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Patent Searching and Data


Matches 551 - 600 out of 5,614

Document Document Title
WO/2013/128054A3
Reinforcing structure (10) incorporated into the internal structure of an aircraft, made from composite material, said structure (10) comprising a skin (3) and a plurality of stringers (4) and at least one pair of lateral reinforcing ele...  
WO/2013/129122A1
Provided is a composite material structural body (3) of a fiber reinforced plastic composite material which extends in one direction and has an opening (5) and which is loaded with tensile load and/or compressive load in the one directio...  
WO/2013/128138A3
The invention relates to a method of forming a thermoplastic composite material with continuous-fibre reinforcement by stamping, characterised in that it comprises the steps consisting of: a. obtaining a planar blank (230), comprising a ...  
WO/2013/128054A2
Reinforcing structure (10) incorporated into the internal structure of an aircraft, made from composite material, said structure (10) comprising a skin (3) and a plurality of stringers (4) and at least one pair of lateral reinforcing ele...  
WO/2013/128219A1
A connection assembly for an emergency aircraft door. The assembly includes a first pair of non parallel links pivotally attached to the fuselage and a second pair of non parallel links attached to the door. One of the links of the first...  
WO/2013/126111A3
An unmanned aerial launch vehicle (UAV) launch apparatus is disclosed that includes a UAV (400) having an exterior surface, an aerial vehicle (AV) tab (510) extending from the exterior surface, a tube (440) containing the UAV (400), the ...  
WO/2013/126111A2
An unmanned aerial launch vehicle (UAV) launch apparatus is disclosed that includes a UAV (400) having an exterior surface, an aerial vehicle (AV) tab (510) extending from the exterior surface, a tube (440) containing the UAV (400), the ...  
WO/2013/122524A1
The present invention relates to a mould system and a method for net moulding of a co-cured integrated structure (1) comprising a skin (26) provided with stringers(4) and rib feet (2) and with a gap (6) between the stringers (4) and the ...  
WO/2013/119305A3
An aircraft cargo door shield releasably attachable to an aircraft cargo door and configured for protecting an aircraft cargo door during loading and unloading of cargo. The aircraft cargo door shield includes a panel configured for cove...  
WO/2013/115859A3
A heat shielded composite panel (20) including a first part including a composite structural panel (22) coated with a ceramic cement coating, and a second part including a foam panel (26) having a fire-safe coating (28) applied to the su...  
WO/2013/111168A1
The invention, called "GI.CA. System", refers to a process of design and construction of artefacts in which is required high structural strength combined with lightness and small size of the structure itself. The main targets of this way...  
WO/2013/108013A1
A structural assembly comprising a first component having a ramped surface, and a fastener assembly for fastening the first component to a second component, the fastener assembly including a receptacle strip of resiliency deformable mate...  
WO/2013/109305A1
A water-tight or air-tight accessible compartment has a removable hatch sealed at the edge with elastically conformable opposing seals, with elongate communication elements extending into the compartment between the opposing seals, seals...  
WO/2013/106500A1
A mounting assembly for mounting a sound-deadening body to a fuselage of an aircraft and a method for attaching a sound-deadening body to a fuselage of an aircraft using the mounting assembly is disclosed herein. In a non-limiting embodi...  
WO/2013/105178A1
An aircraft window exhibiting sufficient electromagnetic shielding properties and environment-resistant sealing properties is easily provided at a low cost. An aircraft and an assembly method for the aircraft window are also provided. A ...  
WO/2013/103426A3
Load-bearing structures constructed from polymer matrix composite (PMC) materials, and processes for their production. The structures are produced from at least one shaped panel formed of a continuous fiber reinforcement in a thermoplast...  
WO/2013/098665A1
A trim panel (10) for the interior (11) of an aircraft (E), the panel having a multilayer structure and including an outer layer (12) made of material impervious to air, and which is positioned in use facing the fuselage of the aircraft ...  
WO/2013/093323A1
The invention relates to a structural element for an aircraft fuselage, generally shaped in the form of a longitudinally elongate section. The element comprises two wings (4, 6), each wing including: a portion (8, 10) that extends uninte...  
WO/2013/093784A1
A window (38) for a vehicle includes at least one transparent pane (42, 44) suspendable within a frame (40). The transparent pane (42, 44) comprises a deformable material. The transparent pane (42, 44) defines a first surface position hi...  
WO/2013/089598A1
The present invention regards an aircraft structure comprising an aerodynamic composite shell (7), the interior face (9) of which in whole or in part is bonded with at least one two- or three-dimensional structural composite part (11) by...  
WO/2013/083268A1
The invention provides a fiber-reinforced composite material (10), comprising a bulk portion (12) comprising a bulk matrix with reinforcing fibers embedded therein, and a surface portion (14) comprising a plurality of laminated first lay...  
WO/2013/083436A1
The present invention relates to a heating system (10) for an aircraft or spacecraft with a control device (5) which comprises at least one power line data transmission transceiver (5a; 5b) and one sensor controller (7), and at least one...  
WO/2013/076389A1
The invention relates to a device for extracting a windshield (16) and/or an instrument panel (14) of a motor vehicle when said vehicle is being taken apart with a view to recycling the components thereof, characterized in that it includ...  
WO/2013/076633A1
Method for manufacturing a support pylon for avionics made of composite materials, adapted to allow the transport of external loads that cannot be directly supported at the primary or secondary structure of the aircraft. Said loads are r...  
WO/2013/074174A2
Technologies for reducing the risk of disbonding between two bonded members (108, 110) at areas of differing strain in the members (108, 110) are provided. Where the difference in strain between the two bonded members (108, 110) becomes ...  
WO/2013/074174A3
Technologies for reducing the risk of disbonding between two bonded members (108, 110) at areas of differing strain in the members (108, 110) are provided. Where the difference in strain between the two bonded members (108, 110) becomes ...  
WO/2013/070061A1
The present invention discloses a vehicle (1) capable of being converted between a flying condition and an automotive riding condition. The vehicle has a telescopically extendable tail (10) comprising a first tubular tail segment (11) an...  
WO/2013/070112A1
In order to increase the operational reliability of a direct vision window in icing conditions, ensure that the window can be opened in flight, reduce the forces on the handle of the window during closing and ensure the airtight compress...  
WO/2013/067885A1
The present invention provides a spoiler for a hatch door on an aeroplane, which spoiler is installed on the inner covering of the hatch door, inside the wind-facing leading edges of the front hatch door on the left and right of the fron...  
WO/2013/066173A1
The invention relates to a fiber-metal laminate of mutually bonded fiber-reinforced composite layers and metal sheets, the laminate comprising a combination of a fiber- reinforced composite layer and an adjacent metal sheet, in which com...  
WO/2013/066537A1
A mechanical fitting for connecting structures includes a base structure (504) and a plate member (506,508). The mechanical fitting also includes a support structure (510,514) for supporting the plate member at a predetermined spacing fr...  
WO/2013/065311A1
The present invention provides a lightning-proof fastener able to reliably seal an arc between a cap and a wing panel. One end (30a) of the cap (30A) on the open side opposing member (22), or member (21), has a flat surface (30d) orthogo...  
WO/2013/060615A1
The present invention relates to a fastening arrangement for plateshaped facing components. The fastening arrangement comprises at least one profiled rail (4) comprising legs (5), an intermediate space (6) being formed between these legs...  
WO/2013/057355A3
Improved impact‑resistant and damage‑tolerant aircraft fuselage. The invention relates to a section (32) of the fuselage of an aircraft suffering impacts from external bodies, the fuselage of the aircraft having a curved form with at...  
WO/2013/055459A1
Apparatus and methods provide for utilizing continuous curved composite stringers (102) to control the loads and corresponding moments within curved regions of an aircraft or other vehicle without delamination or other interlamina failur...  
WO/2013/050698A1
The invention relates to a method of manufacturing a sound absorbing panel (107) according to which a reflective wall (112) is added to at least one part of one of the faces (111, 113) of a set of sound absorbing cells. The method accord...  
WO/2013/048656A2
In another embodiment of the disclosure, there is provided an access door assembly for joining to a structure. The access door assembly has an access door with at least one access door nonlinear edge. The access door assembly further has...  
WO/2013/048698A1
An electrical system responsive to overheating and/or electric arcing of an electrically conductive member, e.g. a heating member of an aircraft windshield, includes a first switch in a first current path, and a second switch in a second...  
WO/2013/048656A3
There is provided an access door assembly for joining to a structure. The access door assembly has an access door (402) with at least one access door nonlinear edge (404). The access door assembly further has a support structure (420) wi...  
WO/2013/048649A3
In an embodiment of the disclosure, there is provided a panel assembly for joining to a structure and method of making the same The assembly has a first panel element (102a) having at least one first panel nonlinear edge (122a), and has ...  
WO/2013/045861A1
The present invention relates to a novel design of the front portion of an aircraft cockpit. The invention provides a viewing device which comprises a screen pivotably mounted on a mounting that allows height adjustment. The invention al...  
WO/2013/045466A1
The present invention provides a window module for an aircraft or spacecraft, comprising a window frame (10) which comprises, at least in portions, a current-generating element (20) for generating an electric current.  
WO/2013/048649A2
In an embodiment of the disclosure, there is provided a panel assembly for joining to a structure and method of making the same. The assembly has a first panel element having at least one first panel nonlinear edge, and has a second pane...  
WO/2013/041812A1
The invention relates to an assembly of luggage containers (10). Each of said luggage containers comprises a platform (12; 14) for receiving luggage, and two storage half-spaces (66, 68; 100, 102) extending substantially parallel to one ...  
WO/2013/042362A1
The present invention relates to a door sealing an opening disposed at a fuselage of an aircraft which may prevent penetration of an electromagnetic wave effectively. According to the present invention, a gasket seal (20) disposed betwee...  
WO/2013/039981A2
The present invention is a bay for an aircraft galley that includes an extractor that retrieves objects from a compartment by slowly bringing the object forward using a free end. The free end is brought out of the compartment, carrying t...  
WO/2013/037379A9
The invention relates to aviation technology and can be used for improving the lift-drag ratio of helicopters and aeroplanes, including classically configured large airliners, and amphibious craft, aerodynamic ground-effect craft and hov...  
WO/2013/040054A1
A window shade assembly including one or more shades, each shade being attached at a second end to a moveable elongate member extending between a first frame member and a second frame member. The assembly further includes one or more man...  
WO/2013/037379A1
The invention relates to aviation technology and can be used for improving the lift-drag ratio of helicopters and aeroplanes, including classically configured large airliners, and amphibious craft, aerodynamic ground-effect craft and hov...  
WO/2013/030527A1
The present invention provides an aircraft structure comprising a structural component (130, 230) and a set of reinforcing straps (140, 240) for reinforcing the structural component, wherein the set comprises a first reinforcing strap (1...  

Matches 551 - 600 out of 5,614