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WO/2011/128858 |
The present invention relates to an acoustic insulation device having at least two panels equipped with resonators intended to acoustically insulate two environments outside these panels, and to a method for manufacturing this device. Th...
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WO/2011/127910 |
The invention relates to a method for the automatic configuration and/or equipment of a vehicle cabin (1), more particularly of an aircraft, wherein the cabin (1) is subdivided into a plurality of zones (A, B, C, D, E) and the method fur...
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WO/2011/127899 |
An aircraft fuselage with an integrated energy-absorbing deformation structure, wherein the fuselage (1) has annular frames (10; 110; 210) and the frames (10; 110; 210) have interconnecting longitudinal fuselage beams (12) and a casing (...
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WO/2011/129696 |
The invention relates to a wing for generating lift and comprises a trailing edge, a leading edge, an inner end, an outer end, a top surface and a bottom surface. The wing comprises an aerofoil with a chord line and a span direction. The...
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WO/2011/127911 |
The invention relates to a method for the automatic configuration and/or equipment of a vehicle cabin, more particularly of an aircraft, wherein the cabin (1) is subdivided into a plurality of zones (A, B, C, D, E) and wherein at least o...
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WO/2011/129721 |
The invention relates to aviation technology and is suitable for improving the aerodynamic characteristics of helicopters, airplanes including large airbuses with a conventional configuration and amphibians, aerodynamic ground-effect cra...
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WO/2011/129696 |
The invention relates to a wing (1) for generating lift and comprises a trailing edge (5), a leading edge (3), an inner end (7), an outer end (9), a top surface (10) and a bottom surface (12). The wing comprises an aerofoil with a chord ...
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WO/2011/127997 |
The present invention relates to a blade (100) for a wind turbine. The blade (100) comprises a heating mat (101) for generating heat, wherein the heating mat (101) is mounted at an outer surface of the blade (100). The heating mat (101) ...
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WO/2011/128069 |
A profile-plate portion (120) for use as an outer wall of a flow body, wherein the profile-plate portion (120) has, at least in part, a first profile-plate panel (121), which is designed to be permeable to fluid such that fluid can flow ...
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WO/2011/127938 |
A fixed wing of an aircraft, having a main wing extending over a half-span with a wing box comprised of spars extending along the spanwise direction of the main wing, a plurality of ribs arranged one in back of the other viewed in the sp...
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WO/2011/130166 |
The disclosure relates to a modular waste liquid separator and collector device (10), comprising component modules. A first module comprises a support structure (12), a second module comprises a droplet separator (14) connectable to said...
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WO/2011/126519 |
An apparatus having a composite sea-based structure with a first carbon nanotube infused material and a second carbon nanotube infused material. The first and second carbon nanotube infused materials each having a range of carbon nanotub...
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WO/2011/126535 |
A system for augmenting ducted fan thrust is provided, the system including a peripheral ejector comprised of an inner cowling member (107) and an outer cowling member (101). With the addition of actuators (111) mounted between the trail...
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WO/2011/124390 |
A mixer assembly (10) for an aircraft air conditioning system comprises a plurality of fresh air lines (12, 18), which are adapted to be flowed through with cold fresh air during operation of the mixer assembly (10), and a plurality of r...
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WO/2011/124904 |
A control surface element skew and/or loss detection system (100) is provided which combines a cable (168, 178) system linked to movement transducers (120) via mechanical links (114, 116) connecting the fixed wing structure (102) to the ...
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WO/2011/126517 |
An apparatus having a composite land-based structure with a first carbon nanotube infused material and a second carbon nanotube infused material. The first and second carbon nanotube infused materials each having a range of carbon nanotu...
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WO/2011/124215 |
A fastening arrangement for connecting two structural elements (1, 2) extending at an angle from each other, especially in a lightweight construction, is disclosed. The first structural element (1) has a recess (10) into which the second...
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WO/2011/124832 |
Unshrouded fan with variable-pitch blades the roots (38) of which are each fitted from the outside into a radial housing of an annular rotor element and guided in rotation about their axis by two rolling bearings (76, 94), one of which i...
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WO/2011/124361 |
The invention relates to a compressor/turbine arrangement (10) for use in an air conditioning unit (200) of an aircraft air conditioning system comprising a process air supply line (12) which is designed to supply process air generated b...
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WO/2011/124207 |
Disclosed is an aircraft comprising: a fuselage shell (1; 101) that has fuselage frames (10; 110); a floor structure (2; 102) that has transverse beams (20; 120) and longitudinal beams (22; 122); and a fastening arrangement for supportin...
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WO/2011/127265 |
Structural connectors for watercrafts, buildings and aircrafts are disclosed. In general, each structural connector includes at least a pair of members extending outwardly from and substantially perpendicular to a body of the structural ...
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WO/2011/126535 |
A system for augmenting ducted fan thrust is provided, the system including a peripheral ejector comprised of an inner cowling member (107) and an outer cowling member (101). With the addition of actuators (111) mounted between the trail...
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WO/2011/124908 |
A rotor blade (31) for a rotorcraft includes a variable aerodynamic element (8), transformable between a first arrangement and a second arrangement and a drive (9,14,17) for transforming the variable aerodynamic element from the first ar...
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WO/2011/126518 |
An apparatus having a composite air-based structure with a first carbon nanotube infused material and a second carbon nanotube infused material. The first and second carbon nanotube infused materials each having a range of carbon nanotub...
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WO/2011/124390 |
A mixer assembly (10) for an aircraft air conditioning system comprises a plurality of fresh air lines (12, 18), which are adapted to be flowed through with cold fresh air during operation of the mixer assembly (10), and a plurality of r...
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WO/2011/125488 |
Disclosed is a spherical suspension which, even in an environment with severe temperature and atmospheric pressure conditions, can be used in a stable manner and provide satisfactory buffering with respect to shocks and vibrations. The s...
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WO/2011/124318 |
The invention relates to a method for structuring a surface (1), in particular for applying a sharkskin to a vehicle or vehicle parts. The known methods comprise films to be glued on or mechanically embossing the plate with the aid of a ...
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WO/2011/126517 |
An apparatus having a composite land-based structure with a first carbon nanotube infused material and a second carbon nanotube infused material. The first and second carbon nanotube infused materials each having a range of carbon nanotu...
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WO/2011/125030 |
A glider 10 comprises a body 12, a closed cockpit 18 and an air extractor 22 for extracting air from the cockpit. The extractor is mounted on the body in a region of negative pressure relative to general ambient or atmospheric pressure, ...
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WO/2011/124391 |
A mixing device (10) for an aircraft air conditioning system comprises a plurality of cold-air supply lines (12, 14), which are devised to supply cold air to the mixing device (10). A plurality of warm-air supply lines (16, 18) is furthe...
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WO/2011/123392 |
An inner barrel structure for an engine nacelle. The inner barrel structure includes an inner skin, a truss core disposed with respect to the inner skin to define a plurality of cavities, and a plurality of septa respective disposed in t...
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WO/2011/121340 |
A method of manufacturing a composite structural member (1), comprising the step of laying up a stack of fibre reinforced laminate plies (12), wherein at least one of the plies is laid up as discrete first (13) and second ply (14) portio...
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WO/2011/120110 |
The present object refers to an aeronautical safety device coupled to the aircraft black box, which will be activated when the equipment submerges to a certain depth, after an air accident occurring on oceans, rivers or lakes. The device...
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WO/2011/120128 |
A duct provides a passageway for a portion of the fluid which contacts the upstream end of a conveyance such as a ship, motor vehicle, train or airship. The intake of the duct is located on the front wall of the conveyance and its outlet...
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WO/2011/123392 |
An inner barrel structure (700) for an engine nacelle. The inner barrel structure (700) includes an inner skin (702), a truss core (706) disposed with respect to the inner skin (702) to define a plurality of cavities, and a plurality of ...
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WO/2011/120995 |
The thermal control device for radiative dissipation equipment comprises: first means, for capturing at least some of the radiation emitted by the dissipative equipment within at least one predetermined wavelength range of the infrared s...
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WO/2011/120939 |
A method of fuelling an aircraft for a flight to a predetermined destination in which the aircraft is loaded, the actual zero fuel weight of the loaded aircraft is determined, the fuel requirement of the loaded aircraft for that destinat...
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WO/2011/120939 |
A method of fuelling an aircraft for a flight to a predetermined destination in which the aircraft is loaded, the actual zero fuel weight of the loaded aircraft is determined, the fuel requirement of the loaded aircraft for that destinat...
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WO/2011/120503 |
The invention relates to a wall component (40) for an aircraft for forming an outer wall (54) comprising at least one first wall element (42), at least one second wall element (44) and at least one connecting device (46) for connecting t...
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WO/2011/120693 |
The invention relates to a method of protecting an aircraft landing gear (1) while the aircraft is being towed using a towing bar (13) coupled to an orientable lower part of the landing gear, comprising the step of generating an alarm wh...
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WO/2011/120916 |
The invention relates to a method of commanding an attitude control system (30) of a space vehicle (10), the attitude of said space vehicle having to be controlled in the course of at least one preparation phase followed by an observatio...
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WO/2011/120918 |
The invention relates to a lock (20) on a luggage box (22), in particular in the cabin of an aircraft. The luggage box (22) has a closable lid (28) which is movable about an axis of rotation (26) and supports a latch bolt support (40) wi...
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WO/2011/120981 |
The invention relates to a device for controlling the temperature of an apparatus for dissipating heat by means of radiation, comprising means for reversibly filtering a portion, included between two predetermined end values, of the radi...
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WO/2011/123204 |
Concepts and technologies described herein provide for a low noise aircraft wing slat system. According to one aspect of the disclosure provided herein, a cove-filled wing slat (202) is used in conjunction with a moveable leading edge el...
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WO/2011/123106 |
An aircraft engine for use in a low-bypass turbofan application has a high pressure turbine having a blade and an engine casing disposed about the blade. A shield is disposed around the casing adjacent to the blade to create an area betw...
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WO/2011/120944 |
A handling system for handling objects (50) in a vehicle has a storage device which can be positioned outside a vehicle cabin, an access device (56) which can be positioned in a vehicle cabin, and a transport device for transporting obje...
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WO/2011/117454 |
The invention comprises a triform fitting (1), essentially made from non-metal composite materials and including several strengthening cross ribs (4) for reinforcing symmetrical flanges (3) and a longitudinal flap (2). The symmetrical fl...
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WO/2011/117619 |
An aerial vehicle is described which comprises: a first compartment for holding a lighter than air gas; a second compartment for holding atmospheric air and having an inlet and an outlet; a solar panel for converting sunlight into electr...
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WO/2011/119164 |
In various examples, a speed limiting apparatus (100, 200) includes a garment (102, 202)) configured to be worn by a user (10). The garment includes an enclosure (110, 220). A speed limiting assembly (120, 220) is coupled to the garment....
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WO/2011/116982 |
A sanitary module arrangement (100) suitable for installation in an aircraft cabin comprises a sanitary module (10), the interior (14) of which is separated by a partition wall (12) from an area (16) of the aircraft cabin adjacent to the...
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