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Matches 1 - 50 out of 5,726

Document Document Title
WO/2019/159478A1
The method for producing an assembly is a method for producing an assembly equipped with a member to be reinforced (20), a reinforcing member body (41), and a filler (42), wherein the reinforcing member body (41) has a pair of flanges (4...  
WO/2019/157830A1
Disclosed are a built-in antenna of an unmanned aerial vehicle, and an unmanned aerial vehicle. The built-in antenna of the unmanned aerial vehicle comprises a substrate and a microstrip antenna provided on the substrate. The substrate i...  
WO/2019/155335A1
An unmanned aerial vehicle (12) includes a fuselage body (20), a lift mechanism (30) coupled to the fuselage body, and a depth sensing and obstacle avoidance system (32) coupled to the fuselage body. The depth sensing and obstacle avoida...  
WO/2019/156604A1
The present invention regards a hollow load-bearing beam structure (1) and a method for manufacturing of the structure. The structure (1) comprises fiber-reinforced composite material. The structure (1) comprises a first plurality of lam...  
WO/2019/147634A1
Disclosed is a modular, palletized system for a deployable sensor that provides for easy deployment with minimal interconnection to the vehicle carrying such system, and with no requirement for modification to the vehicle carrying such s...  
WO/2019/144301A1
Provided are a mechanical arm assembly and an unmanned aerial vehicle, said mechanical arm assembly (100) being used for said unmanned aerial vehicle, the unmanned aerial vehicle comprising a body (200), and the mechanical arm assembly (...  
WO/2019/146431A1
Provided is a flying device in which an arm is turnably attached to a fuselage base out of consideration for transport and the strength of the connecting portion between the arm and the fuselage base is sufficiently ensured. In the prese...  
WO/2019/145584A1
Specially designed for fire fighting, the drone of the invention is in the form of a hexacopter in which the main rotors are distributed according to two parallel alignments of three motors, and the motors are in the form of thermal moto...  
WO/2019/143747A1
A latch mechanism includes a handle connected to a pin by a linkage. The linkage converts rotation of the handle relative to a frame into axial movement of the pin between extended and retracted positions relative to the frame. Furthermo...  
WO/2019/143764A1
A shock absorber includes a first end configured to be mechanically fastened to a first component, a second end configured to be mechanically fastened to a second component, a main body, a main shaft, and a primary piston. The primary pi...  
WO/2019/140659A1
An anmanned aerial vehicle, comprising: a casing (200), a circuit board assembly (100) accommodated in the casing (200), and a load disposed on the casing (200). The circuit board assembly (100) comprises a circuit board (10) and an iner...  
WO/2019/142961A1
Provided is a boom coupling device for an unmanned flying object, the device connecting a blade portion for providing the unmanned flying object with flight power to a body thereof. The boom coupling device comprises: an outer connector ...  
WO/2019/134356A1
Provided are an unmanned aerial vehicle (UAV), a power train, and a method for reducing air resistance in the UAV. A motor is arranged within a support arm or a wing such that a motor shaft is parallel to the longitudinal axis of the sup...  
WO/2019/133354A1
The present invention is directed to multifunctional surfacing films each comprising: (a) a single layer of curable polymer composition having opposing first and second surfaces: (b) a peelable porous sheet disposed at or beneath the sec...  
WO/2019/127217A1
An arm assembly (10) and an unmanned aerial vehicle (100). The arm assembly (10) is rotatably connected to a frame body (101) of the unmanned aerial vehicle (100). The arm assembly (10) comprises an arm body (1), and an electric connecti...  
WO/2019/127394A1
An unmanned aerial vehicle (100), a fuselage assembly (10) and a protective cover (16) of an unmanned aerial vehicle fuselage (12). The fuselage (12) is provided with a data hole (1245), and the protective cover (16) may block the data h...  
WO/2019/129762A1
The invention relates to an assembly for arming/disarming an aircraft door slide, said assembly comprising a system with two releasable connection mechanisms (2) connecting to the door (1) and an aircraft cabin floor, each mechanism (2) ...  
WO/2019/131893A1
Provided is a composite material that achieves weight reduction and separation prevention. The composite material comprises: a body section 16A in which fibers 16C are aligned in a matrix in a first direction X; and a stress relief secti...  
WO/2019/127360A1
Provided is a centre frame applied to an unmanned aerial vehicle, the centre frame comprising a frame assembly (1), wherein the frame assembly (1) comprises multiple frame members (11), the frame members (11) form an integrated structure...  
WO/2019/123334A1
An emergency exit (5a, 5b) for a helicopter (1) is described that comprises: a wall (9) defining an opening (6); a removable part (10) engaging the opening (6) in a removable manner; and a seal (12) interposed between the wall (9) and th...  
WO/2019/123215A1
An aircraft fairing (10) includes a fairing body having an exterior fairing wall (11) and at least one wheel bin (20). The at least one wheel bin (20) has a side wall (22) extending from an opening in the exterior fairing wall (11) to an...  
WO/2019/125322A2
The cover assembly developed by the present invention which provides for the pilot candidate to operate the air vehicle by utilising only the control equipment without seeing the outer environment in which the air vehicle is present, com...  
WO/2019/126275A1
Example implementations may relate to door-enabled loading and release of payloads in an unmanned aerial vehicle (UAV), which could be a type of UAV in a group of UAVs that is assigned to carry out certain transport tasks. In particular,...  
WO/2019/121337A1
The invention concerns an opening system (10) for an auxiliary aircraft door (20) in a fuselage (30), the door and the fuselage having skins in the extension of one another. In an embodiment, this system (10) comprises a frame lintel (11...  
WO/2019/113689A1
A noise attenuating device for reducing acoustic resonance in a cavity of an aircraft with an opening in a skin of the aircraft defining a first surface area and an opening peripheral edge includes a connection mechanism for securing the...  
WO/2019/115233A1
The present invention relates to a freight transfer module (1) for installation in a hold (14), having: a base unit (2) which can be arranged in an inlet region of a hold (14) and covers at least one partial surface of the inlet region o...  
WO/2019/115232A1
The invention relates to a cargo management system for loading and unloading cargo (C) into and out of a cargo area of a mobile object (1), wherein loose piece goods can be provided individually or collectively in a container-type recept...  
WO/2019/115230A1
A conveying device for installation in a hold (10) of an aircraft has a plate-shaped base (1) on the upper side of which there are provided a plurality of exposed bearing bodies (2), for movably mounting cargo items (9), and a plurality ...  
WO/2019/115931A1
Glazing unit (1) comprising at least one structural substrate (10, 15), termed inner substrate, intended to face towards a receiving structure (2) within which the glazing unit is intended to be fastened, and having a face (10A, 15A), te...  
WO/2019/106514A1
The present disclosure relates to an aircraft comprising a frame that includes a plurality of tubes, where the plurality of tubes can include a first tube and a second tube that are fastened with each other using at least one fork plate....  
WO/2019/107009A1
The present invention addresses the problem of providing an unmanned aerial vehicle capable of efficiently reducing the horizontal dimension of the fuselage. The problem is addressed by: an unmanned aerial vehicle equipped with a rotor, ...  
WO/2019/100483A1
An unmanned aerial vehicle-based load control method and device, and an unmanned aerial vehicle. The method comprises: on the basis of a load object, determining a carrying gravity of an unmanned aerial vehicle (101); according to the ca...  
WO/2019/095591A1
The present invention relates to the field of heat dissipation for unmanned aerial vehicles, and disclosed thereby is a heat dissipation system for use with an unmanned aerial vehicle-mounted device, comprising a plurality of rotors that...  
WO/2019/090046A1
An aircraft includes an airframe having a fixed-wing section and a plurality of articulated electric rotors, at least some of which are variable-position rotors having different operating configurations based on rotor position. A first o...  
WO/2019/079897A1
A lock for an aircraft door. The lock includes an outer shell having an inner cavity. A core is rotatably mounted within the inner cavity to rotate about an axis of the core. The core has a keyhole extending through the core from a first...  
WO/2019/081446A1
Mechanism (10) for opening/closing an opening leaf (12) with respect to a frame (14). The mechanism (10) is configured to cause, upon opening, a lifting of the opening leaf (12) from a closure plane to an opening plane parallel to the cl...  
WO/2019/073730A1
An upper skin 11, which is a constituent member of a wing 10, is divided into a plurality of regions 20 along a surface thereof. The plurality of regions 20 include first regions 201 formed from high-strength composite materials, and sec...  
WO/2019/072980A1
The invention is concerned with a noise attenuation element arranged in use for connection to an air directing structure such as a wing flap. The element has a non-uniform lattice density across at least a portion of the body of the elem...  
WO/2019/069498A1
A frame 10 for a multicopter 1 includes a frame body 24 having an opening 34 in a top surface thereof and having a first recessed section 36 that can accommodate a battery 12 and an electrical box 14. A flange section 66 is formed integr...  
WO/2019/070438A1
An emergency vision apparatus includes a housing for attachment underneath an instrument panel in a cockpit, the housing including a front opening, a front cover for the front opening, a bottom portion of the front cover being pivotably ...  
WO/2019/070752A1
An automated flying transport vehicle that capitalizes on the strengths and complexities of a fixed and rotary winged aircraft. The air transport vehicle comprises a body aerodynamically designed to generate lift and a plurality of rotor...  
WO/2019/061100A1
Disclosed are a wing assembly (10) and an unmanned aerial vehicle (100), the wing assembly (10) comprising: a first wing (11), a second wing (12), and a connection mechanism (13) for connecting the first wing (11) to a body (101) of the ...  
WO/2019/061415A1
Disclosed are an unmanned aerial vehicle and a frame assembly thereof. The frame assembly of the unmanned aerial vehicle comprises a central frame, a first arm (10) and a second arm (20), wherein the first arm (10) is provided with a fir...  
WO/2019/063665A1
A thermal or acoustic or thermoacoustic insulation compound includes at least one aerogel, calcite, hydrated lime and a component constituted by at least one flame retardant.  
WO/2019/061473A1
Disclosed are an unmanned aerial vehicle and a frame assembly thereof. The frame assembly comprises a central frame, a first arm (10), a second arm (20), a synchronization device (30), a locking device (40) and a mounting base (50), wher...  
WO/2019/061401A1
Disclosed are an unmanned aerial vehicle frame assembly, and an unmanned aerial vehicle. The frame assembly comprises a central frame, a first arm (10) and a second arm (20), wherein a synchronization device (30) enables the first arm (1...  
WO/2019/060575A1
A cupola fairing (250) for reducing drag and increasing lift on an aircraft fuselage (210) and wings (220). The fairing includes a housing length extending along a longitudinal axis, and a variable width extending normal to the longitudi...  
WO/2019/053658A1
Aircraft (1) comprising a fuselage (2), which in turn comprises an outer wall (12) insulating from the outside an inner volume (13) of the aircraft (1) and an inner wall (16) with respect to the outer wall (12) defining a first volume (1...  
WO/2019/052201A1
An unmanned aerial vehicle and a vibration damping device (100) thereof. The vibration damping device (100) is used for connecting a body (200) of the unmanned aerial vehicle and an inertial measurement unit (300). The vibration damping ...  
WO/2019/048996A1
The present disclosure pertains to non-planar frame structure of a multi-rotor unmanned aerial vehicle (UAV). Aspects of the present disclosure provide frame structure of a UAV that includes at least two rods 102-1 and 102-2, and one or ...  

Matches 1 - 50 out of 5,726