Fuel cell power system for an unmanned surface vehicle

Patent metadata

Field	Value
Publication number	US-11031613-B2
Application number	US-201715640962-A
Country	US
Kind code	B2
Filing date	Jul 3, 2017
Priority date	Jul 3, 2017
Publication date	Jun 8, 2021
Grant date	Jun 8, 2021

Abstract

A power system for an unmanned surface vehicle is disclosed. In one embodiment, the power system includes a fuel cell, a fuel storage, and an air management system. The fuel cell includes a fuel cell stack. The fuel cell stack includes a fuel inlet, an air inlet, and an exhaust outlet. The fuel storage includes 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 air management system is fluidly connected to the air inlet and the exhaust outlet of the fuel cell. An air snorkel is part of the air management system and provides air to operate the fuel cell while the unmanned surface vehicle is deployed on a surface of a body of water. The air snorkel includes an intake and an exhaust.

First claim

What is claimed is:

1. An unmanned surface vehicle, comprising:
a power system, comprising:
a fuel cell including a fuel cell stack, wherein the fuel cell stack includes a fuel inlet, an air inlet, and an exhaust outlet;
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;
a wave sensor in electronic communication with a control module, wherein the wave sensor is configured to indicate a sea state, and wherein the control module decides to either continue or terminate operation of the power system based on at least the sea state;
an air management system fluidly connected to the air inlet and the exhaust outlet of the fuel cell; and
an air snorkel that is part of the air management system and provides air to operate the fuel cell while the unmanned surface vehicle is deployed within a body of water, wherein the air snorkel provides air to operate the fuel cell while the unmanned surface vehicle is deployed on a surface of a body of water, and wherein the air snorkel includes:
an air intake for receiving ambient air supplied to the fuel cell stack; and
an exhaust for expelling exhausted air and exhausted water-vapor created by the fuel cell stack.

2. The unmanned surface vehicle of claim 1 , wherein the air snorkel includes a conduit, a first air valve, and a second air valve, and wherein the ambient air enters the conduit through the air intake, the exhausted air and exhausted water-vapor exit the conduit through the exhaust, the first air valve is fluidly connected to the air intake, and the second air valve is fluidly connected to the exhaust.

3. The unmanned surface vehicle of claim 2 , wherein the conduit defines a sump and the air snorkel includes a water pump fluidly connected to the sump, and water collected within the sump is removed by closing the first air valve and the second air valve and then activating the water pump.

4. The unmanned surface vehicle of claim 1 , wherein the air snorkel includes a conduit, an air blower, and a heater located downstream of the air blower, wherein the air blower circulates forced air throughout the conduit when activated, and the heater elevates the temperature of the forced air circulated by the air blower.

5. The unmanned surface vehicle of claim 4 , wherein the conduit is fluidly connected to the fuel cell stack and the forced air travels from the conduit to the fuel cell stack to warm the fuel cell stack to a warm-up temperature.

6. The unmanned surface vehicle of claim 1 , wherein the air snorkel includes a recirculation valve and a conduit, wherein the recirculation valve is a variable flow valve located along the conduit and mixes the ambient air entering the air intake with the exhausted air from the exhaust.

7. The unmanned surface vehicle of claim 6 , wherein the conduit is fluidly connected to the fuel cell stack and the recirculation valve is opened into either a fully opened position or one of a plurality of variable positions to raise a temperature of the ambient air to a target fuel cell operating temperature.

8. The unmanned surface vehicle of claim 1 , comprising a humidity sensor and an ambient humidity sensor, wherein the humidity sensor is positioned within a conduit of the air snorkel to detect moisture in air exiting the fuel cell stack, and the ambient humidity sensor indicates an ambient air humidity.

9. The unmanned surface vehicle of claim 8 , wherein the control module is in communication with a condenser and an air blower, and wherein the control module activates the condenser and the air blower in response to determining that the ambient air humidity exceeds a threshold relative humidity and the fuel cell stack contains a substantial amount of moisture.

10. The unmanned surface vehicle of claim 1 , comprising an air blower, wherein control module activates the air blower to recirculate air throughout a conduit of the air snorkel.

11. The unmanned surface vehicle of claim 10 , wherein the control module continuously monitors power consumed by the air blower and compares the power consumed by the air blower to an amount of power consumed by a liquid pump of a heat exchanger for cooling the fuel cell stack.

12. The unmanned surface vehicle of claim 11 , wherein the control module continues to keep the air blower activated to cool the fuel cell stack to a target stack temperature in response to determining the power consumed by the air blower is equal to or less than the average power consumption by the liquid pump.

13. The unmanned surface vehicle of claim 11 , wherein the control module deactivates the air blower and activates the liquid pump to cool the fuel cell stack to a target stack temperature in response to determining the air blower consumes more power than the amount of power consumed by the liquid pump of the heat exchanger.

14. The unmanned surface vehicle of claim 1 , comprising a heat exchanger for removing waste heat produced by the fuel cell stack during operation and a primary pump, wherein the primary pump circulates coolant flowing a primary circuit between the fuel cell stack and the heat exchanger.

15. The unmanned surface vehicle of claim 1 , comprising a heat exchanger for removing waste heat produced by the fuel cell stack during operation and a secondary pump, wherein the secondary pump circulates coolant in a secondary circuit between the fuel storage and the heat exchanger.

16. The unmanned surface vehicle of claim 1 , wherein sea state includes at least one of the following parameters: wave height, wave period and wave direction, and instantaneous platform attitude angles.

17. A method of providing air to operate a fuel cell of a power system, wherein the power system provides power to an unmanned surface vehicle, the method comprising:
fluidly connecting a fuel storage including at least one fuel-storage module to a fuel inlet of a fuel cell stack of the fuel cell, wherein the at least one fuel-storage module is a source of is a source of energy for the fuel cell;
fluidly connecting an air management system to an air inlet and an exhaust outlet of the fuel cell;
providing air to operate the fuel cell by an air snorkel that is part of the air management system, wherein the unmanned surface vehicle is deployed in a body of water, and wherein the air snorkel includes an air intake for receiving ambient air supplied to the fuel cell stack and an exhaust for expelling exhausted air and exhausted water-vapor created by the fuel cell stack, and wherein the power system includes the fuel storage, the fuel cell, the air management system, and the air snorkel; and
determining, by a control module in communication with a wave sensor, either to continue or terminate operation of the power system based on at least a sea state, wherein the sea state is indicated by the wave sensor.

18. The method of claim 17 , comprising providing the air snorkel with a conduit, a first air valve, and a second air valve, and the ambient air enters the conduit through the air intake, the exhausted air and exhausted water-vapor exit the conduit through the exhaust, the first air valve is fluidly connected to the air intake, and the second air valve is fluidly connected to the exhaust.

19. The method of claim 18 , comprising removing water collected within a sump by closing the first air valve and the second air valve and then activating a water pump, wherein the sump is defined by the conduit and the water pump is fluidly co

Assignees

• Boeing Co
• Liquid Robotics Inc

Inventors

• Carralero Michael A
• Wilcox Jeffrey Scott

Classifications

• H01M8/04156

  with product water removal · CPC title

• H01M8/04225

  during start-up · CPC title

• H01M8/04291

  Arrangements for managing water in solid electrolyte fuel cell systems (H01M8/04119 takes precedence) · CPC title

• H01M8/04074

  Heat exchange unit structures specially adapted for fuel cell · CPC title

• H01M8/04164

  by condensers, gas-liquid separators or filters · CPC title