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Matches 501 - 550 out of 62,196

Document Document Title
WO/2018/178187A1
The invention relates to a dynamic force generator (100) comprising - a supporting shaft (110); - a first rotor (120) comprising: an internal bore (121) housing said supporting shaft (110) and bearings (R1, R2) arranged between the suppo...  
WO/2018/178276A1
The present invention essentially relates to an arrangement of individual seats intended to be installed in a cabin of an aeroplane (59) comprising at least one module (M1) of two seats (13.1, 13.3) arranged facing each other, said modul...  
WO/2018/182496A1
A device configured to deploy a retractable landing gear having a main landing gear (110) and a secondary landing gear (120) is provided. The device comprises an electrical motor (130) in driving connection with a drive shaft (140) conne...  
WO/2018/182448A1
The invention relates to methods for rescuing the crew of a light helicopter in the event of an emergency involving loss of control in uncontrolled freefall. The technical result of the invention is a more effective method for rescuing t...  
WO/2018/178566A1
A method for controlling a multi-engine bay (10), according to which the following steps are carried out: a) the bay is controlled so that it ensures a desired thrust and so that each engine is used in accordance with a set of operating ...  
WO/2018/178948A1
An air intake unit (3) for an engine of an aircraft (1); the intake unit (3) has: a tubular housing (4); a first inlet opening (7) which is obtained through an outer wall (6) of the tubular housing (4) and through which external air can ...  
WO/2018/178565A1
A device for temporarily increasing power (13) for increasing the power of at least one first turbomachine (5A) and at least one second turbomachine (5B), said device comprising a coolant reservoir (14), a first injection circuit (16A), ...  
WO/2018/175037A1
Electrically operated propellant thrust assist supplements an airplane's takeoff, landing or inflight maneuvers. Unlike conventional SRM propellants, the burn rate of the electrically operated propellant can be varied via an electrical i...  
WO/2018/172815A1
The invention relates to multicopter frames. The multicopter frame according to the present invention comprising: (i) a first housing (1) and a second housing (2), both the first housing and the second housing are substantially centrally...  
WO/2018/173072A2
System for precision irrigation is disclosed, the system comprises a main line. A plurality of sub main lines, wherein the plurality of sub main lines are configured to receive fluid from the main line. Further the system comprises a plu...  
WO/2018/173024A3
This invention is a security method for identifying possible attacks, suicide people or hijacking attempt, which allows identifying physiological behaviour patterns as for example: anxiety, nerves, stress and others, reading internal pat...  
WO/2018/174943A1
An air inlet for a flight vehicle engine includes at least one fin, at least partially upstream of a throat of the engine. The fin protrudes into a flow channel, extending beyond a boundary layer into the main airstream in the inlet. The...  
WO/2018/172252A1
The invention relates to a cabin air inlet module (16). The cabin air inlet module (16) has a flow channel body (8). The flow channel body (8) has at least one wall which delimits a flow channel in which feed air (5) is supplied to a zon...  
WO/2018/172812A1
The invention relates to an aircraft braking landing device and to the emergency landing of an aeroplane. The device comprises a shock-absorbing platform consisting of elastic cells fastened to each other and filled with a gaseous mixtur...  
WO/2018/172737A1
A vehicle comprising: a fuel store (104) configured to store a fuel, the fuel comprising a hydrocarbon; a fuel reformer (108) coupled to the fuel store (104) and configured to: receive an input comprising the hydrocarbon; and process the...  
WO/2018/175606A1
An aircraft for use in fixed wing flight mode and rotor flight mode while maintaining a horizontal fuselage is provided. The aircraft can include a fuselage, wings, rotor, and a plurality of engines. The rotor can comprise a wing attachm...  
WO/2018/172666A1
The invention concerns a method for monitoring at least one engine (2) of an aircraft (1), the aircraft comprising a passenger cabin (4), the method comprising the following steps: - a step of acquiring (110) a signal that is at least in...  
WO/2018/172046A1
A passenger seat (10) comprises a backrest (14), a seat element (16) and a size increasing mechanism (30) which is designed to convert a weight (FG) acting on the seat element (16) when a user sits in the passenger seat (10) into an incr...  
WO/2018/171239A1
A negative pressure low dead oil anti-bubble aeroplane fuel tank apparatus, comprising a fuel tank outer shell, an oil suction hose (3) arranged inside the fuel tank outer shell, a fueling port (9) arranged on the fuel tank outer shell, ...  
WO/2018/173348A1
This low-temperature tank is provided with a container main body (10). The container main body (10) includes: a metal liner (13) that forms a storage space; and a wall member (14) wound on an outer peripheral surface (13a) of the metal l...  
WO/2018/175694A1
Disclosed herein is a modular aerial vehicle system having a fuselage module configured to couple with a plurality of lift generation modules. The modular aerial vehicle system may comprise a fuselage module and a lift generation module....  
WO/2018/175931A1
Display systems for a vehicle are contemplated that comprise a seat display unit coupled with a display screen, where the display screen is affixed to a seat back and the seat display unit is disposed within the seat back. The display sc...  
WO/2018/172754A1
A propeller assembly (200) comprising a propeller hub (201) which can be driven about an axis and at least two propeller blades (203) each mounted to the hub at a point distal from the axis by pivoting means (203, 211, 212) alloying the ...  
WO/2018/174905A1
Some methods and configurations are disclosed for high bandwidth acquisition of magnetometer data with increased sensitivity. Some embodiments provide for increased bandwidth and sensitivity of the magnetometer by eliminating a reference...  
WO/2018/173158A1
A data acquisition device (1) comprises a balloon body (10), a first rope (21), a second rope (22), a first holding member (31), a second holding member (32), a first rail (41), and a second rail (42). The first rope (21) is connected to...  
WO/2018/171089A1
Disclosed is an aircraft (100) with a super high aspect ratio based on self-unfolding folding wing technology, the aircraft comprising: an aircraft body (10); a fixed wing (20); and a movable wing assembly comprising a first movable wing...  
WO/2018/172316A1
The invention relates to a positioning device (10) for positioning a manipulator (11) on an outer wall (101) of an aircraft (100), said device comprising at least one yoke (30) with a first yoke arm (58) and a second yoke arm (59), and a...  
WO/2018/173765A1
This control device (C) controls a linear actuator (1) that raises and lowers a landing gear (L) on the basis of the stroke displacement of the linear actuator (1) as detected by a stroke sensor (10). When the landing gear (L) is to be s...  
WO/2018/173040A1
The present invention provides a method for decelerating and redirecting an airborne platform, comprising the steps of retaining a flexible airfoil in non-deployed form in controllably releasable secured relation with each corresponding ...  
WO/2018/173994A1
The present invention addresses the problem of providing an unmanned aerial vehicle and an airbag device thereof capable of preventing damage to a payload even in the event of difficulties such as a mid-air collision or uncontrolled desc...  
WO/2018/172960A1
Embodiments of the present disclosure relate generally to galley trolley compartment doors that replace traditional trolley retainer latches used to secure trolleys when positioned in galley compartments. The galley trolley compartment d...  
WO/2018/172659A1
The invention relates to a heat transfer device (2) capable of transferring heat, comprising a housing (5) having a first main wall (12) and a second main wall (14), said housing (5) comprising an internal cavity (6) closed in a sealed m...  
WO/2018/174986A3
A method is described for repairing the surface of rotor blades or aircraft wings, comprising (a) a composite substrate; and (b) a protection layer having at least one area of at least partial damage, the method comprising (i) optionally...  
WO/2018/172045A1
A passenger seat (10) comprises a backrest (14) and a seat element (16) that includes a first portion (16a) adjoining the backrest (14) and a second portion (16b) that can pivot between a rest position and an operational position. In the...  
WO/2018/175545A1
A passenger seat assembly includes a riser attached to an upper surface of a floor of the vehicle, a seat attached to an upper surface of the riser, and at least one shell portion attached to the upper surface of the riser. The riser inc...  
WO/2018/167473A1
The present subject matter relates to a system and a method for galactic transportation (100). The galactic transportation system (100) may comprise multiple rails (102) arranged in a first direction (103), a platform (108) for supportin...  
WO/2018/168565A1
[Problem] To provide a drone (unmanned flying body) capable of appropriately capturing images of root position portions and side surfaces of field crops in a field. [Solution] When a camera capable of capturing images in the rearward dir...  
WO/2018/169454A3
´╗┐The invention relates to the field of aviation engines and aeroplane braking devices. A deflecting cascade of a thrust reverser of an engine nacelle includes monolithic sections. Each section is made of a polymer composite material an...  
WO/2018/167472A1
The present subject matter relates to an aircraft stabilization system (200). The aircraft stabilization system (200), amongst other components, may include multiple sensors (202), a processing unit (206), and multiple stabilization unit...  
WO/2018/170158A1
Embodiments of systems, devices, and methods are described that relate to module structures for use in forming a cabin interior of an aircraft (102). Many embodiments relate to a support structure (105) including a lattice (174) configur...  
WO/2018/165728A1
The present invention relates to an anchoring platform for captive aircraft that addresses one of the main problems when handling captive aerostats, which is the excessive workload required to switch same between flying and anchored stat...  
WO/2018/165916A1
Disclosed is a propulsion system for an unmanned aerial vehicle, the system comprising a propulsion motor (121) and a locking device (203). The propulsion motor (121) is used to drive a propeller (122) of the unmanned aerial vehicle (100...  
WO/2018/167840A1
The present invention is configured such that, for each RSO(n), in each combination of observation-possible time periods OT(h) for a number R(n) of requested observations, an evaluation value E(m,n,h) is integrated that was calculated by...  
WO/2018/165937A1
Disclosed is a distance-measuring sensor (1) and a plant protection unmanned aerial vehicle having the distance-measuring sensor (1), the distance-measuring sensor (1) comprising a housing (10), a distance-measuring module (20) arranged ...  
WO/2018/170427A1
Systems and methods are described herein for automatically monitoring a status or position of a vehicle component. Both powered and non-powered (or passive) systems are contemplated. The systems and methods utilize a sensor that signals ...  
WO/2018/169652A1
The present approach relates to the inspection of assets, such as assets having parts that move during operation. As discussed herein, operational data for the asset may be incorporated into planning or adapting the flight plan and/or op...  
WO/2018/167013A1
The invention relates to a device (1) for connecting an end of a first shaft to an end of a second shaft, the end of the first shaft having a radial groove, the device comprising: -a body (2) having a bore (21) into which the end of the ...  
WO/2018/170383A1
In an embodiment of the invention there is a cyclotronic actuator. The actuator is defined by having a high-voltage plasma driver connected to a first electrode. The first electrode is surrounded by a dielectric material. A second electr...  
WO/2018/165882A1
A propulsion system includes a propulsion motor (121) configured to drive a propeller (122) and an apparatus (203) for releasably coupling the propeller (122) to the propulsion motor (121). The apparatus (203) includes an engagement memb...  
WO/2018/167349A3
An autonomous private safety system capable of providing passive and active services and combatting gender violence is formed by at least one robot equipment with a structure based on aerial or terrestrial, drone-like vehicles, incorpora...  

Matches 501 - 550 out of 62,196