Matches 1 - 50 out of 275 1 2 3 4 5 6 >


Match Document Document Title
US20120234976 CEILING PANEL HAVING CURTAIN RAIL IN A TRANSPORT CABIN  
A ceiling panel is configured for attaching a curtain in a cabin of a transportation device with an attachment unit, a mounting unit, and a curtain attachment unit. The ceiling panel is configured...
US20130032669 FASTENING DEVICE PARTICULARLY SUITABLE FOR THE FASTENING BETWEEN AN AIR INTAKE AND AN ENGINE OF AN AIRCRAFT NACELLE  
An aircraft nacelle with a connecting device between a first conduit of an air intake and a second conduit of a motor, both conduits being arranged end-to-end, the connecting device including an...
US20120286094 Helicopter Cargo Basket Mounting Assembly and Method of Using Same  
A mounting assembly for mounting an external cargo basket onto a helicopter and a method of using the mounting assembly. The mounting assembly comprises a plurality of connectors—corresponding...
US20150203190 WINGLET ATTACH FITTING AND METHOD FOR ATTACHING A SPLIT WINGLET TO A WING  
A winglet attach fitting may include a wing attachment portion, an upper winglet attachment portion, and a lower winglet attachment portion. The upper winglet attachment portion may be coupled to...
US20110031349 Pinned lug joint  
A pinned lug joint comprising: a first part comprising two first lugs projecting from a bridge which extends between them; a second part pivotally coupled to the first part, the second part...
US20130043350 PRESSURE RELIEF LATCH  
The invention relates to pressure relief latch for aircraft, able to absorb vibrations and shocks without inopportune opening, as well as to adapt to dimensional stresses during its assembly. The...
US20120061518 APPARATUS AND METHOD FOR QUICKLY RELEASING A DOME IN A DOMED SATELLITE ANTENNA  
An apparatus and method for quickly releasing, without using any tools, the dome from the base of a domed satellite antenna system. An actuator moves in each of a number of quick-release fasteners...
US20110233338 JOINT  
A joint between an aircraft wing box cover and a leading/trailing edge structure, the cover and the structure having flush aerodynamic outer surfaces, wherein the structure has an integrally...
US20120160962 INSTALLATION ASSEMBLY INCLUDING A FIXATION RAIL FOR ATTACHING DEVICES IN AN AIRCRAFT  
The invention relates to a fastening assembly for the fastening of systems in an aircraft comprising frames (104), a skin (102) and connecting parts between the skin and the frames, referred to as...
US20120132756 SHELL SEGMENT FOR PRODUCING A FUSELAGE CELL SECTION FOR A FUSELAGE CELL OF AN AIRPLANE  
The invention concerns a shell segment for the purpose of manufacturing a fuselage cell section for a fuselage cell of an aeroplane, with at least one skin field and with a multiplicity of...
US20110303792 TELESCOPIC STRUT  
A telescopic strut for electrically connecting a fixed structure of an aircraft to a movable structure mounted to the fixed structure, wherein the strut is adapted to be mechanically connected to...
US20110174930 FUSE LINK DEVICE BETWEEN A MOBILE PART AND A FIXED PART OF AN AIRCRAFT NACELLE  
The object of the invention is an aircraft nacelle that comprises at least one part, called a door (14), that moves relative to a stationary part (20) and a connecting device that makes it...
US20110062286 AIRCRAFT EQUIPMENT SUPPORT  
An equipment support for attaching equipment to an aircraft comprises a gripper foot having a T-shaped slot that engages a track mounted to the aircraft floor. The gripper foot is mounted to a...
US20100301166 EXPANDABLE PRECURED JOINT FILLER  
A method of manufacturing an aircraft having adjacent spaced apart surface panels using a hollow filler within the gap between the spaced apart surface panels.
US20110198445 CONNECTION ASSEMBLY FOR AT LEAST ONE ITEM OF ELECTRONIC EQUIPMENT IN AN AIRCRAFT  
The invention relates to an assembly for connection (1; 101) of an electronic equipment item (2) to wiring of an aircraft, in which the item of electronic equipment (2) is disposed in a support...
US20110147523 PIPE COUPLING DEVICE FOR AIRCRAFT WING  
An aircraft wing comprising first and second fuel pipe segments which are coupled together with a pipe coupling device comprising a corrugated tube formed from an elastomer filled with conductive...
US20100294889 DEVICE FOR JOINING TORSION BOXES OF AIRCRAFT  
The invention relates to a device (1) for joining torsion boxes (5, 6) of aircraft structures, said structures carrying fuel therein, characterized in that the mentioned device (1) comprises three...
US20130020440 STRUCTURE FOR JOINING TORSION BOXES IN AN AIRCRAFT USING A TRIFORM FITTING MADE FROM NON-METALLIC COMPOSITE MATERIALS  
The invention comprises a triform fitting 1, essentially made from non-metallic composite materials including several strengthening cross ribs 4 for joining symmetrical flanges 3 and a...
US20110174928 JOINING ARRANGEMENT FOR THE LATERAL BOXES OF A HORIZONTAL TAIL STABILISER WITH A TUBULAR CENTRAL BOX AND MANUFACTURING METHOD FOR SAID BOX  
Joining arrangement for the lateral boxes (11, 11′) of a horizontal tail stabiliser with a central tubular box and manufacturing method for said box. The boxes (11, 11′) are joined using an...
US20090283640 ATTACHMENT SYSTEM AND METHOD  
An attachment system includes a dual sleeve nut comprising at least two spaced-apart nut housings; at least two interiorly-threaded fastener openings extending through the nut housings,...
US20120091275 Weathertight fitting for aircraft tail vertical stabiliser mounting  
Weathertight fitting (41) for the mounting of the tail vertical stabiliser of an aircraft in a rear area of its fuselage, the construction being based on a casing (5) made with a composite...
US20140084110 Wing Root Insert System for an Aircraft Family  
A single, common, fuselage and wing design of an aircraft structure provides for two different aircraft models or configurations. A fuselage (12) has a center section cutout area (212). Each wing...
US20110309194 Mounting System for Attaching a Structural Monument in a Desired Position in an Aircraft Cabin  
The invention relates to a mounting system (10) for attaching a structural monument in a desired position in an aircraft cabin comprises a support element (12) that is connectable to a base body...
US20090026318 Installation system for an airplane  
An exemplary embodiment of the present invention indicates an installation system for an airplane for securing interior equipment, which exhibits longitudinal and transverse rails. The transverse...
US20110215202 WING SPAR SPLICE JOINT  
A wing spar joint is provided for coupling the inboard ends of a right wing spar and a left wing spar. The wing spar joint comprises a forward fitting, an aft fitting, a spar cap a lower chord...
US20110168842 JOINING SYSTEM BETWEEN LININGS AND THE STRUCTURAL ELEMENTS THAT SUPPORT THEM  
The invention relates to a coupling system for use between cladding and structural elements supporting same, said cladding comprising thin sheets (3) of alloys or composite materials. The facing...
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...
US20090314894 AIRPLANE FAIRING PANEL ADJUSTABLE FITTING ASSEMBLY, KIT AND METHOD  
An airplane fairing panel adjustable fitting assembly allows for installation and removal of a fairing panel from outside the fairing. Blind retention features are provided and a pivoting link...
US20140361121 LOWER JOINTS BETWEEN OUTBOARD WING BOXES AND CENTER WING SECTIONS OF AIRCRAFT WING ASSEMBLIES  
Lower joints of aircraft wing assemblies are disclosed. In some embodiments, a lower joint includes an outboard lower wing panel, a center lower wing panel, a rib, and a lower joint assembly that...
US20120132755 AIRFRAME STRUCTURAL ELEMENT  
An airframe structural element, such as an aircraft rib, is disclosed that comprises an integral pipe connector element for connecting pipes through the structural element. The pipe connection...
US20090218445 AIRFRAME ATTACHMENT FITTING  
An airframe attachment fitting includes a fitting base having a base attachment surface and a flange attachment surface, at least one attachment post extending from the base attachment surface of...
US20100314494 ADAPTER PLATE FOR AIRPLANE STRUCTURE  
The invention is directed to an adapter plate (1) for interconnecting of a device with an airplane structure. The adapter plate (1) comprises a central beam (2) area extending in a mounted...
US20120168563 ADJUSTABLE IRON FITTING FOR THE INSTALLATION AND FITTING OF AIRCRAFT FAIRING  
It is intended for installing and fitting, in conjunction with other iron fittings, a fairing on an aircraft in correspondence with a housing located at the junction of a stabiliser and a fuselage...
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...
US20130092793 AIRCRAFT, AND FASTENING ARRANGEMENT FOR A FLOOR STRUCTURE IN AN AIRCRAFT  
An aircraft comprising includes a fuselage shell with fuselage frames, a floor structure with transverse and longitudinal beams, and a fastening arrangement for supporting the floor structure on...
US20130146712 APPARATUS FOR ATTACHMENT OF WING PANELS  
A shroud panel (60) is attached to a wing skin overhang (28) by a series of pivoting butt straps (86) to permit relative strains to occur.
US20120193475 CONNECTOR FOR STIFFENING FRAMES BETWEEN AN AIRCRAFT FUSELAGE AND A WING BOX  
The stiffening frames (14) of an aircraft fuselage (2) remain continuous while passing through an upper panel (5) of the wing box and extend over the ribs (3) situated in that box. The overall...
US20110089292 AIRCRAFT JOINT  
A method of joining a wing to an aircraft fuselage by forming a series of pinned lug joints between a fuselage side and a wing side of a wing box structure. The joint forming process includes...
US20140263836 FISH JOINT DEVICE HAVING AN IMPROVED MECHANICAL HOLD  
The invention relates to a fish joint device intended to attach securely first and second structural elements of an aircraft to one another, having two fishplates positioned either side of the...
US20140131518 JOINT FOR COMPOSITE WINGS  
A wing joint including a T-chord and a splice plate for connecting an inboard wing panel assembly and an outboard wing panel assembly. The wing panel assemblies include a stringer co-bonded or...
US20120085866 INTERCHANGEABLE JOINT CONCEPT FOR AN AIRCRAFT REAR FUSELAGE CONE  
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...
US20060043239 Method for detecting and repairing scratches and cracks proximate aircraft fuselage lap joints  
A method for detecting scratches proximate an aircraft lap joint formed where an outer skin panel overlaps an inner panel comprises trimming a portion of the outer skin panel overlapping the inner...
US20110001010 ARRANGEMENT OF TWO FUSELAGE SECTIONS OF AN AIRCRAFT AND A CONNECTING STRUCTURE FOR CONNECTING FUSELAGE SKINS  
A coupling element for connecting stringers in the process of joining two fuselage sections by means of at least one transverse splicing plate, wherein in each case the fuselage sections on the...
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...
US20090261202 Universal Retaining Device, Particularly For Fastening Panel Elements And/Or Accessory Parts In Aircraft  
A universal bracket for fastening different panel elements and/or additional devices in aircraft, comprises a base plate for fastening to a substructure, a support plate connected to the base...
US20110290941 Attachment system of aircraft components  
An attachment system for attaching a component (11) such as a vertical tail plane to a fuselage (27) of an aircraft; the component (11) being structured as a box comprising front and rear spars...
US20120223188 MOVABLE CONNECTING PLATE FOR CONNECTING TWO OVERHEAD STORAGE COMPARTMENT ELEMENTS  
A fastening device for connecting two overhead storage compartment elements of an aircraft is provided. A passenger service channel (PSC) extends in the overhead storage compartment elements which...
US20100308170 COMPOSITE JOINT PROTECTION  
The present invention relates to a joint between a laminar composite cover (12) and a second cover (15) (which may or may not be also formed from a composite material). The invention also relates...
US20090121079 LOADING FITTING  
In one embodiment, a loading fitting includes at least one of an I, a T, and a J shaped cross-section having a flange attached to at least one supporting structure. In another embodiment, a method...
US20110215203 ATTACHMENT STRUCTURE, ATTACHMENT DEVICE AND ATTACHMENT SYSTEM FOR ATTACHMENT OF A FINISHING COMPONENT IN AN AIRCRAFT  
An attachment device for attaching an equipment component in an aircraft, comprising a second attachment element for attaching an equipment component in an aircraft, the second attachment element...

Matches 1 - 50 out of 275 1 2 3 4 5 6 >