members and improvements therein
#82CARGO AIRCRAFT
#83Rib post
#84Mandrel for autoclave curing applications
#85Reinforced stiffeners and method for making the same
#86Method of locally reinforcing a composite element and reinforced aircraft wing structure central box section
#87METHODS FOR FUEL-EFFICIENT TRANSPORTATION OF CARGO BY AIRCRAFT
#88Reinforcement beam as well as method and fiber laminate for manufacturing the reinforcement beam
#89Cargo aircraft
#90Composite aircraft component
#91Energy absorbing impact band and method
#92Integrated multispar torsion box of composite material
#93Trussed Structure
#94Composite internal beam for reinforcing the structure of an aircraft
#95Aircraft component
#96Composite anti-crash structure with lateral retention, for an aircraft
#97Composite anti-crash structure with controlled buckling for an aircraft
#98Aircraft with palletized functional units
#99Cargo deck and a method for assembling said deck
#100Composite beam with corrugated web
#101Composite structural member having an undulating web and method for forming same
#102Cargo deck for receiving a load in the cargo compartment of an aircraft
#103Composite structural member having an undulating web and method for forming the same
#104Floor for an aircraft cargo compartment and method for the assembly thereof
#105Cargo aircraft
#106Transformable airplane
#107Rudder unit connection to a fuselage without a bolt-fairing structure
#108Formation of complex composite structures using laminate templates
#109Stringer flange extending to composite skin edge