Fuel tank system and method

Patent metadata

Field	Value
Publication number	US-10307708-B2
Application number	US-201615192692-A
Country	US
Kind code	B2
Filing date	Jun 24, 2016
Priority date	Jun 24, 2016
Publication date	Jun 4, 2019
Grant date	Jun 4, 2019

Abstract

A fuel tank system is disclosed that includes a fuel tank and a first fluid flow path between a gas space in the fuel tank and outside of the fuel system. A gas separation membrane is disposed with a first side in communication with the first fluid flow path and a second side in communication with a second fluid flow path. A fluid control device is in communication with the second fluid flow path and is configured to provide fluid flow from the second fluid flow path to a liquid space in the fuel tank or to outside of the fuel system. A prime mover is disposed in communication with the second fluid flow path, and is configured to move fluid on the second fluid flow path from the second side of the separation membrane to the fuel tank liquid space or to outside of the fuel system.

First claim

The invention claimed is:

1. A fuel system, comprising:
a fuel tank including a gas space in the fuel tank and a liquid space in the fuel tank;
a first fluid flow path between the gas space in the fuel tank and outside of the fuel system;
a gas separation membrane comprising a first side in communication with the first fluid flow path and a second side, wherein the gas separation membrane has a greater permeability to water vapor and hydrocarbon vapor than to oxygen or nitrogen;
a second fluid flow path in communication with the second side of the membrane;
a fluid control device in fluid communication with the second fluid flow path, with the liquid space in the fuel tank and with outside of the fuel system, said fluid control device configured to provide fluid flow from the second fluid flow path to a destination selected from the liquid space in the fuel tank and the outside of the fuel system; and
a prime mover in communication with the second fluid flow path, configured to move fluid on the second fluid flow path from the second side of the separation membrane to the fuel tank liquid space or to outside of the fuel system.

2. The system of claim 1 , wherein the membrane comprises a first material having a greater permeability to water vapor than to oxygen or nitrogen, and a second material having a greater permeability to hydrocarbon vapor than to oxygen or nitrogen.

3. The fuel system of claim 1 , comprising a first membrane having a greater permeability to water vapor than to oxygen or nitrogen, and a second membrane having a greater permeability to hydrocarbon vapor than to oxygen or nitrogen.

4. The fuel system of claim 1 , wherein the membrane comprises a material having a greater permeability to water vapor than to oxygen or nitrogen and a greater permeability to hydrocarbon vapor than to oxygen or nitrogen.

5. The fuel system of claim 1 , wherein the fluid control device comprises a three-way valve or a combination of two-way valves.

6. The fuel system of claim 1 , wherein the fluid control device comprises a water-hydrocarbon separator comprising an inlet in communication with the second fluid flow path, a hydrocarbon outlet in communication with the liquid space in the fuel tank, and a water outlet in communication with outside of the fuel system.

7. The fuel system of claim 1 , further comprising a vapor-condensing heat exchanger disposed along the second fluid flow path.

8. The fuel system of claim 7 , wherein the fluid control device comprises a water-hydrocarbon separator comprising an inlet in communication with the second fluid flow path, a hydrocarbon outlet in communication with the liquid space in the fuel tank, and a water outlet in communication with outside of the fuel system.

9. The fuel system of claim 1 , wherein the system is configured for fluid flow from the second fluid flow path to the liquid space of the fuel tank if fluid is moving on the first fluid flow path from the fuel tank gas space to outside of the fuel system, and for fluid flow from second fluid flow path to outside of the fuel system if fluid is moving on the first fluid flow path from outside of the fuel system to the fuel tank gas space.

10. The fuel system of claim 1 , wherein the fuel system is disposed on an aircraft, and is configured for fluid flow from the second fluid flow path to the liquid space of the fuel tank during ascent, and for fluid flow from second fluid flow path to outside of the fuel system during descent.

11. The fuel system of claim 1 , wherein the fuel system is disposed on an aircraft in a wing vent box.

12. The fuel system of claim 1 , further comprising a controller configured to controllably direct fluid flow from the second fluid flow path to the liquid space of the fuel tank or to outside of the fuel system.

13. The fuel system of claim 12 , wherein the controller is configured to direct fluid flow from the second fluid flow path to the liquid space of the fuel tank if fluid is moving on the first fluid flow path from the fuel tank gas space to outside of the fuel system, and to direct fluid flow from second fluid flow path to outside of the fuel system if fluid is moving on the first fluid flow path from outside of the fuel system to the fuel tank gas space.

14. The fuel system of claim 12 , wherein the fuel system is disposed on an aircraft, and the controller is configured to direct fluid flow from the second fluid flow path to the liquid space of the fuel tank during ascent, and to direct fluid flow from second fluid flow path to outside of the fuel system during descent.

15. A method of managing fuel tank vapor, comprising
directing outgoing fuel tank vent gas from a gas space in the fuel tank to a gas separation membrane;
removing hydrocarbons from the outgoing fuel tank vapor through the membrane and directing the removed hydrocarbons to a liquid space in the fuel tank; and
directing incoming vent gas to the fuel tank past the gas separation membrane; and removing water vapor from the incoming vent gas through the membrane.

16. The method of claim 15 , further comprising condensing the removed water or hydrocarbons.

17. The method of claim 16 , further comprising separating liquid water from liquid hydrocarbons in the condensate.

18. The method of claim 15 , wherein the fuel tank is disposed on an aircraft, and the method comprises removing hydrocarbons from outgoing fuel tank vapor through the membrane and directing the removed hydrocarbons to a liquid space in the fuel tank during ascent, and removing water from incoming vent gas through the membrane during descent.

Assignees

• Hamilton Sundstrand Corp

Inventors

• Rheaume Jonathan
• Cordatos Haralambos

Classifications

• B64F1/28

  Liquid-handling installations specially adapted for fuelling stationary aircraft · CPC title

• B64D37/32

  Safety measures not otherwise provided for, e.g. preventing explosive conditions · CPC title

• B64D37/005

  Accessories not provided for in the groups B64D37/02 - B64D37/28 · CPC title

• B01D2259/4516

  for fuel vapour recovery systems · CPC title

• B01D53/22 Primary

  by diffusion (manufacturing semi-permeable membranes B01D67/00; form, structure or properties of semi-permeable membranes B01D69/00; material for semi-permeable membranes B01D71/00) · CPC title