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Patent Searching and Data


Matches 451 - 500 out of 57,454

Document Document Title
WO/2022/024161A1
The invention relates to a multilayer bleed duct 100; 200 and its manufacturing method. The duct, configured to direct a flow of exhaust gases from an aircraft, comprises an inner thermal insulating layer 10 having a tubular surface whic...  
WO/2022/023975A1
Process for manufacturing a structural component (1, 1', 1", 1''', 1"" ) made of composite material comprising a skin (2) and at least one stiffening stringer (3, 3', 3", 3"', 3"") applied rigidly and integrally to one face (2a) of the s...  
WO/2022/026518A1
In an embodiment, proprotor pitch ranges used during nominal cruise flight may be varied. By selecting ideal combinations of proprotor pitch angle and proprotor rpm, instead of the proprotor blade pitch bearing spending most of its time ...  
WO/2022/025334A1
The present invention relates to a drone transportation module connection device which can easily and firmly attach and detach a transportation module, in which loaded items have been loaded, to and from the main body of a drone, the str...  
WO/2022/023696A1
In some examples, a mounting structure for securing a payload to an aerial vehicle and for thermally regulating an electronic support system for the payload comprises a body section defining a housing configured to receive an electronic ...  
WO/2022/023790A1
The design of a modern multi-purpose actuator with the capability of performance similar to flight control surfaces that leads to optimal utilization of ambient airflow and is applied as an auxiliary system in case of failure of the main...  
WO/2022/021028A1
A target detection method, a device (400), an unmanned aerial vehicle (200), and a computer-readable storage medium. The method comprises: acquiring a currently photographed image produced by a photographing device (201) photographing a ...  
WO/2022/026032A1
A flexible solar array for extraterrestrial deployment and a method of manufacturing such a flexible solar array are disclosed. A power generating layer, a durable layer, and an ultraviolet radiation blocking layer are disposed such that...  
WO/2022/023212A1
A device for emergency opening of an aircraft door, comprising: - a tubular actuating member (7) which comprises a first end plate (8) and a second end plate (9); - elastic compression means which comprise a tubular spring (10) compresse...  
WO/2022/024112A1
Refueling devices for use in in-flight refueling operation are provided, including a body configured for being towed by a tanker aircraft and having a boom member that has a fuel delivery nozzle, a spatial control system and a longitudin...  
WO/2022/026857A1
A system for eradicating pathogens employs a mobile unit that includes a lamp. In one embodiment, the lamp emits a far-ultraviolet C (far-UVC) light, ultraviolet C light or light capable of inactivating pathogens for generating an irradi...  
WO/2022/017676A1
The present invention relates to a door system for a vehicle, in particular for a rail vehicle, comprising a door leaf that can be moved from a closed state to an open state and vice versa, with the features of claim 1. Compared to known...  
WO/2022/018351A1
One aspect of the invention relates to a ventilation system (100) intended to be mounted in an aircraft wheel along a central axis (XX), and comprising a rotor (140) that is provided with a plurality of blades (143) and is accommodated b...  
WO/2022/018354A1
Disclosed is a system (34) for controlling the pitch of a propeller blade (10), for an aircraft turbine engine, said system (34) being characterised in that it comprises: - a cup (58) having an annular wall (58a) extending about an axis ...  
WO/2022/020382A1
A magnetohydrodynamic pump for use in pumping molten salts that improves upon existing solutions is disclosed. The magnetohydrodynamic pump utilizes a linear induction motor with a cavity lined with ceramic and an interior piece forcing ...  
WO/2022/016243A1
The present invention relates to a system for obtaining a compound for blocking cosmic, nuclear and electromagnetic radiation, comprising a hydrogen reservoir (110), a hydrocarbon reservoir (120), a vacuum chamber (130), a spark power so...  
WO/2022/020238A1
An unmanned aerial vehicle controller is provided that includes one or more processors and one or more memories storing instructions that, when executed, configures the one or more processors, to set, based on received threshold informat...  
WO/2022/020161A1
Disclosed is an aircraft that includes a sanitization system that includes a monument having a plurality of walls that define a plurality of docking stations including a first docking station, and a sanitization insert positioned in the ...  
WO/2022/018353A1
Disclosed is a system (34) for controlling the pitch of a propeller blade (10) for an aircraft turbine engine, characterised in that it comprises: a cup (58) having an annular wall (58a) extending about an axis (A) intended to be a pitch...  
WO/2022/018358A1
Disclosed is a system (34) for controlling the pitch setting of a propeller blade (10) for an aircraft turbine engine, the system (34) being characterised in that it comprises: - a blade (10) comprising an airfoil (12) connected to a roo...  
WO/2022/019749A1
The invention discloses an unmanned, firefighting drone (100) comprising at least one propulsion unit (101), and a gyroscopic frame (200) which frame (200) carries a launching unit (300), wherein the launching unit (300) is adapted to re...  
WO/2022/018380A1
The invention relates to a turbine engine module having longitudinal axis X, the module comprising: - an unducted propeller (2) intended to be rotated about the longitudinal axis X; - at least one flow straightener (3) comprising a plura...  
WO/2022/018065A1
The invention relates to a device and a method for assisting aircraft guidance. The aircraft guidance assistance method is operated by an aircraft computing platform and comprises the steps: - acquiring state variables characterising an ...  
WO/2022/018722A1
An airport security eco-system comprising: plural client applications each including a hardware processor configured for use by security agents conducting security screening of passengers, thereby to generate individual passenger data ch...  
WO/2022/016251A1
The present invention relates to a super-hard carbon or diamond-like-carbon (DLC) layer obtained using the pulsed DC-PECVD technique modified with an ion- and electron-confinement system and a gas igniter. Said DLC coating is hydrophobic...  
WO/2022/016908A1
A helicopter air separation type emergency flight data recording system, comprising: an emergency state analysis system, an ejection system and a cushioning/floating system, wherein the emergency state analysis system is used for determi...  
WO/2022/018359A1
The invention relates to an assembly comprising a propeller blade (10) and its system (34) for angularly adjusting the pitch of the blade (10) comprising a bowl (42) which is radially delimited by an annular wall (44) extending about an ...  
WO/2022/019856A1
This invention relates to a body (2), at least one control surface (3) located on the body (2), enabling to control the flow of fluid by moving relative to the body (2), at least one actuator (4) produced from an electro-active polymer m...  
WO/2022/018557A1
A system for nondestructive inspection of structures. The system includes an omni-directional unmanned aerial vehicle (UAV) and a support arm extending outward from the UAV body from a first end attached to the body to a second distal en...  
WO/2022/018414A1
According to the present disclosure there is provided a liquid flow influencing duct arrangement comprising: a first duct section arranged to receive a liquid flow therethrough, the first duct section defining a first direction through t...  
WO/2022/016256A1
A method for extending a landing gear system for a vehicle is disclosed. The landing gear system includes a first landing gear assembly and a second landing gear assembly. The method includes the steps of sensing a first load on the firs...  
WO/2022/019432A1
A UAM-dedicated navigation system and an UAM-dedicated navigation system operation method are disclosed. A UAM-dedicated navigation system according to one embodiment of the present invention may comprise a UAM navigation device for tran...  
WO/2022/019857A1
The present invention relates to at least one body (2) provided in air vehicles; at least one wing flap (3) which allows the air flow to be controlled by moving relative to the body (2) located thereon, thus allows the air vehicle to man...  
WO/2022/020128A1
Some example systems and methods for retrofitting bulk product dispersal mechanism of aircraft (e.g., aerial crop dusters, air tankers, airplanes and helicopters) involve replacing one link of the dispersal mechanism's linkage assembly w...  
WO/2022/019852A1
The invention relates to a body (2), at least one actuator (3) produced from an electro¬ active polymer material that changes form due to electrical energy, thereby actuating the body (2), at least two strengtheners (4) allowing the act...  
WO/2022/017822A1
The present invention relates to a suite (10), in particular for an aircraft cabin, comprising: - a seat (19), - an ottoman (21), and - a storage cupboard (22), - the suite (10) further comprising a movable table (27) capable of assuming...  
WO/2022/018416A1
According to the present disclosure there is provided an arrangement (110) for influencing fluid flow, the arrangement comprising: a first section (1110) selectively configurable to provide a vortex generator surface, the vortex generato...  
WO/2022/020438A1
One embodiment of a hub feed oil system is used to provide oil to components on the rotating side of an aircraft rotor hub system. A pump is configured so that a portion of the pump rotates with the rotating portion of the rotor system a...  
WO/2022/018357A1
Disclosed is a variable pitch propeller blade (10) for an aircraft turbine engine, said blade (10) comprising an airfoil (12) connected to a root (14), the root (14) comprising a body (24) housed in an annular barrel (26) that extends ar...  
WO/2022/017046A1
An air supply air diffuser and a manufacturing method therefor. The air supply air diffuser is particularly applicable to the field of civil airliners. The air supply air diffuser comprises an open upper end; an open lower end; and an ai...  
WO/2022/018355A1
The invention relates to an assembly comprising a propeller blade (10) and a pitch adjustment system (34) for setting the pitch of the blade (10), wherein a root (14) of the blade (10) has a bulb (32) and the pitch adjustment system (34)...  
WO/2022/018381A1
Disclosed is a method and system for detecting a target in space, based on images taken from a spacecraft such as a visual inspection satellite. The invention relates to a method for remotely detecting one or more targets (1) in space in...  
WO/2022/019854A1
This invention relates to a body (2) located in an air and/or space vehicle, at least one control surface (3) which is located on the body (2) and which by moving relatively to the body (2), enables air flow to be controlled and the air ...  
WO/2022/017629A1
The invention relates to an engine (2) for an aircraft (1), comprising a ring-shaped vortex guide element (3) which has, in a sectional view, an air inlet opening (6) which is located centrally in relation to a longitudinal center axis (...  
WO/2022/018280A1
The invention relates to an aircraft seat device (10a; 10b; 10c; 10d; 10e; 10f; 10g; 10h; 10i) comprising at least one aircraft seat (12a; 12b; 12c; 12d; 12e; 12f; 12g; 12h; 12i) which has a backrest (14a; 14b; 14c; 14d; 14e; 14f; 14g; 1...  
WO/2022/018790A1
The objective of the present invention is to enable easy selection of an unmanned aerial vehicle which is of a plurality of unmanned aerial vehicles autonomously flying and is to be manually operated. An operation terminal device 401 dis...  
WO/2022/018356A1
The invention relates to an assembly for an aircraft turbine engine, including an unducted propeller blade (10) and a system (34) for setting the pitch of the blade (10) and further comprising: - a blade (10) of which the root (14) has a...  
WO/2022/018415A1
According to the present disclosure there is provided an arrangement (110) for influencing liquid flow, the arrangement comprising: a first section (1100) selectively configurable to provide a vortex generator surface (3100) to induce vo...  
WO/2022/018103A1
The invention relates to a heat shield assembly for a braked aircraft wheel (1, figure 1), comprising a heat shield (10) and at least one expander (20, 30), which comprises a main body (21, 31) projecting from an external surface of the ...  
WO/2022/019257A1
Provided are a detection system, a suspended device, and a detection method capable of detecting a situation below the water surface under various environments. A flying body 1, including an unmanned flying body, such as a drone, and a...  

Matches 451 - 500 out of 57,454