An aircraft having at least one transport pipe in which dihydrogen flows and, for each transport pipe, an embedding channel in which the transport pipe is housed. The embedding channel has a gutter that has a bottom and an opening opposite the bottom and a cover that covers the opening of the gutter. The cover constitutes an outer wall of the aircraft in direct contact with external air surrounding the aircraft. The cover has ventilation windows passing through it that allow the passage of the dihydrogen towards the outside. With such an arrangement, even in the event of dihydrogen leaking into the embedding channel, the dihydrogen is automatically evacuated towards the outside of the aircraft.

A mobile drone communication control station which has capabilities of fueling hydrogen or liquid hydrogen drone, communication control for the drone, communication to the remote pilot center and the edge computing system for analyzing the photos taken from the drone.

A mobile drone communication control station which has capabilities of fueling hydrogen or liquid hydrogen drone, communication control for the drone, communication to the remote pilot center and the edge computing system for analyzing the photos taken from the drone.

Disclosed is a device and method to load stores on an aircraft. The device may include a controller configured to: assign one or more stores to the aircraft; and control at least one actuator to: control a position of the aircraft; load the one or more stores onto one or more corresponding lift portions; position the one or more stores relative to a position of the aircraft determined in accordance with sensor information from at least one sensor; and secure the one or more stores to the aircraft.

Disclosed is a device and method to load stores on an aircraft. The device may include a controller configured to: assign one or more stores to the aircraft; and control at least one actuator to: control a position of the aircraft; load the one or more stores onto one or more corresponding lift portions; position the one or more stores relative to a position of the aircraft determined in accordance with sensor information from at least one sensor; and secure the one or more stores to the aircraft.

A refueling system for hydrogen fuel cell-powered aircraft is disclosed. The system includes a compressor to receive a source of low temperature, high pressure hydrogen gas and compress the low temperature, high pressure hydrogen gas into a higher temperature, higher pressure hydrogen gas. A compression chamber within the compressor to receive the higher temperature, higher pressure hydrogen gas from the compressor. A valve coupled with the compression chamber to reduce the pressure of the higher temperature, higher pressure hydrogen gas to a higher temperature, lower pressure hydrogen gas. A storage container on an aircraft to receive the higher temperature, lower pressure hydrogen gas via the pressure relief valve. A heat exchanger in thermal cooperation with the compression chamber, the heat exchanger configured to absorb heat from the compression chamber and convert the heat into storable energy.

Methods, apparatus, systems, and articles of manufacture are disclosed to house a vehicle, including a first container leg disposed on a first corner of a first container, a second container leg disposed on a second corner of the first container, a third container leg disposed on a third corner of the first container, a fourth container leg disposed on a fourth corner of the first container, at least one of the first, second, third, and fourth container legs each having an upper portion with a ramped receiving slot and a lower portion with a first ramped foot, and wherein the ramped receiving slot is to receive a protrusion associated with a second ramped foot of a second container different from the first container.

Methods, apparatus, systems, and articles of manufacture are disclosed to house a vehicle, including a first container leg disposed on a first corner of a first container, a second container leg disposed on a second corner of the first container, a third container leg disposed on a third corner of the first container, a fourth container leg disposed on a fourth corner of the first container, at least one of the first, second, third, and fourth container legs each having an upper portion with a ramped receiving slot and a lower portion with a first ramped foot, and wherein the ramped receiving slot is to receive a protrusion associated with a second ramped foot of a second container different from the first container.

A system for monitoring components of an aircraft ground refueling system includes a first computing device and a second computing device hosting a data base. The first computing device is caused to read a component identification tag secured to a component of an aircraft ground refueling system; the tag contains a unique component identifier. The first computing device transmits the component identifier to the second computing device which verifies that the component identifier is active in the data. The first computer, responsive to the verification, displays a user interface to receive data representative of an operational status of the component and transmits the operational status. The second computing device stores the data in the database to create an operational history of the component. The second computing device analyzes the history of the data to determine a characteristic operational parameter of the component of the aircraft ground refueling system.

A system for monitoring components of an aircraft ground refueling system includes a first computing device and a second computing device hosting a data base. The first computing device is caused to read a component identification tag secured to a component of an aircraft ground refueling system; the tag contains a unique component identifier. The first computing device transmits the component identifier to the second computing device which verifies that the component identifier is active in the data. The first computer, responsive to the verification, displays a user interface to receive data representative of an operational status of the component and transmits the operational status. The second computing device stores the data in the database to create an operational history of the component. The second computing device analyzes the history of the data to determine a characteristic operational parameter of the component of the aircraft ground refueling system.