Method for operating a closed Brayton engine and engine adapted for use with method

• US 5,131,231 A
• Filed: 08/02/1991
• Issued: 07/21/1992
• Est. Priority Date: 08/02/1991
• Status: Expired due to Term

• Current Assignee: Alliedsignal Inc. (Honeywell International Inc.)
• Original Assignee: Allied-Signal
• Inventors: Trimble, Steven W., Bons, Robert, Mathis, David M.
• Primary Examiner(s): Ostrager, Allen M.
• Application Number:
  US07/739,938
• Time in Patent Office: 354 Days
• Field of Search: 60/652, 60/650, 60/682, 60/649, 60/668
• US Class Current: 60/649
• CPC Class Codes: F02C 1/10 Closed cycles
• CPC Class Codes: F02C 9/24 Control of the pressure level in closed cycles

Abstract

A process for operating a closed Brayton-cycle engine (14) at two substantially differrent levels of output power by selectively changing the molecular weight of the working fluid, and an engine adapted for use with the process.

Claims

1. A process for operating a closed Brayton-cycle engine at relatively high efficiency under at least two markedly different conditions of engine output power by changing the inventory of a gaseous working fluid in a closed-cycle flow path, comprising the steps of:

first, running the engine by continuously adding heat to and extracting heat from the working fluid during a first operating condition in which the engine produces relatively low output power and the working fluid is a first gas having a first mean molecular weight;

second, effecting a running transition to a second operating condition in which the engine produces relatively high output power by;

(a) injecting into the flow path a second gas having a second mean molecular weight lower than the first mean molecular weight, whereby the working fluid becomes a mixture of the first and second gases and has a third mean molecular weight lower than the first mean molecular weight; and

(b) adding heat to the working fluid at a rate which maintains the working fluid at a substantially constant turbine inlet temperature.

2. A process as recited in claim 1 wherein the ratio of the first mean molecular weight to the third mean molecular weight is at least 5:

1.

3. A process as recited in claim 1 wherein the first gas comprises a noble gas.

4. A process as recited in claim 3 wherein the first gas comprises xenon.

5. A process as recited in claim 3 wherein the second gas comprises helium.

6. A process as recited in claim 1 wherein the second gas comprises helium.

7. A process as recited in claim 1 wherein the ratio of the first mean molecular weight to the second mean molecular weight is less than 33.0.

8. A process as recited in claim 7 wherein the ratio of the first mean molecular weight to the third mean molecular weight is at least 5:

1.

9. A process as recited in claim 8 wherein the first gas comprises xenon and the second gas comprises helium.

10. A process as recited in claim 1 wherein each of the first and second gasses comprises a noble gas.

11. A closed Brayton-cycle engine, comprising:

a compressor for a working fluid to be compressed therein so as to form a compressed working fluid,

a heat exchanger connected to be in fluid communication with said compressor for receiving and heating said compressed working fluid so as to form a hot compressed working fluid,

a turbine connected to be in fluid communication with said heat exchanger for receiving said hot compressed working fluid and providing mechanical power in response to expansion of said hot compressed fluid therethrough so as to form an expanded hot working fluid,

another heat exchanger connected to be in fluid communication with said turbine for receiving and cooling said expanded hot working fluid, and connected to be in fluid communication with said compressor so as to form a continuous-cycle flow path,

wherein said working fluid is comprised of a first gas of a first mean molecular weight, and

means operable to access said flow path for supplying thereto as a component of said working fluid a second gas of a second mean molecular weight which is less than said first mean molecular weight.

12. A closed Brayton-cycle engine as set forth in claim 11, wherein said means for suppling said second gas comprises:

a pressure vessel containing said second gas and connected so as to be operable to enable fluid communication of said second gas from said vessel to said continuous-cycle flow path.

13. A closed Brayton-cycle engine as set forth in claim 12, wherein said means for suppling said second gas further includes:

an injection valve connected between said pressure vessel and said continuous-cycle flow path so as to be operable to enable fluid communication of said second gas from said vessel to said continuous-cycle flow path.

14. A closed Brayton-cycle engine as set forth in claim 13, further including:

a second pressure vessel containing said first gas and connected so as to be operable to enable fluid communication of said first gas between said second vessel and said continuous-cycle flow path.

15. A closed Brayton-cycle engine as set forth in claim 11, wherein said first gas is a noble gas.

16. A closed Brayton cycle engine as set forth in claim 15, wherein said second gas is a noble gas.

17. A closed Brayton-cycle engine as set forth in claim 11, wherein said second gas is helium.

18. A closed Brayton-cycle engine as set forth in claim 17, wherein said first gas is xenon.

19. A closed Brayton-cycle engine as set forth in claim 11, wherein said first mean molecular weight is less than 33 times said second mean molecular weight.

20. A closed Brayton-cycle engine as set forth in claim 19, wherein said second gas is helium.