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WO/2011/039285 |
The invention relates to a device for boundary layer suction on the outer skin (1) of an aircraft, on which a suctionable surface (3) penetrated by apertures (10) is connected to a suction source (7) by means of at least one suction line...
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WO/2011/038889 |
A system (10) for cooling and/or heating aircraft devices to be cooled and/or heated comprises a first individual cooling and/or heating system (20, 22) associated with a first aircraft device (12, 14) to be cooled and/or heated, and a s...
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WO/2011/038889 |
A system (10) for cooling and/or heating aircraft devices to be cooled and/or heated comprises a first individual cooling and/or heating system (20, 22) associated with a first aircraft device (12, 14) to be cooled and/or heated, and a s...
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WO/2011/040834 |
The invention proposes "A position for a solar cell in an electronic device". Said invention relates to the field of electrical engineering and is intended for arranging a solar cell in an electronic device in a convenient, reliable and ...
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WO/2011/041343 |
A tray table assembly comprises a table body, at least one arm, and at least one table stop. The at least one arm is pivotally coupled to the table body. The at least one arm is also pivotally coupled to a pivot shaft interior to at leas...
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WO/2011/041503 |
Various embodiments of the present invention include assemblies and methods for minimizing the amplitude of attitude jitter. In one embodiment, a split flywheel assembly includes a plurality of independent concentric flywheels axially al...
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WO/2011/041760 |
A light-weight and low-power integrated system module suitable for installation at a passenger seat disposed aboard a passenger vehicle and methods for manufacturing and using same. By integrating selected interface system components wit...
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WO/2011/039402 |
Joining of a structural aircraft element (1 ) that has a section in an omega shape, to another structural aircraft element (10) with a differently shaped section, with the aforementioned joint of these structural elements (1, 10) with a ...
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WO/2011/039402 |
Joining of a structural aircraft element (1 ) that has a section in an omega shape, to another structural aircraft element (10) with a differently shaped section, with the aforementioned joint of these structural elements (1, 10) with a ...
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WO/2011/038889 |
A system (10) for cooling and/or heating aircraft devices to be cooled and/or heated comprises a first individual cooling and/or heating system (20, 22) associated with a first aircraft device (12, 14) to be cooled and/or heated, and a s...
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WO/2011/038888 |
A system (10) for controlling a cooling system (100) for use especially on board an aircraft comprises a operating state detection unit (30) that is designed to detect operating state signals characteristic of the operating state of the ...
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WO/2011/041503 |
Various embodiments of the present invention include assemblies and methods for minimizing the amplitude of attitude jitter. In one embodiment, a split flywheel assembly includes a plurality of independent concentric flywheels axially al...
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WO/2011/041343 |
A tray table assembly comprises a table body, at least one arm, and at least one table stop. The at least one arm is pivotally coupled to the table body. The at least one arm is also pivotally coupled to a pivot shaft interior to at leas...
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WO/2011/039309 |
The invention relates to a lighting unit for lighting airfields on an airport, in particular for delivering signals to an airplane. It comprises a light source, which has at least one light-emitting diode (4) for generating light to be e...
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WO/2011/038888 |
A system (10) for controlling a cooling system (100) for use especially on board an aircraft comprises a operating state detection unit (30) that is designed to detect operating state signals characteristic of the operating state of the ...
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WO/2011/041000 |
A system and method is provided for thruster control in a flight vehicle. The system and method uses a proportional derivative matrix control technique to determine thrust commands in a Divert and Attitude control (DAC) system. The propo...
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WO/2011/039285 |
The invention relates to a device for boundary layer suction on the outer skin (1) of an aircraft, on which a suctionable surface (3) penetrated by apertures (10) is connected to a suction source (7) by means of at least one suction line...
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WO/2011/039399 |
Aircraft ring frame and method for the production thereof, said ring frame being produced from composite material, said ring frame comprising a number of partitions (20) that, when connected together, form said ring frame in its entirety...
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WO/2011/039399 |
Aircraft frames and method for obtaining them, which frames are made of composite material, and they comprise several partitions (20) that form, when joined, the aforementioned frame in its entirety, with these partitions (20) comprising...
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WO/2011/039285 |
The invention relates to a device for boundary layer suction on the outer skin (1) of an aircraft, on which a suctionable surface (3) penetrated by apertures (10) is connected to a suction source (7) by means of at least one suction line...
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WO/2011/038888 |
A system (10) for controlling a cooling system (100) for use especially on board an aircraft comprises a operating state detection unit (30) that is designed to detect operating state signals characteristic of the operating state of the ...
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WO/2011/037855 |
An aerial vehicle is configured to operate in a base fuel cell operating mode and a fuel cell boost operating mode. A method for controlling the aerial includes providing a base fuel cell upper power limit. The method further includes co...
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WO/2011/037716 |
An array of aerodynamic riblets is formed with a surface layer for adhering to an aerodynamic surface and a plurality of riblet tips having a parabolic cross section extending from the surface layer.
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WO/2011/037852 |
An electric power management system of a vehicle may interconnect a power plant, a propeller drive unit, and a battery via a bus. A controller may direct the operation of the power plant and the propeller drive unit. In a slow control mo...
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WO/2011/035838 |
The invention relates to a system (10) for configuring an aircraft passenger cabin, said system comprising a first database (12) that stores cabin equipment component data pertaining to cabin equipment components selected for and include...
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WO/2011/037850 |
A method for managing power flow within an aerial vehicle includes determining a fuel cell power limit and a battery energy reserve. The method further includes determining a flight operation power requirement. The method further include...
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WO/2011/036386 |
The invention relates to an engine (22) attached to an engine pylon (23, 24) via an intermediate structure (39) assembled by flanges (40, 41), to the pylon and to the engine, a rigid structure (42) connecting the flanges. Said arrangemen...
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WO/2011/036385 |
The invention relates to an engine (22) suspended from the linear main portion (23) of a pylon attached to an airplane fuselage or wing. The coupling comprises flat, symmetrical flanges (25a, 25b) forming an angle, for supporting a brack...
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WO/2011/035845 |
The invention relates to a cabin equipment component connection system. In at least one zone of said connection system, said zone being assigned to a predetermined region of an aircraft cabin, a number and an arrangement of connecting el...
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WO/2011/035845 |
The invention relates to a system for connecting cabin equipment components in an aircraft, said system comprising a plurality of connecting elements, each of which is configured to be connected to a cabin equipment component, thus linki...
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WO/2011/036255 |
The invention relates to a regulating system (2) for regulating the cabin pressure P C of an airplane (4), comprising at least one cabin pressure regulating unit (6), which is equipped, by controlling at least one air removal or air supp...
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WO/2011/037716 |
An array of aerodynamic riblets is formed with a surface layer for adhering to an aerodynamic surface and a plurality of riblet tips having a parabolic cross section extending from the surface layer.
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WO/2011/037719 |
An array of aerodynamic riblets incorporates a high elongation elastomeric layer having spaced tips and optionally a protective cladding. The elastomeric layer may be adhered to an aerodynamic surface directly or as an appliqu in combina...
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WO/2011/037855 |
An aerial vehicle is configured to operate in a base fuel cell operating mode and a fuel cell boost operating mode. A method for controlling the aerial includes providing a base fuel cell upper power limit. The method further includes co...
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WO/2011/036255 |
The invention relates to a regulating system (2) for regulating the cabin pressure P C of an airplane (4), comprising at least one cabin pressure regulating unit (6), which is equipped, by controlling at least one air removal or air supp...
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WO/2011/037850 |
A method for managing power flow within an aerial vehicle includes determining a fuel cell power limit and a battery energy reserve. The method further includes determining a flight operation power requirement. The method further include...
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WO/2011/035845 |
The invention relates to a cabin equipment component connection system. In at least one zone of said connection system, said zone being assigned to a predetermined region of an aircraft cabin, a number and an arrangement of connecting el...
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WO/2011/037719 |
An array of aerodynamic riblets incorporates a high elongation elastomeric layer having spaced tips and optionally a protective cladding. The elastomeric layer may be adhered to an aerodynamic surface directly or as an appliqu in combina...
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WO/2011/034236 |
The present invention relates to a flight control system for an unmanned aerial vehicle (UAV) using the postural change of a controller, and to a method for operating the flight control system. First, a UAV flight control system accordin...
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WO/2011/032909 |
The invention relates to components (100, 120, 140) of an aircraft network (200), which can automatically configure and repair said network (200). The invention also relates, in particular, to a control device (100) for an aircraft netwo...
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WO/2011/032937 |
The invention relates to a method for simulating the movements of a virtual vehicle, a user being in physical contact with a simulator including a force-feedback haptic interface, wherein said physical contact corresponds to at least one...
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WO/2011/032806 |
The invention relates to a device, in particular for attachment to the rear side of a seat. The device comprises a plate having a flat recess (44) and an insert (49) that can be removably mounted in the flat recess of the plate and is de...
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WO/2011/032641 |
The invention relates to a braking device for braking freight objects in the freight loading area of aircraft. The braking device comprises a braking roller (10), which is rotatably accommodated in a housing (12). A divided friction ring...
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WO/2011/032996 |
The invention relates to a covering device (2) for an interior (4) of an aircraft, comprising at least one material web (6), at least one guide unit (10), and at least one tensioning element. The guide unit (10) is set up for being attac...
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WO/2011/035259 |
A way of using narrowband irradiation to de-ice or release ice from a surface is provided. The methodology can be applied to a range of different types of de-icing from windshield de-icing to aircraft wing de-icing to releasing ice from ...
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WO/2011/034992 |
An aircraft fluid application system includes a structure, and nozzles coupled to the structure and able to move in relation to the structure. The structure may be a fixed structure, or may be a movable structure. The nozzles may be moun...
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WO/2011/033525 |
A system and method for an adaptable oxygen regulator with an electronic control device is disclosed. In one embodiment, an oxygen regulator system includes an electronic control device which includes a non-volatile memory for storing a ...
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WO/2011/034531 |
An easily removable and lightweight horizontal stabilizer configured to provide aerodynamic stability for a rotorcraft. The horizontal stabilizer comprising a spar removably coupled to a tailboom with a removable spar attachment means, t...
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WO/2011/033204 |
The invention relates to a turbine engine with contra-rotating upstream and downstream non-ducted propellers (12, 14) including a power turbine which is mounted axially between the two propellers (12, 14) and which includes an outer roto...
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WO/2011/034992 |
An aircraft fluid application system (10) includes a structure (16), and nozzles (14) coupled to the structure and able to move in relation to the structure. The structure may be a fixed structure, or may be a movable structure. The nozz...
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