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WO/2024/097197A1 |
A UAV having a fuselage body including a cavity that forms a cargo bay for transporting a payload, and a lower access opening providing an exit for the payload from the cargo bay, the lower access opening including a lower cargo bay door...
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WO/2024/088472A1 |
The invention relates to an aircraft (1) having a fuel-cell propulsion system (2), wherein the fuel-cell propulsion system (2) comprises - a fuel cell (3) for supplying electricity to an electric propulsion apparatus (4) of the aircraft ...
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WO/2024/088721A1 |
The invention relates to a device for securely locking an adjustment system (1) of a fastener (2) of an opening panel, this fastener comprising at least one splined washer (4) translating along a cylindrical body (3a) of an adjustment sl...
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WO/2024/089336A1 |
The subject matter of the present invention is glazing (7) for flush attachment with a frame (10), the glazing (7) having at least one recessed area (8), by which the glazing (7) is configured to be fixed to the frame (10), the at least ...
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WO/2024/078900A1 |
Locking/unlocking mechanism for controlling the passage of an aircraft door, with lateral escape of the stops, from the closure position to the unlocking position, and vice versa, said mechanism having: - a guide track (29) extending alo...
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WO/2024/079407A1 |
The invention relates to laminated glazing comprising a first outer glass sheet (2) having a thickness of between 0.5 and 5 mm and at least one structural glass sheet (3, 3') bonded in pairs by an intermediate adhesive layer (4, 6), the ...
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WO/2024/078437A1 |
The present disclosure relates to an aircraft seat and an aircraft. The aircraft seat includes: a headrest; a backrest; and a seat plate pivotably mounted to the backrest and configured to be pivotable relative to the backrest from a sea...
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WO/2024/077365A1 |
The present patent application relates to a support ladder (E) for a boarding region or landing structure (A1) of an aircraft (A), such as a helicopter. The ladder (E) comprises an attachment region (1) for attaching a ladder structure (...
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WO/2024/068275A1 |
The invention relates to an assembly with a mechanism (2) for locking a door (1a) in circular translation, the door being of the vehicle semi-plug type. The mechanism (2) comprises a handle (3) actuating a rotation of the door (1a) on it...
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WO/2024/066601A1 |
A preparation method for an aircraft cargo hold floor, and an aircraft cargo hold floor. The preparation method comprises the following preparation steps: separately preparing phenolic resin upper panel layers (4), phenolic resin lower p...
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WO/2024/069633A1 |
During aircraft descent, flight control systems seek and maintain a glide slope determined from a single pilot input parameter; e.g., the position of a control axis of a flight stick. Appropriate guide slope selection by the pilot is rea...
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WO/2024/064434A1 |
A mechanism for attachment and detachment of a fixed or controllable airfoil to an airframe includes a base adapted for attachment to a root of the airfoil and a slot beam adapted for attachment along the airframe (e.g., parallel to the ...
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WO/2024/056878A1 |
The invention relates to a glazed system (100, 200, 300) comprising a glass panel (110) comprising structural plies (111, 112), the glass panel being clamped in place by a structure. Said glazed system further comprises: - at least one b...
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WO/2024/055499A1 |
An anti-false-touch safety switch (7), a locking mechanism (100), and a locking system, relating to the technical field of aviation machinery. The anti-false-touch safety switch (7) comprises: a rotary locking member (71), used to be in ...
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WO/2024/056879A1 |
The invention relates to a glazed system (100, 200, 300) comprising a glazing (110), for example a laminated glazing, comprising structural folds (111, 112), the glazing being clamped in place by a structure. Said glazed system further c...
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WO/2024/055899A1 |
A connector and method for connecting a motor and an arm of a multi-rotor aircraft. The connector comprises a base (1), a locking disk component (2), and a guided positioning component (3), wherein one side of the base (1) is connected t...
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WO/2024/055506A1 |
The present invention relates to the field of aviation machinery. Provided is a locking mechanism used for a helicopter tail cabin door. The locking mechanism comprises: two lock box assemblies, respectively installed on two sides of a t...
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WO/2024/052237A1 |
The invention relates to a hybrid metal/plastic spring rod (1) comprising a guiding system (3) made up of a metal pin (4) and a plastic sliding body (5), a compression spring (2) and two plastic-moulded connecting members (6a, 6e). The c...
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WO/2024/054195A1 |
A closed-wing vertical take-off and landing aircraft comprising: a fuselage (1); a tail unit comprising two angularly inclined stabilizers (12); and a closed wing, comprising a front wing formed by two planes (2) mounted to the fuselage ...
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WO/2024/020222A1 |
A system for an electrically powered aircraft can comprise: a truss configured to couple to a structure of an aircraft; a battery system supported by the truss, the battery system including a first array of battery modules and a second a...
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WO/2024/017810A1 |
The invention relates to a method for automated alignment of a stationary part (1) with a movable part (2) capable of being moved towards the stationary part by a robot (3), the stationary part (1) and the movable part (2) each comprisin...
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WO/2024/015756A1 |
An unmanned aerial vehicle (UAV) including a fuselage body having a cavity that forms a cargo bay for transporting a payload, and a lower access opening for lowering the payload from the cargo bay, the lower access opening including a ca...
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WO/2024/015961A1 |
A unmanned aerial vehicle (UAV) includes a fuselage body including a cavity that forms a cargo bay for transporting a payload, an upper access opening for receiving the payload into the cargo bay from a first direction, and a lower acces...
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WO/2024/015482A1 |
A vehicle (600, 700) is disclosed. The vehicle (600, 700) includes a body forming a door opening. The vehicle (600, 700) also includes a first hinge (607, 707) coupled to the body. The vehicle (600, 700) further includes a door (608, 708...
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WO/2024/013496A1 |
The present invention is concerned with an aircraft comprising an elongate fuselage for containing cargo or passengers. The fuselage comprises a lower floor and an upper ceiling and opposing fuselage sides extending between the ceiling a...
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WO/2024/009105A2 |
An enclosure is provided which defines an internal volume for housing an electrochemical power unit, wherein at least a region of the enclosure is formed of a material comprising a ceramic matrix composite (CMC). The enclosure disclosed ...
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WO/2024/003527A1 |
The disclosure concerns an unmanned aircraft for carrying of cargo, comprising a fuselage (10) extending in a fore-aft direction and configured to receive cargo in an unpressurized interior space thereof; a wing (20) extending in a spanw...
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WO/2024/004301A1 |
The purpose of the present invention is to provide a panel member that is lightweight and has high strength with respect to an impact from the outside.　This panel member (100) comprises a first skin member (1) and a second skin member ...
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WO/2024/001980A1 |
Provided is a glass stacking and a preparation process thereof, comprising: a glass substrate; a low-emissivity layer; and an overcoat layer; wherein the low-emissivity layer is between the glass substrate and the overcoat layer; the low...
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WO/2024/006164A1 |
An aircraft has a boom, a propulsion assembly coupled to a first end of the boom, and a first wing coupled to a second end of the boom. The first wing can be coupled to the boom by a (first) articulated joint. The propulsion assembly can...
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WO/2024/006171A1 |
An aircraft has a fuselage, a propulsion system, and a vacuum control system. The vacuum control system includes a conduit having an inlet configured to receive exhaust air from the propulsion system. The conduit can be configured to dir...
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WO/2023/246948A1 |
A new foldable convenient manned aircraft comprises a fuselage, four arms arranged on the fuselage, a rotor motor, a rotor and an anti-collision radar which are symmetrically arranged on the outer end of each arm, four anti-collision air...
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WO/2023/250214A1 |
Embodiments are directed to an anti-rattle device, including a plurality of handle bracket assemblies, and a wedge assembly. Each of the handle bracket assemblies includes an adjustable handle, a bracket, and a threaded rod. The wedge as...
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WO/2023/247455A1 |
The present invention relates to a method for obtaining underfloor heating for vehicles, in particular rail vehicles, comprising a core (4) between an upper panel (50), intended to be covered with a floor covering, and a lower panel (51)...
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WO/2023/249671A1 |
A flexible aircraft privacy door for a passenger cabin environment, comprising a first edge and a second edge. The flexible privacy door is configured to be slidable between a stowed position leaving an opening between spaced structures ...
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WO/2023/227850A1 |
Flexible door (10) for accessing a seat unit (100) for an aircraft passenger, in particular for an aeroplane passenger, characterized in that the door comprises a plurality of parallel slats (11) articulated longitudinally with respect t...
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WO/2023/223119A1 |
A fuselage (2, 2', 2'') for a convertible aircraft (1) is described, comprising a nose (4) and a tail (5) arranged on mutually opposite sides along a first longitudinal axis (Y) of the fuselage (2); a first portion (100) and a second por...
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WO/2023/220093A1 |
The present disclosure provides doorway protection assemblies with a base portion and two leg portions that can be positioned over and protect the exterior surrounding a doorway of a vehicle, such as an aircraft, from damage while cargo ...
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WO/2023/213373A1 |
The invention relates to "mobile units" which inseparably include: a cylindrical outer casing with low taper or constant cross-section; one or more motorised longitudinal fluid channels which are each "convergent" at the inlet and subseq...
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WO/2023/202055A1 |
A flexible connecting structure (100) for an arresting wall and a fuselage. The flexible connecting structure is configured to fix an arresting wall (200) to the interior of an aircraft (300), and comprises: a first connecting joint (10)...
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WO/2023/204708A1 |
The invention relates to the transport of air cargo on the passenger-deck of an airliner and in possible presence of passengers. The container (1) of the invention is substituted in lieu of one passenger seat. The container of the invent...
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WO/2023/199236A1 |
The invention relates to equipment (10) for making a structural element (1) of composite material having a longitudinal axis (A) and an axial cavity (2). The equipment (10) comprises a support frame (11) and a laminating mandrel (12), wh...
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WO/2023/195876A1 |
The invention relates to the field of aviation and cosmonautics. A high-heat tile for use in areas of a surface that are subject to high heat loads is formed in the shape of a circular cylinder of a given radius, having two parallel base...
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WO/2023/194139A1 |
The invention relates to a method for producing a composite stiffened structure comprising a panel (3) and at least one stiffener (4). The production method comprises the following steps for obtaining a one-piece core (2): - covering the...
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WO/2023/178687A1 |
An unmanned aerial vehicle (100). The unmanned aerial vehicle (100) comprises a main body (10), first rotation portions (20), and first arms (30). The first arms (30) can rotate around the first rotation portions (20) relative to the mai...
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WO/2023/180449A1 |
The invention relates to a vehicle, which can be used either as an aircraft or ground effect vehicle or as an aircraft and ground effect vehicle, comprising a fuselage (4) and at least two front wings (2), wherein the fuselage (4), when ...
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WO/2023/183522A1 |
An electrically operated window shade system includes a frame that is mounted on the outer side of the inner wall of an aircraft cabin. A cassette is mounted in the frame and includes one or more motors and drive systems and one or two s...
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WO/2023/180166A1 |
The present invention relates to a device for automatically locking an adjusting member comprising an outer element (2), secured to a mechanical system, provided on its inner wall with an internal thread and intended to receive a movable...
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WO/2023/173374A1 |
An unmanned aerial vehicle and an arm assembly. The unmanned aerial vehicle comprises a fuselage (10); at least one arm assembly (20), which comprises an arm (21) and a fuselage connection part (22) for being connected to the fuselage (1...
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WO/2023/173205A1 |
An aircraft has retractable landing gear configured to reciprocate between a deployed position and a stowed position. A landing gear door installation includes a first door rotatably coupled to the aircraft about a first axis for movemen...
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