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WO/2021/021412A1 |
A themed aerial vehicle entertainment system or platform useful for generating crowd-pleasing shows or displays through the use of dynamically-coordinated show systems. Instead of use of a fixed flight plan, the new entertainment platfor...
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WO/2021/018503A1 |
The invention relates to an aircraft window consisting of a monolithic inner pane (1) made of a polymer material and a laminated outer pane (2) made of glass, the panes being separated by an air space (3).
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WO/2021/017235A1 |
A connecting corner box for the root part of a civil aircraft wing upper panel. The connecting corner box comprises a bottom side (9), an upright side (10) and reinforcing ribs (11), wherein the bottom side (9) is provided with notches (...
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WO/2021/019487A1 |
The problem addressed by the present invention is that of enhancing the functionality and efficiency of a lightweight aircraft designed for use on short-haul routes. The technical effect to be achieved by the use of the invention is that...
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WO/2021/013583A1 |
A fastening system (10) comprises a structure holding element (12) which can be fastened to a structural component (104). The fastening system (10) further comprises a component holding element (20) which can be fastened to a component (...
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WO/2021/016177A1 |
A mounting system 220 for mounting an element 222 to a surface 212 includes a mounting post 260 having a base 262 configured for mounting to a surface 212. The mounting post 260 is threaded on an outer surface. A mounting plate 270 is co...
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WO/2021/014033A1 |
The invention relates to a pressure bulkhead (1) comprising: a laminate body (2) made of composite material with a polymer matrix reinforced with fibres in a laminate arrangement; a general bulging (3) of the laminate body (2), which ext...
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WO/2021/009433A1 |
Aircraft propulsion unit comprising a fuselage (10) extending along a longitudinal axis (X) and incorporating an internal chamber, at least one ducted engine (20) attached to the fuselage (10) and comprising an air inlet section (20a), t...
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WO/2021/009399A1 |
An internal structural reinforcement element for fuselages, where the internal structural reinforcement element has a longitudinal direction adapted for its placement in the longitudinal direction of the fuselage and a transverse directi...
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WO/2021/008603A1 |
Disclosed by the present invention is a multifunctional bionic thermal protection structure formed on the basis of the SLM technology. The multifunctional bionic thermal protection structure comprises surface layers and a functional laye...
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WO/2021/005021A1 |
The invention relates to an emergency opening device of an aircraft door, comprising: - a tubular actuating member (2); - resilient compression means (11); - a member for retaining the tubular actuating member (2), comprising a retaining...
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WO/2021/006725A1 |
A fuselage structure of an aircraft is described. The fuselage structure comprises a fuselage skin, and a plurality of frame elements (30), spaced apart from one another in a direction parallel to the aircraft longitudinal axis for suppo...
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WO/2021/002232A1 |
The present invention provides a resin composition which is capable of effectively blocking neutrons and is suitable as a material for aircraft. The present invention specifically provides a resin composition which contains an aromatic p...
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WO/2021/001295A1 |
The invention relates to an electronic arrangement for an aircraft (1), an aircraft having a structure and such an electronic arrangement (3) and a method for providing such an electronic arrangement (3). The electronic arrangement has a...
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WO/2020/259748A1 |
The invention relates to a device for preventing access to an area on an aircraft, having a first vertical jamb (8) and a second vertical jamb (9) for fastening to a structure of the aircraft and having a barrier element (13), which is d...
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WO/2020/264306A1 |
A fuselage may include a base plate including one or more attachment points for securing the base plate to an unmanned aerial vehicle, a cover removably securable to the base plate, and a cargo compartment disposed in a space between the...
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WO/2020/264467A1 |
A dust cover for an aerospace window that comprises dust cover having an exterior substrate and an interior substrate in a spaced apart relationship with a substantially transparent coupling agent therebetween. The dust cover is disposed...
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WO/2020/253985A1 |
Disclosed is an aircraft door comprising: - a first handling arm and a first forearm; - a second handling arm and a second forearm; - a holding device movable between: an immobilising position in which the first forearm and the second fo...
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WO/2020/254386A1 |
The application relates to a pipe support block for an aircraft fluid system. The pipe support block is arranged to support a pipe on a structural member, such as a bracket. The pipe support has a first part and a second part which toget...
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WO/2020/253986A1 |
Aircraft door comprising a support arm (10) connecting a door leaf (5) and a door frame (13), the locking/unlocking mechanism of which comprises: • a control shaft (17) extending along a substantially vertical axis; • a guide track (...
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WO/2020/253987A1 |
The invention relates to an aircraft door comprising a support arm (6) connected to a support forearm (9) by a first pivot connection (7) about a first pivot axis (8), the support forearm (9) being connected to the leaf (5) by a second p...
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WO/2020/250479A1 |
Provided is an antenna control device that is mounted on a flight vehicle and irradiates the ground with a beam to thereby control an antenna for forming a wireless communication area, wherein the antenna control device comprises: an are...
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WO/2020/245188A1 |
The invention concerns an aircraft door comprising a lever (3) for emergency opening from outside, disposed in a lever window. The lever (3) for emergency opening from outside comprises: ● a main arm (7) comprising a first aerodynamic ...
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WO/2020/239469A1 |
The invention relates to a method for producing a load-bearing element for a means of transportation, comprising the steps of: - providing a flat base flange, which is made of a first material and has a first surface and a second surface...
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WO/2020/237678A1 |
A connection structure, comprising: an elastic body (100), which is used to connect to one among an arm (20) and a fuselage (30); a rotary shaft assembly (200), which is connected to the elastic body (100) and is used to connect to the o...
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WO/2020/239888A1 |
An aircraft assembly comprises a longitudinal spar and an aerofoil cover integrally formed from a composite laminate material to form a spar-cover such that the composite material of the spar extends continuously into the cover through a...
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WO/2020/232645A1 |
An unmanned aerial vehicle, comprising a center body (10), multiple mechanical arms (20), multiple electric motors (30), multiple propellers, and multiple antennas (50). The multiple mechanical arms (20) are rotatably connected to the ce...
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WO/2020/233132A1 |
The present application provides an unmanned aerial vehicle component. The component has a waterproof function and is configured to prevent unmanned aerial vehicle parts in the component from contacting water; the component comprises a f...
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WO/2020/235595A1 |
This aircraft member joining structure employs a joining tool to join a first plate and a second plate in an overlapping state. The first plate includes a first insertion hole, and a first serration formed around the first insertion hole...
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WO/2020/229501A1 |
An aircraft panel assembly with: a panel; and a plurality of stiffeners on the panel. Each stiffener has an attachment part attached to the panel and a structural part spaced apart from the panel. A rib foot beam crosses the stiffeners a...
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WO/2020/225397A1 |
Noise-attenuating devices, such as acoustic liners, and associated methods of manufacture are disclosed herein. The noise-attenuating devices have a perforated facing sheet with a coating applied thereto. The coating defines an exposed s...
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WO/2020/223246A1 |
An aircraft that includes a fuselage that includes a cabin interior that is at least partially defined by a floor, a ceiling and first and second side walls, a cockpit, a forward passenger zone positioned aft of the cockpit that includes...
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WO/2020/212087A1 |
The invention pertains to a filler preform in a wedge form (1) comprising reinforcing fiber bundles (2) consisting of reinforcing fiber filaments, wherein the filaments are directed parallel to each other within the fiber bundle, wherein...
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WO/2020/214532A1 |
A grommet (200, 300, 400), a stud (102), an assembly of a grommet and a stud forming a fastener (100), and a method of assembling a grommet and a stud to form a fastener has the grommet with an interengaging element (250) in a channel wa...
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WO/2020/212424A1 |
An aircraft comprising a fuselage, a pair of wings connected to an upper portion of the fuselage, and a pair of wing support struts, each wing support strut being connected between a lower portion of the fuselage and an underside of the ...
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WO/2020/208402A1 |
An aircraft (A, A.1, A.2) comprising at least one bay (1, 1.1, 1.2) for receiving different types of standardized modules, the bay (1, 1.1, 1.2) being configured to receive at least two different types of energy modules (6, 7, 8, 9, 10, ...
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WO/2020/208802A1 |
This joint structure 10 is provided with a connecting member 5 that is provided between and connects a member 1 to be reinforced and a reinforcing member 3. The connecting member 5 has a first coupling part 5a and a second coupling part ...
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WO/2020/210759A1 |
A modular aerial cargo aerodynamic encasement and a method for modular aviation cargo transport is provided. The aviation cargo aerodynamic encasement comprises a platform having a planar upper surface configured to accept cargo and a lo...
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WO/2020/203971A1 |
A panel structure (10A) is provided with a baseplate part (11) and at least two ribs (12) vertically erected on the baseplate part (11) and intersecting each other. Using at least a matrix resin, a baseplate material part (24) that const...
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WO/2020/202076A1 |
The method includes providing a composition that includes a polythiol, a second component, and at least one of a photoinitiator or photosensitizer that absorbs light having a wavelength greater than 400 nanometers; positioning the compos...
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WO/2020/194533A1 |
This waterproof container (50) has: a container body (52) having an opening (56) on a bottom surface while an unmanned aircraft is landed; a waterproof door (58) attached to the container body (52) so as to open to the outside and close ...
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WO/2020/190223A1 |
VTOL aircraft that takeoff and land as a multirotor and cruises as airplane. The aircraft comprises two major parts: First; winged carrier frame comprises wings, engines, propellers and landing gears. Second; tilting fuselage comprises c...
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WO/2020/190204A1 |
A method for operating a cargo door of an aircraft. The method comprises, opening the cargo door inwardly in relation to a cargo door opening by pivoting the cargo door to an open position adjacent a ceiling of a cargo space. The cargo d...
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WO/2020/190404A1 |
An aircraft door latch apparatus having a latched configuration and an unlatched configuration can include a door structure (18) of an aircraft door assembly (12), a handle (17) coupled to the door structure (18) and pivotably moveable w...
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WO/2020/182766A1 |
Aircraft door (1) comprising an inside door opening lever (6) coupled to a vent flap (5) by a conditional opening mechanism having two modes and comprising a flap stop (20) that is able to cooperate with a stop surface (21). The stop (20...
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WO/2020/181855A1 |
A dihedral trapezoidal lifting and floating integrated aircraft, comprising an aircraft body (1) and a power system. The aircraft body (1) comprises a head part provided with an equipment front compartment (2) and a tail part provided wi...
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WO/2020/178283A1 |
Disclosed is an aircraft pressurised cabin door (1), comprising a fuselage panel (2) and a door structure (3) that comprises: two circumferential beams (4) arranged on the lateral edges of the door (1); a plurality of longitudinal beams ...
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WO/2020/176666A1 |
A method of in-flight operational assessment for an electric aircraft comprising detecting by a sensor an electrical parameter of an energy source. The method further includes receiving by a controller the electrical parameter from the s...
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WO/2020/171722A1 |
Aircraft is equipped with a telescope built in the fuselage (1) with the initial angular mirror (2) installed in the open part of the fuselage (1) and the main mirror (7) installed in the cylindrical part of the fuselage. The open part o...
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WO/2020/167867A1 |
Load control apparatuses, systems and methods to control a location, orientation, or rotation of a suspended load by imparting thrust vectors to the suspended load or to a structure that holds the load. The load control apparatuses, syst...
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