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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 ...
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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...
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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...
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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...
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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...
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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...
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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),...
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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...
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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...
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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...
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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...
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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...
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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 ...
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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...
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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...
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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...
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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 ...
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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...
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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...
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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...
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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...
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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...
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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...
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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...
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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...
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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...
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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...
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WO/2018/064657A1 |
An unmanned aerial vehicle (UAV) landing system is disclosed. The UAV landing system includes a memory; an imaging device; and a processor in communication with the memory and imaging device, wherein the processor is configured to: acqui...
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WO/2018/063945A1 |
The present disclosure is directed to a fan section positioned on a tail section of an aircraft, in which the fan section defines a circumferential direction, a radial direction, and an axial direction. The fan section includes a fan and...
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WO/2018/061502A1 |
[Problem] To provide a mechanism of wireless communication for a device that flies around freely in three-dimensional space. [Solution] A circuit provided with: an acquisition unit that acquires altitude information indicating a measurem...
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WO/2018/063019A1 |
The present invention relates to a vertical take-off and landing ("VTOL") aircraft and especially to this having hybrid or electric drive, used to transport people or goods from one point to the other without the necessity of airport run...
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WO/2018/063650A1 |
Methods, apparatus, systems and articles of manufacture to wirelessly power an unmanned aerial vehicle are disclosed. An example unmanned aerial vehicle (UAV) includes a first electrode assembly to capacitively couple to a first power ca...
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WO/2018/060808A1 |
An aircraft (A) comprising at least a component part (1, 2, 3, 4, 5, 6, 7, 8) provided with thermal de-icing means (S) suitable to eliminate and/or prevent the formation of ice on said component part, said de-icing means (S) are directly...
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WO/2018/063076A1 |
The present disclosure relates to a portable close air support system (200) and a payload carrier (20) for use in the system. The portable close air support system comprises a remote control station, an unmanned aerial system, UAS, and a...
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WO/2018/061112A1 |
The purpose of the present invention is to provide an application system and application method with which it is possible to reduce costs and improve work efficiency. An application system (1), (11), (21), (31) is provided with: a paint ...
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WO/2018/058771A1 |
Disclosed are a battery clamping mechanism (100), a battery (200) and an unmanned aerial vehicle (300), and a charging device (400), wherein the battery clamping mechanism (100) comprises: a metallic elastic piece (110) and a plastic fas...
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WO/2018/061176A1 |
[Problem] To provide a drone control system, a drone control method, and a program with which to control a drone so as to capture images in high resolution only when a prescribed condition is satisfied. [Solution] Provided is a drone con...
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WO/2018/061281A1 |
A composite material structure according to an embodiment of the present invention includes: a corrugated stringer that is formed of a composite material and has a plurality of hat portions; and a panel that is formed of a composite mate...
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WO/2018/061955A1 |
The present invention is a molded male hook-and-loop fastener that excels in fire retardancy and low fuming property and has on the surface of a substrate a large number of engaging elements projecting from the substrate, wherein both th...
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WO/2018/062983A1 |
In summary, the operation of the ultra-high-frequency (UHF) magnetic motor of this invention is based on generating extremely short and powerful electric, magnetic or electromagnetic field pulses and separating or disassociating said fie...
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WO/2018/058328A1 |
Disclosed is an airscrew protection cover (10). The airscrew protection cover comprises a protective support (100), and the airscrew protection cover also comprises a locking mechanism (103) provided on the protective support, wherein th...
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WO/2018/058297A1 |
Disclosed is a navigation lamp of an unmanned aerial vehicle. The navigation lamp comprises a light source (3) used for generating light, a light guiding element (4), and a light reflecting element (5). The light guiding element (4) comp...
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WO/2018/058769A1 |
Provided is a blade (100) used for an airscrew (300). At a position on the blade (100) where the distance from a centre of gyration of the airscrew (300) is 52.38% of the radius of gyration of the airscrew (300), the attack angle of the ...
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WO/2018/058672A1 |
A control method and device for an unmanned aerial vehicle, and an unmanned aerial vehicle (100). The method comprises: determining whether an unmanned aerial vehicle (100) has a fault according to monitoring information obtained by moni...
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WO/2018/058768A1 |
Provided is a blade (100) used for an airscrew (300). At a position on the blade (100) where the distance from a centre of gyration of the airscrew (300) is 51.28% of the radius of gyration of the airscrew (300), the attack angle of the ...
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WO/2018/061226A1 |
An artificial satellite (100) is provided with two pointing mechanisms (110, 120). Each pointing mechanism is provided with a main body-side gimbal (111, 121), an expansion boom (112, 122), a thruster-side gimbal (113, 114), and a thrust...
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WO/2018/064324A1 |
An aircraft passenger seat has a seat back including a lower portion pivotably mounted to a seat bottom and an upper portion rotatably coupled to the lower portion. The upper portion may rotate in a forward direction relative to the lowe...
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WO/2018/060361A1 |
A trolley (2) for collecting waste includes: wheels (24), a steering handle (26), and a housing (4) with a bottomwall (6) and a sidewall (8) extending vertically from the bottomwall (6), wherein the housing (4) forms a waste chamber (10)...
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WO/2018/057241A1 |
An aircraft is provided including a boundary layer ingestion fan mounted to an aft end of a fuselage. A stabilizer is mounted to the fuselage and extends between a root portion and a tip portion to define a span-wise length and extends b...
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WO/2018/057230A1 |
An aircraft is provided including a fuselage that extends along a longitudinal direction between a forward end and an aft end. A boundary layer ingestion fan is mounted to the fuselage at the aft end and is configured for ingesting bound...
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