Heat-actuated space conditioning unit with bottoming cycle

• US 4,347,711 A
• Filed: 07/25/1980
• Issued: 09/07/1982
• Est. Priority Date: 07/25/1980
• Status: Expired due to Term

• Current Assignee: The Garrett Corporation
• Original Assignee: The Garrett Corporation
• Inventors: Noe, James C., Friedman, David W.
• Primary Examiner(s): Makay, Albert J.
• Assistant Examiner(s): Tanner, Harry
• Application Number:
  US06/172,127
• Time in Patent Office: 774 Days
• Field of Search: 62/467 PR, 62/467 R, 62/140, 62/209, 62/208, 62/238.4, 62/196 B, 62/196 C, 62/228 B, 62/229, 60/39.18 B, 60/39.18 R, 60/39.14 M, 60/39.29, 415/27, 415/28, 415/49
• US Class Current: 62/160
• CPC Class Codes: F01K 23/101 Regulating means specially adapted therefor F01K23/105, F01K23/108 take precedence
• CPC Class Codes: F02G 2250/03 Brayton cycles
• CPC Class Codes: F25B 13/00 Compression machines, plants or systems, with reversible cycle defrosting cycles F25B47/02
• CPC Class Codes: F25B 27/00 Machines, plants or systems, using particular sources of energy F25B30/06 takes precedence

Abstract

A heat-actuated space conditioning system comprising a sub-atmospheric natural-gas-fired Brayton cycle engine driving a Rankine cycle heat pump. A centrifugal Freon compressor is driven directly from the Brayton engine rotating group through a permanent magnet coupling. The system utilizes an in-line combustor which is operated to burn natural gas at atmospheric pressure by virtue of the associated sub-atmospheric Brayton cycle engine. Ambient stoichiometric air is drawn through an associated recuperator where it is preheated before being introduced into the combustor. Compressor discharge gas is also cycled through the recuperator and used as diluent to provide added flow and the desired turbine inlet temperature. Waste heat is used to power a boiler for the Freon in the Rankine cycle side, and this converted energy is used to drive a second turbine providing added power to the Freon compressor. A boiler feed pump is included which also serves as a starting mechanism for the rotating assembly.

Claims

1. Space conditioning apparatus comprising:

a Brayton cycle circuit including a combustor and a turbo-compressor comprising a turbine coupled to the output of the combustor for expanding combustor exhaust to sub-atmospheric levels and driving an associated compressor mounted together with the turbine on a single shaft;

a recuperator connected to the outlet of the turbine for preheating combustion air supplied to the combustor, the exhaust gas flow outlet of the recuperator being connected to the inlet of the compressor;

a Rankine cycle heat pump circuit comprising indoor and outdoor heat exchanger coils, a centrifugal compressor coupled to a compressor drive shaft for directing refrigeration fluid through the coils, and a transfer valve for selecting operation of the system in the heating or cooling mode;

means for deriving power to drive the Rankine cycle compressor from the Brayton cycle circuit including a bidirectional coupling for driving one shaft from the other shaft;

means for developing useful power from waste heat in the Brayton cycle circuit including a boiler interconnecting the Brayton cycle circuit and the Rankine cycle circuit to vaporize the refrigeration fluid from waste heat in the Brayton cycle circuit, and a second turbine coupled to the compressor shaft and connected to the boiler to be driven by the pressurized refrigeration fluid; and

means for starting the apparatus prior to firing off the combustor by pumping refrigerant fluid to the second turbine to initiate rotation of the turbo-compressor through the coupling.

2. The apparatus of claim 1 wherein the starting means comprises a boiler feed pump connected to the refrigeration cycle circuit between the indoor and outdoor coils for supplying the refrigeration fluid in liquid form to the boiler under pressure.

3. The apparatus of claim 2 wherein the second turbine includes an inlet connected to receive vaporized refrigeration fluid from the boiler and an outlet connected to the outlet of the Rankine cycle compressor.

4. The apparatus of claim 3 wherein the second turbine is mounted on a common shaft with the Rankine cycle compressor to provide auxiliary driving power to the compressor.

5. The apparatus of claim 2 wherein the starting means includes means for driving the boiler feed pump to pressurize the refrigeration fluid system and power the second turbine.

6. The apparatus of claim 5 wherein the second turbine is mounted on the compressor shaft to drive the compressor shaft and compressor.

7. The apparatus of claim 1 further including means for switching the Rankine cycle circuit between heating and cooling modes of operation, the switching means being connected at the outlet of the Rankine cycle compressor to direct compressed fluid from that compressor to the indoor coil in the heating mode and to the outdoor coil in the cooling mode.

8. The apparatus of claim 1 further comprising a surge valve connected between the inlet and outlet of the Rankine cycle compressor, and means responsive to the pressure differential across that compressor to open the surge valve upon the development of a surge condition in the compressor.

9. The apparatus of claim 7 further comprising a second valve connected between the outlet of the Rankine cycle compressor and the end of the outdoor coil which is remote from the mode switching means, and means responsive to a predetermined pressure differential in ambient air being driven across the outdoor coil for controlling the second valve to direct heated refrigeration fluid from the compressor to defrost the outdoor coil.

10. The apparatus of claim 1 wherein the Brayton cycle circuit includes means defining a flow path for exhaust gas from the combustor to the turbo-compression turbine, thence to the recuperator, and from the outlet of the recuperator through the hot side of the boiler to transfer waste heat to the Rankine cycle circuit.

11. The apparatus of claim 10 wherein the Brayton cycle circuit gas flow path further includes means directing gas flow from the boiler to the inlet of the turbo-compressor compressor for pressurization to atmospheric pressure level, thence to the recuperator for heat transfer with the exhaust from the turbine, and finally to the combustor for addition to the combusted gases therein as a diluent.

12. The apparatus of claim 11 further comprising means for exhausting a portion of the gas from the outlet of the turbo-compressor compressor so that only a part of the gas circulating in the Brayton cycle circuit is re-introduced into the combustor as diluent.

13. The apparatus of claim 11 further comprising a relief valve connected across the compressor of the turbo-compressor combination and pressure sensing means connected at the inlet of that compressor for controlling the relief valve.

14. The apparatus of claim 1 further including means for controlling flow of fuel supplied to the combustor in accordance with the temperature of the conditioned space relative to outside temperature and a selected indoor temperature setting.

15. The apparatus of claim 14 wherein the fuel controlling means includes means for sensing indoor and outdoor temperatures, comparing the sensed temperature levels relative to the selected indoor temperature setting, and modulating a gas valve for supplying gas to the combustor in accordance with the result of said comparison.

16. The method of conditioning a space by heating or cooling relative to outside ambient temperatures comprising the steps of:

coupling a rotary compressor to drive a refrigerant fluid in a Rankine cycle circuit through indoor and outdoor heat exchanging coils;

driving the compressor by means of a hermetically sealed magnetic coupling from the shaft of a turbo-compressor operated in an associated Brayton cycle circuit;

developing useful power from the waste heat of the Brayton cycle circuit by coupling the waste heat to evaporate the refrigerant fluid in the Rankine cycle circuit and direct the evaporated fluid to a second turbine; and

prior to lighting the burner of the Brayton cycle circuit, initiating the operation of the system by pumping refrigerant fluid to drive the second turbine and thereby initiate rotation of the turbo-compressor and gas flow in the Brayton cycle circuit to a point where it is safe to fire up the Brayton cycle system.

17. The method of claim 16 further including the step of coupling the second turbine directly to the shaft of the Rankine cycle compressor to provide additional shaft power.

18. The method of claim 16 further comprising the step of protecting the Rankine cycle compressor against surge conditions by detecting the onset of a surge condition and bleeding refrigeration fluid directly from the outlet to inlet of the compressor to terminate the surge condition.

19. The method of claim 16 further comprising the step of sensing the buildup of frost on the outdoor coil and bleeding fluid from the outlet of the Rankine cycle compressor to the outdoor coil to eliminate the frost.