Fuel cell power system for an unmanned surface vehicle

Patent metadata

Field	Value
Publication number	US-11742502-B2
Application number	US-202117240544-A
Country	US
Kind code	B2
Filing date	Apr 26, 2021
Priority date	Jul 3, 2017
Publication date	Aug 29, 2023
Grant date	Aug 29, 2023

Abstract

A power system for an unmanned surface vehicle includes a fuel cell including a fuel cell stack, where the fuel cell stack includes a fuel inlet. The power system also includes a fuel storage including at least one fuel-storage module fluidly connected to the fuel inlet of the fuel cell stack. The fuel-storage module is a source of energy for the fuel cell. The power system also includes a fuel and thermal management system fluidly connected to the fuel inlet of the fuel cell stack. The fuel and thermal management system includes a heat exchanger in thermal communication with the fuel cell stack for removing waste heat produced by the fuel cell stack during operation. The fuel and thermal management system also includes a flow valve, a pressure regulator, and a conduit.

First claim

What is claimed is:

1. An unmanned surface vehicle including a power system, the power system comprising:
a fuel cell including a fuel cell stack, wherein the fuel cell stack includes a fuel inlet;
a fuel storage including at least one fuel-storage module fluidly connected to the fuel inlet of the fuel cell stack, wherein the at least one fuel-storage module is a source of energy for the fuel cell; and
a fuel and thermal management system fluidly connected to the fuel inlet of the fuel cell stack, wherein the fuel and thermal management system comprises:
a heat exchanger in thermal communication with the fuel cell stack for removing waste heat produced by the fuel cell stack during operation;
a primary circuit and a secondary circuit, wherein the primary circuit circulates coolant between the fuel cell stack and the heat exchanger, and the secondary circuit circulates the coolant between the fuel storage and the heat exchanger;
a liquid valve and a diverter conduit, wherein the liquid valve is opened in order to allow the coolant circulating in the secondary circuit to flow through the diverter conduit;
a water-cooled heat exchanger, wherein the coolant flowing through the diverter conduit flows to the water-cooled heat exchanger, wherein the water-cooled heat exchanger is cooled by a body of water the unmanned surface vehicle is deployed within; and
a flow valve, a pressure regulator, and a conduit, wherein the conduit fluidly connects the fuel storage to the fuel cell stack to deliver fuel from the fuel storage to the fuel cell stack by the conduit, and the flow valve and the pressure regulator are both located along the conduit.

2. The unmanned surface vehicle of claim 1 , further comprising a control module in communication with a heater, wherein the heater is in thermal communication with and heats fuel contained within the fuel storage.

3. The unmanned surface vehicle of claim 2 , wherein the fuel storage includes a metal-hydride fuel-storage substrate, and wherein the control module activates the heater to warm the metal-hydride fuel-storage substrate to a target temperature to achieve a target gaseous hydrogen fuel generation rate.

4. The unmanned surface vehicle of claim 2 , further comprising a pressure sensor and temperature sensor in communication with the control module, wherein the pressure sensor indicates a gas pressure of the at least one fuel-storage module and the temperature sensor indicates an internal temperature of the at least one fuel-storage module.

5. The unmanned surface vehicle of claim 4 , wherein the control module monitors the pressure sensor and the temperature sensor, and wherein the control module deactivates the heater in response to determining at least one of the following:
the gas pressure of the at least one fuel-storage module has reached a predefined limit, and
the internal temperature of the at least one fuel-storage module is at a target temperature.

6. The unmanned surface vehicle of claim 1 , wherein the fuel storage stores metal hydride, and wherein waste heat produced by the fuel cell stack is conducted by coolant flowing through the heat exchanger.

7. The unmanned surface vehicle of claim 6 , wherein the coolant flowing through the heat exchanger circulates to the fuel storage to heat the metal hydride.

8. The unmanned surface vehicle of claim 1 , wherein the heat exchanger draws waste heat from the fuel cell stack through the primary circuit.

9. The unmanned surface vehicle of claim 1 , further comprising an air blower for cooling the fuel cell stack to a target stack temperature.

10. The unmanned surface vehicle of claim 9 , further comprising a control module in communication with the air blower and a primary pump, wherein the primary pump circulates coolant flowing within the primary circuit between the fuel cell stack and the heat exchanger.

11. The unmanned surface vehicle of claim 10 , wherein the control module executes instructions for:
continuously monitoring power consumed by the air blower and power consumed by the primary pump;
comparing the power consumed by the air blower to the power consumed by the primary pump; in response to determining the power consumed by the air blower is equal to or less than the power consumed by the primary pump, continuing to power the air blower to cool the fuel cell stack to the target stack temperature; and
in response to determining the power consumed by the air blower is greater than the power consumed by the primary pump, reducing a speed of the air blower and activating the primary pump cool the fuel cell stack to the target stack temperature.

12. The unmanned surface vehicle of claim 1 , further comprising a secondary pump that circulates the coolant in the secondary circuit.

13. The unmanned surface vehicle of claim 12 , wherein the secondary pump is a variable displacement pump.

14. The unmanned surface vehicle of claim 1 , further comprising a three-way valve fluidly connected to the heat exchanger.

15. The unmanned surface vehicle of claim 1 , further comprising a three-way valve fluidly connected to the fuel storage.

16. A method of delivering fuel to and removing reaction waste heat from a fuel cell stack of a fuel cell by a fuel and thermal management system that is part of a power system for an unmanned surface vehicle, the method comprising:
fluidly connecting a fuel storage including at least one fuel-storage module to a fuel inlet of the fuel cell stack of the fuel cell, wherein the at least one fuel-storage module is a source of energy for the fuel cell;
removing the reaction waste heat produced by the fuel cell stack by a heat exchanger in thermal communication with the fuel cell stack;
fluidly connecting the fuel storage to the fuel cell stack by a conduit, wherein a flow valve and a pressure regulator are both located along the conduit;
circulating coolant by a primary circuit between the fuel cell stack and the heat exchanger and a secondary circuit between the fuel storage and the heat exchanger;
opening a liquid valve in order to allow the coolant circulating in the secondary circuit to flow through a diverter conduit;
allowing the coolant flowing through the diverter conduit to flow to a water-cooled heat exchanger, wherein the water-cooled heat exchanger is cooled by a body of water the unmanned surface vehicle is deployed within; and
delivering the fuel from the fuel storage to the fuel cell stack by the conduit.

17. The method of claim 16 , further comprising:
activating, by a control module, a heater to warm a metal-hydride fuel-storage substrate of the fuel storage to a target temperature to achieve a target gaseous hydrogen fuel generation rate, wherein the heater is in thermal communication with and heats fuel contained within the fuel storage.

18. The method of claim 16 , further comprising:
monitoring, by a control module, a pressure sensor and temperature sensor, wherein the pressure sensor indicates a gas pressure of the at least one fuel-storage module and the temperature sensor indicates an internal temperature of the at least one fuel-storage module.

19. The method of claim 18 , wherein the fuel and thermal management system further comprises a heater in thermal communication with and heats fuel contained within the fuel storage, and wherein the method further comprises:
deactivating, by a control module, the heater in response to the control module determining at least one of the following:
the gas pressure of the at least one fuel-storage module has reached a predefined limit, a

Assignees

• Boeing Co
• Liquid Robotics Inc

Inventors

• Carralero Michael A
• Willcox Jeffrey Scott

Classifications

• H01M8/04216 Primary

  characterised by the choice for a specific material, e.g. carbon, hydride, absorbent · CPC title

• B63H21/00

  Use of propulsion power plant or units on vessels · CPC title

• B63H21/38

  Apparatus or methods specially adapted for use on marine vessels, for handling power plant or unit liquids, e.g. lubricants, coolants, fuels or the like ({in outboard drives B63H20/001; } lubricating or cooling machines or engines in general F01 - F04) · CPC title

• H01M8/04007 Primary

  related to heat exchange · CPC title

• H01M8/04014

  Heat exchange using gaseous fluids; Heat exchange by combustion of reactants · CPC title