Classifications

• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
  • F01C—ROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
  • F01C1/00—Rotary-piston machines or engines
  • F01C1/30—Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members
  • F01C1/34—Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in group F01C1/08 or F01C1/22 and relative reciprocation between the co-operating members
  • F01C1/344—Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in group F01C1/08 or F01C1/22 and relative reciprocation between the co-operating members with vanes reciprocating with respect to the inner member
  • F01C1/3441—Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in group F01C1/08 or F01C1/22 and relative reciprocation between the co-operating members with vanes reciprocating with respect to the inner member the inner and outer member being in contact along one line or continuous surface substantially parallel to the axis of rotation
  • F01C1/3442—Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in group F01C1/08 or F01C1/22 and relative reciprocation between the co-operating members with vanes reciprocating with respect to the inner member the inner and outer member being in contact along one line or continuous surface substantially parallel to the axis of rotation the surfaces of the inner and outer member, forming the working space, being surfaces of revolution
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
  • F01C—ROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
  • F01C1/00—Rotary-piston machines or engines
  • F01C1/30—Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members
  • F01C1/34—Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in group F01C1/08 or F01C1/22 and relative reciprocation between the co-operating members
  • F01C1/344—Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in group F01C1/08 or F01C1/22 and relative reciprocation between the co-operating members with vanes reciprocating with respect to the inner member
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
  • F01C—ROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
  • F01C11/00—Combinations of two or more machines or engines, each being of rotary-piston or oscillating-piston type
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
  • F01C—ROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
  • F01C11/00—Combinations of two or more machines or engines, each being of rotary-piston or oscillating-piston type
  • F01C11/002—Combinations of two or more machines or engines, each being of rotary-piston or oscillating-piston type of similar working principle
  • F01C11/004—Combinations of two or more machines or engines, each being of rotary-piston or oscillating-piston type of similar working principle and of complementary function, e.g. internal combustion engine with supercharger
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
  • F01C—ROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
  • F01C11/00—Combinations of two or more machines or engines, each being of rotary-piston or oscillating-piston type
  • F01C11/006—Combinations of two or more machines or engines, each being of rotary-piston or oscillating-piston type of dissimilar working principle
  • F01C11/008—Combinations of two or more machines or engines, each being of rotary-piston or oscillating-piston type of dissimilar working principle and of complementary function, e.g. internal combustion engine with supercharger
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
  • F01C—ROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
  • F01C21/00—Component parts, details or accessories not provided for in groups F01C1/00 - F01C20/00
  • F01C21/06—Heating; Cooling; Heat insulation
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
  • F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
  • F04C23/00—Combinations of two or more pumps, each being of rotary-piston or oscillating-piston type, specially adapted for elastic fluids; Pumping installations specially adapted for elastic fluids; Multi-stage pumps specially adapted for elastic fluids
  • F04C23/02—Pumps characterised by combination with, or adaptation to, specific driving engines or motors
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
  • F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
  • F04C29/00—Component parts, details or accessories of pumps or pumping installations, not provided for in groups F04C18/00 - F04C28/00
  • F04C29/0007—Injection of a fluid in the working chamber for sealing, cooling and lubricating
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
  • F25B—REFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
  • F25B11/00—Compression machines, plants or systems, using turbines, e.g. gas turbines
  • F25B11/02—Compression machines, plants or systems, using turbines, e.g. gas turbines as expanders

Definitions

• the present invention relates to a vane expander and an energy recovery circuit using such an expander.
• Vane expanders comprising a stator provided with an inlet port and an outlet port, and a rotor eccentrically housed in the stator, internally tangent to a side wall of the stator and provided with a plurality of vanes sliding radially relative to the rotor and cooperating in a sealed manner with the stator.
• the stator and rotor delimit between them a circumferential chamber with width varying from zero in the tangency area to a maximum value near one end of the outlet port; the vanes divide the chamber into a plurality of compartments with volume varying with the rotation of the rotor, each of which has a minimum volume at the inlet port and a maximum volume near the beginning of the outlet port.
• the operating fluid entering a compartment communicating with the inlet port is thus expanded and discharged at the outlet port; the expansion makes mechanical energy available at an outlet shaft rotationally connected to the rotor .
• vane volumetric expanders in energy recovery systems (e.g. based on a Rankine cycle using a high molecular weight organic operating fluid, known as ORC) from waste heat sources in the industrial, automotive or civil sectors, etc.
• ORC high molecular weight organic operating fluid
• Volumetric vane expanders offer important advantages in terms of efficiency and power produced compared to other available technologies especially when the enthalpic content of thermal sources is very low, for example when the temperature of the thermal source is between 80° and 120 °C .
• vane volumetric expanders compared to other technologies available for energy recovery systems are the low-rotation speed operating capacity, automatic starting without the need to be driven by an electric motor, reduced noise emission, low vibration, and a structure based on simple components and absence of flow control valves.
• Known vane volumetric expanders are usually sized and optimized to operate in a predetermined range of operating conditions, and have a limited capacity to adapt to any variations in the thermal load imposed by the hot source.
• an excess of thermal power made available by the hot source causes an increase in the flow rate of operating fluid circulating in the ORC system which must therefore be disposed of by the expander.
• the excess flow rate can be managed in three ways:
• the increase in rotation speed results in two negative effects: it reduces the filling time of the compartments and therefore negatively affects volumetric efficiency; it increases the friction losses that vary with the square of the expander speed and therefore determines a reduction in the mechanical efficiency of the machine.
• the purpose of the present invention is to provide a vane expander which overcomes the drawbacks described above .
• a vane expander comprising a stator provided with an inlet port and an outlet port for an operating fluid, a rotor housed in the stator and provided with a body internally tangent to a side wall of the stator and a plurality of vanes sliding in respective seats made in the body of the rotor and pushed in a centrifugal direction to cooperate in a sealed manner with the side wall of the stator, the stator and the body of the rotor delimiting between one another a circumferential chamber with varying radial width communicating with the inlet port and the outlet port and divided by the vanes into a plurality of compartments; the expander comprising at least one supplementary inlet for the supplementary introduction of operating fluid in the vapour state into an expansion portion of the chamber isolated from the inlet port and the outlet port.
• the present invention also relates to an energy recovery circuit using such expander.
• the supplementary introduction of operating fluid may be made via one or more axial or radial holes communicating with a closed compartment of the expander.
• the expander is used in an ORC circuit and the operating fluid can be tapped downstream of the evaporator by means of an on-off control valve; in this way, by appropriately calibrating the diameter of the additional operating fluid inlet hole(s), the inlet flow rate is determined by the difference between the filling pressure of a compartment and the pressure in the compartment during expansion, at the time of introduction of the supplementary flow rate.
• the flow rate of liquid injected into the expander is less than 50% of the total flow rate processed by the circulation pump of the circuit.
• Figure 1 is a cross-section of a first embodiment of a vane expander according to the invention
• Figure 2 is a cross-section of a second embodiment of a vane expander according to the invention.
• Figure 3 is a diagram of a first embodiment of an energy recovery circuit according to the present invention.
• Figure 4 is a diagram of a second embodiment of an energy recovery circuit according to the present invention.
• Figure 5 is a graph showing the pressure in the expander compartments as a function of the rotation angle of the rotor, with the varying of the supplementary flow rate .
• reference numeral 1 globally denotes a vane expander comprising a stator 2 and a rotor 3 eccentrically housed rotationally free inside the stator 2 and provided with at least one output shaft not shown .
• the stator 2 comprises a substantially hollow cylindrical stator barrel 4 and a pair of axial closing heads 5, of which only one is visible in Figure 1.
• the stator barrel 4 has an inner cylindrical surface 6 of axis
• the rotor 3 comprises a cylindrical body 7 of axis B tangent to the inner surface 6 of the stator barrel 4 and a plurality of vanes 9 sliding in respective radial seats 10 of the body 7.
• the vanes 9 are pushed in a centrifugal direction, e.g., by means of springs or ejection and motion control rings, fluid pressure or a combination thereof, to cooperate in a sealed manner with the inner surface 6 of the stator barrel 4.
• the stator barrel 4 and the body 7 of the rotor 3 delimit between them a circumferential chamber 14 of radial width varying from a substantially null value at the tangent generatrix T to a maximum value at a diametrically opposite generatrix S.
• the chamber 14 is divided by the vanes 9 into a plurality of compartments 15.
• the chamber 14 communicates with an inlet port 16 and an outlet port 17 for an operating fluid made in the stator
• the inlet port 16 is placed at one end of the chamber 9 near the tangent zone between the body 7 of the rotor 3 and the stator barrel 4, the outlet port extends from the area of maximum width of the chamber 14 to an opposite end of said chamber, near the tangent zone.
• the chamber 14 therefore has an expansion zone (with increasing radial width) and an outlet zone (with decreasing radial width) ; depending on the number of vanes 9, in the example shown seven, a certain number of compartments 15 are located in the expansion zone and a certain number of compartments are located in the outlet zone .
• the expander comprises a supplementary injection system of operating fluid in the liquid state into an expansion portion 18 of the chamber isolated from the inlet port and the outlet port .
• This portion 18, indicated by a lined section in Figure 1, is angularly distant from each of the inlet 16 and outlet ports 17 by an angle equal to the angular width of a compartment 15, and therefore extends along an angle equal to the angular distance between the inlet port 16 and the outlet port 17 minus twice the angular width of a compartment 15.
• the rotor 3 is shown by a solid line in a first position where a first compartment 15 of the expansion zone begins to be isolated from the inlet port 16 by a vane 9.
• the vanes 9 are also illustrated (lined) in a second position in which a last compartment 15 of the expansion zone is in an incipient outlet position, i.e. a position in which a vane 9 still isolates such compartment
• the injection of operating fluid in the vapour state occurs through a calibrated radial hole 20 made in the stator barrel 4, and provided with a threaded fitting 21 for connection to a supply pipe.
• the fitting 21 is arranged in an initial area of the portion 18.
• the injection takes place via a pair of axial holes 22 arranged one after the other in a circumferential direction and made in one of the heads 5.
• FIG 3 illustrates a simple (non-recovery) type ORC energy recovery circuit 25.
• the thermal source the residual energy of which is to be recovered is the lubricating oil of a compressor C.
• the circuit 25 uses an organic operating fluid, conveniently consisting of a hydrofluorocarbide (HFC) or a hydrofluoroolefin (HFO) to which a compatible lubricant is added, e.g. a polyester-based oil (POE), e.g. in a 5% by mass percentage.
• HFC hydrofluorocarbide
• HFO hydrofluoroolefin
• POE polyester-based oil
• the ORC circuit comprises, in a known manner:
• HTHX high-temperature heat exchanger
• evaporator a first high-temperature heat exchanger HTHX, or evaporator, wherein the operating fluid exchanges heat with the fluid the thermal energy of which is to be recovered, in the example illustrated the lubricating oil of the compressor, and passes to the vapour state;
• LTHX low-temperature heat exchanger
• condenser a second low-temperature heat exchanger LTHX, or condenser, wherein the operating fluid exchanges heat with a coolant fluid, conveniently water, for cooling and condensing the operating fluid.
• the operating fluid in the liquid state is tapped downstream of the HTHX evaporator and is injected into the expander 1 as described above.
• a duct 26 connects a node 27 of the circuit downstream of the HTHX evaporator to the fitting 21 or holes 22.
• the supplementary flow rate that is introduced during the expansion phase is controlled by a valve 28 located on the duct 26.
• the valve 28 is of the on-off type.
• the fluid flow rate through the duct 26 is determined, once the diameter of the inlet holes 20 or 22 is fixed, by the pressure difference between the node 27 (which coincides with the filling pressure of the compartments 15) and the pressure in the compartments 15 in the portion of the expansion phase in which the introduction occurs.
• the circuit in Figure 4, denoted by reference numeral 29, differs from that of Figure 3 described in that it is a recovery circuit, in which that is, the operating fluid in output from the pump P is subjected to a heat exchange with the vapour at the outlet of the expander 1 in a heat exchanger RHX.
• the tapping and supplementary introduction of operating fluid are made in a similar manner to that described above.
• Figure 5 is a graph showing the pressure trend in a compartment 15 as a function of the rotation angle of the rotor, as the flow rate of the supplementary operating fluid introduced varies.
• Curve A refers to a comparative example, relative to a vane expander without a supplementary injection of operating fluid, supplied at the nominal flow rate.
• Curves B, C and D refer to three embodiments of the invention in which, with the same machine and nominal flow rate, a supplementary flow rate of 20%, 30% and 50% of the nominal flow rate respectively is introduced.
• the first part of the expansion remains unchanged and takes place in compliance with the nominal design conditions of the machine, while the second part of the expansion is characterized by thermo-fluidodynamic conditions favourable to the development of greater power, which can be obtained at the same size and speed of rotation of the machine.
• Table 1 below shows the mechanical power, volumetric efficiency and percentage power increase values as a function of the percentage of supplementary flow rate, 5 under the same conditions as the graph in Figure 5.

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• Engineering & Computer Science (AREA)
• Mechanical Engineering (AREA)
• General Engineering & Computer Science (AREA)
• Chemical & Material Sciences (AREA)
• Combustion & Propulsion (AREA)
• Physics & Mathematics (AREA)
• Thermal Sciences (AREA)
• Control Of Turbines (AREA)
• Applications Or Details Of Rotary Compressors (AREA)

Applications Claiming Priority (2)

Publications (2)

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• 2018
  • 2018-12-28 WO PCT/IB2018/060703 patent/WO2019130268A1/en unknown
  • 2018-12-28 EP EP18839733.5A patent/EP3732351B1/de active Active

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