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WO/2013/068575 |
The invention relates to a cleaning machine for windows (F) façade elements, solar modules, and smooth-surfaced surface elements of that kind, in particular at great height, which cleaning machine enables quick and efficient cleaning in...
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WO/2013/070258 |
Water is mixed with fire suppressant polymer in a mixer absent a power source. The mixer receives water through a water inlet with water exhibiting high velocity and associated hydrodynamic force. Such velocity is achieved by locating th...
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WO/2013/068671 |
The invention relates to a composite panel (30) including at least one inner skin (3) and one outer skin (2) and having at least one opening (5) for receiving a sampling scoop, which forms a channel and the sampling opening of which is i...
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WO/2013/070112 |
In order to increase the operational reliability of a direct vision window in icing conditions, ensure that the window can be opened in flight, reduce the forces on the handle of the window during closing and ensure the airtight compress...
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WO/2013/070296 |
An aircraft apparatus is disclosed that has a fuselage boom (102) having proximal (110) and distal (103) ends, a wing (108) coupled to a proximal end (110) of the fuselage boom (102) and at least one transparent stabilizer (104, 106) cou...
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WO/2013/067886 |
A refrigeration system (200) for aircraft is provided, which includes: a first stage heat exchanger (102) for receiving hot bleed air from an engine; a second stage heat exchanger (106) with an inlet communicated with an outlet of the fi...
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WO/2013/067885 |
The present invention provides a spoiler for a hatch door on an aeroplane, which spoiler is installed on the inner covering of the hatch door, inside the wind-facing leading edges of the front hatch door on the left and right of the fron...
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WO/2013/070061 |
The present invention discloses a vehicle (1) capable of being converted between a flying condition and an automotive riding condition. The vehicle has a telescopically extendable tail (10) comprising a first tubular tail segment (11) an...
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WO/2013/068496 |
The invention relates to an anchoring harpoon that includes a bistable actuator (34) comprising a rod (56) for actuating the finger (32) that is movable between a retracted rest position and an extended deployment position of the finger ...
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WO/2013/066477 |
A motor assembly that includes a motor (102) having a rotatable shaft (100), a hub (106) coupled to the rotatable shaft (100), the hub (106) having a propeller indexer (118) to receive a propeller (104), when the propeller (104) is prese...
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WO/2013/066954 |
An emergency vision apparatus comprises an inflatable first enclosure, the first enclosure being made of airtight material and having an expanded form when deployed and a deflated form when not in use; and first and second clear members ...
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WO/2013/066690 |
A system and method for improving the lift-drag ratio of an aerodynamic surface or hydrodynamic surface such as a wing or blade-structure of a propeller, rotor or a turbine, in a fluid such as air or water, is disclosed. The aerodynamic ...
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WO/2013/066475 |
A motor assembly that includes a motor (102) having a motor casing (112), a rotatable shaft (100) extending from said motor casing (112) to a shaft length and a hub (106) coupled to said rotatable shaft (100), the hub (106) having a circ...
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WO/2013/066674 |
A method for tensioning a membrane includes affixing a first wire to a first portion of the membrane and affixing a second wire to a second portion of the membrane. The membrane is tensioned between the first wire and the second wire by ...
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WO/2013/066173 |
The invention relates to a fiber-metal laminate of mutually bonded fiber-reinforced composite layers and metal sheets, the laminate comprising a combination of a fiber- reinforced composite layer and an adjacent metal sheet, in which com...
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WO/2013/063869 |
A lighting/sound-producing device activated by an inflated balloon comprising a lamp/sounder, a battery (4), and an enclosure (5). Enclosed in the enclosure (5) is at least a lamp/sounder. The enclosure (5) comprises a gas inlet end (51)...
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WO/2013/066319 |
A vibration isolator (100) includes a flexure (102), a constrained VEM layer coupler (104), and a constrained VEM layer (106) configured to oppose relative translational and rotational motion between points of the flexure. The flexure ma...
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WO/2013/066462 |
An aircraft store ejector systems and subsystems thereof. Embodiments can include a two-reservoir re-pressurization system wherein a remote reservoir is used to maintain desired pressure in a local ejector reservoir. The system can inclu...
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WO/2013/066570 |
A latch (10) includes a base (12), a drive shaft (100) and cam (102), and a handle (110) attached pivotally to the drive shaft (100). The handle (110) is moveable between a closed position, a pop-up position, and an open position. A slid...
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WO/2013/067021 |
An aircraft that includes a cabin that has a floor, side walls, a ceiling and an interior, a first class section positioned in the interior that includes a longitudinally extending first aisle extending therethrough, a first door positio...
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WO/2013/066390 |
A flying device is provided, including a disk configured to rotate around its axis, a ring in parallel with the disk, multiple loads coupled to the disk and the ring, multiple first pivots circularly arranged in the peripheral region of ...
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WO/2013/064768 |
A turbo engine attachment pylon, configured to connect a turbo engine to a structural element of an aircraft, said pylon (30) having an aerodynamic profile defined by two opposing lateral faces and delimited longitudinally between a lead...
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WO/2013/064856 |
Method for storing a respiratory mask (10) comprising: providing a respiratory equipment (1) including: a respiratory mask (10) having a front side (10a) and a rear side (10b), the respiratory mask (10) comprising a cavity (15) having an...
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WO/2013/066439 |
An air vehicle wing includes foldable ribs (52) coupled to a leading-edge spar (32). The ribs each have multiple rib segments (52a-52d) which are foldable (hinged) relative to each other. Extension linkages (54), each with multiple exten...
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WO/2013/065795 |
Provided is a device for removing space debris and a method for removing the space debris which enable the installation of a deceleration device with ease with respect to the space debris which is undergoing a tumbling motion. The presen...
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WO/2013/065311 |
The present invention provides a lightning-proof fastener able to reliably seal an arc between a cap and a wing panel. One end (30a) of the cap (30A) on the open side opposing member (22), or member (21), has a flat surface (30d) orthogo...
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WO/2013/066537 |
A mechanical fitting for connecting structures includes a base structure (504) and a plate member (506,508). The mechanical fitting also includes a support structure (510,514) for supporting the plate member at a predetermined spacing fr...
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WO/2013/065722 |
An artificial satellite is provided with at least one hatch formed in the wall of the artificial satellite which is in contact with the dead space therein, and a hatch opening/closing mechanism for opening the hatch; an antenna is mounte...
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WO/2013/062312 |
The present invention relates to a flying submarine probe, comprising: airplane-type wings arranged at the left and right sides of an enclosed hull, such that the wings are adjustable in the horizontal and vertical directions by up to 18...
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WO/2013/063606 |
A hand-held interactive entertainment device which winds and unwinds a lighter- than-air balloon on a tether by applying pressure to the device.
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WO/2013/060318 |
An unmanned high altitude aircraft, in particular a stratosphere aircraft, comprising at least one fuselage (10), wings (13, 14), control surfaces (13", 14", 20', 20", 21', 21") and at least one drive device (15, 16, 17) that has at leas...
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WO/2013/062608 |
An aircraft defining an upright orientation and an inverted orientation, a ground station; and a control system for remotely controlling the flight of the aircraft. The ground station has an auto-land function that causes the aircraft to...
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WO/2013/063599 |
A passenger seating arrangement for an aircraft cabin that includes first and. second adjacent columns of at least two seats that define a first longitudinally extending center axis that extends approximately parallel to a longitudinal a...
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WO/2013/062706 |
Described herein is a self-powered system for detecting a current spike. The current spike is delivered through a current return network that energizes a resonant circuit to produce an alternating electrical output. The output is rectifi...
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WO/2013/060615 |
The present invention relates to a fastening arrangement for plateshaped facing components. The fastening arrangement comprises at least one profiled rail (4) comprising legs (5), an intermediate space (6) being formed between these legs...
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WO/2013/061563 |
A dispersal assistance apparatus provides assistance information to a pilot dropping dispersal matter so that the dispersal is efficiently accomplished when dispersing dispersal matter from an aircraft over a target location on the groun...
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WO/2013/061276 |
A fluidic system is disclosed. The system comprises a plurality of fluidic oscillatory actuators, and at least one synchronization conduit connecting two or more of the actuators such as to effect synchronization between oscillations in ...
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WO/2013/060455 |
The invention relates to a construction element (1) and a corresponding system which allow the use of vacuum-properties in the field of construction with the lowest possible use of resources in a particularly easy manner. In particular, ...
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WO/2013/061351 |
An aerodynamic profile is described, comprising at least one portion of aerodynamic profile (1) composed of at least one first supporting profile (3a) and at least one second supporting profile (3b) adapted to support at least one layer ...
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WO/2013/060916 |
Optimized stringer run-out zones in aircraft components. These are arranged in a panel (11) of a composite material formed by a skin (13) and at least one reinforcing stringer (15) formed by a web (17) and a flange (19) connected to said...
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WO/2013/061348 |
The invention relates to a constant velocity universal joint for each type of transmission and in particular for helicopters with rotors called gimballed, in which the hub (2) of a rotor equipped with blades (7) is supported on a transmi...
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WO/2013/056492 |
A composite aircraft consisting of a fixed-wing and electrically driven propellers and having helicopter functions comprises a fixed-wing aircraft assembly. The assembly comprises an aircraft body (1), wings (2), and a fixed-wing rudder ...
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WO/2013/056626 |
Disclosed is a tool for aircraft fuel oil precipitate discharge, which is used within an aircraft wing rectifier hump for opening an aircraft fuel oil precipitate discharge valve to discharge precipitate in a fuel tank. The tool for airc...
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WO/2013/058171 |
This aircraft is provided with the following: a target-attitude-control-command calculation unit (42) that computes a target-attitude control command on the basis of the amount that a control stick is manipulated; a gain-value generation...
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WO/2013/057193 |
The invention relates to a device for expelling/containing a predetermined liquid, said device being capable of being built into a liquid tank that is to operate at low or zero gravity, and including a unitary three-dimensional so-called...
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WO/2013/056300 |
A vortex generator (9) is formed in a nozzle (9) having an inlet (10) and an outlet (11). A toroidal chamber (13) is provided in the midsection (12) of the nozzle, opening into the inner surface (15) of the nozzle through a narrow circum...
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WO/2013/058173 |
This aircraft (10) is provided with the following: a mechanical linkage (18) that mechanically transmits manipulation of a control stick (12) to a steering mechanism (16); a manipulation-amount sensor (22) that detects manipulation amoun...
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WO/2013/057192 |
The subject matter of the invention is a method for surveying a production plant (13) having production facilities (19a, 19b, 19c, 19d). The invention provides for the survey to be performed by means of an aircraft (12), which to this en...
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WO/2013/058929 |
A mounting system for tubular structures within a wing structure provides for positioning of the tubular structure as it passes through wing ribs. The system provides for electrostatic protection from discharges between the rib and the t...
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WO/2013/057137 |
A cabin attendant seat (10) comprises a carrier element (12) which comprises a backrest section (14) and a base section (16) that carries said backrest section (14). A seat element (18) is fastened to the carrier element (12). At least o...
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