Patent Application
20110259010
The present invention relates to the field waste heat recovery systems. More particularly, the invention relates to a waste heat recovery system employing a directly heated organic motive fluid.
Many waste heat recovery systems employ an intermediate heat transfer fluid to transfer heat from waste heat gases, such as the exhaust gases of a gas turbine, to a power producing organic Rankine cycle (ORC). One of these waste heat recovery systems is disclosed in U.S. Pat. No. 6,571,548, for which the intermediate heat transfer fluid is pressurized water. Another prior art waste heat recovery system is disclosed in U.S. Pat. No. 6,701,712, for which the intermediate heat transfer fluid is thermal oil.
The thermal efficiency of such prior art waste heat recovery systems is reduced due to the presence of the intermediate heat transfer fluid. In addition, the capital and operating costs associated with the intermediate fluid system are relatively high.
It would therefore be desirable to obviate the need of an intermediate fluid system by providing a direct heating organic Rankine cycle, i.e. one in which heat is transferred from waste heat gases to the motive fluid without any intermediate fluid circuit. However, a directly heated organic motive fluid achieves higher temperatures than one in heat exchanger relation with an intermediate fluid, and therefore suffers a risk of degradation and ignition when brought to heat exchanger relation with waste heat gases and heated thereby.
The present invention provides a waste heat recovery system based on a direct heating organic Rankine cycle.
In addition, the present invention provides a direct heating organic Rankine cycle which safely, reliably and efficiently extracts the heat content of waste heat gases to produce power.
Other advantages of the invention will become apparent as the description proceeds.
The present invention provides a waste heat recovery system, comprising a closed fluid circuit through which an organic motive fluid flows, heat exchanger means for transferring heat from waste heat gases to said motive fluid, means for flashing the motive fluid which exits said heat exchanger means into a high pressure flashed vapor portion, means for flashing liquid non-flashed motive fluid producing a low pressure flashed vapor portion, a high pressure turbine module which receives said high pressure flashed vapor portion to produce power, and a low pressure turbine module which receives a combined flow of motive fluid vapor comprising said low pressure flashed vapor portion and discharge vapor from said high pressure turbine module whereby additional power is produced.
The flashing means preferably comprises a high pressure flash chamber for receiving the motive fluid exiting the heat exchanger means and producing the high pressure flashed portion, and, in addition, a low pressure flash chamber receives a non-flashed discharge from said high pressure flash chamber and produces the low pressure flashed portion.
The system preferably further comprises a direct contact recuperator, a condenser for condensing a discharge from the low pressure turbine module, and a condensate pump for delivering at least a portion of the motive fluid condensate to said direct contact recuperator for mixing with the high pressure turbine module vapor discharge, a mixed flow exiting from said direct contact recuperator combining with the low pressure flashed portion to produced the combined flow introduced to the low pressure turbine module.
According to another aspect of the present invention, the system further comprises a second recuperator for heating a second portion of the motive fluid condensate using the low pressure turbine module discharge.
In accordance with a further aspect of the present invention, the system further comprises a preheater for preheating condensate from the second recuperator using non-flashed discharge from the low pressure flash chamber.
According to an additional aspect of the present invention, heat depleted low pressure flash chamber discharge is combined with condensate from the second recuperator.
In accordance to a still further aspect the present invention, the system further comprises a feed pump for delivering the condensate to the heat exchanger means at a sufficiently high pressure so that the condensate will be retained in a liquid phase.
According to an still additional aspect of the present invention, the system further comprises a first control valve in communication with a fluid line extending from the high pressure flash chamber to the high pressure turbine module, a second control valve in communication with a fluid line extending from the low pressure flash chamber and the low pressure turbine module, and a third control valve in communication with a fluid line extending from the condensate pump to the direct contact recuperator.
Moreover, in accordance to a still further aspect the present invention, the system further comprises a first safety valve in communication with a fluid line extending from the heat exchanger means and the high pressure flash chamber, and a second safety valve in communication with a fluid line upstream to the heat exchanger means.
In accordance to a still additional aspect the present invention, the system further comprises a controller for controlling operation of the condensate pump, first control valve, second control valve, third control valve, first safety valve and second safety valve in accordance with sensed operating conditions.
According to an even additional aspect of the present invention, the high pressure and low pressure turbine modules can be separate turbine modules which can be coupled to a common generator.
Moreover, in accordance to a still further aspect the present invention, the high pressure and low pressure turbine modules are first and second stages, respectively, of a common turbine coupled to a generator.
In the drawings:
The present invention is a flash chamber based waste heat recovery system. A heated organic motive fluid, e.g. butane, such as n-butane or isobutane, pentane e.g. n-pentane or isopentane, or hexane, e.g. n-hexane or isohexane is introduced into a flash chamber system as a heated motive fluid liquid supplied from a waste heat heat exchanger and is separated into high and low pressure portions. Other organic motive fluids such as alkalyted substituted aromatic fluids, dodecane, isododecane, etc. can also be used in the present invention. The high pressure portion is delivered to a high pressure turbine module and is expanded therein, thereby producing power. The discharge from the high pressure turbine module is combined with a low pressure portion, and is delivered to a low pressure turbine module. Thus, the waste heat recovery system of the present invention is able to realize an increased level of power while advantageously ensuring the use of liquid motive fluid in the waste heat heat exchanger thereby preventing a risk of degradation of the motive fluid.
The heated motive fluid exiting heat exchanger 20 is introduced via line 29 to high pressure flash chamber 30, in which its pressure is quickly reduced to produce motive fluid vapor. The motive fluid vapor produced flows through line 32 with which control valve 35 is in communication and is delivered to high pressure turbine module 5 wherein the vapor expands to produce power. The liquid motive fluid which is not flashed exits high pressure flash chamber 30 via line 38 to low pressure flash chamber 40 in which low pressure motive fluid vapor is produced. The low pressure motive fluid vapor produced flows through line 42 with which control valve 45 is in communication and is supplied to low pressure turbine module 15 wherein the vapor expands to produce power. The liquid motive fluid which is not vaporized exits low pressure flash chamber 40 via line 41 and is supplied to preheater 54, in order to transfer heat to condensate.
In the illustrated embodiment, high pressure turbine module 5 and low pressure turbine module 15 are two separate turbine modules which can be both coupled to a common generator 9, by which electricity is produced. Alternatively, a single two-stage turbine having a high pressure stage and a low pressure stage which is coupled to generator 9 can be used. The turbines may be configured with large shafts about which each turbine component is independently rotatable and with correspondingly large bearings on which the shafts are rotatably mounted. By employing such a cost effective turbine configuration of relatively large dimensions, the rotational speed of the turbines can be lowered. Thus, the rotational speed of the turbines can be synchronized with that of generator 9, to a relatively low speed of e.g. 1500-1800 rpm, thereby enabling the use of a relatively inexpensive generator.
The motive fluid discharged from low pressure turbine module 15 is delivered via line 16 to condenser 17. Cycle pump 19 can deliver a first portion of the condensate to direct contact recuperator 14 via line 24 and control valve 23 in communication therewith, and a second portion of the condensate to recuperator 44 via line 43. Recuperator 14 can receive expanded motive fluid vapor discharged from high pressure turbine module 5 via line 12, and the first portion of the condensate flowing through line 24 can be mixed with the high pressure turbine module vapor discharge to increase the mass flow rate of motive fluid introduced to low pressure turbine module 15 and thereby the power output of turbine module 15. In addition, motive fluid introduced to low pressure turbine module 15 further includes motive fluid vapor discharged from low pressure flash chamber 40 via line 42. The motive fluid vapor discharged from low pressure flash chamber 40 can be combined with the discharge from recuperator 14 at junction 52 before being delivered to turbine module 15.
Advantageously, the discharge from turbine module 15 can be supplied to recuperator 44 via line 56, in order to heat the second condensate portion supplied thereto by line 43. Heat depleted turbine discharge exiting recuperator 44 is delivered via line 16 to condenser 17.
The heated motive fluid condensate exiting recuperator 44 is combined at junction 61 with the heat depleted liquid discharge from low pressure flash chamber 40 which flows to junction 46 via line 55, and the combined flow flows to the suction side of pump 48. Pump 48 delivers the combined flow to preheater 54 via line 57, and the combined flow is heated by the liquid discharge from low pressure flash chamber 40. Cycle pump 19 together with pump 48 are adapted and controlled to ensure that the preheated condensate flowing to heat exchanger 20 via line 58 is in a liquid phase. Safety valves 66 and 67 are deployed upstream and downstream, respectively, of heat exchanger 20, to ensure that a sufficiently high flow rate of liquid motive fluid is supplied thereto and thereby, in addition, prevent a risk of degradation of the motive fluid.
Waste heat recovery system 10 is also provided with controller 60, for controlling the operation of cycle pump 19, condensate pump 48, control valves 23, 35 and 45, and of safety valves 66 and 67. The dashed lines represent the connections of the control system.
The control system is adapted to activate/deactivate and control the operation of cycle pump 19 as well as condensate pump 48 and to actuate safety valves 66 and 67 to ensure sufficient flow rate of liquid motive fluid flows in waste heat heat exchanger 20 as well as in lines 29 or 58. Control valves 35 and 45 are regulated by controller 60 in order to deliver a desired pressure level of motive fluid vapor to turbine modules 5 and 15, respectively. Control valve 23 is regulated so that an optimal flow rate of motive fluid condensate can be supplied to direct contact recuperator 14, in order that, on one hand, a sufficiently high flow rate of motive fluid vapor will be delivered to low pressure turbine module 15 for the production of power thereby, as well as ensuring that the condensate flow rate supplied by control valve 23 will be such that the motive fluid vapor supplied to low pressure turbine module 15 will have a certain level of superheat to ensure effective power production by low pressure turbine module 15. In such a manner, the blades of low pressure turbine module 15 are not liable to become corroded since the temperature entropygraph of organic fluid is skewed. That is, the critical point on an entropy-temperature diagram delimiting the interface between saturated and superheated regions is to the right of the centerline of an isothermal boiling step and of the centerline of an isothermal condensing step. Accordingly, expansion of vapor within low pressure turbine module 15 will cause the organic motive fluid to become superheated.
While some embodiments of the invention have been described by way of illustration, it will be apparent that the invention can be carried out with many modifications, variations and adaptations, and with the use of numerous equivalents or alternative solutions that are within the scope of persons skilled in the art, without departing from the spirit of the invention or exceeding the scope of the claims.
