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Patent Searching and Data


Matches 251 - 300 out of 6,868

Document Document Title
WO/2015/161280A1
The present disclosure provides an airplane ground deicing installation that minimizes the impact of deicing operations on the airport during icing conditions. The installation does not require alteration of a normal taxi pattern and can...  
WO/2015/160394A2
An asymmetric aircraft (1) and an aircraft (1) that can operate from small ships (8) and be stored in high density with three aircraft or more in one helicopter hangar (107) without needing a landing gear or wing fold. These aircraft sli...  
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/2015/160394A3
An asymmetric aircraft (1) and an aircraft (1) that can operate from small ships (8) and be stored in high density with three aircraft or more in one helicopter hangar (107) without needing a landing gear or wing fold. These aircraft sli...  
WO/2015/156857A3
The present disclosure is generally directed to a composite trailing edge control surface (600) including a contiguous one-piece composite control surface skin (200) wrapped around a plurality of stiffening cores (300), a plurality of hi...  
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/2015/155541A3
A device for marking a runway section, the device comprising: a light source; and a light director.  
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/2015/130374A3
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/2015/127178A1
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/2015/108588A3
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/2015/109077A1
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/2015/102855A3
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/2015/103000A1
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...  

Matches 251 - 300 out of 6,868