Space heating system with fuel cells and a connection to a public electrical network

Abstract

The space heating system with fuel cells (11) has a connection to a public electrical network (50). In this system a fuel (B) can be supplied to the fuel cells in gaseous form through a main gas valve (200) for the production of thermal and electrical energy. The main gas valve has a control which, on an interruption of the current supplied, results in an automatic operating shutdown. The possibilities exist for the system to feed the electrical energy at least partly into the network and to deliver the thermal energy to a heating circuit which is operable with electrical energy from the network. An electrical inverter (4), with which direct current of the fuel cells can be converted into alternating current, can be operated in two operating states, on the one hand, for a feed into the public network, and, on the other hand, for a feed into the island network of the system. Means are provided with respect to a power cut of the public network by which a short-term maintenance of necessary functions of the space heating system—the fuel supply into the fuel cells having first priority—is ensured without support by, for example, galvanic batteries. Moreover, controls and circuits are provided with which at least the necessary functions of the space heating system can continue to be maintained by means of electrical energy from the fuel cells.

Description

[0001] The invention relates to a space heating system with fuel cells and a connection to a public electrical network in accordance with the preamble of claim 1 as well as to a method for the operation of the system.

[0002] A space heating system is known from EP-A-1 205 993 in which thermal and electrical energy is recovered, and can be used, from a gas mixture containing hydrogen and carbon monoxide by means of high temperature fuel cells. A particular control is described with which a reliable and hazard-free operation of the system is ensured. The thermal energy can be used for a heating of service water and/or for space heating. The electrical energy can be used for the actuation of sensors and actuators (e.g. for the operation of pumps). A surplus of this form of energy can also be supplied to a public network. The gas mixture is led through a main gas valve arranged upstream of the fuel cells. The control of this valve is designed such that, on an interruption of the current required for the valve control, the valve closes and the energy-delivering operation of the fuel cells is thus stopped. An interruption over a longer period results in the fuel cells cooling. Interruptions to operation are damaging for the fuel cells; for thermal cycles with cooling and renewed heating cause the electrochemically active components of the cells to age rapidly. Power interruptions in the public network therefore result in an ageing of the fuel cells which would not necessary have to occur. With the aid of, for example, galvanic batteries or emergency power generators, the operation of the space heating system could be maintained if required on a network power cut. Such support measures, however, mean added costs which only arise due to possible network power cuts; they also require a regular inspection and maintenance, e.g. recharging or replacing the batteries.

[0003] It is therefore the object of the invention to provide a space heating system in which precautionary measures are installed by which the operation of the system can be continued on a network power cut, with these measures not being support measures of the kind associated with a maintenance effort. This object is satisfied by the space heating system defined in claim 1.

[0004] The space heating system with fuel cells has a connection to a public electrical network. In this system, a fuel is supplied in gaseous form to the fuel cells through a main gas valve for the production of thermal and electrical energy. The main gas valve has a control which results in an automatic operating shutdown on an interruption of the current supplied. The possibilities exist for the system of feeding the electrical energy at least partly into the network and of releasing the thermal energy to a heating circuit, with the heating circuit also being operable with electrical energy from the network. An electrical inverter with which direct current of the fuel cells can be converted into alternating current can be operated in two operating modes: on the one hand, for a feed into the public network and, on the other hand, for a feed into an island network of the system. Means are provided with respect to a power cut of the public network by which a short-term maintenance of required functions of the space heating system is ensured—the fuel supply into the fuel cells having first priority—without support by, for example, galvanic batteries. Moreover, controls and circuits are provided with which at least the required functions of the space heating system can continue to be maintained by means of electrical energy from the fuel cells.

[0005] The dependent claims 2 to 5 relate to advantageous embodiments of the space heating system in accordance with the invention. Methods for the operation of the system in accordance with the invention form the subject matter of claims 6 to 10.

[0006] The invention will be explained in the following with reference to the drawings. There are shown:

[0007] FIG. 1 a schematic representation of a part of a space heating system; and

[0008] FIG. 2 the whole space heating system in which measures have been realised for the prevention of interruptions to operation.

[0009] A part system 100—a part of the space heating system of FIG. 2—shown in FIG. 1 is described in detailed form and with reference to diverse variants in the aforesaid EP-A-1 205 993. It includes a fuel cell battery 10 which has a stack 11 of fuel cells connected in series and in which electrical energy (voltage U) and hot exhaust gas are produced with two gaseous educts A and B. The electrical energy is delivered to a further part of the space heating system via two poles 12a, 12b. This further part is shown in FIG. 2. The two poles 12a, 12b appear there as one single terminal point, the electrical output 12. The educts A and B are supplied to the battery 10 through lines 1 and 2 and inputs 13a and 13b respectively. The hot exhaust gas is sucked off by a fan 16 at an outlet 13c, with it being transported through a line 3 as well as a heat exchanger 15. Cooled exhaust gas C is delivered to the environment. The fan 16, with which exhaust gas is sucked in, is arranged downstream of the battery 10 for safety reasons. This suction member could also be replaced by a fan disposed upstream of the battery 10; then, however, overpressure would result in the fuel cells in operation.

[0010] The waste heat recovered from the hot exhaust gases by the heat exchanger 15 is transported to a heat accumulator 18 by means of a heat transfer medium (advantageously water) via a circuit 17 with a pump 17′. The waste heat can be supplied from the accumulator 18 via a second circuit 19 with a pump 19′ to a consumer 20, for example radiators of a building. The two heating circuits, namely the circuit 17 and the circuit 19, are termed the “producer circuit” and the “consumer circuit” respectively in the following, with the reference numerals 17 and 19 still being used for these heating circuits.

[0011] The educt A is as a rule air which is sucked in from the environment. The educt B is a fuel which is gaseous or is put into gaseous form. This gas is led through a plant part 200 in which a main gas valve and means for the control of performance are arranged (cf. EP-A-1 205 993). On an interruption of power, the main gas valve closes such that the battery operation is stopped. The control of the main gas valve is exerted by a plant part 14. This control unit 14 is connected via lines 140a to sensors of the battery 10, via lines 140b to the plant part 200 and via lines 142 to the fan 16. The infeeds of the educts A and B are coupled to one another via a connection 1a and the plant part 200.

[0012] The characteristic features for the invention are shown in FIG. 2. Lines for line transports are shown with double lines, lines for controls (actuators) with single lines and lines for information transfers (sensors) with broken lines. The part plant 100 of FIG. 1 is connected via the electrical output 12 to an electrical inverter 4 with which direct current of the fuel cells is converted into alternating current. The inverter 4 can be operated in two operating modes. In the one state, the alternating current is supplied to the public network via lines 40, 50; in the other state, the alternating current is fed via a line 41 into an island network which belongs to the system in accordance with the invention. For the case that an interruption of power occurs in the public network, a “network release” is arranged between the lines 40 and 50, namely a device 5 with which the feed of the alternating current into the network is stopped and suitable operations are initiated in the island network.

[0013] The island network is in a programmed state which is set by a system control 6. The system control 6 also includes an energy management of the space heating with which, for example, the charge state of the heat accumulator 18 is managed. A first switch 51 (control 651) and a second switch 52 (control 652) can be actuated by means of the system control 6. The main gas valve and the performance control of the part system 100 (plant part 200) are respectively connected to the system control 6 via a control line 62 and 63 respectively. A further control line 64 leads to the inverter 4. The network release 5 and the system control 6 are connected via an information line 56. The control line 62 includes a “network power cut bridge” by which a short-term maintenance of necessary functions of the space heating system is ensured—the fuel supply into the fuel cells having first priority—without support by, for example, galvanic batteries.

[0014] Lines 67a, 70a and 67b respectively are present between system sensors 7a, which are associated with the producer circuit 17 (arrows 71), and system actuators 7b, which are likewise associated with the producer circuit 17 (arrows 72). A line 60 is present for a feed of alternating current from the public network, or from the inverter 4, into the system control 6 and a “network power cut bridge” 60′ is also provided in said line 60. The system actuators 7b are supplied with electrical energy via a branch line 70b. Finally, the system control 6 is connected via lines 86 and 68 to a system part 8 which contains sensors and actuators for the consumer circuit 19 (arrows 81 and 82 respectively). The alternating current required for this system part 8 is supplied via the line 80 linked at the switch 52. The alternating current can be taken from the network (line 50′) or form the inverter 4 (line 42).

[0015] The inverter 4 can be switched from the one operating mode into the other within a relatively short time period At. This time period At is not larger than approximately 0.1 seconds. The power supply of the valve control by the control line 62 is secured during a time period which is larger than At by a buffer which, for example, includes a capacitor 62′ such that the fuel supply into the fuel cells takes place without interruption.

[0016] The space heating system in accordance with the invention can be operated in accordance with the following three modes:

[0017] Mode M1: the switches 51 and 52 have the states represented in FIG. 2. The part plant 100 with the battery 10 is not in operation, or it is just being put into operation. The electrical power delivered by the battery 10 is less than 100 W (this is an illustrative numerical example which will be maintained in the following. The value of 100 W can also be modified. This also applies to further value figures). The inverter 4 is in its first operating mode. The total produced electrical power is supplied to the public network. The producer circuit 17 and the consumer circuit 19 receive electrical power from the network.

[0018] Mode M2: the electrical performance of the part system 100 is larger than 100 W and less than 200 W. The switch 51 is thrown and the inverter 4 produces sufficient alternating current so that the system control 6 and the actuators 7b can be fed directly from the inverter 4.

[0019] Mode M3: the electrical performance of the fuel cells is larger than 200 W. The inverter 4 produces sufficient alternating current to supply both the producer circuit 17 and the consumer circuit 19. For this purpose, the switch 52 is actuated such that electrical energy from the inverter is also deliverable to the consumer circuit 19. The consumer circuit 19 includes means for the further transport of heat from the heat accumulator 18 to the consumer 20 and for a control of this heat transport.

[0020] On a network power cut, the network release 5 cuts the lines 40 and 50; the switch 51 is thrown so that the system control 6 and the actuators 7b can be fed directly from the inverter 4. During the switch over time At, the network power cut bridge of the supply line 60 ensures that the system control 6 maintains necessary functions of the space heating system until after a switch over of the inverter 4, on the one hand, and the network power cut bridge of the line 62 ensures that the main gas valve (for the educt B) also continues to remain open on a short power cut of the power supply, on the other hand. The operation of the producer circuit 17 remains interrupted during the switch over time At. The consumer circuit 19 can be out of operation for some minutes after the network power cut thanks to a thermal buffer effect of the consumer 20 (heated building). This time is sufficient to increase the gas supply and so to increase the production of the electrical power to a sufficient degree. This power must exceed a threshold value N2.

[0021] There are two thresholds N1 and N2 which are pre-set due to properties of the system for the electrical power produced with the fuel cells, namely the requirement for power to operate the producer circuit 17 and the requirement for power to operate both heating circuits 17 and 19. In the above described numerical example, N1=100 W and N2=200 W. Depending on the power requirement with respect to the two threshold values, the operation is carried out in one of the three modes, with the two switches 51, 52 being switched in accordance with the mode to be selected by the system control 6. So that the plant does not switch off on a network power cut, the gas supply is controlled by the system control such that the threshold value N1 is permanently exceeded. The gas supply can be modulated in a wide range due to the splitting of the operation into modes by means of the thresholds N1 and N2.

[0022] In accordance with the three modes, different methods of operation also result:

[0023] The electrical power produced with the fuel cells is less than N1 (Mode M1). This power is not sufficient for operation of all components of the system. Current is therefore taken from the public network.

[0024] The electrical power produced with the fuel cells is larger than N1 (Mode M2). This power is delivered to the producer circuit 17. If the network release 5 connects the lines 40 and 50, the excess power is delivered to the public network.

[0025] The electrical power produced with the fuel cells is larger than N2 (Mode M3). This power is delivered to the producer circuit, to the consumer circuit and—if the network release 5 connects the lines 40 and 50—to the public network.

Claims

1. A space heating system with fuel cells (11) and a connection to a public electrical network (50), in which system a fuel (B) can be supplied to the fuel cells in gaseous form through a main gas valve (200) for the production of thermal and electrical energy, with the main gas valve having a control which, on an interruption of the current supplied, results in an automatic operating shutdown, and with possibilities existing for the system to feed the electrical energy at least partly into the network and to deliver the thermal energy to a heating circuit which is operable with electrical energy from the network,

2. A space heating system in accordance with claim 1, characterised in that the inverter (4) can be switched from the one operating state into the other within a relatively short time period Δt; in that this time period Δt is, in particular, not larger than 0.1 seconds; and in that the power supply to the control of the main gas valve is secured for a time period larger than At by a buffer, which for example includes a capacitor (62′), such that the fuel supply into the fuel cells takes place without interruption; and in that the power supply to a system control (6) is also secured by a buffer, which for example includes a further capacitor (60′), such that the system control remains functional.

3. A space heating system in accordance with claim 2, characterised in that a producer circuit (17) and a consumer circuit (19) connected thereto are provided, with the producer circuit including a heating circuit for the transporting of waste heat which can be recovered in a heat exchanger (15) from hot exhaust gases of the fuel cells; and in that the producer circuit can be operated by means of electrical energy from the fuel cells (11) on the basis of the one operating state of the inverter.

4. A space heating system in accordance with claim 3, characterized in that the producer circuit (17) includes a heat accumulator (18); in that heat can be transported from this heat accumulator to a consumer (20), in particular to radiators of the space heating, by the consumer circuit (19); and in that, for the case of a longer power cut of the public network and with a sufficient supply of electrical energy by the fuel cells (11), the consumer circuit can be set in operation by the electrical power delivered by the fuel cells.

5. A space heating system in accordance with any one of claims 1 to 4, characterised in that an electrical island network, a system control (6) and two switches (51, 52) are components of the system; in that the switches are operatively connected to the system control; and in that the system can be operated in one of three modes depending on the setting of the switches.

6. A method for operating the system in accordance with any one of claims 1 to 5, characterized in that two threshold values N1 and N2 are pre-set on the basis of properties of the system for the electrical power produced with the fuel cells; and in that the operation is carried out in one of three modes depending on the power with respect to the two threshold values, with two switches being switched according to the mode to be selected by a system control and with the first threshold value N1 being smaller than the second threshold value N2.

7. A method in accordance with claim 6, characterized in that the electrical power produced with the fuel cells is less than N1 and this total power is delivered to the public network, while the power for an operation of all components of the system is taken from the public network.

8. A method in accordance with claim 6, characterized in that the electrical power produced with the fuel cells is larger than N1; and in that this power is delivered to a producer circuit (17) and—if possible—to the public network.

9. A method in accordance with claim 8, characterized in that the electrical power produced with the fuel cells is larger than N2; and in that this power is delivered to the producer circuit (17), to a consumer circuit (19) and—if possible—to the public network.

10. A method in accordance with any one of claims 6 to 9, characterized in that, on a power cut of the public network, the system is operated in one of the two modes, and is optionally set into one such mode, in which the electrical power produced with the fuel cells is greater than N1.