Patents Assigned to Brulic Ltd.
  • Patent number: 11945601
    Abstract: 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 to deploy from the receiver aircraft; controlling at least one of the supply aircraft and the drogue to engage the drogue with a first end of an electrical cable of the supply aircraft, a second end of the electrical cable being connected to the supply aircraft; and transmitting a return command signal from the communication unit of the supply aircraft to the communication unit of the receiver aircraft, to cause the line and drogue to return to the receiver aircraft with the first end of the electrical cable. The supply aircraft is located behind the receiver aircraft and the deploy command signal is for causing the line and drogue to deploy rearwardly of the receiver aircraft.
    Type: Grant
    Filed: September 19, 2019
    Date of Patent: April 2, 2024
    Assignee: Brulic Ltd.
    Inventor: James Pitman
  • Patent number: 11718412
    Abstract: 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 supply line from the propellant supply aircraft to the host aircraft when the propellant supply aircraft is located behind the host aircraft; a propellant inlet configured for connection with the propellant supply line; a propellant outlet in communication with the propellant inlet and configured for connection with a propellant system of the host aircraft; an electrical power unit for powering the propellant-handling module; and a communication and control system for receiving a deploy command signal and a return command signal from the supply aircraft and configured to: receive said deploy command signal and in response control the motorised drum unit to deploy the line and drogue for said engagement with the propellant supply line; and receive said return command signal and i
    Type: Grant
    Filed: September 26, 2019
    Date of Patent: August 8, 2023
    Assignee: Brulic Ltd.
    Inventor: James Pitman
  • Publication number: 20210362872
    Abstract: 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 to deploy from the receiver aircraft; controlling at least one of the supply aircraft and the drogue to engage the drogue with a first end of an electrical cable of the supply aircraft, a second end of the electrical cable being connected to the supply aircraft; and transmitting a return command signal from the communication unit of the supply aircraft to the communication unit of the receiver aircraft, to cause the line and drogue to return to the receiver aircraft with the first end of the electrical cable. The supply aircraft is located behind the receiver aircraft and the deploy command signal is for causing the line and drogue to deploy rearwardly of the receiver aircraft.
    Type: Application
    Filed: September 19, 2019
    Publication date: November 25, 2021
    Applicant: Brulic Ltd.
    Inventor: James Pitman
  • Publication number: 20210362873
    Abstract: 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 lengthwise along the flexible inner tube. The rigid parts are movable by the actuator to provide continuous lengthwise cover over the flexible inner tube, so as to be able to resist radial expansion of the flexible inner tube when the flexible inner tube is pressurised. The rigid parts are further movable by the actuator to uncover lengthwise portions of the flexible inner tube between the rigid parts, so as to allow bending of the flexible inner tube when the flexible inner tube is unpressurised.
    Type: Application
    Filed: October 21, 2019
    Publication date: November 25, 2021
    Applicant: Brulic Ltd.
    Inventor: James Pitman
  • Publication number: 20210362871
    Abstract: 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 supply line from the propellant supply aircraft to the host aircraft when the propellant supply aircraft is located behind the host aircraft; a propellant inlet configured for connection with the propellant supply line; a propellant outlet in communication with the propellant inlet and configured for connection with a propellant system of the host aircraft; an electrical power unit for powering the propellant-handling module; and a communication and control system for receiving a deploy command signal and a return command signal from the supply aircraft and configured to: receive said deploy command signal and in response control the motorised drum unit to deploy the line and drogue for said engagement with the propellant supply line; and receive said return command signal and i
    Type: Application
    Filed: September 26, 2019
    Publication date: November 25, 2021
    Applicant: Brulic Ltd.
    Inventor: James Pitman