Methods and apparatus to cool a vehicle heat source

Patent metadata

Field	Value
Publication number	US-10994857-B2
Application number	US-201815875958-A
Country	US
Kind code	B2
Filing date	Jan 19, 2018
Priority date	Jun 20, 2013
Publication date	May 4, 2021
Grant date	May 4, 2021

Abstract

Methods and apparatus to cool a vehicle heat source are disclosed herein. An example apparatus includes a first tank and a second tank. The first tank and the second tank are disposed on a vehicle. The second tank is in fluid communication with the first tank. An engine of the vehicle is to be supplied with fuel from at least one of the first tank or the second tank. The example apparatus also includes a cooling system disposed on the vehicle to cool the fuel flowing from the first tank to the second tank. The example apparatus further includes a heat exchanger operatively coupled to a heat source disposed on the vehicle. The fuel from the second tank is to flow to the first tank via the heat exchanger to cool the heat source.

First claim

What is claimed is:

1. An apparatus comprising:
a first tank disposed on a vehicle;
a second tank disposed on the vehicle, the second tank in fluid communication with the first tank, an engine of the vehicle to be supplied with fuel from at least one of the first tank or the second tank;
a cooling system disposed on the vehicle to cool fuel flowing from the first tank to the second tank;
a heat exchanger operatively coupled to a heat source disposed on the vehicle; and
a heat source management system configured to cool the heat source in response to the controller determining that an operating temperature of the heat source exceeds a heat source temperature threshold, the heat source management system including a controller configured to determine a first fuel level in the first tank and a second fuel level in the second tank, the controller configured to cause cooled fuel to flow from the second tank to the heat exchanger in response to determining that the second fuel level in the second tank exceeds a first fuel level threshold, the controller configured to cause cooled fuel to flow from the cooling system to the heat exchanger via a first bypass in response to determining that the second fuel level does not exceed the first fuel level threshold and the first fuel level of the first tank exceeds a second fuel level threshold.

2. The apparatus of claim 1 , further including a first pump and a second pump, the first pump to pump fuel from the first tank toward the second tank at a first flow rate, the second pump to pump fuel from the second tank toward the first tank at a second flow rate greater than the first flow rate.

3. The apparatus of claim 1 , wherein the heat source includes a component of a weapon system.

4. The apparatus of claim 1 , wherein the cooling system includes an evaporator.

5. The apparatus of claim 1 , further including a bypass valve disposed between the cooling system and the second tank, the bypass valve to direct cooled fuel from the cooling system into at least one of the second tank or the heat exchanger.

6. The apparatus of claim 1 , wherein the heat source management system is to cause cooled fuel from the second tank to flow to the heat exchanger when a fuel level of the second tank exceeds the second fuel level and is to cause cooled fuel to flow from the cooling system to the heat exchanger via the bypass when a fuel level of the second tank does not exceed the second fuel level.

7. The apparatus of claim 1 , wherein the heat source management system is configured to cause cooled fuel from the second tank to flow to a feed tank prior to flowing fuel in the first tank to the feed tank when the operating temperature of the heat source is less than a heat source threshold temperature.

8. An apparatus comprising:
a fuel feed system that includes a feed tank to provide fuel to an engine of an aircraft; and
a heat source management system including a first tank to store fuel at a first temperature and a second tank to store cooled fuel at a second temperature less than the first temperature, the heat source management system including a cooling system interposed in a first fuel line between the first tank and the second tank, the heat source management system to cool a heat source of the aircraft via the cooled fuel, wherein the heat source management system is configured to cool the heat source based on an operating temperature of the heat source, and wherein the heat source management system is configured to provide cooled fuel from the second tank to the feed tank prior to flowing fuel in the first tank to the feed tank in response to the operating temperature of the heat source being less than a heat source threshold temperature.

9. An apparatus comprising:
a fuel feed system that includes a feed tank to provide fuel to an engine of an aircraft; and
a heat source management system including a first tank to store fuel at a first temperature and a second tank to store cooled fuel at a second temperature less than the first temperature, the heat source management system including a cooling system interposed in a first fuel line between the first tank and the second tank, the heat source management system to cool a heat source of the aircraft via the cooled fuel, wherein the heat source management system is configured to cool the heat source based on an operating temperature of the heat source, and wherein in response to the operating temperature being greater than a heat source threshold temperature, the heat source management system is configured to cause fuel from the second tank having the second temperature to flow to a heat exchanger positioned between the second tank and the first tank to cool the heat source via a second fuel line fluidly coupling the second tank to an inlet of the heat exchanger and an outlet of the heat exchanger to the first tank.

10. The apparatus of claim 8 , wherein the heat source management system is configured to determine an operational status of the heat source, the operational status including at least one of a pre-operational mode, a standby mode, or an operational mode.

11. The apparatus of claim 10 , wherein in response to the heat source being in the pre-operational mode, the heat source management system is configured to cause fuel from the second tank to flow to the engine prior to flowing fuel in the first tank to the engine.

12. The apparatus of claim 10 , wherein in response to the operational status of the heat source being in at least one of a standby mode or an operational mode, the heat source management system is configured to cause fuel from the second tank to flow into a heat exchanger to cool the heat source disposed on the aircraft, the heat exchanger being interposed in a second fuel line that is coupled to the second tank and the first tank.

13. The apparatus of claim 8 , wherein the heat source management system is configured to substantially empty fuel in the second tank to operate the engine prior to emptying fuel in the first tank.

14. The apparatus of claim 8 , wherein the heat source management system is configured to fill a portion of the second tank with the fuel from the first tank when the second tank has an amount of fuel less than a volume threshold.

15. An apparatus comprising:
a first tank disposed on a vehicle, the first tank to hold fuel having a first temperature;
a second tank disposed on the vehicle, the second tank to hold fuel having a second temperature less than the first temperature, an engine of the vehicle to be supplied with fuel from at least one of the first tank or the second tank;
a first fuel line to fluidly couple the first tank and the second tank;
a cooling system located between the first tank and the second tank to cool fuel flowing from the first tank to the second tank, the cooling system being interposed in the first fuel line such that the first fuel line is to fluidly couple the first tank and an inlet of the cooling system and the first fuel line is to fluidly couple an outlet of the cooling system to the second tank, the cooling system to cool the fuel flowing from the first tank to a predetermined temperature prior to the fuel entering the second tank;
a second fuel line fluidly coupling to the second tank and the first tank;
a heat exchanger operatively coupled to a heat source disposed on the vehicle, fuel from the second tank to flow to the first tank via the heat exchanger to cool the heat source, the heat exchanger being interposed in the second fuel line such that the second fuel line fluidly couples the second tank to an inlet of the heat exchanger and the second fuel line fluidly c

Assignees

• Boeing Co

Inventors

• Bowman Timothy Edward
• Behrens William Webster
• Omohundro Thomas W
• Roach Jeffrey M

Classifications

• B64D37/34 Primary

  Conditioning fuel, e.g. heating (during filling B64D37/18) · CPC title

• Y02T50/40

  Weight reduction · CPC title

• B64D37/005 Primary

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

• B64D37/00

  Arrangements in connection with fuel supply for power plant (refuelling during flight B64D39/00) · CPC title