Heat exchanger

Patent metadata

Field	Value
Publication number	US-11085713-B2
Application number	US-201816030917-A
Country	US
Kind code	B2
Filing date	Jul 10, 2018
Priority date	Jul 10, 2017
Publication date	Aug 10, 2021
Grant date	Aug 10, 2021

Abstract

There is provided a fuel tank inerting system for an aircraft. The system comprises: a catalytic heat exchanger comprising a first flow path and a second flow path for heat exchange with the first flow path, wherein the first flow path comprises a plurality of core flow paths each fluidly isolated from one another within the catalytic heat exchanger and each arranged to exchange heat with the second flow path; and a control valve arranged upstream of the first flow path of the catalytic heat exchanger and arranged to selectively control a flow to each of the core flow paths.

First claim

The invention claimed is:

1. A fuel tank inerting system for an aircraft, the system comprising:
a catalytic heat exchanger arranged upstream of a fuel tank to generate an inert environment in an ullage of the fuel tank, the catalytic heat exchanger comprising a first flow path and a second flow path for heat exchange with the first flow path, wherein the first flow path comprises a plurality of core flow paths each containing a catalyst and fluidly isolated from one another within the catalytic heat exchanger and each arranged to exchange heat with the second flow path; and
a control valve arranged upstream of the first flow path of the catalytic heat exchanger and arranged to selectively control a flow to each of the core flow paths;
wherein the plurality of core flow paths are arranged in parallel through the catalytic heat exchanger;
wherein the catalytic heat exchanger comprises a plurality of distinct cores and each core defines one of the plurality of core flow paths of the first flow path;
wherein each of the plurality of distinct cores has a different cooling capacity; and
wherein a second core of the plurality of cores has twice the cooling capacity of a first core of the plurality of cores.

2. A system as claimed in claim 1 , wherein the second flow path first encounters the core with the greatest capacity.

3. A system as claimed in claim 1 , wherein the second flow path encounters each core flow path sequentially.

4. A system as claimed in claim 1 , wherein the control valve is an electromechanical servo valve.

5. A method of controlling a catalytic heat exchanger of a fuel inerting system, the catalytic heat exchanger arranged upstream of a fuel tank to generate an inert environment in an ullage of the fuel tank, the catalytic heat exchanger comprising a first flow path and a second flow path for heat exchange with the first flow path, wherein the first flow path comprises a plurality of core flow paths each containing a catalyst and fluidly isolated from one another within the catalytic heat exchanger and each arranged to exchange heat with the second flow path;
the method comprising using a control valve to control flow to the each of the core flow paths to change capacity of the catalytic heat exchanger;
wherein the plurality of core flow paths are arranged in parallel through the catalytic heat exchanger;
wherein the catalytic heat exchanger comprises a plurality of distinct cores and each core defines one of the plurality of core flow paths of the first flow path;
wherein each of the plurality of distinct cores has a different cooling capacity; and
wherein a second core of the plurality of cores has twice the cooling capacity of a first core of the plurality of cores.

6. A method as claimed in claim 5 , comprising preventing flow to a core flow path to reduce heat exchanger capacity.

7. A method as claimed in claim 5 , comprising starting flow to a core flow path to increase heat exchanger capacity.

8. A method as claimed in claim 5 , comprising preventing flow to a core flow path in response to a reduced demand for inert gas.

9. A method as claimed in claim 5 , comprising starting flow to a core flow path in response to an increased demand for inert gas.

10. A method as claimed in claim 5 , wherein the system includes a control valve arranged upstream of the first flow path of the catalytic heat exchanger, wherein controlling flow to the each of the core flow paths to change capacity of the catalytic heat exchanger includes operating the control valve.

Assignees

• Hs Marston Aerospace Ltd

Inventors

• Phillips Paul
• Pollard Berwyn

Classifications

• B64D37/32

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

• F28D2021/0021

  for aircrafts or cosmonautics · CPC title

• F28F27/02 Primary

  for controlling the distribution of heat-exchange media between different channels ({static flow control means in header boxes F28F9/026}; arrangements of guide plates or guide vanes F28F9/22, F28F25/12) · CPC title

• F28D9/0093

  Multi-circuit heat-exchangers, e.g. integrating different heat exchange sections in the same unit or heat-exchangers for more than two fluids · CPC title