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Matches 551 - 600 out of 5,784

Document Document Title
WO/2014/053298A1
This invention relates to a connection set that is used to attach and transfer force and torque between a wing (2a, 2b), comprising a lifting surface and a control surface (9) connected together by a hinge, and the central body (1 ) of a...  
WO/2014/053816A1
The present invention provides an aircraft structure comprising a first sub-structure (110), having a first box cross-section, a second sub-structure (120), having a second box cross-section, and a joint joining a first end region of the...  
WO/2014/051859A1
An electrically conductive multilayer stack including a first metal oxide layer including titanium oxide, a metal layer on the first metal oxide layer, and a second metal oxide layer including titanium oxide on the metal layer, at least ...  
WO/2014/051923A1
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 (16) has an airfoil over substantially it...  
WO/2014/046764A2
A method of forming an airfoil with an integrated platform includes: a) providing an airfoil core; b) wrapping a first overwrap ply around the airfoil core; c) darting a first end of the first overwrap ply to allow the overwrap ply to ex...  
WO/2014/044981A1
The invention relates to a body panel (1) for a transport vehicle — in particular for an aircraft — including a supporting plate (2) and a heat-exchange device (6), said supporting plate forming (2) on the outer surface (4) thereof f...  
WO/2013/160591A3
The invention seeks to provide bonded (equipotential) connections between the various parts of a current return network. To do this, the invention provides a wiring loom with a layer of conductors coated in a fluidtight jacket. Such a wi...  
WO/2012/146858A3
Such a fuselage comprises cross-members (104) for constructing a floor, at least one of said cross-members (104) comprising an upper part (124), a lower part (126), means (140-150) for connecting the lower part to the upper part, and at ...  
WO/2014/011130A3
The present invention relates to a locking mechanism (1) that provides for the door moving inside a guide rail in aircrafts to stay safely at an open position and released during a flight or when the aircraft is parked. Said mechanism (1...  
WO/2014/036553A2
A module of a transportable segmented enclosure system, including a first walled structure encompassing a volume having a longitudinal axis, the walled structure having at least a first opening, the longitudinal axis passing through the ...  
WO/2013/184419A9
A low drag passenger-cabin window (12) for use on an aircraft fuselage having a generally cylindrical shape, in which the as- manufactured geometry of the window is modified so that the shape of the window at cruise altitudes is aerodyna...  
WO/2014/031047A1
The invention relates to a laminate structure (10, 20, 30, 40, 50) of stacked sheets of composite material and method of manufacturing a laminate structure (10, 20, 30, 40, 50) of composite material. The structure (10, 20, 30, 40, 50) co...  
WO/2013/162671A3
Embodiments of reinforced composite structures for aircrafts and methods for making such reinforced composite structures are provided herein. A reinforced composite structure for an aircraft comprises a fiber reinforced composite stringe...  
WO/2014/027919A1
The invention relates to a controllable missile weapon, and more specifically, to the design of aeroballistic missiles (ABMs) with target-seeking guidance in the final portion of the trajectory. The problem addressed by the proposed inve...  
WO/2013/009907A3
A method for creating a layup of reinforcing fibers comprises mounting a face sheet to a spindle of a mandrel tool support, the face sheet having a layup surface for the reinforcing fibers, and counterbalancing the mounted face sheet for...  
WO/2014/008507A3
A panel assembly that includes a first panel having an inner surface and an outer surface, and a second panel having an inner surface and an outer surface. The second panel includes a plurality of rib members formed, therein that extend ...  
WO/2014/027215A1
Door assemblies for aircraft interiors are described. Such door assemblies may comprise a door (18) for opening and closing an aperture (20) between zones (12, 14) of the aircraft interior and an interface (40) configured to couple the d...  
WO/2014/025944A2
Digital flexural materials are kits of discrete parts that can be assembled into a lattice structure to produce functionally useful assemblies. Digital flexural materials enable design of materials with many small and inexpensive flexure...  
WO/2014/014136A1
The aircraft capable of takeoff/landing via the fuselage thereof and the takeoff/landing system of the aircraft according to the present invention are configured such that multiple takeoff/landing rollers are arranged in a sliding direct...  
WO/2014/009615A1
The invention relates to an actuating device (1) for opening an aircraft hatch (4), which is embedded in a recess (2) provided in said hatch (4), said device (1) comprising an actuating means (6), a gripping handle (18), and a rocking me...  
WO/2014/008549A1
An aerolance system for an aerospace vehicle including a head for positioning adjacent a nose of the aerospace vehicle. The head includes a divergent section and a convergent section wherein a base of the convergent section is positioned...  
WO/2014/008507A2
A panel assembly that includes a first panel having an inner surface and an outer surface, and a second panel having an inner surface and an outer surface. The second panel includes a plurality of rib members formed, therein that extend ...  
WO/2014/001304A1
The present invention pertains to a heated floor panel (10) for an airborne vehicle (20) and an airborne vehicle having at least one heated floor panel. The floor panel comprises a controller housing (9), a first heated panel (6) configu...  
WO/2014/001593A1
Method of manufacturing T-shaped stringers (7) made of composite material, comprising a second shaping step for shaping laminates (4) into L-shaped preforms (6), which comprises providing a set of tools formed by a fixed tool (1) compris...  
WO/2013/191835A1
Apparatus and methods provide a spring clip for use in a bracket assembly, such as a bracket assembly used to secure a ceiling panel to an aircraft or other vehicle or structure. According to embodiments described herein, a spring clip (...  
WO/2013/143701A3
The invention relates to a unitary panel for the floor of a vehicle, comprising a self-sustained plate (2) having a shorter dimension, referred to as the thickness, extending in a first direction of the self-sustained plate (2), and two ...  
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/2013/139714A3
The invention concerns a method for producing a frame comprising a section extruded according to a guide contour, said section comprising a flange and a web extending in section in directions concurrent and perpendicular to the guide con...  
WO/2013/182566A1
The invention relates to a pressurized fuselage of an aircraft, with a fuselage structure (2) and a pressure bulkhead (3) mounted therein for forming a fuselage-internal pressure region (a), which pressure bulkhead (3) is attached on the...  
WO/2013/183429A1
The problem addressed by the present invention is providing an interior lighting method, which resolves the sense of confinement and sense of oppression in the passenger compartment of a moving body for travelers and achieves a comfortab...  
WO/2013/184419A1
A low drag passenger-cabin window (12) for use on an aircraft fuselage having a generally cylindrical shape, in which the as- manufactured geometry of the window is modified so that the shape of the window at cruise altitudes is aerodyna...  
WO/2013/153537A3
A vacuum bag (18) is placed around the inner forming surface (IML) of an inner mandrel with radially retractable sectors (11a, 11b) having parallel longitudinal slots (17). Stringers (30) of composite material are positioned in the slots...  
WO/2013/179150A1
The present invention relates to a detection mechanism (1), located on the tail, which enables to receive the electromagnetic waves in the air by being cleared of the platform effects via the detectors present on the helicopter. The inve...  
WO/2013/180982A1
An auxiliary power unit is composed of a gas turbine engine, a gearbox, and a gearbox driven generator. A mount bracket is mechanically attached to the gearbox. The bracket is for connecting to an aircraft strut system. The aircraft stru...  
WO/2013/180980A1
An auxiliary power unit has a gas turbine engine, a generator, and a gear box. A mount bracket is mechanically attached to the gear box. The bracket is for connecting to a plurality of struts. The struts are for connecting to an aircraft...  
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/2013/172804A1
This invention relates to a door latch mechanism (1) that allows for safe opening and closing of doors in aircraft during flight or at parking position. In addition to its capability of being used under any circumstances including but no...  
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/2013/165586A1
A combined hydraulic and pneumatic actuation system (10) including a cylinder (12), a first piston (22), and a second piston (24). The cylinder may include a first cylinder portion (36) configured to hold or retain a first fluid and a se...  
WO/2013/166419A1
A mounting system for a fire detection system (208, 210, 400) for a turbofan engine propulsion system is provided to mount fire detection sensors (404, 500) on the inner fixed structure (IFS) of the nacelle (100). The mounting system mou...  
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/2013/153216A1
The present invention relates to aircraft with a daylight input system. In order to provide improved illumination with a reduced energy demand, an aircraft (10) with a fuselage construction (12) and at least one interior area (14) arrang...  
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/2013/151617A1
A hat stiffener (50) with canted web portions(52a and 52b) and a method of producing the same are disclosed. The hat stiffener has a cap (56). The hat stiffener further has a first web (52a) and a second web (52b) extending from opposite...  
WO/2013/139716A1
The invention relates to a pressure bulkhead of an aircraft with a fuselage shell (2) and a pressure bulkhead (3) disposed therein preferably in the rear region (1) for forming a fuselage-internal pressure region (a), which pressure bulk...  
WO/2013/138103A1
A mount for a turbine engine has a semi-circular yoke with a first leg and a second leg. The mount also has a stanchion with a cylindrical section attached to the yoke, and a conical section attached to the cylindrical section. A mountin...  
WO/2013/135855A1
An aircraft fuselage structure is shown and described, comprising a plurality of ribs (5) extending at intervals from one another in planes perpendicular to the longitudinal axis (X), comprising a floor (7) extending in a plane parallel ...  
WO/2013/137915A1
An airplane (30) includes a wing (42, 44)mounted mid-level on a tubular fuselage (32). The wing (42, 44) includes carry-through that passes transversely through the fuselage (32) and divides a cabin deck into fore and aft sections. At le...  
WO/2013/135856A1
An aircraft fuselage structure is shown and described, said aircraft fuselage structure comprising an outer skin (3), comprising a plurality of circumferential ribs (5), wherein a recess (7) is provided for receiving a wing torsion box i...  
WO/2013/135670A1
Passenger cabin (100) for a means of transport, which comprises an upper passenger deck (116) and a lower passenger deck (117). The floor (102) of the upper passenger deck (116) comprises a lower and an upper region (203, 201) arranged t...  

Matches 551 - 600 out of 5,784