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WO/2011/066030 |
An unmanned aerial vehicle (UAV) launch tube (100) that comprises at least one inner layer of prepreg substrate (370) disposed about a right parallelepiped aperture (305), at least one outer layer of prepreg substrate (380) disposed abou...
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WO/2011/066400 |
Methods (160), systems (200), and devices (110) for determining system/device configuration and setting a mode of operation based on the determined configuration. An air vehicle processor (110): (a) receives a component information (14) ...
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WO/2011/063978 |
The invention relates to an aircraft seat assembly (10) for aircraft passengers having restricted mobility comprising a seat base assembly (14) that can be mounted in an aircraft cabin (12) and comprises a first carrier device (22) and a...
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WO/2011/064565 |
There is herein described an unmanned aerial vehicle capable of inspecting, identifying, and/or categorising defects on objects to be inspected using visible and/or non-visible wavelengths from infra-red to ultraviolet. More particularly...
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WO/2011/063978 |
The invention relates to an aircraft seat assembly (10) for aircraft passengers having restricted mobility comprising a seat base assembly (14) that can be mounted in an aircraft cabin (12) and comprises a first carrier device (22) and a...
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WO/2011/063978 |
The invention relates to an aircraft seat assembly (10) for aircraft passengers having restricted mobility comprising a seat base assembly (14) that can be mounted in an aircraft cabin (12) and comprises a first carrier device (22) and a...
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WO/2011/066373 |
Liquid dispensing assemblies including adhesive anchoring assemblies configured to adhere to a support surface external to a device such as a vehicle. An air vehicle (310) includes (a) a fluid adhesive container assembly (1010) detachabl...
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WO/2011/062905 |
Embodiments of a modular condenser unit are provided. The modular condenser unit may include a housing and a first condenser coil and a second condenser coil disposed within a volume of the housing. A fan may also be disposed in an end o...
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WO/2011/061567 |
The present invention relates to a device for reducing vibrations produced in the seat of helicopter pilots owing to the movement of the blades of said aircraft. Said device is based on a low-weight, low-cost pneumatic system that counte...
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WO/2011/062696 |
A method and apparatus may be present for processing parts. A first part may be positioned in a first position. A first number of features may be formed on the first part using a feature forming system at a number of points for attachmen...
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WO/2011/063399 |
Embodiments of the present invention include a table stop assembly comprising a mounting block having at least one receptacle, at least one stop coupled to the receptacle, and at least one arm knuckle. The arm knuckle includes a side, a ...
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WO/2011/063399 |
Embodiments of the present invention include a table stop assembly comprising a mounting block having at least one receptacle, at least one stop coupled to the receptacle, and at least one arm knuckle. The arm knuckle includes a side, a ...
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WO/2011/061227 |
A method of reducing vibration in a rotary system (120, 130) of a motor vehicle, for example a car (100), comprising: balancing said rotary system (120, 130), characterized by providing a rotational element (300, 302-306) comprising a ch...
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WO/2011/061770 |
A method for detecting physical associations between electronic identifiers and objects to which the electronic identifiers are physically coupled. The method 'includes the steps of: detecting the electronic identifiers in respective det...
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WO/2011/062783 |
A helicopter auxilary anti-torque system for efficiently supplying thrust and control at the tail of a helicopter during failure of the helicopter tail rotor. The helicopter auxilary anti-torque system generally includes a fluid thrust a...
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WO/2011/062682 |
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WO/2011/062783 |
A helicopter auxilary anti-torque system for efficiently supplying thrust and control at the tail of a helicopter during failure of the helicopter tail rotor. The helicopter auxilary anti-torque system generally includes a fluid thrust a...
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WO/2011/061260 |
The invention relates to nose parts of the fairing of vertical and horizontal tails and wings of an aircraft with a skin and a support structure, the skin being disposed on the support structure. The support structure is provided with a ...
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WO/2011/062639 |
A rotary wing aircraft bearing that provides a constrained relative motion between a first rotary wing aircraft member and a second rotary wing aircraft member. The bearing includes an elastomeric mold bonded laminated bearing stack, the...
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WO/2011/063404 |
Embodiments of the present invention include a passenger seat with a seat frame having at least one coupling projection and a seat pan assembly having at least one coupling retainer. The coupling retainer is configured to releasably enga...
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WO/2011/061181 |
The invention relates to a carrier system for receiving containers in a vehicle, comprising at least one container (6), at least one electrical consumer (16) disposed in the container, at least one primary winding in a first core, and at...
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WO/2011/062682 |
A method for minimizing the weight of an internally pressurized aircraft fuselage of a type that includes an elongated tubular shell having a near-elliptical cross-section with a radius R(φ)-and a curvature Curv(φ), where φ is a roll ...
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WO/2011/061260 |
The invention relates to nose parts of the fairing of vertical and horizontal tails and wings of an aircraft with a skin and a support structure, the skin being disposed on the support structure. The support structure is provided with a ...
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WO/2011/061729 |
A method of overcoming gravity, comprising forming a magnetic field covering the area occupied by a flight vehicle and by means of the flight vehicle itself in such a way that this magnetic field has a component perpendicular to the dire...
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WO/2011/061306 |
The invention relates to a carriage (1) for transporting an aircraft engine module (2) from a preparation station (3) to an assembly station (4), said carriage comprising, on a rolling chassis (8), a framework (10) that can be rendered h...
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WO/2011/061234 |
The invention relates to a supporting structure for an aircraft floor panel, which consists of a three-dimensional truss (1) consisting of a single part made of a composite material comprising a plurality of long-fibre plies arranged sub...
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WO/2011/062639 |
A rotary wing aircraft bearing that provides a constrained relative motion between a first rotary wing aircraft member and a second rotary wing aircraft member. The bearing includes an elastomeric mold bonded laminated bearing stack, the...
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WO/2011/061260 |
The invention relates to nose parts of the fairing of vertical and horizontal tails and wings of an aircraft with a skin and a support structure, the skin being disposed on the support structure. The support structure is provided with a ...
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WO/2011/062893 |
Embodiments of a modular air conditioning (AC) unit include a base unit and a blower selected from a group of blowers configured for different cooling capacities. The module AC unit also includes at least one heat exchanger unit selected...
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WO/2011/061437 |
The invention relates to an intermediate housing (20) for a jet engine air blower compartment (Cs), said housing comprising: a cylinder (22) centered on a longitudinal axis (X-X) of the turbine engine; an annular flange (24) centered on ...
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WO/2011/062639 |
A rotary wing aircraft bearing that provides a constrained relative motion between a first rotary wing aircraft member and a second rotary wing aircraft member. The bearing includes an elastomeric mold bonded laminated bearing stack, the...
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WO/2011/061181 |
The invention relates to a carrier system for receiving containers in a vehicle, comprising at least one container (6), at least one electrical consumer (16) disposed in the container, at least one primary winding in a first core, and at...
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WO/2011/061227 |
A method of reducing vibration in a rotary system (120, 130) of a motor vehicle, for example a car (100), comprising: balancing said rotary system (120, 130), characterized by providing a rotational element (300, 302-306) comprising a ch...
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WO/2011/061770 |
A method for detecting physical associations between electronic identifiers and objects to which the electronic identifiers are physically coupled. The method 'includes the steps of: detecting the electronic identifiers in respective det...
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WO/2011/062677 |
A blended wing body cargo aircraft is disclosed. A body section defines a cargo volume, where an outer surface of the body section is shaped to provide an aerodynamic lifting surface. A cargo door and ramp structure (306,308) is located ...
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WO/2011/061307 |
The invention relates to an assembly for handling a module (1) especially comprising a carriage (2), a part (5) that pivots at the top of the carriage, equipment (12) for supporting the module, and complementary means (19) for joining th...
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WO/2011/063404 |
Embodiments of the present invention include a passenger seat with a seat frame having at least one coupling projection and a seat pan assembly having at least one coupling retainer. The coupling retainer is configured to releasably enga...
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WO/2011/061513 |
A dual-skin structure (10, 210) comprises a first skin (12, 112, 212), a second skin (14, 114, 214) and an intermediate structure (16, 116, 216). The intermediate structure (16, 116, 216) comprises a plurality of first contact portions (...
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WO/2011/058514 |
An aircraft trim panel structure includes a thermoplastic resinated quadraxial fiberglass lay-up prepreg first open structure skin layer having at least a 28 % open area. A thermoplastic resinated quadraxial fiberglass lay-up prepreg sec...
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WO/2011/058075 |
The present invention relates to a kitchen appliance for an aircraft. The kitchen appliance comprises a receiving chamber (or cooking chamber) for receiving at least one food container in the kitchen appliance, a heating device arranged ...
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WO/2011/057817 |
The invention pertains to a flap adjusting system of an aircraft that features: - at least one regulating flap (A1, A2; B1, B2) that is respectively mounted on one of the airfoils of an aircraft by means of at least two bearing devices (...
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WO/2011/057669 |
A pod (100) for flights to and/or from space or near-space, comprising a pressurized body (10) for hosting passengers, said pressurized body having a substantially ring-like shape provided around a central axis (7) and having a central o...
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WO/2011/058447 |
The present invention provides a rotor assembly for helicopter vehicles for stabilizing the aircraft and thus providing an easy way of controlling pitch and roll of the aircraft by respectively associated magnetic actuators. The rotor as...
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WO/2011/057819 |
The invention relates to a transmission assembly for a drive system of storage spaces of an aircraft, in particular for a high lift system, for transferring a rotary movement from a first shaft at an angle α > 0 to a second shaft, where...
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WO/2011/060234 |
An aircraft seating arrangement including a single-piece seat bottom frame having a plurality of laterally spaced-apart fore and aft legs for being attached to and supporting the seat frame on an aircraft deck and a plurality of seat bot...
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WO/2011/058076 |
The invention relates to an integrated end-to-end maintenance platform (1) for maintenance of an aircraft (8) comprising a customer interface for selecting a customized service package including modular services of different aircraft mai...
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WO/2011/059571 |
An adaptive structural core includes a plurality of core members arranged in a repeating pattern, a plurality of actuator attachment points provided on the plurality of core members and at least one actuator engaging the plurality of act...
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WO/2011/058281 |
The invention relates to a method and device for the remote collection of data from aircraft or ship recorders using a buoy (3) which can be ejected in the event of sinking and contains a double memory which stores the positions of the b...
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WO/2011/057778 |
Trailing-edge flap system comprising a trailing-edge flap and a movement means, the movement means comprising at least a translatory mover for the translation of the trailing-edge flap and at least a rotational mover for the rotation of ...
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WO/2011/056285 |
An aircraft system for improved cooling efficiency comprises at least one air conditioning pack (44), coupled to an aircraft, having at least one air compression device (50) powered by at least one power source (62) and having an air com...
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