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Patent Searching and Data


Matches 201 - 250 out of 6,715

Document Document Title
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...  
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...  
WO/2015/082854A1
The invention relates to a method for mounting an engine module (1) in a mount comprising a first structure (3) and a second structure (2) that is offset relative to the first structure (3), which method is intended to position at least ...  
WO/2015/078823A1
The invention relates to a method for operating a noise-emitting installation (11), which emits noise subject to noise protection provisions into the environment at specifiable times in the form of operationally determined noise events t...  
WO/2015/079032A1
The invention relates to a method for cleaning a jet engine by means of a cleaning medium that contains solids, which are introduced into the engine by means of a carrier gas using at least one nozzle. The pressure of the carrier gas is ...  
WO/2015/079124A1
This support (2) comprises: a frame (2.1); at least three suction cups (2.2); and connecting elements (2.4) for connecting an infrared emitter (4) to the frame (2.1). The frame (2.1) defines a closed outline. The support (2) further comp...  
WO/2015/073091A1
Embodiments of the present invention provide improvements to UAV launching systems. The disclosed launching system eliminates the use of hydraulic fluid and compressed nitrogen or air by providing an electric motor-driven tape that cause...  
WO/2015/067797A1
The invention relates to a system for detecting parameters of the environment and surroundings in connection with agricultural working machines. The system has at least one unmanned aerial vehicle (UAV) (1) which is designed for perpendi...  
WO/2015/068082A1
The present disclosure describes devices, assemblies, apparatus and methods useful in conducting health monitoring of structures including monitoring for structural damage and liquid (e.g., water, fuel, anti-Icing fluid, moisture, etc.) ...  
WO/2015/068923A1
The present invention relates to a mobile boarding bridge including an internal tunnel, and an external tunnel which is arranged to surround at least a portion of the internal tunnel from the rear side of the internal tunnel, and which i...  
WO/2015/069316A1
An apparatus for the cleaning of a turbine engine comprises a towable wash cart having a reservoir for cleaning fluid. The reservoir is connected through a pump system to a wash ring operatively mounted to the cart. The wash ring has a p...  
WO/2015/063750A1
A guiding apparatus for replicating the outline of a second component to a first component, the guiding device comprising a gripping unit adapted to grippingly engage the first component. A guide unit is adapted to contact an edge of the...  
WO/2015/059241A1
The invention relates to a device (100) for visually inspecting the external surfaces (90) of an aircraft, which comprises an inspection area for receiving an aircraft, at least one visual inspection robot (10), and a control center (50)...  
WO/2015/057832A1
A motor vehicle system includes a motor vehicle including an aircraft landing portion, and an actively propelled unmanned aircraft configured to be supported on the aircraft landing portion. The vehicle and aircraft are configured such t...  

Matches 201 - 250 out of 6,715