71818 ⎘
Fuselages; Constructional features common to fuselages, wings, stabilising surfaces and the like; Frames; Stringers; Longerons ; Fuselage sections Stringers; Longerons
TEMPERATURE SENSING ASSEMBLY AND FIRE DETECTION SYSTEM FOR AN AIRCRAFT
#2STRUCTURAL COMPONENT, METHOD FOR MANUFACTURING A STRUCTURAL COMPONENT AND AIRCRAFT
#3Clamp Holder For Attaching Components To Structural Components Of A Vehicle
#4INTEGRATED STRINGER PANEL AND METHOD OF MAKING THEREOF
#5ELONGATE AIRCRAFT STRUCTURAL COMPONENT AND METHOD OF FABRICATING AN ELONGATE AIRCRAFT STRUCTURAL COMPONENT
#6AIRCRAFT FUSELAGE WING ATTACHMENT CUTOUT CONFIGURATIONS INCORPORATING PERIMETER BOX BEAMS
#7STIFFENING STRUCTURE AND METHOD FOR STIFFENING A SHEET ELEMENT
#8METHOD FOR THE MANUFACTURE OF A STRUCTURAL COMPONENT IN COMPOSITE MATERIAL REINFORCED WITH STIFFENING STRINGERS AND STRUCTURAL COMPONENT
#9SYSTEM AND METHOD FOR FORMING A COMPOSITE STIFFENER
#10METHOD FOR PRODUCING A FUSELAGE STRUCTURAL COMPONENT FOR A TRIANGLE REGION, AND INTEGRAL FUSELAGE STRUCTURAL COMPONENT
#11METHOD OF FORMING A REINFORCED PANEL COMPONENT AND A RELATED APPARATUS
#12SUPPORT DEVICE AND SUPPORT METHOD
#13AIRCRAFT STRUCTURAL COMPONENT AND A METHOD OF FABRICATING AN AIRCRAFT STRUCTURAL COMPONENT
#14METHOD FOR MANUFACTURING STRINGERS FOR AIRCRAFT AND STRINGER OBTAINED BY SAID METHOD
#15FLOOR ARRANGEMENT IN AN AIRCRAFT
#16METHOD AND DEVICE FOR MANUFACTURING A STRUCTURAL ELEMENT IN COMPOSITE MATERIAL WITH A Z-SHAPED PROFILE
#17SYSTEMS AND METHODS FOR ASSEMBLING STIFFENED COMPOSITE STRUCTURES
#18LIQUID RETENTION DEVICE FOR EQUIPMENT CARRIED BY A VEHICLE
#19MANUFACTURING METHOD OF A STIFFENED PANEL WITH OPEN-SECTION STRINGERS FOR AERONAUTICAL APPLICATION
#20STIFFENER INTEGRATION IN AN ISOGRID STRUCTURE
#21METHOD AND SYSTEMS USING INDEPENDENTLY CONTROLLED PALLETS FOR FABRICATING COMPOSITE STRINGERS
#22Duct stringers having ovaloid vents for aircraft wing boxes
#23Methods and devices for supporting of variety of different pre-cured composite stringers
#24Method and apparatus for fabricating reformable stiffening elements
#25VEHICLE HEAT EXCHANGER SYSTEM
#26IMPROVED STIFFENING STRUCTURE INTENDED TO STIFFEN A COMPONENT MADE OF THERMOSETTING COMPOSITE MATERIAL, AND ASSOCIATED STIFFENING METHOD
#27PROCESS FOR MANUFACTURING A STRUCTURAL COMPONENT IN COMPOSITE MATERIAL STIFFENED WITH AT LEAST ONE STRINGER
#28Method of manufacturing an assembly having a nominal thickness skin panel
#29Composite Assembly For Unhardened Fuselage Components
#30Utilizing a customizable fuselage assembly for an unmanned aerial vehicle
#31Bulb stiffener with sinusoidal web
#32Hat-stringer assemblies for an aircraft and methods of forming same
#33Vented hat stringers and methods of forming the same
#34Method for the assembly of frames in an aircraft shell
#35Aircraft
#36COMPOSITE STRUCTURE AND METHOD OF MANUFACTURING SAME
#37Fuselage barrel assemblies and methods of assembling fuselage barrel assemblies
#38Assembly and method connecting an aircraft wing aft spar root to an aircraft body fuselage
#39Structures and methods for repairing composite members
#40Fuselage structure of an aircraft and method for manufacturing the same
#41Composite structures containing finite length tapes and methods for manufacturing and using the same
#42Connector for a structurally integrated line system
#43Keel beam assembly for an aircraft
#44Method and apparatus for producing at least part of a structural frame of a vehicle
#45Composite structure and method of forming
#46Continuous manufacturing process for composite parts
#47Demolding
#48Aircraft with rear spar integration assemblies and methods of manufacturing thereof
#49JOINT STRUCTURE AND ASSEMBLY METHOD FOR SAME
#50Method and apparatus for fabricating reformable stiffening elements
#51Composite assembly for unhardened fuselage components
#52System and method for securing a structural member to a wing and a fuselage of an aircraft
#53Aircraft fuselage longitudinal splice for joining half barrel fuselage sections and other spliced fuselage sections
#54Method and device for molding laminate
#55METHOD FOR PRODUCING A TORSION BOX FOR A STRUCTURE OF AN AIRPLANE AND A TORSION BOX FOR A STRUCTURE OF AN AIRPLANE
#56Tool and method for forming contoured composite stringers having reduced wrinkling
#57Bladder mandrel package
#58Composite fabric hat stringers having interleafed tape plies
#59Aircraft panel assembly
#60Reinforcement structure and process for reinforcement of a panel element
#61Aerial vehicle airframe design and manufacturing
#62Automated system and method for preparing a mandrel for use in composite stringer manufacturing
#63Operator-assisted system and method for preparing a bladder for use in composite stringer manufacturing
#64Modular container transport systems
#65Connector and method for connecting a frame and a stringer of a fuselage structure of an aircraft, fuselage structure and aircraft
#66Stringer assemblies and methods of forming thereof
#67Composite stringer assembly and methods for transmitting a load through a composite stringer assembly
#68Pressure bulkhead assembly support tool
#69Pressurized monocoque structure with abrupt change in shape
#70Aircraft tail assembly
#71Monolithic wing to side body upper chord assembly for aircraft
#72Pivot fittings back up beam architecture
#73Composite-material aircraft part and method of manufacturing same
#74COMPOSITE MATERIAL AND METHOD OF SHAPING COMPOSITE MATERIAL
#75Method and systems using independently controlled pallets for fabricating composite stringers
#76Assembly tool for fuselage structure splice
#77Fuselage structure splice
#78Methods and devices for supporting of variety of different pre-cured composite stringers
#79Methods and systems for forming curved composite charges for stringers
#80Methods for fabricating solid laminate stringers on a composite panel
#81Stringer and associated composite structure and method for reinforcing a base structure
#82System and method for mounting items to an aircraft floor
#83Composite-material aircraft part and method of manufacturing same
#84Method and apparatus for fabricating reformable stiffening elements
#85Method and apparatus for forming a composite fuselage structure
#86Compression chord for a fuselage
#87Caul plate for irregular surface
#88Shape holding fixture and method for manufacturing aircraft panel
#89Composite structure having a variable gage and methods for forming a composite structure having a variable gage
#90Bulb stiffener with sinusoidal web
#91Fuselage assembly for an aircraft
#92Stringers for aircraft skin structures and related methods
#93Continuous manufacturing process for composite parts
#94Lattice reinforced radius filler
#95Structured panel with non-parallel cavity walls
#96Pressure bulkhead
#97Pressure bulkhead system, pressure bulkhead assembly support tool, and method for assembling a pressure bulkhead system
#98Frame component and method for producing a frame component, frame and fuselage structure for an aircraft
#99Permeable radius filler for composite structure
#100Aircraft flooring and methods of manufacturing the same
#101Modular fuselage assemblies for aircraft, aircraft including modular fuselage assemblies, and MEl'hods of assembling modular fuselage assemblies
#102Method of forming a reinforced panel component
#103Splice fittings that are affixed to stringers via web-installed fasteners
#104Composite stringer and methods for forming a composite stringer
#105Composite stringer and methods for forming a composite stringer
#106Composite structure having a variable gage and methods for forming a composite structure having a variable gage
#107Composite structure having a variable gage and methods for forming a composite structure having a variable gage
#108Composite stringer and methods for forming a composite stringer
#109Composite structure having a variable gage and methods for forming a composite structure having a variable gage
#110Polymeric stiffened sheet-like component and process for producing the same
#111Moisture control systems and methods for controlling moisture in an aircraft
#112Solid laminate stringer
#113Contoured composite stringers
#114Bladder mandrel package
#115STRUCTURES MADE VIA ADDITIVE MANUFACTURING HAVING MULTIPLE LOAD PATHS
#116Aircraft fuselage structure having a grid-stiffened panel
#117FRAME ASSEMBLY FOR A REAR SECTION OF AN AIRCRAFT AND REAR SECTION OF AN AIRCRAFT COMPRISING SAID FRAME ASSEMBLY
#118Stringer plug
#119BULKHEAD JOINT ASSEMBLY
#120Frame for fuselage shells of an aircraft and fuselage shell
#121Method for assembling an aircraft fuselage section from two superposed upper and lower parts, multipurpose mounting support, gear and fuselage section production unit for implementing said method
#122Forming contoured elongate composite structures
#123Elongate structures, structural assemblies with elongate structures, and methods for supporting a structural load
#124Expandable tooling systems and methods
#125Methods for manufacturing elongated structural elements of composite material
#126Method for manufacturing a rear section of an aircraft and aircraft rear section manufactured by said method
#127Aircraft stringers having CFRP material reinforced flanges
#128Fuselage structure for an aircraft
#129Methods for forming a composite blade stiffener and facilitating application of barely visible impact damage treatments
#130Methods of manufacturing a panel having a composite stringer for a vehicle
#131Method for forming a composite structure
#132Fuselage assembly for an aircraft
#133PANEL STRUCTURE OF OPTIMALLY CONSTRUCTED AND SUBSEQUENTLY INTEGRATED COMPONENTS AND METHOD OF MAKING SAME
#134Stringer transition through a common base charge
#135Mechanical support tooling and/or mandrel for composite part curing
#136Solid laminate stringer
#137Preform, framework part, and method for producing such a preform
#138AIRCRAFT PANEL AND METHOD OF CONSTRUCTING
#139METHOD FOR REPAIRING A COMPOSITE STRINGER WITH A COMPOSITE REPAIR CAP
#140Stiffener for an aircraft assembly
#141Adjustable Fuselage Location Joint Method
#142Aircraft rear fuselage section and manufacturing method thereof
#143Adaptive mounting bracket assembly
#144Systems and methods for making composite structures
#145Aircraft fuselage assembling jig and method of using the same
#146Aircraft framework assembly, aircraft structural framework and aircraft with an aircraft structural framework
#147Stiffened-cavity for modular wrap ply assembly for hat stringer
#148Method for making a hat stiffener pre-form with under-cut chamfered flange
#149Wing-fuselage integrated airframe beams for tiltrotor aircraft
#150Panel assembly including stringer and reinforcement elements
#151Stringer stiffened composite panels having improved pull-off strength
#152Pressure bulkhead system
#153Panel structure and associated method
#154Stringer with plank ply and skin construction for aircraft
#155Low stress stiffener runout in Pi bonded structure
#156Systems and methods for composite radius fillers
#157Clamping system for holding a composite charge during forming over a forming mandrel
#158Apparatus, systems, and methods for automated part installation
#159Camera assisted robotic system for locating the end of a fastener extending through an aircraft part during manufacture thereof
#160METHOD AND APPARATUS FOR FORMING A COMPOSITE SKIN-STIFFENER ASSEMBLY
#161Modular container transport systems
#162Boundary layer ingestion integration into aft fuselage
#163Aircraft with an airframe and at least one electrically powered thrust producing unit
#164Stringer-frame intersection of aircraft body
#165Elongated structures and related assemblies
#166Assembly body manufacturing device and assembly body manufacturing method
#167Aircraft assembly comprising a self-stiffened panel assembled with a structural element by means of an alternation of terminal ribs and terminal tabs
#168Aircraft assembly comprising a self-stiffened panel comprising a portion of increasing height by means of which the panel is fixed to a structural element
#169Method of making joint for structure
#170Isogrid stiffening elements
#171Methods for forming a composite blade stiffener and facilitating application of barely visible impact damage treatments
#172Process for handling, installing, compacting, splicing, and/or assembling composite stringers
#173Open-channel stiffener
#174Aircraft wings and aircraft including such aircraft wings
#175Rotary wing aircraft with a fuselage that comprises at least one structural stiffened panel
#176Aircraft with a fuselage and a composite tail boom
#177Window frame system, window frame attachment system and vehicle hull window frame attachment system
#178METHOD FOR JOINING SKIN PORTIONS OF A CIRCUMFERENTIALLY CLOSED FUSELAGE
#179Particulate prepreg forming aid
#180Structure having joined unitary structures
#181Tab-and-slot frame members with a stringer
#182COMPOSITE STRUCTURES WITH STIFFENERS AND METHOD OF MAKING THE SAME
#183Composite filler
#184COMPOSITE STRUCTURE, AIRCRAFT, AND DESIGN METHOD FOR CORNER FILLET PART
#185AIRFRAME COMPONENT AND METHODS FOR MANUFACTURING AN AIRFRAME COMPONENT
#186Radially extending composite structures
#187Disbond resistant composite stiffener runout
#1882-stage extrusion apparatus and method of extrusion
#189Extrusion apparatus and method using variable extrusion gate
#190Pressure bulkhead
#191System for holding a forward pressure bulkhead via non-parallel rods attached to the floor
#192Metrology Assisted Part Forming System and Method
#193Aircraft side of body joint
#194Pressure bulkhead for an aircraft fuselage
#195Composite filler
#196System and method for interconnecting composite structures
#197Aircraft engine pylon
#198Composite stiffener with integral conductive element
#199Elongated structures and related assemblies
#200Systems and methods for composite radius fillers
#201Methods for manufacturing an I-stringer of an aircraft and devices for use in such methods
#202METHOD FOR JOINING THERMOSET COMPONENTS
#203Systems and methods for making composite structures
#204Fuselage structure and method for manufacturing a fuselage structure
#205Aircraft external part with inflatable panels
#206Aircraft strength testing apparatus and aircraft strength testing method
#207Aircraft structural component that is adapted for absorbing and transmitting forces in an aircraft
#208Apparatuses and methods for flexurally controlling elongated structures
#209Method and apparatus for producing a component by use of a vacuum film
#210Stiffening element and reinforced structure
#211Method and device for series production of components made of a fiber-reinforced composite material
#212Manufacturing method of reinforcing structure
#213Manufacturing method of reinforced structure
#214SINGLE-PIECE STRINGER FOR AERONAUTIC STRUCTURE
#215Stringer alignment tool
#216Structural component
#217Method for connecting fiber-reinforced structural components
#218FUSELAGE SECTION AND TRANSVERSE BUTT JOINT CONNECTING TWO FUSELAGE SECTIONS OF AN AIRCRAFT OR SPACECRAFT
#219AIRCRAFT ADAPTED FOR TRANSPORTING CARGO
#220Lightweight structural panel
#221Crown cabin configuration for an aircraft
#222Apparatuses and methods for creating layered tape composite structures
#223Laminate composite wing structures
#224Joint assembly and method connecting an aircraft belly fairing to the fuselage provided with a particularly positioned stringer
#225Compacting uncured composite members on contoured mandrel surfaces
#226Composite Blade Stringer Edge Protection and Visual Damage Indication
#227Splice assembly for joining structural components
#228Injection molding method for the manufacture of a primary-structure connection element
#229AIRCRAFT STRUCTURE HAVING CABLES LOCATED IN STRINGERS
#230Structural component and method for producing a structural component
#231Panel structure and associated method
#232Assembly having individual components made of a fibre-reinforced composite material
#233Methods for manufacturing elongated structural elements of composite material
#234Process and apparatus for handling, installing, compacting, splicing, and/or assembling composite stringers
#235Composite structural member
#236Aircraft structure
#237Low stress stiffener runout in Pi bonded structure
#238Aircraft structural component
#239Elongated structures and related assemblies
#240Aircraft fuselage stiffener formed from a sheet folded over onto itself
#241Lattice reinforced radius filler
#242Composite structure for an aircraft and manufacturing method thereof
#243Method for manufacturing a load bearing structure and such a load bearing structure
#244Integrated lamination process for manufacturing a shell element
#245Methods for manufacturing an i-stringer of an aircraft and devices for use in such methods
#246LAMINATED I-BLADE STRINGER
#247Apparatus and method for stiffeners
#248Subfloor structure with an integral hull for a rotary wing aircraft
#249Aircraft structure made of composite material
#250Manufacturing method for a stiffener element
#251Disbond resistant composite stiffener runout
#252Method of manufacturing T-shaped stringer with a rounded web end
#253Self-stiffened composite panel and method of producing same
#254Continuous preform device for composite stringer
#255Pressure bulkhead for an aircraft and device as well as method for manufacturing an aircraft structural component
#256Rotary wing aircraft airframe
#257Laminated composite radius filler with geometric shaped filler element and method of forming the same
#258Device and method of manufacturing omega stringers
#259Method and device for compacting and consolidating a thick composite panel having a thermoplastic matrix
#260Pre-formed thermoplastic filler for thermoset structure
#261Structural element for an aircraft fuselage that prevents lateral-torsional buckling
#262Methods for treating aircraft structures
#263Composite stringer beam joint structure of an aircraft
#264Aircraft fuselage frame element integrating tabs for the fastening of stiffeners
#265LINKING AN AIRCRAFT FUSELAGE MEMBER AND A FRAME BY A CLIP AND A SPACER
#266Composite hat stiffener
#267Aircraft comprising an improved connection zone between a front beam and a front lower fuselage section
#268System and method for mounting aircraft system components in the crown area of an aircraft
#269Apparatus for fabricating highly contoured composite stiffeners with reduced wrinkling
#270Compacting uncured composite members on contoured mandrel surfaces
#271Composite hat stiffener, composite hat-stiffened pressure webs, and methods of making the same
#272Transfer system and method for applying a film material to an elongate member
#273System and method for interconnecting composite structures
#274Composite laminate including beta-reinforcing fibers
#275Aircraft structure
#276Aircraft frame
#277Joining process for the cohesive connection, in sections, of at least two components
#278Processes to fabricate composite tubular-reinforced panels integrating skin and stringers and the panels thereby fabricated
#279Composite tubular-reinforced integrated structural panels with mutually intersecting stiffeners and fabrication processes
#280Reinforced stringer and method of manufacture thereof
#281Aircraft structure with integrated reinforcing elements
#282Self-stiffened skin for aircraft fuselage including stringers with a closed section and associated manufacturing method
#283Fiber-reinforced composite material
#284Method for the production of a connecting element, connecting element, and aircraft or spacecraft
#285Vertically integrated stringers
#286High pulloff capability hat stringer
#287Stringer made of composite material with an elastic run-out and method of manufacturing same
#288Circumference splice for joining shell structures
#289Structural component
#290Laminated composite bending and stiffening members with reinforcement by inter-laminar metal sheets
#291Composite hat stiffener, composite hat-stiffened pressure webs, and methods of making the same
#292Methods and apparatus for reducing noise in reinforced skin structures
#293Skin-stiffener transition assembly, method of manufacture and application of said skin-stiffener transition assembly
#294SECURING PLATE AND AIRCRAFT STRUCTURE
#295Reinforced stiffeners and method for making the same
#296Composite, aircraft or spacecraft, and method
#297Disbond resistant composite stiffener runout
#298Method of forming a reinforced foam-filled composite stringer
#299Hat stiffeners with canted webs
#300Composite material structure, and aircraft wing and aircraft fuselage provided therewith