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Patent Searching and Data


Matches 351 - 400 out of 61,901

Document Document Title
WO/2018/178589A1
The invention concerns an aircraft propulsion unit (1), comprising: - a turbojet engine (3); - a lateral pylon (7), connected to the fuselage of said aircraft, - a nacelle (5) mounted on said lateral pylon (7), comprising: - an upstream ...  
WO/2018/178776A1
The present disclosure relates to a control system for a retractable belly mounted payload in an Aerial vehicle for retraction, pan and tilt movements of the payload, comprising a first mechanism to rotate the payload about a vertically ...  
WO/2018/178750A1
A method and apparatus in an unmanned aircraft traffic management system are described. Flight data is received from a network device. The flight data includes data about an event related to a flight of the UAS in an airspace, a timestam...  
WO/2018/183750A1
A panel assembly that is configured to be secured to a frame that includes a panel having a top and a bottom, a first bracket assembly and a second bracket assembly. The first bracket assembly includes a first pivot member and a first br...  
WO/2018/178145A1
The invention concerns a mechanical reduction gear (156) comprising: - an input shaft (158) rotated by a motor, - an output shaft (160) coaxial with the input shaft (158), - an endless screw (250) mounted coaxially on the input shaft (15...  
WO/2018/178908A1
An aircraft lighting system includes a light unit configured to emit light, a portable measurement device, and a control unit. The portable measurement device is configured to measure at least one attribute of the light emitted from the ...  
WO/2018/183428A1
In some embodiments, systems, apparatuses and methods are provided herein that enable delivery of retail products. Some embodiments provide delivery systems comprising: a package support frame comprising first and second package supports...  
WO/2018/177449A1
The invention relates to a cabin lining element (18') for an aircraft cabin arranged in the interior of an aircraft fuselage structure (12), having a fuselage structure side (30) and a cabin side (32). On the fuselage structure side (30)...  
WO/2018/182797A1
This document describes a system and method through which unmanned aerial vehicles (UAVs) and other vehicles (e.g., unmanned underwater vehicles (UUVs), also known as autonomous underwater vehicles (AUVs), unmanned water-surface vehicles...  
WO/2018/177873A1
The invention relates to an automation system (10), comprising: a control device (20) for controlling at least one machine, at least one unmanned aircraft (40, 40a, 40b, 40c, 40d), the control device (20) being designed to control the un...  
WO/2018/176291A1
Hollow motor apparatuses and associated systems and methods for manufacturing the same are disclosed herein. In representative embodiment, a hollow motor apparatus includes a rotor assembly rotatable about a rotation axis, a stator assem...  
WO/2018/183040A1
An load adaptive lift assist for a pivoting stowage bin includes an assembly housing having an interior and a pair of opposing end fittings. A piston rod is disposed within the assembly housing and operatively coupled to one of the end f...  
WO/2018/178729A1
The present disclosure relates to seating apparatus. In particular, the present application relates to an aircraft seat (1). The aircraft seat (1) includes a seat chassis (4) and a seat assembly (5). The seat assembly (5) has a seat pan ...  
WO/2018/182576A1
A system that includes a vehicle fuel-receiver comprising a port located on a vehicle surface; and an onboard computer programmed to: send a fuel delivery request to an unmanned aerial vehicle (UAV); actuate the port to permit the UAV to...  
WO/2018/183731A1
A solid state liquid-chilled bar unit for an aircraft galley includes a multilevel frame dimensioned to fit the galley and including stacked slots, each slot configured to fit a compartment. Warmer compartments include a liquid thermoele...  
WO/2018/182564A1
A drone pod includes a pod shell, a door, a motor and a computer. The pod shell includes a base, a top, and a wall. The top has an opening sized to receive a drone. The wall connects the base and the top. The door is disposed in the open...  
WO/2018/177474A1
The invention relates to a receiving apparatus (200, 300, 400, 500) for packages (1) or packets delivered by air, having an enclosure (201, 301) that protects against weathering and has an opening (202) for inserting a package (1) or a p...  
WO/2018/182944A1
An autonomous drone integrated with wide bandwidth, high energy acoustic wave generators sent to evict and eradicate agricultural pests within a patrolling area. The drone hovering close to a plant bombards its leaves and fruits with hig...  
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...  

Matches 351 - 400 out of 61,901