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WO/2011/110875 |
The safety seat according to the invention contains a lower fastening structure (5), seat surface, squab and head support (9) and safety belt, and further it is provided with a casing (1) surrounding said seat surface (8), squab and head...
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WO/2011/110833 |
A system for determining whether the relative rate of deployment of all the slats (11) extending from a leading edge (12) of an aircraft wing (10) is the same as a predetermined relative rate of deployment is disclosed. Each slat include...
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WO/2011/110719 |
Equipment for inspecting persons and luggage for accessing restricted areas which comprises a machine for controlling the content of hand luggage, preferably an X-ray machine; a walk through gate detector for detecting the presence of me...
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WO/2011/110327 |
A high lift system with a main wing and control flaps, wherein the respective guiding device are at least partially provided with a fairing, having a flow control device for purposes of controlling the flow around the high lift system wi...
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WO/2011/110701 |
System for adjusting the position and attitude of orbiting bodies using guide satellites that includes a satellite (1) fitted with a system for outputting a high-speed ion stream (3) and a secondary propulsion system (4), said satellite ...
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WO/2011/107691 |
The invention relates to a device for controlling the orientation of fan blades of a turboprop engine comprising at least one set (24a, 24b) of adjustable-orientation fan blades rotatably secured to a rotary ring (28a, 28b) mechanically ...
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WO/2011/107690 |
According to the invention, said device (1) comprises two substantially parallel flanges (4, 5) which are provided with rupture areas (16, 17), respectively, located in the same element (2) of the elements (2, 3) to be connected. In said...
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WO/2011/109140 |
Structures and methods are disclosed regarding deployable structures with expandable longerons adjustably coupled with supporting structures such that an angle between the supporting structures can be adjusted. Such structures can includ...
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WO/2011/107066 |
The invention relates to a component, comprising a first section, a second section, and a third section, of which at least one of the sections is made of a titanium material and at least one further section is made of an aluminum materia...
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WO/2011/109436 |
A deployable structure that may include a slit-tube longeron and a flat panel coupled with the slit-tube longeron. The slit-tube longeron may include a tubular member having a slit that runs along the longitudinal length of the slit-tube...
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WO/2011/107066 |
The invention relates to a component, comprising a first section, a second section, and a third section, of which at least one of the sections is made of a titanium material and at least one further section is made of an aluminum materia...
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WO/2011/107733 |
The invention relates to a method of manufacturing a composite acoustic panel employed in an inlet passage of a gas turbine engine (1). The acoustic panel comprises a permeable face-layer (8), an impermeable backing sheet (9) and a sound...
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WO/2011/107682 |
The invention relates to a nacelle comprising a component (23) to be cooled and a cooling assembly (30) for cooling the component (23), said assembly (30) comprising at least one composite wall (20) separating a cold zone (8) and a hot z...
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WO/2011/107682 |
The invention relates to a turbojet engine nacelle component (23) cooling assembly (30), said assembly (30) comprising at least one composite wall (20) separating a cold zone (8) and a hot zone (16) containing said component (23), said a...
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WO/2011/108962 |
A bladed propeller is proposed comprising: a blade provided with apertures; controllable flaps designed to open and close said apertures in order to alter the flow resistance of the blade; a blade drive; and a control unit designed to co...
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WO/2011/104488 |
The invention relates to an aircraft pylon for mounting a dual- or triple-flow jet engine (1), said pylon comprising an upper surface for connection to the aircraft, two side flanks, and a flange on the lower portion of the pylon. Said p...
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WO/2011/104167 |
A method of recording the location of a point of interest on an object, the method comprising capturing a digital image of an object having a point of interest, accessing a three-dimensional virtual model of the object, aligning the imag...
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WO/2011/105345 |
Disclosed is a vibration reduction device provided with actuators which apply forces to beams supporting a cabin, in such a way as to bend the beams; acceleration sensors which measure accelerations of the cabin; and a control device whi...
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WO/2011/104635 |
A method for determining a characteristic such as partial pressure or percentage of a gaseous constituent in a first gas mixture flow (32) in a flow chamber (30) where flows alternatively said first gas mixture flow (32) and a second gas...
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WO/2011/104476 |
The invention relates to a control member (A) comprising actuation members (F) such as a rudder bar and brakes for a pilot in an aircraft, said actuation members comprising a rotary shaft (2) that is rotatable around an axis (40). Said s...
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WO/2011/104488 |
The invention relates to an aircraft pylon for mounting a dual- or triple-flow jet engine (1), said pylon comprising an upper surface for connection to the aircraft, two side flanks, and a flange on the lower portion of the pylon. Said p...
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WO/2011/106623 |
A method and associated illumination system are provided for illuminating an interior of a vehicle with a modular area illumination system, the modular area illumination system comprising: a system controller; and a plurality of an intel...
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WO/2011/106050 |
A rotary wing aircraft bearing for providing 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 subassembly, the ela...
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WO/2011/106320 |
An aerial vehicle includes independently controlled horizontal thrusters and vertical lifters to provide design and operational simplicity while allowing precision flying with six degrees of freedom and use of mounted devices such as too...
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WO/2011/105536 |
In order to enable stable flight without needing a complicated throttle operation by a pilot even when part or all of a control surface has malfunctioned, a control system of an aircraft is provided with a calculation means (15) for calc...
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WO/2011/101513 |
The invention relates to a method for producing a stringer from a pair of angular half-stringers, the webs of which are joined with the insertion therebetween of laminar half-bodies that are in contact with one another, said half-bodies ...
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WO/2011/103194 |
In a propulsion system, an electrohydrodynamic (EHD) body force is used to control the flow of a propellant through a micro channel, expansion slot, plenum chamber, or other flow region and thereby increase the specific impulse created b...
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WO/2011/101385 |
The invention relates to a toilet assembly for a means of transportation comprising a first toilet space (10), a thereto adjoining second toilet space (12) and a partition (28, 30) located between the first toilet space (10) and the seco...
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WO/2011/102611 |
Disclosed is a structure for a flying apparatus that facilitates the operation, assembly, and repair of a power switch, charging device, etc. of a small unmanned rotary wing aircraft. The structure comprises: a cylindrical motor operated...
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WO/2011/101611 |
An aircraft radio system comprising a plurality of radios interconnected by a digital communications network, each radio having a transceiver and a dedicated processor platform, the aircraft radio system being configured to cause the ded...
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WO/2011/101210 |
The invention relates to a storage compartment having no housing for a passenger cabin of an aircraft, having a storage compartment body, at least one fastening strut, and a support disposed between the storage compartment body and an en...
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WO/2011/103078 |
A variable stiffness liquid inertia vibration isolation device includes a liquid inertia vibration elimination isolator and a variable stiffness spring operably associated with the liquid inertia vibration elimination isolator for varyin...
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WO/2011/102304 |
Disclosed is a vibration reduction device provided with an elastic body, a dynamic mass, and a control mass. The dynamic mass is supported by a subject of vibration control via the elastic body. The relevant actuator causes the control m...
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WO/2011/101275 |
The invention relates to an arrangement of aerodynamic auxiliary surfaces, set up for being disposed on the lower face of an aircraft, and further comprising a longitudinal axis (32) and at least one aerodynamic auxiliary surface (20), w...
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WO/2011/101050 |
The invention relates to a multi-layer flame-retardant film, comprising at least one upper layer made of a thermoplastic polyurethane, which contains halogen-free flameproofing agent and is adhesively bound at least to a layer of textile...
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WO/2011/103255 |
A cloud of small to medium-sized space debris is mitigated by releasing drag-reducing particles into the cloud from a dispenser vehicle, causing the particles to collide or otherwise interact with, and thereby exchange momentum with, the...
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WO/2011/102611 |
Disclosed is a structure for a flying apparatus that facilitates the operation, assembly, and repair of a power switch, charging device, etc. of a small unmanned rotary wing aircraft. The structure comprises: a cylindrical motor operated...
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WO/2011/101782 |
The invention relates to a plane tractor (1) which grips the nose gear of a plane, including: a chassis (5); wheel modules (3) connected to the chassis, each wheel module including at least one actuator for inducing a vertical movement o...
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WO/2011/100948 |
The invention relates to a device for fixing a test person on a standing surface, wherein at least one rope is tensioned between a hip belt placed on the test person and a retaining plate arranged below the standing surface.
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WO/2011/101211 |
The invention relates to an inlet air system for passengers in a passenger compartment, wherein the inlet air duct need not be modified in the event of a change in the seating configuration. This is ensured by means of an air distributin...
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WO/2011/102448 |
Provided is a connecting and separating device such that it is possible to reduce the shock of separation when separating a launch vehicle and a structure from each other. The connecting and separating device is equipped with a clamp ban...
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WO/2011/102393 |
A connection-separation device comprises a clamp band, which hooks a mounting member of a launch vehicle and a structure that is mounted on the mounting member; and a first connecting unit that either connects or separates both end porti...
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WO/2011/101513 |
The invention relates to a method for producing a stringer from a pair of angular half-stringers, the webs of which are joined with the insertion therebetween of laminar half-bodies that are in contact with one another, said half-bodies ...
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WO/2011/103194 |
In a propulsion system, an electrohydrodynamic (EHD) body force is used to control the flow of a propellant through a micro channel, expansion slot, plenum chamber, or other flow region and thereby increase the specific impulse created b...
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WO/2011/101275 |
The invention relates to an arrangement of aerodynamic auxiliary surfaces, set up for being disposed on the lower face of an aircraft, and further comprising a longitudinal axis (32) and at least one aerodynamic auxiliary surface (20), w...
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WO/2011/101134 |
The invention relates an aircraft seat, comprising at least one electronic unit (10; 10a; 54; 76; 96) and at least one seat frame unit (12), wherein the electronic unit (10; 10a; 54; 76; 96) is at least partially arranged in a hollow spa...
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WO/2011/100482 |
A combination motorized and propelled apparatus and moment imparting device is provided to improve the stability of the apparatus in motion with regard to pitch, roll and yaw. The moment imparting device uses one or more rotational membe...
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WO/2011/099275 |
Provided is a highly lightning-resistant, inexpensive-to-produce closure member for an opening. In the disclosed door body (30), the outer surface (31a) of the plate section (31) is made of a composite material layer (60), and the inner ...
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WO/2011/099276 |
Disclosed are a high lift generator and a wing capable of suppressing the generation of aerodynamic noise while suppressing increase in the weight of the body. The backward-extending lower surface plate (7) of the lower surface of a slat...
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WO/2011/098712 |
The invention relates to an assembly, in a turbine machine, for controlling a plurality of toothed pivoting blades (30), said assembly comprising an actuation gear (40) for controlling the position of the vanes. Racks (50), mounted on th...
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