Classifications

• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
  • F02C1/00—Gas-turbine plants characterised by the use of hot gases or unheated pressurised gases, as the working fluid
  • F02C1/04—Gas-turbine plants characterised by the use of hot gases or unheated pressurised gases, as the working fluid the working fluid being heated indirectly
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
  • F01K—STEAM ENGINE PLANTS; STEAM ACCUMULATORS; ENGINE PLANTS NOT OTHERWISE PROVIDED FOR; ENGINES USING SPECIAL WORKING FLUIDS OR CYCLES
  • F01K27/00—Plants for converting heat or fluid energy into mechanical energy, not otherwise provided for
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
  • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
  • F02C7/08—Heating air supply before combustion, e.g. by exhaust gases
  • F02C7/10—Heating air supply before combustion, e.g. by exhaust gases by means of regenerative heat-exchangers
  • F02C7/105—Heating air supply before combustion, e.g. by exhaust gases by means of regenerative heat-exchangers of the rotary type
• • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
  • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
  • Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
  • Y02E20/00—Combustion technologies with mitigation potential
  • Y02E20/14—Combined heat and power generation [CHP]

Definitions

• Power generation system especially electric, with a gas turbine and a rotary regenerative heat exchanger.
• the present invention relates to a system for producing energy, in particular electrical energy, comprising a gas turbine with a compressor, an expansion turbine and a device for heating the compressed gases leaving the compressor to send them to the relaxation turbine.
• the production of electrical energy generally results from a generator which is coupled to the expansion turbine of this gas turbine.
• the hot gas source used for this power generation system can come from high temperature heat recovery on an industrial process, such as a furnace, or from a combustion of a solid fuel, such as biomass, in a burner type combustion chamber device.
• the present invention proposes to overcome the drawbacks mentioned above by means of an electrical energy production system which makes it possible to obtain a high energy efficiency by using a high performance heat exchanger which can increase the heating temperatures of the compressed gases. .
• the present invention relates to a system for producing energy, in particular electrical power, comprising a gas turbine with at least one compressor with at least one compression stage, at least one expansion turbine, a heat exchanger between said compressor and said expansion turbine, and a source of hot gases, characterized in that the exchanger is a rotary regenerative heat exchanger traversed by the hot gases from said source and by compressed gases from said compressor.
• the rotary regenerative exchanger may comprise a disk with a multiplicity of radial sectors traversed alternately by said hot gases and by said compressed gases.
• the regenerative heat exchanger may comprise compressed gas inlet and hot gas inlet boxes and compressed gas and hot gas outlet boxes.
• the electric power generation system may comprise a hot fluid generator traversed by the hot gases leaving the exchanger.
• the electric power generation system may include a hot fluid generator placed between the compressor and the heat exchanger.
• the compressor may comprise at least two compression stages and a hot fluid generator may be disposed between the two stages.
• the source of hot gases may comprise a combustion chamber.
• the combustion chamber may comprise at least one air inlet from the expansion turbine.
• the combustion chamber may include at least one fresh air inlet.
• the fresh air inlet can be connected by a line to the expansion turbine and this line can pass through a cooling radiator.
• the combustion chamber may include an intake of a solid fuel.
• the fuel may comprise biomass.
• the source of hot gases can come from a high temperature heat recovery on an industrial process
• the heat exchanger is a rotary regenerative heat exchanger of sequential type.
• FIG. 1 is a diagram illustrating the system electric power generation apparatus according to the invention
• FIG. 2 is a detailed perspective view of the heat exchanger used in the system according to the invention.
• FIG. 3 is a diagram of a first variant of the system of FIG. 1;
• FIG. 4 is a diagram illustrating another variant of the system of FIG.
• FIG. 5 is a diagram illustrating another variant of the system of FIG. 4.
• the energy production system comprises a gas turbine 10 with a gas compressor 12 with at least one compression stage, a regenerative type heat exchanger 14, the description of which will be more detailed in the following. the description, an expansion turbine 16 connected by a shaft 18 to the compressor, and a means for producing electrical energy 20 controlled by the expansion turbine.
• this means of producing electrical energy comprises an electric generator 22 connected by a shaft 24 to the expansion turbine 16.
• the compressor comprises a gas inlet, here external air 26, connected to an air inlet line 28 and a compressed air outlet 30 connected by a line 32 to a compressed air inlet 34 of the exchanger 14.
• the air outlet compressed 36 of this exchanger is connected by a line 38 to the inlet 40 of the expansion turbine 16.
• the outlet 42 of this turbine is connected to a line 44 which allows the hot exhaust gases to be evacuated to any suitable means.
• the exchanger 14 comprises an inlet 46 for hot gases, such as that which may come from a heat recovery at high temperature on an industrial process or from a combustion of a solid fuel, and which is connected by a line 48 to the source of these hot gases. After having traversed this exchanger, the hot gases are evacuated through an outlet 50 and a line 52 to all means of evacuation and treatment, such as a chimney (not shown).
• hot gases such as that which may come from a heat recovery at high temperature on an industrial process or from a combustion of a solid fuel
• FIG. 2 shows an exemplary embodiment of the regenerative heat exchanger which is based on the principle of Lugjstrom type rotary exchangers, as described by way of example in US 1,522,825.
• This exchanger comprises a rotating heat exchange disc 54 rotated about its axis XX for all known means, such as an electric motor (not shown), in a continuous or sequential movement.
• This disk is shared by radial partitions 56 in a multiplicity of radial exchange sectors 58, here twelve sectors of 30 ° each, which will be alternately traversed by compressed air leaving the compressor 12 and by the hot gases coming from the hot gas line 48.
• Each sector comprises a material for storing and retrieving calories, such as a mullite-type ceramic or cordierite.
• each face of the disk is in relation to fixed fluid inlet and outlet casings.
• the face 60 that seen on the left of FIG. 1, is in relation with a compressed air inlet box 62 carrying the inlet 34 connected to the line 32 and with a hot gas outlet box 64 carrying the hot gas outlet 50 connected to the line 52.
• a compressed air outlet housing 68 with the outlet 36 connected to line 38 and a hot gas inlet box 70 including the hot gas inlet 46 connected to line 48.
• each housing has a half-moon shape and two housings are disposed on each face of the disk, each facing each other, so that these two housings cover the whole of the considered face of the disc.
• devices are provided to ensure the seal between each face and the housings, and in an almost perfect manner between the different parts.
• these sealing devices may be those described in US Pat. No. 5,259,444.
• the position is maintained for a sufficient time and necessary so that, on the one hand, the fumes are cooled by transmitting the maximum of calories to the constituents of each sector of the upper half of the disc and, on the other hand, that the calories contained in the sectors of the lower half of the disk are transmitted to the compressed air to heat it to a high temperature.
• the disk is then driven in a rotational movement of a quarter turn around its axis XX under the impulse of the electric motor and remains in this position for a sufficient and necessary duration, as mentioned above.
• This rotational movement of a quarter of a turn is then repeated throughout the operation of the turbine.
• the outside air preferably at ambient temperature and pressure
• This compressed air is then sent via line 32 to the inlet 34 of the rotary regenerative heat exchanger to be heated therein, as mentioned above. It comes out with a high temperature (of the order of 900 ° C) to be brought by the line 38 to the inlet 40 of the expansion turbine 16.
• This very hot compressed air produces a rotation of this turbine which leads to its turn in rotation the compressor 12 by the shaft 18 and the generator 24 by the shaft 26.
• the expanded air leaving the expansion turbine 16, which is substantially at atmospheric pressure, is sent via line 44 to all appropriate means.
• the hot gases which are sent via the line 48 into the exchanger 14, pass through this exchanger between the inlet 46 and the outlet 50, yielding a very large part of their heat to a portion of the sectors 58 of the disk 54. cooled out of the exchanger 14 to be brought via line 52 to the chimney.
• FIG. 3 differs from the system illustrated in FIG. 1, on the one hand by the configuration of the source of hot gases from a combustion and, on the other hand, by a device making it possible to produce water. hot.
• this source is advantageously a burner type combustion chamber 72 comprising an inlet of an oxidant 74 and an intake of a fuel 76.
• the relaxed air coming from the Expansion turbine 16 is used as the oxidizer by the burner via line 44 but any other configuration for supplying this burner with fuel can be used, such as an external air supply.
• the fuel inlet 76 is connected to a supply line 78 of a solid fuel, such as biomass, but any other type of fuel may be envisaged, such as biogas.
• this oxidizer mixes with biomass introduced at the inlet 76 of the burner 72 to generate combustion under the effect of any means, such as a flame.
• This burner also comprises a discharge 82 of the hot gases (or smoke) resulting from the combustion and which is connected to the line 48.
• This system also comprises a hot fluid generator 84, such as hot water, which is traversed by the fumes exiting the exchanger 14 and which makes it possible to use part of the heat generated by the burner 72 to produce this water hot.
• a hot fluid generator 84 such as hot water
• this generator consists of a radiator traversed by the fumes exiting the exchanger and flowing in the line 52 and by the water introduced therein by a line 86 in liquid form and which emerges from a line 88 under heated form.
• the gas turbine is called a co-generation turbine (electricity + heat).
• this system makes it possible to compress the air by the compressor 12, heating this compressed air through a portion of the radial sectors of the disk 54 of the exchanger 14 and an expansion of the hot compressed air in the expansion turbine 16 by generating a rotation of this turbine and consequently a rotation of the generator 22 to produce electricity.
• the expanded air leaving the turbine is then sent to the burner 72 in which combustion is performed with the biomass fuel introduced therein.
• the fumes resulting from this combustion pass through the other part of the radial sectors of the exchanger 14 while cooling and then the hot water generator 84 in which they heat the water supplied to it.
• FIG. 4 differs from that of FIG. 3 in cooling the compressed air leaving the compressor 12 while allowing a fluid, such as water, to be heated, not from the heat of the fumes, but from this compressed air and a cooling of a portion of the expanded air leaving the expansion turbine 16.
• a fluid such as water
• the generator 84 which was placed on the line 52 of FIG. 3, is placed, in the case of FIG. 4, on the line 32 between the outlet 30 of the compressor 12 and the inlet 34 of the exchanger 14 .
• the temperature of the compressed air is substantially at a constant level and the calories it conveys are used to obtain hot water at the output of the generator and whatever the temperature of the fumes that can undergo not insignificant variations.
• This variant also offers the possibility of cooling a portion of the expanded air leaving the expansion turbine 16 to inject it into the inlet of the burner 72 in addition to the expanded air already injected at the inlet 74 via the line 44.
• a bypass line 90 connecting a point 92 of the line 44 and a fresh air inlet 94 at the burner 72.
• a cooling radiator 96 is placed on this line and allows to lower the temperature of the relaxed air which passes through it at a level of ambient temperature, for example by exchange with outside air.
• This injection of fresh air is more particularly intended for the injection of primary air in burners of the grid type which do not withstand high temperatures at the air inlet.
• This system thus makes it possible to compress the air by the compressor 12, cooling this air by passing through the generator 84 by producing hot water, heating this compressed air by a portion of the exchanger 14, an expansion of the hot compressed air in the expansion turbine 16 with a rotation of this turbine and the generator 22 to produce electricity.
• the expanded air leaving the turbine is then sent to the burner 72, for a portion of this air expanded, directly and, for the other part, after passing through the radiator 96 to cool.
• This relaxed air is then used to achieve combustion with the biomass that is introduced into the burner.
• the fumes resulting from this combustion pass through the other part of the exchanger while cooling and are then discharged to the chimney.
• Figure 5 differs from that of Figure 4 in that it is expected to increase the overall efficiency of the system by reducing the compression work.
• FIG. 4 it is planned to place a two-stage compressor 12a and 12b in place of the compressor 12.
• the inlet of the first stage 12a is connected to the outside air inlet line 28
• the output of the second stage 12b is connected via the line 32 to the exchanger 14 through the generator 84 and a line 98 connects the output of the first stage with the input of the second compression stage.
• An additional hot fluid generator 84a is placed on line 98 between the two compression stages and is used to generate hot water.
• the outside air admitted by the line 28 is compressed at a first level by the first compression stage 12a.
• the hot compressed air circulates in the line 98 and passes through the additional generator 84a to exchange the calories it conveys with the water circulating therein producing hot water.
• the cooled compressed air leaving the additional generator then enters the second compression stage 12b from which it leaves to circulate in line 32 through the generator 84 before entering the exchanger 14.

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• Engineering & Computer Science (AREA)
• Chemical & Material Sciences (AREA)
• Combustion & Propulsion (AREA)
• Mechanical Engineering (AREA)
• General Engineering & Computer Science (AREA)
• Engine Equipment That Uses Special Cycles (AREA)

Applications Claiming Priority (2)

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• 2007
  • 2007-05-15 FR FR0703552A patent/FR2916240B1/fr not_active Expired - Fee Related
• 2008
  • 2008-05-14 WO PCT/FR2008/000677 patent/WO2009004133A1/fr active Application Filing
  • 2008-05-14 EP EP08805575A patent/EP2158391A1/fr not_active Withdrawn
  • 2008-05-14 US US12/599,975 patent/US20110036097A1/en not_active Abandoned
  • 2008-05-14 JP JP2010507951A patent/JP5357866B2/ja not_active Expired - Fee Related

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