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Patent Searching and Data


Matches 501 - 550 out of 60,402

Document Document Title
WO/2018/066753A1
An unmanned aerial vehicle and an automatic charging device for the unmanned aerial vehicle are disclosed. In one embodiment, the unmanned aerial vehicle comprises a main body and a connection part. The main body includes: a battery; and...  
WO/2018/064918A1
Disclosed are a photographic device and an unmanned aerial vehicle comprising same. The photographic device comprises: a plurality of photographic units (9); a fixing unit (7) for fixing the plurality of photographic units (9); and a pow...  
WO/2018/067982A1
In a preferred embodiment, a modular lavatory system for replacing a conventional lavatory monument in an aircraft cabin includes a base lavatory module including a fore sidewall, an aft sidewall, and an aisle wall that form a housing en...  
WO/2018/064900A1
The present invention relates to a near space aircraft pod comprising a pod body (1) and a covering piece (2), wherein a heat dissipating part (11) is provided on the pod body for dissipating heat inside the pod body; and the covering pi...  
WO/2018/065737A1
The invention relates to a system for measuring the distance of an obstacle (14), in which an optical flow is radially measured in rotation around a circle (12) in a plane intersecting the obstacle; and the distance of the obstacle is de...  
WO/2018/067296A1
Systems, devices and methods are disclosed for detecting, characterizing and engaging unmanned vehicles. In one aspect, a method includes detecting an object, such as an unmanned aerial, land or aquatic vehicle that communicates using a ...  
WO/2018/067029A1
The invention relates to aviation engineering. Each variant of an aircraft canopy comprises a glazed housing having a front portion, an upper portion and convex lateral portions which protrude beyond the upper portion. The housing has tr...  
WO/2018/065704A1
The invention relates to a device for mechanical locking/separation by rotation, comprising a main body (1) secured to a first system, provided with an actuator (2) for rotatably actuating a rotatable rod (3) inserted into the main body;...  
WO/2018/066043A1
Provided is a delivery rotary-wing aircraft capable of stably landing on a destination free of influence from an updraft occurring in a region, such as tall buildings. This rotary-wing aircraft comprising a plurality of rotary wings, a c...  
WO/2018/067231A3
A gas turbine engine includes a compressor section and a turbine section together defining a core air flowpath. Additionally, a rotary component is rotatable with at least a portion of the compressor section and at least a portion of the...  
WO/2018/067028A1
The claimed invention relates to rotary wing aircraft and, in particular, helicopters having a single-rotor configuration. In one of its possible embodiments, the claimed helicopter comprises a fuselage, a tail boom, a tail rotor secured...  
WO/2018/065159A1
The invention relates to a method for replacing an aircraft part; in particular an aircraft turbine engine; the method comprising the following steps: (a) deciding (100) to replace a part, in particular a faulty part; (b) landing (102) t...  
WO/2018/066819A1
An unmanned aerial vehicle (UAV) according to various embodiments may comprise: a housing; a motor arranged in the inner space of the housing; a rotor which is rotated by the motor, and which comprises at least one cam structure; and at ...  
WO/2018/064831A1
Provided is a tripod head (100), comprising: a bracket (10), a roll axis motor assembly (21), a pitch axis motor assembly (22), a first camera (31) and a second camera (32); the first camera (31) and the second camera (32) are provided o...  
WO/2018/065703A1
The invention is directed to an attachment device (1) for attaching a booster (200) along a main body (100) of a space launch vehicle, comprising a combination of two pivots (2, 3) and of an annular linear connection (4), and to a space ...  
WO/2018/067499A1
In some embodiments, systems and methods are provided that limit the change in temperature and/or control a temperature of a product during delivery. Some embodiments provide systems comprising an unmanned delivery vehicle (UDV) comprisi...  
WO/2018/065336A1
An aircraft having a longitudinal axis determining a fore-aft direction, comprising at least two floats (111, 121)) configured to support the aircraft on a ground medium located below the floats with a ground-facing side of the floats, w...  
WO/2018/065274A1
Air start unit for starting and servicing jet engines in aircraft and other flying machines, wherein at least one compressor (1) is provided for generating air and a power supply (10) for supplying electrical power consumers. The propose...  
WO/2018/065882A1
The present discloses a system for washing and de-icing of aircrafts. The preset invention provides a hangar comprising three gantries to ensure different steps of the washing or the de-icing process. The structure of the gantries is ess...  
WO/2018/067310A1
An air intake assembly for an aircraft includes an auxiliary power unit intake that is defined by a skin of the aircraft. The auxiliary power unit intake is in fluid communication with an auxiliary power unit. The air intake assembly als...  
WO/2018/065731A1
The invention relates to a method for locating defects in an electrical line of an aircraft, said line comprising a plurality of electrical harnesses, said method comprising the following steps: determining a distance of a defect on the ...  
WO/2018/067329A1
A method of supersonic thrust generation includes generating a thrust supersonic exhaust plume (522) having a first average velocity from an engine (500), and expelling a bypass exhaust plume (532) having a second average velocity from t...  
WO/2018/067370A1
An air duct includes a first chamber and a second chamber, the first chamber being defined between an air handling device and the second chamber, and the second chamber being defined between the first chamber and an environment exterior ...  
WO/2018/065857A1
This disclosure relates to systems and methods for determining predicted risk for a flight path of an unmanned aerial vehicle. A previously stored three-dimensional representation of a user-selected location may be obtained. The three-di...  
WO/2018/066918A2
A flapping flight device according to the present invention is a flight device having at least one wing on each of the left and right sides of a fuselage so as to make a relative movement with regard to the fuselage by means of a driving...  
WO/2018/065977A1
A method for determining a route for a drone to deliver a package from an origin to a destination using vehicles that are not actively participating in a delivery of the package; a method for delivering the package from the origin to the...  
WO/2018/060970A2
An oblique rotor-wing aircraft may be capable of vertical take-off and landing, subsonic cruise, transonic cruise, and/or supersonic cruise. The oblique rotor-wing aircraft may comprise one or more of a fuselage, a rotor-wing, a thrust-v...  
WO/2018/058314A1
A control method, a control device (110), and an electronic device (100). The control method is used for controlling the electronic device (100). The electronic device (100) comprises a display (101) and a communication module (102). The...  
WO/2018/060392A1
Aircraft comprising a fuselage (1) divided by a floor (2) into an o upper volume (3) and a lower volume (4) through which joists (5) extend that support the floor and delimit, along with the fuselage and the floor, two side chambers (6),...  
WO/2018/059244A1
An aircraft, comprising: a power unit, used for generating air flow and comprising one or more exhaust ends; a lift assembly, comprising a wing body and one or more jetting pipes (301, 302); the jetting pipes (301, 302) are disposed at a...  
WO/2018/060186A1
The invention relates to a cabin wall element for thermal and acoustic insulation of an aircraft fuselage section located between two frames of an aircraft fuselage, wherein the cabin wall element has an outer wall which comprises a ther...  
WO/2018/060830A1
The present invention relates to a system for ice detection/prevention and flow control based on the impression of sliding plasma actuators with dielectric discharge barrier. This invention has advantages such as: reduced weight, low mai...  
WO/2018/061138A1
If a first number of operating thrusters, which is the number of thrusters brought into operation in a first thruster group (115), differs from a second number of operating thrusters, which is the number of thrusters brought into operati...  
WO/2018/061280A1
A flight restriction setting system according to an embodiment comprises a damage detection unit and a flight restriction calculation unit. The damage detection unit detects damage that occurred on a structure that constitutes an aircraf...  
WO/2018/058191A1
The present invention concerns a line release assembly and a connecting mechanism for use with an unmanned aerial vehicle ("UAV"), a UAV including the line release assembly and methods of use thereof. The line release assembly including ...  
WO/2018/063373A1
Disclosed are systems and methods of managing grey water or other recycled water onboard an aircraft based on demand within the aircraft. In some cases, the grey water is obtained from a lavatory or galley sink of the aircraft and is tre...  
WO/2018/060591A1
In order to reduce the weight of a hybrid propulsion system (30) for a multi-rotor rotary-wing aircraft, the system comprises at least one inverter (36) configured to supply power in parallel to multiple electric motors (46A, 46B) intend...  
WO/2018/060853A1
Methods and composite repair caps (26) for repairing composite stringers (12) of structures (10) of mobile platforms are disclosed. In one exemplary embodiment, a stringer repair method includes overlaying a pre-cured composite repair ca...  
WO/2018/062738A1
A hatch position indicating device for a boarding bridge is provided in the cab of a boarding bridge, which makes contact with an aircraft so as to form a passage for the movement of passengers, so as to indicate the position of a hatch ...  
WO/2018/059058A1
Disclosed is a landing control method for an aerostat, comprising sending a landing signal to the aerostat by means of a controller; a capsule body of the aerostat starting to discharge air to make the aerostat start to land until the la...  
WO/2018/063630A1
In an example, there is disclosed a drone operator computing apparatus having : a network interface; and one or more logic elements providing a broker agent to: communicatively couple to a drone brokerage engine via the network interface...  
WO/2018/060531A1
A secondary power unit for an aircraft comprises: a gas turbine engine (14) having at least one drive shaft, a twin load compressors (3) including first and second load compressors both coupled with the drive shaft, a first Ram-air intak...  
WO/2018/060830A4
The present invention relates to a system for ice detection/prevention and flow control based on the impression of sliding plasma actuators with dielectric discharge barrier. This invention has advantages such as: reduced weight, low mai...  
WO/2018/064209A1
In various embodiments, a tilt-wing aircraft includes a fuselage; a first wing tiltably mounted at or near a forward end of the fuselage; and a second wing rotatably mounted to the fuselage at a position aft of the first wing. A first pl...  
WO/2018/061823A1
An example of a control system shown in the present disclosure is a multi-copter control system provided with a plurality of motors for rotating a propeller, and a control unit for reading drive information of the motors, wherein said co...  
WO/2018/061230A1
A cable (130) comprises a flat wire (134). A parallel wire (133) is configured from a first wire (131) and a second wire (132) forming a pair and arranged side-by-side without being twisted together. The flat wire is configured such that...  
WO/2018/061667A1
The purpose of the present invention is to improve production efficiency and achieve cost reduction. When bonding a conical surface 3204 of a skirt part 32 and a conical surface 2204 of an inner liner 22 together using an adhesive, the s...  
WO/2018/062336A1
This flight control device 10 comprises a route information acquisition unit 11, a position identification unit 12, an environmental information acquisition unit 13, and a flight control unit 14. The route information acquisition unit 11...  
WO/2018/060579A1
The invention relates to an aircraft electrical network comprising an electrical device (28, 29) for protecting an outer surface of the aircraft from frost, which is suitable for being able to be supplied with power by a shared electrica...  
WO/2018/059991A1
A system for driving and guiding of a trailing edge control surface (24) arranged on a trailing edge region (6) of a wing (2) of an aircraft comprises a first guide device (9) attachable to the wing (2) and coupled with the control surfa...  

Matches 501 - 550 out of 60,402