Login| Sign Up| Help| Contact|

Patent Searching and Data


Matches 1 - 50 out of 6,313

Document Document Title
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...  
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...  
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...  
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...  
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...  
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...  
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...  
WO/2020/243364A3
The subject matter described herein relates to aircraft designs and more particularly to aircraft designs using tandem wings and a distributed propulsion system. The embodiments described enable synergies between aerodynamics, propulsion...  
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...  
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...  
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...  
WO/2020/222718A3
The invention is related to an ULD apparatus (1) which helps loading cargo packages to ULD pallets used in air transportation, comprises a frame (2) which is in different structures according to the type of the airplane and pallet, forms...  
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...  
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...  
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 (...  
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...  
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...  
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 ...  
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...  
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...  
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...  
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...  
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...  
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...  
WO/2020/180368A3
An aircraft includes a fuselage defining a longitudinal axis between a forward end and an aft end. The aircraft includes an electrical system having an electric storage. The electric storage is positioned within the fuselage.  
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...  
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...  
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...  
WO/2020/180376A3
An aircraft includes a fuselage defining a longitudinal axis between a forward end and a aft end. At least one airfoil is laterally extending from the fuselage defining an airfoil axis. An electrical system has an electric storage. The e...  
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...  
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...  
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 ...  
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, ...  
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 ...  
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...  
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...  
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...  
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 ...  
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...  
WO/2020/149907A3
An aircraft includes a fuselage, an engine, a pylon, a nacelle cowling, and a gearbox assembly. The engine is spaced apart from the fuselage and the pylon is disposed between the fuselage and the engine. The accessory gearbox is fixed to...  
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...  
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...  
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...  
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...  
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 ...  
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...  
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...  
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...  
WO/2020/097042A9
This disclosure discloses a method comprising: positioning a stencil having an opening onto an aerospace part such that the aerospace part is accessible through the opening; positioning a masking medium onto the aerospace part through th...  
WO/2020/106343A3
A novel mechanism for reducing boundary layer friction and inhibiting the effects of uncontrolled fluid turbulence and turbulent layer separation, thus reducing the body drag, kinetic energy losses and lowering engine and pump fuel consu...  

Matches 1 - 50 out of 6,313