| Document |
Document Title |
|
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 ...
|
|
WO/2019/041221A1 |
Provided are a deformable frame (10) and an aerial vehicle (100) using the same. The deformable frame (10) comprises a central frame portion (12) and two arm assemblies (14). The two arm assemblies (14) are respectively provided at two s...
|
|
WO/2019/041876A1 |
Provided are a foldable frame and an unmanned aerial vehicle. The frame comprises: a body; a connection arm (1) connected to the body and capable of rotating between an unfolded position and a folded position; and a rotating member (3) a...
|
|
WO/2019/041220A1 |
Provided are an arm locking mechanism (10), and an aerial vehicle (100). The arm locking mechanism (10) comprises an arm connection assembly (12) and a locking mechanism (14). The arm connection assembly (12) comprises at least two rotat...
|
|
WO/2019/041174A1 |
Disclosed is an unmanned aerial vehicle (1), comprising a machine body (10) and a plurality of arm assemblies (201, 202) arranged on the machine body (10), wherein each of the arm assemblies (201, 202) comprises an arm (221, 222) connect...
|
|
WO/2019/041097A1 |
A frame assembly of an unmanned aerial vehicle, and an unmanned aerial vehicle. The frame assembly comprises a center frame (1) and two sets of arm assemblies (2) respectively disposed on two sides of the center frame (1); each of the ar...
|
|
WO/2019/044161A1 |
This composite material structure body is provided with a main body and a first cover ply, wherein the main body has a stepped part configured by stacking a plurality of plies so that the end faces thereof are misaligned with each other,...
|
|
WO/2019/041126A1 |
Provided is a frame, comprising: a triangular arm (130) and a central frame (110), wherein one of apexes of the triangular arm (130) is hinged to the central frame (110); the triangular arm (130) comprises a first arm (131) and a second ...
|
|
WO/2019/041502A1 |
Provided are a vehicle arm assembly of an unmanned aerial vehicle, and an unmanned aerial vehicle. The vehicle arm assembly (100) of the unmanned aerial vehicle comprises a first joint member (1), a second joint member (2) and a locking ...
|
|
WO/2019/043344A1 |
The invention relates to an acoustic panel (12) with a cellular core (24) comprising cells (28) that are provided with one or more obstacles (36, 38), each of said obstacles (36, 38) extending transversely in relation to the main axis of...
|
|
WO/2019/041875A1 |
Provided are a foldable frame and an unmanned aerial vehicle. The foldable frame comprises: a body (2); a connection arm (1) rotatably connected to the body (2); a first magnetic element (3) mounted on the connection arm (1); and at leas...
|
|
WO/2019/037242A1 |
Disclosed are an arm assembly, a frame, and an unmanned aerial vehicle, wherein the arm assembly (10) is fitted on a main frame body (101), and the arm assembly (10) comprises a main arm body (11), a power assembly (12) arranged on the m...
|
|
WO/2019/029387A1 |
An aircraft and an arm assembly (10) and frame thereof, the arm assembly (10) comprising: an elastic locking member (100), a fixing seat (200) and an arm (300); the arm (300) is rotatably connected to the fixing seat (200) such that the ...
|
|
WO/2019/024806A1 |
Disclosed is an unmanned aerial vehicle, comprising a fuselage (1), a shell assembly (3) and a functional component. The fuselage comprises a fuselage body (10). The shell assembly (3) is connected at a front end of the fuselage body. Th...
|
|
WO/2019/026350A1 |
A landing gear for a rotary-wing aircraft according to one embodiment of the present invention comprises two skid-tubes, and a cross-tube for linking the two skid-tubes and attaching the two skid-tubes to a fuselage of the rotary-wing ai...
|
|
WO/2019/025343A1 |
The invention relates to a fastening unit (100) for movably fastening an aircraft component (300) to a support structure (400) of an aircraft (500). The fastening unit (100) has a connection element (5) having a hole (5a). The fastening ...
|
|
WO/2019/024541A1 |
An arm (11) and an unmanned aerial vehicle (100). The unmanned aerial vehicle (100) comprises a body (20), arms (11) connected to the body (20), and a power device disposed on the arms (11); the folded arms (11) can be attached to the ex...
|
|
WO/2019/024215A1 |
An arm (10), comprising a first sub-arm (12), a second sub-arm (14), and a sleeve (16); the second sub-arm (14) is rotatably connected to the first sub-arm (12); a connection joint (13) is formed between the first sub-arm (12) and the se...
|
|
WO/2019/019397A1 |
An unmanned aerial vehicle arm assembly, an unmanned aerial vehicle frame, and an unmanned aerial vehicle. The unmanned aerial vehicle arm assembly (100) is applied to the unmanned aerial vehicle (300) and comprises an unmanned aerial ve...
|
|
WO/2019/018621A1 |
An example embodiment includes a landing pad having a housing and a power terminal configured to draw electric power from a power source. The landing pad further includes an electrically conductive landing terminal dorsal to the housing ...
|
|
WO/2019/018847A1 |
A mounting system for mounting an element to a surface includes a mounting element 76 having a base 78 and a threaded shaft 80 extending from the base along an axis. The base is configured for mounting to a surface. An incremental nut 92...
|
|
WO/2019/015129A1 |
Disclosed is a portable multi-rotor unmanned aerial vehicle, comprising a frame (10) and a plurality of arms (20). Electric motors (30) and blades (40) are arranged at tail ends of the arms (20). Each of the arms (20) comprises a first a...
|
