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WO/2011/146349 |
An unmanned air module includes one or more rotors, engines, a transmission and avionics. Any of several different ground modules may be attached to the air module. The air module may fly with and without the ground module attached. The ...
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WO/2011/143794 |
A droop panel linkage (2) for aircraft comprises a lever arm (5), a main lever (4), a main tube (7) and at least one drive strut (6). The lever arm (5) is pivotally attached at a first end to a flap (3) and is pivotally connected at a se...
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WO/2011/144836 |
The nacelle (1) comprises a stationary shroud (9) and an intake lip (8) that can move axially in relation to the shroud (9) between a rear operating position and a front maintenance position. The aerodynamic element (15) is flexible and ...
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WO/2011/146543 |
A radome comprise a substrate having a first material and an outer layer having a second material, which is positioned adjacent to the substrate. The first material of the radome can comprise a generally rigid polymeric material. The gen...
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WO/2011/144696 |
The invention relates to a tilt wing aircraft having a rear drive/control unit which is designed to generate propulsion and to generate an upward or downward directed propulsion component and/or a laterally directed propulsion component ...
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WO/2011/144629 |
The invention relates to a single device for locking and unlocking the locking member of a landing gear having a folding strut, comprising an unlocking device including: a rotary actuator having an axis parallel to a hinge axis of the co...
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WO/2011/144497 |
The present invention makes reference to a remotely operated air reconnaissance device, designed in stages, which comprises means of guidance during its stages both in ascent (injection) and descent (gliding), together with means for the...
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WO/2011/144850 |
According to the invention, the upper end of the inclined front strut (9i) of the landing gear is connected to the structure (2A) of the fuselage by connecting means (13, 17).
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WO/2011/141890 |
The present invention relates to an arrangement (or structure) (1) for passenger (2) on a means of transportation, in particular an aircraft. It comprises a seat (3) with a variable arrangement, and a shelf (5), and offers to the passeng...
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WO/2011/143642 |
A system of spacecraft radiators comprising pre-formed thermal-transfer modules joined together by at least one solid-state welding process. Critical failure points are eliminated by forming the thermal-transfer modules as a single unita...
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WO/2011/142915 |
A system and a method for detecting a hard landing or other high load event of an aircraft and then automatically triggering a report of such hard landing event. A sink rate algorithm is used to estimate the altitude rate of a main gear....
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WO/2011/143648 |
Described are portable electronics device coupling assemblies (10) including a cradle (12) configured to electronically couple and releasably engage a portable electronics device (20), and an adaptor (14) configured to electronically cou...
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WO/2011/141134 |
The invention is based on a seat arrangement of a passenger cabin, with at least two seat groups (10, 12), wherein the at least two seat groups (10, 12) are arranged consecutively between two passenger aisles (24) running parallel to a l...
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WO/2011/140825 |
A device for enhancing buoyancy is set in transport. It includes a body (1) and a linkage (2). The body (1) is an elongated planar plate. The linkage (2) is connected to the transport. One end of the linkage (2) is connected to the botto...
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WO/2011/143662 |
A method for searching for airline travel based upon seat characteristics specified, by a traveler is disclosed. Travel information is received indicating an origin, a destination, one or more travel dates and one or more seat characteri...
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WO/2011/141647 |
The invention relates to an aluminum-based alloy comprising, in % by weight, 2.1 to 2.4% of Cu, 1.3 to 1.6% of Li, 0.1 to 0.51% of Ag, 0.2 to 0.6% of Mg, 0.05 to 0.15% of Zr, 0.1 to 0.5% of Mn, 0.01 to 0.12% of Ti, optionally at least on...
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WO/2011/141680 |
The invention essentially relates to an aeroplane seat base (110) characterised in that said base comprises: a plate (1) suitable for moving along a horizontal path between an extended position and a stored position, a supporting arm (4)...
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WO/2011/142864 |
A passively torque-balanced device includes (a) a frame; (b) a drivetrain including a drive actuator mounted to the frame and configured for reciprocating displacement, an input platform configured for displacement by the drive actuator,...
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WO/2011/142844 |
Air vehicles and associated aerodynamic structures are provided which include ridged solar panels to both reduce the drag and increase the solar energy harvested by the solar panel. The air vehicle may include an airframe and a solar pan...
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WO/2011/143648 |
Described are portable electronics device coupling assemblies including a cradle configured to electronically couple and releasably engage a portable electronics device, and an adaptor configured to electronically couple and releasably e...
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WO/2011/143642 |
A system of spacecraft radiators comprising pre-formed thermal-transfer modules joined together by at least one solid-state welding process. Critical failure points are eliminated by forming the thermal-transfer modules as a single unita...
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WO/2011/142835 |
A platform leveling system for an aircraft cargo loader comprises first and second hydraulic cylinders for lifting and lowering corresponding first and second sides of the platform, at least one sensor for generating signals representati...
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WO/2011/141450 |
The invention relates to a piece goods treatment system for treating piece goods (12) designed as pieces of luggage or packages, comprising a receiving station (16) where piece goods (12) to be sorted are received, a sorting unit (32) fo...
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WO/2011/138571 |
The invention relates to a unit for an aircraft thruster which includes a first ferrule (10) intended for being attached to a second ferrule (20) and a first connection flange (30) intended for being secured to a corresponding second con...
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WO/2011/137656 |
A dual-power device with a transfer case (2) of a container lift platform truck comprises an engine (1), a hydraulic pump (3) and a hydraulic transmission device (4) driven by the hydraulic pump (3). The dual-power device is provided wit...
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WO/2011/138566 |
Device for rapidly separating two subassemblies, under the action of a pyrotechnic gas generator. The device comprises a segmented nut (17) held by a release sleeve (40) that can move under the action of the gas generator (15); a motive ...
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WO/2011/139316 |
A lift device is disclosed that can be used to provide vertical lift to an aircraft or other vehicle. The lift device can include a fan that produces an airflow and a vane box that can direct the airflow. In one form the fan can be orien...
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WO/2011/137529 |
An all-terrain self-propelling landing cart for a helicopter, comprising a platform having a front end and a surface area sufficient to receive a landing helicopter; a wheeled undercarriage attached below the platform; a gasoline motor l...
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WO/2011/139316 |
A lift device is disclosed that can be used to provide vertical lift to an aircraft or other vehicle. The lift device can include a fan that produces an airflow and a vane box that can direct the airflow. In one form the fan can be orien...
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WO/2011/140551 |
A multi-modal vehicle ("MMV") 20a-20d. The MMV 20a-20d includes a fuselage 22 and a chassis 26 supporting at least three wheels 44 having deployed and stowed states. Extending away from the fuselage 22 is a canard wing system 28 and a ma...
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WO/2011/134614 |
The invention relates to a service supply system (10) for supplying passengers in a passenger compartment of a vehicle, in particular an aircraft, comprising a service supply line (12) and a number of service supply modules (14) which ca...
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WO/2011/136612 |
Disclosed are a baggage-transporting apparatus and a baggage-transporting method using same. The baggage-transporting apparatus according to the present invention comprises: a discharge unit which discharges the transported baggage; a co...
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WO/2011/135343 |
A fluid flow control device (10) for an aerofoil (11) comprises an aerofoil -tip body (17) of aerofoil shape, coupling apparatus (36) adapted to couple one end of the body (17) to an aerofoil (11), and a passive tip blowing assembly (16)...
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WO/2011/135135 |
The invention relates to a device (1) for installing a conducting component (2) on a structure (3) made of compound material, the inside of said structure (3) including a starter substance, that includes an installation element (4) on wh...
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WO/2011/135216 |
The present invention relates to a thrust reverser (1) having doors, which thrust reverser includes at least one stationary structure (3) on which at least one door (7) is mounted so it can pivot between a closed position in which said d...
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WO/2011/135214 |
The present invention relates to a support half structure for a nacelle of an aircraft engine, which half structure includes at least one longitudinal beam (1 a, 1 b) and a front half frame (3a, 3b), which are connected to each other and...
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WO/2011/134278 |
A joint equipment of a boarding bridge is provided, which is suitable for joining with a downwardly turned boarding gate of the aircraft and comprises a floor frame having a concave notch at its front end; a first floor arranged at the o...
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WO/2011/135605 |
A reduced dimensions platform (1) for the landing of an aircraft on an access facility (B) comprising a support base (2), suitable to be fixed on a reference surface (P) belonging to said access facility (B), and a landing footboard (3),...
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WO/2011/136805 |
An aerostatic platform (201) for monitoring an earth-based sensor network (210). The aerostatic platform (201) includes an aerostat (231), at least one antenna (241) coupled with the aerostat (231), and a plurality (251) of restraints (2...
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WO/2011/137335 |
A sonar buoy includes a fuselage having a tube-like shape, one or more wings coupled to the fuselage, an engine coupled to the fuselage and operable to propel the sonar buoy through flight, and a guidance computer operable to direct the ...
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WO/2011/135343 |
A fluid flow control device (10) for an aerofoil (11) comprises an aerofoil-tip body (17)of aerofoil shape, coupling apparatus (36) adapted to couple one end of the body (17) to an aerofoil (11), and a passive tip blowing assembly (16). ...
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WO/2011/134945 |
A water system (2) for a vehicle has at least one water supply source (4, 32), at least one water-conducting device, at least one shut-off valve (36, 38) and at least one germ reduction connection (34), wherein the germ reduction connect...
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WO/2011/134924 |
System and method for minimising buffeting in the case of an aircraft (2), wherein buffeting load control elements (10) which are provided in aerofoils of the aircraft (2) can be at least partly moved out of the aerofoils by a control me...
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WO/2011/134839 |
The invention relates a fastening system (10) for overhead storage bins (12) on a supporting structure that can be mounted in a suspended manner. Said system comprises at least one pair of suspension eye lugs (20, 22) attached to a suppo...
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WO/2011/134924 |
System and method for minimising buffeting in the case of an aircraft (2), wherein buffeting load control elements (10) which are provided in aerofoils of the aircraft (2) can be at least partly moved out of the aerofoils by a control me...
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WO/2011/137101 |
A deployment system (100) for user interface devices (200) with enhanced interface capabilities and methods for manufacturing and using same. The deployment system includes a main rotating joint system (110) and a device mounting assembl...
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WO/2011/135599 |
An active platform (1) for the landing of an aircraft on an access facility (B) including a support basement (2), suitable to be fixed on a reference surface (P) belonging to the aforesaid access facility (B), and a landing footboard (3)...
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WO/2011/134614 |
The invention relates to a service supply system (10) for supplying passengers in a passenger compartment of a vehicle, in particular an aircraft, comprising a service supply line (12) and a number of service supply modules (14) which ca...
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WO/2011/134917 |
The invention relates to an aircraft fuselage structure comprising a circumferential reinforcing frame (2) and a plurality of stringers (3) substantially perpendicular to the frame. The frame comprises a mechanically weakened area capabl...
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WO/2011/134984 |
Elevated airfield lighting device (10), comprising a main body (11) securable to a support (14) enabling the main body (11) to be fixed at an elevated position from ground (15), and at least one light unit (12, 13) comprising at least on...
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