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WO/2019/239047A1 |
The invention relates to the field of aeronautics propulsion, and more specifically to a device and a method for emptying and monitoring (10) for emptying and monitoring a fluid drained from an engine (101) of an aircraft (100). The empt...
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WO/2019/232941A1 |
A wing of an unmanned aerial vehicle comprises a mid-wing, an outer wing, and a connecting device. The connecting device comprises a first connecting part and a second connecting part. One of the first connecting part and the second conn...
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WO/2019/232598A1 |
The example non-limiting technology herein provides an alternative way to control window heater temperature by delivering to the heater a DC voltage with variable level.
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WO/2019/233060A1 |
Disclosed are a control system and a control method for an oil-electric hybrid multi-rotor unmanned aerial vehicle, the control system comprising a fuselage (1) and a plurality of rotors (2) evenly arranged on side faces of the fuselage ...
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WO/2019/227445A1 |
An unmanned aerial vehicle, comprising a rack (1), a rotating shaft (2) assembled to the rack (1), and an arm (3) assembled to the rotating shaft (2). The rack (1) comprises a top wall (10) and a bottom wall (11) opposite to each other, ...
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WO/2019/229076A1 |
An aircraft cabin component for use in an aircraft cabin of an aircraft includes a component part having at least one parametric surface. A flexible OLED display assembly adheres to the at least one parametric surface of the component pa...
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WO/2019/231413A1 |
Therefore, the current invention is a mobile sun shade system (35) which is positioned on and around the window and it can be automatically opened and closed by the passenger, in addition it is kept open and locked during the landing and...
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WO/2019/229074A1 |
Aircraft pressurized cabin door (1) comprising an outer panel (2) and a door structure (3). The door structure (3) comprises: - two circumferential beams (4) fastened to the lateral edges of the door (1); - a plurality of longitudinal be...
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WO/2019/229083A2 |
Disclosed is an emergency exit door (2) for an aircraft cabin, said door comprising an opening assist mechanism and an opening/closing device having a control lever (7) which can selectively be actuated to either unlock the door (2) and ...
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WO/2019/222798A1 |
This invention relates in general to a method of controlling a drone to fly an autonomous grid pattern while capturing images or data of a target area. The method reduces ground sampling distance and provides greatly improved survey accu...
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WO/2019/225607A1 |
[Problem] To provide an aircraft wherein the need for additional components for heat radiation is eliminated by making the structure of the aircraft itself suitable for heat radiation, and a frame for the aircraft. [Solution] This aircra...
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WO/2019/222632A1 |
Fire protective compositions include colloidal silica solids, clay, a low biopersistence fiber or refractory ceramic fiber, water, and optionally a chelating agent. Methods of using the fire protective compositions include providing a po...
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WO/2019/222595A1 |
A system for monitoring a pressure change within at least one compartment of an aircraft and operating a pyrotechnic device associated with a door latch, includes a securing mechanism arranged in an aircraft door that includes a pyrotech...
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WO/2019/217839A1 |
A high temperature thermal protection systems for rockets, and associated methods, is disclosed. A representative system includes a launch vehicle having a first end and a second end generally opposite the first end. The launch vehicle i...
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WO/2019/216990A1 |
A system and a method for reducing drag on the aft-fuselage of an aircraft are provided, which system and method utilize at least one finlet provided on each side of the aft-fuselage of an aircraft for reducing drag -on the aft-fuselage,...
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WO/2019/216723A1 |
A drone includes a harness to be attached to a human body to enable the drone to be mounted on the human body. The drone has a propeller formed at an end of an arm thereof, wherein the arm is formed as a foldable type to be retracted int...
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WO/2019/210407A1 |
A unmanned tandem two rotor aircraft is provided. Rotor systems each containing drive motors and power sources are interconnected by a connecting body structure for supporting a payload. A payload rack may support one of more payloads th...
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WO/2019/213529A1 |
A composite wingbox structure formed of reinforced thermoplastic. The composite includes carbon fiber reinforcement and a plurality of insulation elements to localize the heat formed during the process of manufacturing the structure. The...
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WO/2019/207997A1 |
An agricultural multicopter (1) according to an embodiment of the present invention is provided with: a main body part (10) disposed on a central axis line; a plurality of rotary blade parts (30) disposed in the vicinity of the main body...
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WO/2019/209755A1 |
An item to be secured to an aircraft floor can be secured to a Load Transfer Structure that resides under the floor, via access passages provided in selected floor panels. The Load Transfer Structure transfers the weight of the item to m...
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WO/2019/210011A1 |
A mechanical joiner for an airframe includes a joiner core and first and second caps. The joiner core has a first side with a first cradle shaped to hold a first structural member and a second side with a second cradle shaped to hold a s...
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WO/2019/209150A1 |
The invention concerns an aerial vehicle (1) comprising a fuselage structure (3) having an aperture (7) and a door structure (5), which is latched and locked to the fuselage structure (3), and a method for securing the door structure (5)...
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WO/2019/209151A1 |
The present invention regards an interlock arrangement (1) comprising a latch fitting member (3) of a first body (5) and a laterally moveable latch bar member (7) of a second body (9), which interlock arrangement (1) is configured for la...
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WO/2019/207558A1 |
In order to provide an unmanned aerial vehicle with good space efficiency and portability,　this unmanned aerial vehicle (10) is characterized by: comprising rotors (R) having horizontal rotary blades, and arms (70) for supporting the r...
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WO/2019/205457A1 |
An unmanned aerial vehicle (100), comprising a body (10), wherein the body (10) is provided thereon with an accommodating cavity (20) for accommodating an electronic component (90), and an opening of the accommodating cavity (20) is deta...
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WO/2019/202325A1 |
Methods, apparatus, systems and a vertical take-off and landing (VTOL) vehicle are provided. The VTOL vehicle includes: a fuselage having longitudinally a front section, a central section and a rear section; a first lifting surface compr...
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WO/2019/200948A1 |
An anti-misoperation device for an aircraft passenger cabin door. The anti-misoperation device for an aircraft passenger cabin door comprises a guiding groove (6), a rocker (8), a torsion spring (11), a clamp hook (12), a spline shaft (1...
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WO/2019/197425A1 |
The invention relates to a vehicle device, in particular an aircraft device, comprising at least one screening unit and/or light protection unit (12, 12'), at least some portions of which can be electrically operated, said unit having at...
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WO/2019/200088A1 |
A package delivery drone comprises at least one propeller for generating lift and an article containment area for containing an article to be carried by the drone. The floor of the article containment area comprises a dynamic support sur...
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WO/2019/195150A1 |
A door damper assembly that includes a housing, a damper that includes a fixed end and a movable end disposed within the housing, a carriage assembly that is movable within the housing between a closed position and an open position, a cl...
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WO/2019/193131A1 |
Method for an aerospace structural component (19) comprising a stiffener structure (10), wherein the stiffener structure (10) comprises stiffeners (12) extending along the aerospace structural component (19), and wherein the stiffeners (...
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WO/2019/191167A1 |
A hinge is coupled to a first component and a second component and supports the second component for movement relative to the first component between a closed position covering an opening through the first component and an opened positio...
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WO/2019/181184A1 |
Provided are: a composite material structure obtained by joining of composite materials in which reinforcing fibers are impregnated with a resin, wherein appropriate lightning-proofing measures are taken; and a method for manufacturing t...
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WO/2019/181607A1 |
Provided is a composite material assembly (100) comprising: a first composite material member (1) in which a first hole (51) is formed, a second composite material member (2) in which a second hole (52) is formed, and a fastener (3) that...
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WO/2019/178064A1 |
A wing-to-body fairing on an aircraft having a fuselage, wing, and a wing root fairing. The wing-to-body fairing includes forward and trailing edges. The forward edge is configured for positioning adjacent a first predetermined location ...
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WO/2019/176793A1 |
A composite material lamination device (10) laminates a composite material (22) on a lamination surface (3), which is an outer surface (1a) of a mold (1) that includes one side surface (1aa) and another side surface (1ac), or an outer su...
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WO/2019/170302A1 |
An integrated drain mast structure for use in draining fluids emanating from aircraft components, such as turbine engines and fuselages, for facilitating the detection of fluids leaking from said components. A self-supporting tube sectio...
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WO/2019/169469A1 |
The invention relates to a spacer (100') for a cylindrical conduit, comprising a first component (10) provided with a first part (11) having a plane of symmetry (PS) and a longitudinal axis (AL) pertaining to said plane, said first part ...
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WO/2019/163173A1 |
This rectifying structural body 100 of a flying object is provided with a rectifying part 30, a heat input control part 20, and a vacuum heat insulated part 10. The rectifying part 30 has a rectifying surface 30a and a rear surface 30b. ...
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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...
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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...
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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...
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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...
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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...
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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 (...
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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...
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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...
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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...
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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...
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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...
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