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Matches 1 - 50 out of 5,289

Document Document Title
WO/2018/108148A1
An unmanned aerial vehicle, comprising a fuselage (1) and multiple arms (2) disposed at left and right sides of the fuselage (1), said unmanned aerial vehicle also comprising a sliding mechanism; open grooves (3,11) are provided on the f...  
WO/2018/107972A1
An arm and an unmanned aerial vehicle, the arm comprising a first arm segment (11) and a second arm segment (12), the first arm segment (11) being provided with a locking part (112) and the second arm segment (12) being provided with a l...  
WO/2018/109255A1
The invention relates to a method for producing reinforced monocoque structures and to the structure obtained, the method comprising: using base components (1) made from a partially cured composite material and joining the base component...  
WO/2018/111346A1
A device is provided for controlling fluid flow over a window of a movable optical instrument housing. The device includes a generally annular body having an inner peripheral edge configured to correspond to a peripheral edge of the wind...  
WO/2018/104403A1
The invention relates to a cabin floor (2) suitable for being installed horizontally in a peripheral fuselage segment of an aircraft, said cabin floor (2) comprising a first planar structural portion (21) and a second planar structural p...  
WO/2018/103641A1
A retractable drone, comprising: a main cabin (1) and a motor blade mechanism; a left and a right side of the main cabin (1) are provided with a protective cover (2) respectively, and the protective cover (2) slidably connects the motor ...  
WO/2018/103026A1
Disclosed is a multi-rotor unmanned aerial vehicle, comprising: a body (1), and a plurality of arms (2) arranged on the body (1) in a foldable manner. When the arms (2) are in an unfolded state, the arms (2) extend toward the periphery o...  
WO/2018/096933A1
This composite member 1 is provided with a web part 21 and a flange part 22 provided at the end of the web part 21. The flange part 22 comprises multiple laminated fiber sheets, and the surface on one side in the lamination direction is ...  
WO/2018/090435A1
Disclosed is an aircraft (100), comprising a centre frame (1), an antenna (3), and an arm assembly (2) connected to the centre frame. The arm assembly comprises arms (21). The antenna is disposed at a position on the arm away from the ce...  
WO/2018/091475A1
The invention relates to an electrohydraulic module (1) for driving at least one component of an aircraft, in particular an airplane, wherein the electrohydraulic module (1) comprises at least one electric motor (2) and at least one comp...  
WO/2018/088149A1
The purpose of the present invention is to facilitate the attachment of a second member to a sheet-like first member, while supporting the first member in a state of being capable of being deformed by gravity. This component production m...  
WO/2018/088140A1
The purpose of the present invention is to facilitate the riveting of a second member to a first member when superposing and assembling the two members. This component production method is provided with: a step (S2) in which an attaching...  
WO/2018/087213A1
The present invention relates to an aircraft (100) comprising: a fuselage (101) comprising a plurality of panels (105) adapted to define an aerodynamic shape for a cockpit or a cargo hold of the aircraft (100);at least one wing (103) str...  
WO/2018/086496A1
A telescopic propeller arm assembly (12) and an unmanned aerial vehicle (10). One end of the telescopic propeller arm assembly (12) is connected to a body (11) of the unmanned aerial vehicle (10), and the other end is connected to a powe...  
WO/2018/089934A1
Commercial supersonic aircraft and associated systems and methods. A representative commercial supersonic aircraft includes a fuselage configured to carry a crew and between 20 and 60 passengers, a delta wing mounted to the fuselage, and...  
WO/2018/088138A1
The purpose of the present invention is to achieve accurate alignment when superposing and assembling two members. This component production method is provided with: a step (S14) for calculating a first virtual line which is parallel to ...  
WO/2018/085038A1
Some embodiments are directed to an apparatus, such as a panel that might be appropriate for aircraft or space vehicle fuel tanks. According to some embodiments, a plurality of stiffening elements may be attached to a matrix stiffened la...  
WO/2018/083077A1
The present invention is concerned with actuating aircraft components to tailor their configuration to achieve improved performance in one or more flight phases. In general terms, the invention provides a method and system for actuating ...  
WO/2018/076471A1
Disclosed is an unmanned aerial vehicle (100), comprising a metal housing (10), a GPS module (20) and a cover plate (30). The metal housing (10) comprises an accommodation portion (111) with an opening; the GPS module (20) is provided wi...  
WO/2018/080905A1
The present invention provides high security polycarbonate laminates integrated with insulated glazing units (IGU) to produce high security windows. The laminate comprises at least nine layers, in the following order: (i) an insulated gl...  
WO/2018/080989A1
In one example, a structure is provided that includes a plastic body having a unitary, single-piece construction. The plastic body further includes a substantially hollow interior, and a parting line that extends around a portion of the ...  
WO/2018/076470A1
Disclosed is an unmanned aerial vehicle (100), comprising a body (10), an arm (20) connected to the body (10), and a connection assembly (30). The arm (20) is detachably connected to the body (10). The connection assembly (30) comprises ...  
WO/2018/077968A1
The present invention pertains to a fluoropolymer composition (C) comprising a polymer (A) of ethylene and tetrafluoroethylene and/or chlorotrifluoroethylene, and a certain amount of specific acid scavenger (AS), optionally a colorant,an...  
WO/2018/076253A1
Disclosed is a connection assembly (30), an unmanned aerial vehicle arm (20) having the connection assembly (30) and an unmanned aerial vehicle (100). The connection assembly (30) is used for connecting and locking two components, and th...  
WO/2018/072324A1
Disclosed is an unmanned aerial vehicle, which comprises a fuselage (10), a vehicle arm (20) and a vehicle arm clamping device (30). The vehicle arm (20) comprises an oppositely-arranged free end (222) and a fixed end (224). The vehicle ...  
WO/2018/074423A1
This fan rotor blade consists of a composite material including a thermoplastic resin and reinforcing fibers, and is provided with: an outer covering member forming a blade surface shape having a positive pressure surface and a negative ...  
WO/2018/067100A1
The group of inventions relates to aviation. An aeroplane comprises a fuselage which consists of a body of an upper load-bearing piloted part and a capsule in the form of a body of a lower part which is capable of automatically separatin...  
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/2018/060186A1
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/2018/061281A1
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...  
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...  
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...  
WO/2018/053837A1
A frame assembly for an unmanned aerial vehicle, and the unmanned aerial vehicle provided with the frame assembly. The unmanned aerial vehicle comprises a body, arms connected to the body, and propellers disposed on the arms. The body co...  
WO/2018/057242A1
An aircraft is provided including a fuselage that extends along a longitudinal direction between a forward end and an aft end. A stabilizer assembly and a boundary layer ingestion fan is mounted to the fuselage at the aft end and is conf...  
WO/2018/051060A1
The invention relates to a method of fastening panels to a substrate, and a fastener, accordingly there is a method of fastening a panel to a substrate, comprising the steps of i. providing on the substrate a first projection, ii. attach...  
WO/2018/049720A1
Disclosed are an aircraft arm assembly of an aircraft and an aircraft, the aircraft arm assembly (10) of the aircraft comprising an aircraft arm housing (12) and an air guide mechanism (14), wherein the aircraft arm housing (12) is inter...  
WO/2018/047089A1
A window (7) with an emergency exit function for a helicopter (1) is described that comprises: a frame shaped as a framework (8) that can be coupled to a door (6) of said helicopter provided with an opening (9); and a transparent element...  
WO/2018/048858A1
Systems, apparatuses, and methods are provided herein for unmanned flight optimization. A system for unmanned flight comprises a set of motors configured to provide locomotion to an unmanned aerial vehicle, a set of wings coupled to a bo...  
WO/2018/045825A1
A folding device for avoiding clearances in an aircraft, comprising two parallel fixed plates (101), a fixed rod (102) fixed between the two fixed plates (101), a limiting rod (105), a spring (103) and a rotary arm (201). The fixed plate...  
WO/2018/040426A1
An unmanned aerial vehicle, comprising a body (1) and wings (2). The body (1) comprises an upper body part (11) and a lower body part (12). The lower body part (12) is provided with a cargo compartment (121) for accommodating cargoes. A ...  
WO/2018/040312A1
Disclosed is an unmanned aerial vehicle of folding wing-type, comprising a fuselage (1) and arms, wherein the arm comprises a non-folding section (2), a folding mechanism (3) and a foldable section (4); the non-folding section (2) is fix...  
WO/2018/040116A1
An unmanned aerial vehicle (100, 200, 300), comprising: a rack (110, 210, 310) which comprises a body (110a, 210a, 310a) and an arm (110b, 210b, 310b); the arm (110b, 210b, 310b) is connected to the body (110a, 210a, 310a), and the arm (...  
WO/2018/041992A1
The invention relates to a preform (3) defining two parts (21, 23) and comprising: a first group (C1) of layers of warp yarns, which is external in the first part, a second group (C2) of layers of warp yarns immediately beneath said firs...  
WO/2018/036231A1
An unmanned aerial vehicle (20) includes a support (21) having a plurality of receiving slots (27); a plurality of arms (22) attached to the support (21); and a plurality of propellers (23) respectively attached to the plurality of arms ...  
WO/2018/035959A1
An unmanned aerial vehicle (100) comprises a frame (10), a battery and a magnetic sensor. The battery is installed at the frame (10). The battery comprises one or more cores wound by multiple tabs. The core wound by multiple tabs compris...  
WO/2018/032723A1
Provided are an unmanned aerial vehicle, a tool for molding a housing of an unmanned aerial vehicle, and a molding process. The unmanned aerial vehicle comprises a housing (1). The housing (1) has a layered structure comprising an outer ...  
WO/2018/027684A1
A mechanism for quickly folding and unfolding wings of an unmanned aerial vehicle, comprising an arm (1) and an arm mounting base (2); a guide post (20) is arranged on an upper surface of the arm mounting base (2), a sliding sleeve (21) ...  
WO/2018/027682A1
A wing folding structure for an unmanned aerial vehicle, comprising an arm (1) and an arm mounting base (2), a blind hole (20) being provided on an end of the arm mounting base (2); also comprised is a connecting post (3) connected to a ...  
WO/2018/027681A1
A foldable wing of a small unmanned aerial vehicle, comprising an arm (1) and an arm mounting base (2); an end of the arm mounting base (2) is provided with a blind hole (20) matching the arm (1); a first through hole (21) communicating ...  
WO/2018/027683A1
A quick disassembling and assembling wing of an unmanned aerial vehicle, comprising: a vehicle arm (1), and a vehicle arm installation base (2) provided with a first blind hole. The quick disassembling and assembling wing further compris...  

Matches 1 - 50 out of 5,289