US-12617546-B2 - Modular hydrogen-fuel storage assembly

US12617546B2US 12617546 B2US12617546 B2US 12617546B2US-12617546-B2

Abstract

The present disclosure provides modular hydrogen-fuel storage assemblies with an external form factor corresponding to Unit Load Device (ULD) cargo containers, allowing the assemblies to be easily loaded into and stored in a cargo bay area of an aircraft. Each assembly can house one or more hydrogen fuel tanks containing liquid and gaseous hydrogen, which can be used to power an APU or other power system of the aircraft. Each assembly can include an internal cradle system for securing the tanks within the assembly, a ground servicing panel for refueling, a quick connection assembly for quickly coupling the assembly to the APU or other power system, a cold box for managing various fluid flow, and an avionics bay for controlling the various components of the assembly.

Inventors

Christopher K. Gilmore
James Mark Cousin
John-Paul Clarke

Assignees

SAS Beyond Aerosapce

Dates

Publication Date: 20260505
Application Date: 20230502

Claims (14)

1 . A modular hydrogen-fuel storage assembly, comprising: a refillable, reusable hydrogen fuel tank configured to contain hydrogen fuel; a housing with a front portion, a rear portion, a top portion, a bottom portion, and an interior portion, wherein the hydrogen fuel tank is contained within the interior portion, and wherein the housing is configured to have a size and shape corresponding to a Unit Load Device (ULD) cargo container; a hydrogen-fuel plumbing system positioned within the housing and connected to the hydrogen fuel tank for carrying hydrogen fuel to and from the hydrogen fuel tank; a cold box contained within the housing, and at least a portion of the hydrogen-fuel plumbing system is contained in the cold box; a quick connection assembly coupled to the hydrogen fuel tank and positioned adjacent to the top portion of the housing, the quick connection assembly having one or more connectors configured to releasably connect with one or more external fuel lines coupled to an auxiliary power unit (APU) of an aircraft; a ground servicing panel coupled to the housing and coupled to the hydrogen fuel tank; and an electronics bay operatively coupled to the hydrogen fuel tank and removably contained in the interior portion of the housing; wherein the modular hydrogen-fuel storage assembly is configured to be loaded into a cargo bay of the aircraft.
2 . The modular hydrogen-fuel storage assembly of claim 1 , wherein the quick connection assembly comprises: a gaseous hydrogen outlet coupled to the hydrogen fuel tank; a coolant inlet coupled to the cold box; a coolant outlet coupled to the cold box; a vent and vacuum outlet coupled to the cold box; and a latch connected to the connectors and being movable between locked and released positions; wherein the gaseous hydrogen outlet, the coolant inlet, the coolant outlet, and the vent and vacuum outlet are configured to be coupled to the APU; wherein the gaseous hydrogen outlet, the coolant inlet, the coolant outlet, and the vent and vacuum outlet are configured to be open when the latch is in the locked position, and wherein the gaseous hydrogen outlet, the coolant inlet, the coolant outlet, and the vent and vacuum outlet are configured to be closed when the latch is in the released position.
3 . The modular hydrogen-fuel storage assembly of claim 1 , wherein the ground servicing panel comprises: a liquid hydrogen inlet; and a gaseous hydrogen venting outlet, wherein the liquid hydrogen inlet is configured to be coupled to a liquid hydrogen supply when the modular hydrogen-fuel storage assembly is outside of the aircraft.
4 . The modular hydrogen-fuel storage assembly of claim 1 , wherein the electronics bay comprises a plurality of electrical components retained on a support tray, wherein the support tray is movable relative to the housing between a stowed and deployed positions, in the stowed position the support tray and electronic components are within the housing, and in the deployed position the support tray and electronic components are at least partially exterior of the housing.
5 . The modular hydrogen-fuel storage assembly of claim 4 , wherein the housing has rails adjacent to the bottom portion, and the support tray is slidably coupled to rails and movable along the rails between the stowed and deployed positions.
6 . The modular hydrogen-fuel storage assembly of claim 1 , further comprising sensors configured to monitor the one or more hydrogen fuel tanks, wherein the electronics bay comprises a controller operatively coupled to the sensors, and wherein the controller is configured to switch between a ground mode and a flight mode.
7 . The modular hydrogen-fuel storage assembly of claim 1 , further comprising a ventilation line coupled to the interior portion of the housing and configured to vent gaseous hydrogen out of the interior portion to the cargo bay or to an ambient environment exterior of the aircraft.
8 . A modular hydrogen-fuel storage assembly, comprising: a refillable, reusable liquid hydrogen fuel tank; a housing with an interior portion, wherein the hydrogen fuel tank is contained within the interior portion, and wherein the housing has a size and shape corresponding to a Unit Load Device (ULD) cargo container; a hydrogen-fuel plumbing system positioned within the housing and connected to the hydrogen fuel tank for carrying hydrogen fuel to and from the hydrogen fuel tank; a connection assembly coupled to the hydrogen fuel tank and positioned adjacent to the top portion of the housing, the connection assembly having one or more connectors configured to releasably connect with one or more external fuel lines coupled to an external power train of an aircraft; and a controller operatively coupled to the hydrogen fuel tank and removably contained in the interior portion of the housing; wherein the modular hydrogen-fuel storage assembly is configured to be loaded into a receiving bay of a vehicle and connected to a hydrogen-powered powertrain of the vehicle.
9 . The modular hydrogen-fuel storage assembly of claim 8 , further comprising a hydrogen-fuel plumbing system positioned within the housing and connected to the liquid hydrogen fuel tank for carrying hydrogen fuel to and from the liquid hydrogen fuel tank, and a cold box contained within the housing, and at least a portion of the hydrogen-fuel plumbing system is contained in the cold box.
10 . The modular hydrogen-fuel storage assembly of claim 8 , wherein the housing comprises an internal frame structure and a plurality of closure panels attached to the internal frame to define an interior portion of the housing that contains the liquid hydrogen fuel tank, wherein at least one of the panels is an openable panel movable between open and closed positions, wherein the openable panel in the open position is spaced apart from an interior portion of the housing to allow access to the liquid hydrogen tank, and the openable panel in the closed position covers the interior portion encloses the interior portion of housing to block access to the liquid hydrogen fuel tank.
11 . A method of providing a modular hydrogen-fuel storage assembly to an aircraft, comprising: loading the modular hydrogen-fuel storage assembly into a cargo bay of the aircraft, wherein the modular hydrogen-fuel storage assembly contains a liquid hydrogen fuel tank and a quick connection assembly fluidly coupled to the liquid hydrogen fuel tank; securing the modular hydrogen-fuel storage assembly at a first position inside the cargo bay; and coupling a plurality of lines extending from a hydrogen-powered powertrain of the aircraft to a quick connection assembly of the modular hydrogen-fuel storage assembly, wherein the quick connection assembly is positioned at a top portion of the modular hydrogen-fuel storage assembly, and wherein the modular hydrogen-fuel storage assembly is configured to have a size and shape corresponding to a Unit Load Device (ULD) cargo container corresponding to a configuration of the cargo bay of the aircraft.
12 . The method of claim 11 , further comprising: prior to loading the modular hydrogen-fuel storage assembly into the cargo bay of the aircraft, filling the liquid hydrogen fuel tank stored inside the modular hydrogen-fuel storage assembly with liquid hydrogen through a ground servicing panel of the modular hydrogen-fuel storage assembly at a location remote from the aircraft.
13 . The method of claim 11 wherein the modular hydrogen-fuel storage assembly has a housing that contains the liquid hydrogen fuel tank and an electronics bay with electronic components on a support tray and coupled to the liquid hydrogen fuel tank, the method further comprising accessing the interior area of the housing and moving the support tray relative to the housing from a stowed position within the interior area to a deployed position at least partially exterior of the interior area of the housing.
14 . The method of claim 11 wherein the modular hydrogen-fuel storage assembly is a first modular hydrogen-fuel storage assembly, and wherein the liquid hydrogen fuel tank is filled with the liquid hydrogen fuel to a fill level, and the method further comprises removing the first modular hydrogen-fuel storage assembly from a cargo bay after liquid hydrogen fuel has been withdrawn from the fuel tank via activation of the powertrain, and loading a second modular hydrogen-fuel storage assembly into the cargo bay to replace the first modular hydrogen-fuel storage assembly.

Description

CROSS-REFERENCE TO RELATED APPLICATION This non-provisional patent application claims priority to and the benefit of U.S. Provisional Patent Application No. 63/337,972, titled MODULAR HYDROGEN-FUEL STORAGE ASSEMBLY, filed May 3, 2023, which is incorporated herein in its entirety by reference thereto. TECHNICAL FIELD The present technology is directed toward hydrogen fuel storage and delivery systems for vehicles, and more particularly toward modular hydrogen-fuel storage and delivery systems for planes or other aircraft. BACKGROUND Hydrogen is a clean energy source that can be used to power various vehicles, including aircraft or other vehicles. The hydrogen fuel is typically stored in tanks or other selected vessels as a gaseous fuel or stored at cryogenic conditions in a liquid state. Hydrogen fuel provides a distinct advantage over other types of power sources. For example, aviation gas or jet fuel has specific energies that may generally range from about 43 MJ/kg to about 48 MJ/kg. In contrast, hydrogen has a specific energy that may generally range from about 120 MJ/kg to about 140 MJ/kg. Thus, using hydrogen as a fuel source for vehicles can reduce the fuel weight onboard vehicles, while providing a comparable amount of energy as other traditional sources of fuel. Further, burning carbon-based fuels generates exhaust with a variety of atmospheric contaminates, such as carbon dioxide. Consuming hydrogen for fuel, however, only emits benign or nontoxic byproducts, such as water, thereby reducing the environmental impacts of various modes of transportation that use hydrogen as a fuel source. Even among aircraft having hydrogen-powered engines, APUs, or other powerplants, most do not have space to specifically house hydrogen fuel tanks. Moreover, hydrogen fuel tanks require various structures and systems unique to storing and managing hydrogen fuel. Requiring aircraft to be outfitted with such space and equipment can be costly and time-consuming and can deter the use of hydrogen fuel in aircraft. Thus, there is a need for systems and methods for loading and operatively coupling hydrogen fuel tanks to aircraft in an easy and quick manner. SUMMARY The technology of the present disclosure overcomes the above drawbacks and provides additional benefits. For example, one or more embodiments of the present technology provides a modular hydrogen-fuel storage assembly comprising housing that contains a refillable, reusable hydrogen fuel tank configured to contain hydrogen fuel. The housing has a front portion, a rear portion, a top portion, a bottom portion, and an interior portion. The housing has a size and shape corresponding to a Unit Load Device (ULD) cargo container. A hydrogen fuel plumbing system is positioned within the housing and connected to the hydrogen fuel tank for carrying hydrogen fuel to and from the hydrogen fuel tank. A cold box is contained within the housing, and at least a portion of the hydrogen fuel plumbing system is contained in the cold box. A quick connection assembly is coupled to the hydrogen fuel tank and positioned adjacent to the top portion of the housing. The quick connection assembly has one or more connectors configured to releasably connect with one or more external fuel lines coupled to an auxiliary power unit (APU) of an aircraft. A ground servicing panel is coupled to the housing and coupled to the hydrogen fuel tank, and an avionics bay is operatively coupled to the hydrogen fuel tank and removably contained in the interior portion of the housing. The modular hydrogen-fuel storage assembly is configured to be loaded into a cargo bay of the aircraft. Another embodiment of the present technology provides a modular hydrogen-fuel storage assembly configured to be loaded into a cargo bay of an aircraft. The assembly has a modular housing that contains at least one liquid hydrogen fuel tank configured to contain liquid hydrogen fuel in a substantially cryogenic environment. The exterior of the housing has a size and shape corresponding to a Unit Load Device (ULD) cargo container. A hydrogen fuel plumbing system is positioned within the housing and connected to the liquid hydrogen fuel tank for carrying hydrogen fuel to and from the liquid hydrogen fuel tank. A quick connection assembly is coupled to the liquid hydrogen fuel tank and positioned on a top portion of the housing. The quick connection assembly has one or more connectors configured to releasably connect with one or more external fluid lines. The quick connection assembly is movable between locked and released positions, wherein the connectors are in sealable engagement with mating connectors of the external fluid lines when in the locked position, and the wherein the connectors are disengaged from the mating connectors of the external fluid lines when in the released position. The quick connection assembly is positioned to connect to the fluid lines that extend over the top portion of the housing. Another embodiment