| Document |
Document Title |
|
WO/2024/038247A1 |
A fuel delivery device for air-to-air refuelling, the device comprising: a fuel outlet; and an optical transceiver, wherein the optical transceiver is configured to: illuminate the fuel delivery device to provide visual indication to an ...
|
|
WO/2024/015397A1 |
Embodiments of a recovery and deployment pylon (2000) for recovering and launching/relaunching a target aircraft (T) that can include a housing configured to be coupled with an aircraft, a motorized winch, a towline (102) coupled with th...
|
|
WO/2023/194253A1 |
Improved device and method for indoor monitoring The invention provides, amongst other aspects, an aircraft (1) for indoor monitoring, comprising a lifting means; a propulsion means (4, 4', 51, 61); a positioning means (2a, 2b); and a mo...
|
|
WO/2023/112023A1 |
A boom member for in-flight refueling includes a first boom member portion, a second boom member portion, and a connect/disconnect mechanism. The first boom member portion includes a first boom lumen, a first boom axis, and a fuel receiv...
|
|
WO/2023/079590A1 |
A power feeding system 1 comprising: a floating body 11 having power and control functions; and an unmanned aircraft 21 that observes environmental information using the floating body 11 as a base, wherein the floating body 11 is equippe...
|
|
WO/2023/009643A1 |
A mobile microgrid charging system may comprise a first battery array that is configured to be transported from location to location and facilitate fast charging of electric aircrafts. The mobile microgrid charging system is mobile and c...
|
|
WO/2022/248742A1 |
System for inspecting the hose used in refueling operations, consisting of a set of image sensors and electromagnetic radiation emitters in a ring that follows the vertical movement and inclination of the hose and allows the hose to pass...
|
|
WO/2022/150798A1 |
A multiply redundant safety system that protects humans and assets while transfer(s) and/or fuelling of on road/off road, rail, marine, aircraft, spacecraft, rockets, and all other vehicles and/or vessels utilizing Compressed and or Liqu...
|
|
WO/2022/147529A1 |
An exemplary rapid electrical charging system is disclosed for autonomous electrical vehicle refueling. The system can be used for in-air refueling, on-the-ground refueling, and refueling application. The system employs a charging and di...
|
|
WO/2022/137202A1 |
This disclosure is directed to a payload attachment and payload management and control device for an unmanned aircraft for supporting a payload having a payload handle, the payload attachment device. The payload attachment device includi...
|
|
WO/2022/073616A1 |
A conveyor arrangement (106) for airborne battery replacement between an aerial supply vehicle (102) having a store (108) of replacement batteries (114) suitable to power electric aerial vehicles (104) and an electric aerial vehicle (104...
|
|
WO/2022/049639A1 |
Provided is a device that can be attached to an unmanned aerial vehicle that can hold a number of parcels and put down each parcel at the desired location. This luggage-holding device is attached to the underside of the body of an unma...
|
|
WO/2022/039181A1 |
It is difficult for a flying mobile body to which power is transmitted wirelessly to have a large power reception antenna. In the present invention, a flying mobile body 4 comprises: a rotary wing 8 that rotates and generates lift; a f...
|
|
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/2021/234688A1 |
Examples of a refueling device for use in in-flight refueling operation are provided. In at least one example the refueling device includes a body, a boom member and a spatial control system. The body is configured for being towed by a t...
|
|
WO/2021/195274A1 |
Material transfer interfaces for space vehicles, and associated systems and methods, are disclosed. A representative system includes a coupling mechanism including a support structure, a latch-arm base movably connected to the support st...
|
|
WO/2021/140259A1 |
Camera and lights positioning system for inspecting air-to-air refueling hoses, which comprises a substructure that can be attached to a container or capsule or pod, one or two guidance substructures (13) that enclose the hose, a toroida...
|
|
WO/2021/119851A1 |
The present disclosure relates to a robotically controlled satellite refueling tool and associated robotically controlled support and site preparation tools which facilitates on-orbit refueling by teleoperation of fill/drain valves of va...
|
|
WO/2021/054521A1 |
The present invention relates to a system and a method for supplying fuel to an electric cart by using an aerial refueling drone. A fuel supply control server for controlling supply of fuel to at least one electric cart by using at least...
|
|
WO/2020/249447A1 |
The invention relates to a power assistance system (1) for supporting an electrically drivable aircraft (2) capable of vertical start and landing, wherein the power assistance system (1) is designed to support the aircraft (2) during asc...
|
|
WO/2020/235161A1 |
Provided is an image processing system capable of detecting the location of an unmanned mobile body and measuring the timing when the unmanned mobile body passed a predetermined location. An image processing system S is provided with: ...
|
|
WO/2020/156931A1 |
The present invention relates to system for transferring a fluid from a first spacecraft to a second spacecraft, the first spacecraft comprising a fluid transfer system comprising: a pressurant supply system, a first fluid tank configure...
|
|
WO/2020/121067A2 |
A metal air battery electrolyte replenishment system comprised of a base station with docking receptor apparatus and matching docking probe on a flying drone. The probe onboard the drone has a sensor that guides the drone to connect with...
|
|
WO/2020/084291A1 |
A fuel hose assembly for inflight fuelling of aircraft comprises: a flexible inner tube for conveying fuel under pressure; an outer cover comprising a plurality of rigid parts; and an actuator configured to move the rigid parts lengthwis...
|
|
WO/2020/079935A1 |
Provided is a flying body comprising: an antenna for forming a terrestrial communication area and providing wireless communication services to user terminals in the communication area; and an attachment/detachment unit that physically at...
|
|
WO/2020/079934A1 |
Provided is a control apparatus controlling a plurality of flying bodies including a first flying body which forms communication area by using a beam radiated to the ground, and includes an antenna for providing a radio communication ser...
|
|
WO/2020/065322A1 |
A propellant-handling module for installation in a host aircraft comprises: a motorised drum unit comprising a line and drogue for engagement with a propellant supply line of a propellant supply aircraft and for drawing the propellant su...
|
|
WO/2020/065271A1 |
A method of operating a supply aircraft for in-flight recharging comprises: transmitting a deploy command signal from a communication unit of the supply aircraft to a communication unit of a receiver aircraft, to cause a line and drogue ...
|
|
WO/2020/065247A1 |
A method of operating a fuel tanker aircraft for in-flight fuelling comprises: transmitting a deploy command signal from a communication unit of the tanker aircraft to a communication unit of a fuel receiver aircraft, to cause a line and...
|
|
WO/2020/028118A1 |
Systems, apparatuses, and methods are provided herein for charging an unmanned aerial vehicle (UAV) in flight. A method comprises controlling motions of a UAV via a locomotion system, wherein the UAV comprises a charging antenna coupled ...
|
|
WO/2019/208440A1 |
The present invention relates to a fire extinguishing system for carrying the nozzle of a fire hose connected to a drone to a high place. The fire extinguishing system comprises: a fire hose (10) having a nozzle (11) for spraying a fire ...
|
|
WO/2019/137919A1 |
A flow booster for optimizing flow of fuel passing into an aircraft. The flow booster includes a fuel intake fluidly coupled to the fuel circuit, and includes a housing and a piston. The piston has a piston head slidably movable in the h...
|
|
WO/2019/035080A1 |
A system and method for distributing power to racing aircraft systems is provided. The system includes a race course, a power transmitter directed towards a power delivery section of the race course, the power transmitter configured to r...
|
|
WO/2019/012523A1 |
Computerized system and method of controlling a refueling device including, when the device is in a non-engaged state: receiving a first roll angle of a tanker, determining a first desired roll angle, and providing a command for controll...
|
|
WO/2018/235071A1 |
A method for controlling maneuver of a refueling device, that includes: a refueling device is attached by a hose to a component of an aircraft. That component maintains a reference force on the hose. The desired position and current posi...
|
|
WO/2018/218321A1 |
Cargo aircraft having a cargo ramp and cargo door oppositely hinged relative to one another to allow access to the aircraft's cargo space may be provided with a flying boom mast that is physically mounted at the aft portion of the fusela...
|
|
WO/2018/190944A1 |
Capture assemblies and compliant extension assemblies may be utilized for insertion into a nozzle of a liquid engine of a spacecraft. The capture assembly may include an apparatus such as a probe for insertion into the nozzle and an asse...
|
|
WO/2018/182577A1 |
A computer that includes a processor and memory which stores instructions executable by the processor. The instructions include: initiate, from a vehicle, a fuel delivery request for fuel delivery by an unmanned aerial vehicle (UAV); in ...
|
|
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/2018/142925A1 |
An in-flight battery changing method for multicopters according to an aspect of the present invention is provided with: a first step of securing a supply path for supplying a battery between both multicopters while both a supply-side mul...
|
|
WO/2018/105054A1 |
The purpose of the present invention is to efficiently supply power to a power storage device (battery 260), and efficiently and safely deliver goods when goods are being transported by an unmanned flying body 3. The unmanned flying body...
|
|
WO/2018/020077A1 |
The present invention relates to a device comprising a set of means for creating points of light of different sizes and colours, which together form figures intended to create a sign in front of the eyes of a driver or operator, in order...
|
|
WO/2017/182686A1 |
The invention relates to a system for detecting the tip of the pole of the flying boom of a tanker and the mouth of the receptacle of a receiver, for semiautomatic or automatic contact for in-flight refuelling with a boom, ensuring that ...
|
|
WO/2017/178683A1 |
In operations that require a 3-D view and need a global view of a work area when it is advisable to have an enlarged view of a part of said area, having two pairs of cameras, one pair being stationary and the other being moveable and con...
|
|
WO/2017/139730A1 |
An aerial refueling system for refueling a receiver aircraft in flight comprises a hose reel assembly mounted onto a fuel supply aircraft's fuselage. The hose reel assembly has a rotatable drum defined by an outside diameter. A hose is w...
|
|
WO/2017/093584A1 |
The invention relates to a system for detecting the tip of the pole of the flying boom of a tanker plane and the mouth of the receptacle of the receiver for semiautomatic or automatic contact for refuelling during flight with a boom, whi...
|
|
WO/2017/066607A1 |
A system including a coupling (100) configured to couple a hose associated with a tanker aircraft to a nozzle associated with a receiving aircraft. The coupling may include a housing that houses a main poppet and a pilot poppet. The main...
|
|
WO/2017/051056A1 |
The invention relates to a haptic augmented reality device for facilitating actions to control a boom in full flight, allowing the boom to be controlled with a single hand, without the need for any training in what the manoeuvres refer t...
|
|
WO/2017/051057A1 |
The invention relates to a position-finding system comprising means for locating the position of the receiver, and means for locating the position of the end of the boom, which allow the exact determination of the positions and inclines ...
|
|
WO/2016/181116A1 |
Disclosed is a data transfer method comprising: performing a refuelling process including receiving, by an aircraft (104), aircraft fuel from a first entity (for example, a tanker aircraft (102)), the first entity being remote from the a...
|
