Catalyst decay monitoring of catalytic inerting system

Patent metadata

Field	Value
Publication number	US-10858119-B2
Application number	US-201815945292-A
Country	US
Kind code	B2
Filing date	Apr 4, 2018
Priority date	Apr 4, 2018
Publication date	Dec 8, 2020
Grant date	Dec 8, 2020

Abstract

A fuel tank inerting system includes a primary catalytic reactor comprising an inlet, an outlet, a reactive flow path between the inlet and the outlet, and a catalyst on the reactive flow path. The catalytic reactor is arranged to receive fuel from the fuel tank and air from an air source that are mixed to form a combined flow, and to react the combined flow along the reactive flow path to generate an inert gas. The system also includes an input sensor that measures a property of the combined flow before it enters the primary catalytic reactor and an output sensor that measures the property of the combined flow after it exits the primary catalytic reactor.

First claim

What is claimed is:

1. A fuel tank inerting system, comprising:
a primary catalytic reactor comprising an inlet, an outlet, a reactive flow path between the inlet and the outlet, and a catalyst on the reactive flow path, said primary catalytic reactor arranged to receive fuel from a fuel tank and air from an air source that are mixed to form a combined flow, and to react the combined flow along the reactive flow path to generate an inert gas;
a secondary catalytic reactor coupled in parallel with the primary catalytic reactor, the secondary catalytic reactor having an inlet and an outlet, said secondary catalytic reactor arranged to receive the combined flow;
an input sensor that measures a property of the combined flow before it enters the secondary catalytic reactor;
an output sensor that measures the property of the combined flow after it exits the secondary catalytic reactor; and
a computing device that receives the sensor data from the input and output sensors;
wherein the computing device determines a fuel quality of fuel used by the system based on the sensor data.

2. The system of claim 1 , wherein the computing device determines catalyst activity in the secondary catalytic reactor based on the sensor data for use in making an aircraft operation decision.

3. The system of claim 2 , wherein the aircraft operation decision is related to the maintenance of the primary catalytic reactor or the catalyst in the primary catalytic reactor.

4. The system of claim 1 , wherein the determination of fuel quality is made by comparison of the sensor data to predicted sensor data.

5. The system of claim 4 , wherein the predicted sensor data is based on a mathematical model.

6. The system of claim 5 , wherein the model is a model of catalytic activity for a catalyst in the secondary catalytic reactor versus time.

7. The system of claim 6 , wherein the catalyst in the secondary catalytic reactor is the same as the catalyst on the reactive flow path.

8. The system of claim 2 , wherein the aircraft operation decision is a refueling fuel choice based on the fuel quality.

9. The system of claim 2 , wherein the aircraft operation decision is a flight routing decision based on the fuel quality.

10. A fuel tank inerting system, comprising
a primary catalytic reactor comprising an inlet, an outlet, a reactive flow path between the inlet and the outlet, and a catalyst on the reactive flow path, said primary catalytic reactor arranged to receive fuel from a fuel tank and air from an air source that are mixed to form a combined flow, and to react the combined flow along the reactive flow path to generate an inert gas;
an input sensor that measures a property of the combined flow before it enters the primary catalytic reactor;
an output sensor that measures the property of the combined flow after it exits the primary catalytic reactor; and
a computing device that receives sensor data from the input and output sensors;
wherein the computing device determines a fuel quality of fuel used by the system based on the sensor data.

11. The system of claim 10 ,
wherein the computing device determines catalyst activity in the primary catalytic reactor based on the sensor data for use in making an aircraft operation decision.

12. The system of claim 11 , wherein the aircraft operation decision is related to the maintenance of the primary catalytic reactor or the catalyst in the primary catalytic reactor.

13. The system of claim 10 , wherein the determination of the fuel quality is made by comparison of the sensor data to predicted sensor data.

14. The system of claim 13 , wherein the predicted sensor data is based on a mathematical model.

15. The system of claim 14 , wherein the model is a model of catalytic activity for the catalyst in the primary catalytic reactor versus time.

16. The system of claim 11 , wherein the aircraft operation decision is a refueling fuel choice based on the fuel quality.

17. The system of claim 11 , wherein the aircraft operation decision is a flight routing decision based on the fuel quality.

Assignees

• Hamilton Sundstrand Corp

Inventors

• Emerson Sean C
• Dardas Zissis A
• Mcgee Randolph Carlton
• Surawski Eric

Classifications

• B01D53/265

  by refrigeration (condensation) · CPC title

• A62C3/08

  in aircraft {(A62C3/0207 takes precedence)} · CPC title

• B01J19/2445

  placed in parallel · CPC title

• B64D37/32 Primary

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

• B01J2219/24

  Stationary reactors without moving elements inside · CPC title