| Document |
Document Title |
|
WO/2015/160697A1 |
A vehicle-based airborne wind turbine system having an aerial wing, a plurality of rotors each having a plurality of rotatable blades positioned on the aerial wing, an electrically conductive tether secured to the aerial wing and secured...
|
|
WO/2015/160836A1 |
An airfield lighting system can comprise a control system, a constant current regulator, and a plurality of light fixtures. The control system can command the constant current regulator to output a current level transition sequence. One ...
|
|
WO/2015/155086A1 |
The invention relates to an assembly comprising an unmanned transport device (1) for delivering a shipment (2) and a transfer device (4), said transfer device (4) being designed to lower the shipment (2) from the unmanned transport devic...
|
|
WO/2015/155166A1 |
A service vehicle for aircraft comprising a wheeled chassis (2) having an operators cab (8) at a forward end thereof, a container body (10) being mounted on the chassis behind the operators cab via a lifting means (12) enabling the conta...
|
|
WO/2015/155541A2 |
A device for marking a runway section, the device comprising: a light source; and a light director.
|
|
WO/2015/155487A1 |
The invention relates to a device for aiding remote-diagnosis in the course of an endoscopy of an aircraft engine, comprising at least one endoscope (2) used in situ by a first operator (20) to capture images of said engine and to perfor...
|
|
WO/2015/155087A1 |
The invention relates to a method for delivering a shipment by an unmanned transport device (1) to a receiving container (2) for said shipment (6), the method comprising the following and additional steps: moving the unmanned transport d...
|
|
WO/2015/150027A1 |
The invention relates to a method for pre-assembling parts (90, 91), with the insertion of mastic, comprising surface preparation carried out by spraying cold plasma produced by a plasma gun carried by a preparation robot, onto the surfa...
|
|
WO/2015/150842A1 |
Thermal column generator that -through its big metallic surfaces with changeable characteristics placed against the sunray - is creating easy-to-find thermal columns (upbound warm air columns) for the engine-free flying structures and by...
|
|
WO/2015/150421A1 |
The invention relates to equipment for cleaning jet engines, said equipment comprising a supply device (13) for providing a cleaning agent (15), a nozzle device (16) for introducing the cleaning agent (15) into the jet engine (17) and a ...
|
|
WO/2015/143545A1 |
A system and method for troubleshooting problems in complex systems using multiple knowledgebases comprises a first knowledgebase that has a case-based reasoning engine and knowledge from which a first set of possible solutions can be de...
|
|
WO/2015/148876A1 |
The present invention is directed to a method of mitigating ice build-up on a substrate, comprising applying to the substrate curable film-forming compositions comprising isocyanate-functional curing agents, film-forming compositions wit...
|
|
WO/2015/143478A1 |
A method of landing an aircraft which is overweight or whose landing wheels are not operatively deployed, including: providing a carriage assembly which may travel along a landing path at the landing speed of the aircraft; providing brak...
|
|
WO/2015/140863A1 |
Provided is a testing device for testing the strength of an aircraft using a curved specimen, the testing device being capable of safely and quickly generating desired stress by reliably applying inner pressure to the specimen, the testi...
|
|
WO/2015/136191A1 |
The invention concerns a deployable device for covering the path of passengers between a terminal building and a transport means, for example an aerial transport means (4), comprising a rigid structure (1) defined by parallel upper segme...
|
|
WO/2015/136388A1 |
An apparatus for providing preconditioned air to at least one aircraft parked on the ground wherein internal heat exchangers lower or raise the discharge air temperature. The apparatus comprises a main housing unit comprising a vent for ...
|
|
WO/2015/134707A1 |
Embodiments of the present invention provide systems and methods for vehicle arresting systems made from low-density particles and appropriate binders. The systems are designed to provide a barrier or a bed that is placed at the end of a...
|
|
WO/2015/134463A1 |
Embodiments of the present disclosure relate generally to macro-patterned materials and methods of their use in connection with vehicle arresting systems. Certain embodiments provide 3-D folded materials, honeycombs, lattice structures, ...
|
|
WO/2015/132511A1 |
The invention relates to an aircraft landing strip infrared beacon (10) comprising: a mounting plate (12) and a housing (8) that is attached onto the mounting plate. The transverse sizes of the mounting plate (12) are greater than the tr...
|
|
WO/2015/130374A2 |
Wind energy systems, such as an Airborne Wind Turbine ("AWT"), may be used to facilitate conversion of kinetic energy to electrical energy. An AWT may include an aerial vehicle that flies in a path to convert kinetic wind energy to elect...
|
|
WO/2015/127503A1 |
A processing station for registering a piece of passenger's luggage for a trip, wherein the processing station comprises: an injector for receiving the piece of luggage associated with the passenger; at least one sensor associated with t...
|
|
WO/2015/127178A1 |
A payload launch system is described that provides one launch solution suitable for multiple applications. A payload, such as a UAV, is launched from a sealed launch tube using compressed gas or other energy source. The launch tube can b...
|
|
WO/2015/124888A1 |
Methods (100, 200) of determining an overall performance of air-conditioning system(s) including transmitting data (102, 202) from a sensor operably coupled to at least one air-conditioning pack, comparing (104, 204) the transmitted data...
|
|
WO/2015/122939A1 |
An aircraft fuselage is constructed of a plurality of cylindrical semi-monocoque fuselage sections that are each constructed with mirrored screw threads on either their interior or exterior surfaces. The screw threads of adjacent fuselag...
|
|
WO/2015/123500A1 |
A method for balloon launching may include loading a pre-packaged balloon and payload into a shell structure. The pre-packaged balloon may be pulled out of its packaging in a vertical direction, for instance using a gantry crane. The gan...
|
|
WO/2015/114276A1 |
Structure (310) for transporting and hoisting a turbomachine (312), said structure comprising a hoisting interface (328) arranged on a rigid hoisting arm (318) which extends over the turbomachine and is connected to a rigid transport arm...
|
|
WO/2015/115751A1 |
The present invention relates to a system and a method for wireless control of a pilot display unit, wherein the system can comprise: a central operating system for authorizing control rights to control the pilot display unit; a type det...
|
|
WO/2015/113945A1 |
The present invention concerns an apparatus for treating surfaces or carrying out maintenance/inspection tasks of the top of a vertical stabilizer (31) of an aerial vehicle by at least one technician comprising:- a single overhead crane ...
|
|
WO/2015/111998A1 |
The invention relates to a method for producing a protective housing for the turbine of an aircraft engine, and checking same for internal impacts. Said method has the following steps: receiving specifications and tolerances; design, pro...
|
|
WO/2015/108850A1 |
A method and system for identifying a data recorder based upon a unique signature generated for the data recorder. Configuration information is received, the information specifying a plurality of data recording input parameters which are...
|
|
WO/2015/107558A1 |
The present invention concerns a landing and/or docking system for aerial vehicles, comprising two infrared emitters, respectively a position emitter (10), and an axis emitter (11), located on a landing surface and able to transmit respe...
|
|
WO/2015/109077A1 |
A composite bonded repair method for an aircraft is provided. The method includes generating a doubling patch of a portion of the aircraft from topographic data, filling damage at the portion of the aircraft with filler material, applyin...
|
|
WO/2015/108588A2 |
Provided herein are systems and method for autonomously or semi-autonomously landing an unmanned aerial vehicle (UAV) on a landing pad. The landing pad can include features configured to correct misalignment of the UAV on the landing pad...
|
|
WO/2015/102870A1 |
An airborne wind turbine system including an aerial vehicle having a fuselage, an electrically conductive tether having a first end secured to the aerial wing and a second end secured to a platform, a rotatable drum positioned on the pla...
|
|
WO/2015/103013A1 |
A method may involve operating an aerial vehicle to travel along a first closed path on a tether sphere while oriented in a crosswind-flight orientation. A tether may be connected to the aerial vehicle on a first end and may be connected...
|
|
WO/2015/103000A1 |
Systems and methods are provided for a wiring harness for an aerial vehicle. A wing of the aerial vehicle comprises a pocket for insertion of the wiring harness. The wiring harness provides wiring and associated connections capable to at...
|
|
WO/2015/102855A2 |
A drum for storing an electrically conductive tether having a first end secured to an aerial vehicle and a second end secured to a ground station that includes a drum frame rotatable about a drum axis, a drum surface positioned over the ...
|
|
WO/2015/099865A1 |
Apparatus are disclosed that are configured to distribute internal loads from a drive mechanism to a solid fixed shaft and rotatable tubular shaft coupled to a propeller, for example. An example apparatus involves: (a) a stator, (b) a ce...
|
|
WO/2015/097105A1 |
The invention relates to a test and simulation system comprising a first level comprising a communication layer in the form of a ring computer network provided with communication nodes consisting of interconnected routing means, a second...
|
|
WO/2015/100242A1 |
Methods and systems are provided to wrap a faired tether around a drum. The tether may be connected to an aerial vehicle. The method may involve guiding a faired tether around an exterior surface of a drum, wherein the drum comprises a h...
|
|
WO/2015/099846A1 |
A retrieval device for an unmanned aircraft. The retrieval device may include a frame that supports a flexible material. The flexible material may form a receptacle portion shaped to receive the unmanned aircraft. The flexible material m...
|
|
WO/2015/100005A1 |
Methods and systems described herein relate to power generation control for an aerial vehicle of an air wind turbine (AWT). More specifically, the methods described herein relate to balancing power generation or preventing a component of...
|
|
WO/2015/097457A1 |
An air conditioning system (32) for an aircraft mover (10) motively powered by a driving engine (28). The air conditioning system (32) comprises a supplementary internal-combustion engine (62), a hydraulically powerable compressor (38),a...
|
|
WO/2015/090263A1 |
In order to simplify an integration of systems on an aircraft fuselage, the invention provides a production method for producing a supporting fuselage panel (10) for a fuselage portion of an aircraft fuselage in a region of an aircraft c...
|
|
WO/2015/092422A1 |
There is provided a method of moving an aircraft using an aircraft mover (10), preferably an aircraft tractor. The method comprises the steps of: a] accelerating the aircraft up to speed using one or more electric motors (16) drivable by...
|
|
WO/2015/094941A1 |
An assembly (500) that includes a table (400) having first and second levels (402 and 404), an indicator (406) disposed on the first level (402) and a sealing component (450). The first level (402) is arranged to receive a first sheet po...
|
|
WO/2015/095222A1 |
Wind energy systems, such as an Airborne Wind Turbine ("AWT"), may be used to facilitate conversion of kinetic energy to electrical energy. An AWT may include an aerial vehicle that flies in a path to convert kinetic wind energy to elect...
|
|
WO/2015/088971A1 |
Unless otherwise indicated herein, the materials described in this section are not prior art to the claims in this application and are not admitted to be prior art by inclusion in this section. Power generation systems may convert chemic...
|
|
WO/2015/088338A1 |
A ground support system (1) for an aircraft having a turbine engine, which ground support system comprises; an intermittent combustion engine (2), a generator (3) which is driven by the combustion engine to supply electrical power with a...
|
|
WO/2015/088612A1 |
An aircraft ground power connector (18) for use in an aircraft ground power support system providing electrical power from a ground power unit (12) through a ground power cable (16) to the ground power receptacle (20) of a parked aircraf...
|
