Method of increasing the safety of a power plant, and a power plant suitable for implementing the method

Abstract

The present invention relates to a method of increasing the safety of a power plant provided with at least one heat engine and a gearbox (BTP), the engine driving the gearbox (BTP), the gearbox (BTP) having a lubrication system implemented using an aqueous medium stored in a reserve, in which method a fluid comprising water is injected into the heat engine to increase the power developed by the heat engine without increasing the temperature of a member of the heat engine or to decrease the temperature without modifying the power developed by the engine, the fluid being taken from the reserve.

Claims

1. A power plant provided with a heat engine and with a gearbox and a reserve, the heat engine driving the gearbox, wherein the reserve is hydraulically connected via a hydraulic connection to the gearbox and to the heat engine to lubricate the gearbox and to increase a power of the heat engine without increasing a temperature of the heat engine or to reduce the temperature of the heat engine without reducing the power of the heat engine, the power plant including at least one main closure means between the heat engine and the reserve, and at least one secondary closure means between the gearbox and the reserve, the power plant including a control member for controlling the main and secondary closure means, the power plant including a mixer; wherein the reserve comprises a first bottle configured to contain pure water and a second bottle configured to contain an intermediate solution; wherein the control member is configured to control the mixer to only inject fluid from the first bottle into the heat engine; and wherein the control member is configured to control the mixer to inject fluid from the first bottle and the second bottle as a fluid mixture into the gearbox.

2. The power plant according to claim 1, wherein the at least one main closure means comprises a main admission valve, and the at least one secondary closure means comprises a secondary admission valve.

3. The power plant according to claim 1, wherein, for the gearbox including at least one member to be lubricated, the hydraulic connection includes a duct opening out into an injection nozzle directed towards the at least one member to be lubricated, the nozzle being suitable for injecting a fluid from the reserve in the form of a jet or a mist.

4. The power plant according to claim 1, wherein for the heat engine being a turbine engine having a free turbine and a gas generator, and for the gas generator comprising an air inlet and a combustion chamber into which a fuel is injected, the hydraulic connection comprises at least one injection pipe selected from a fourth list comprising at least one of the following injection pipes: a first injection pipe opening out into a fuel feed pipe of the heat engine in order to inject a fluid into the combustion chamber together with the fuel; a second injection pipe opening out into the combustion chamber in order to inject the fluid into the combustion chamber independently of the fuel; and a third injection pipe opening out into the air inlet.

5. The power plant according to claim 1, wherein the intermediate solution includes an antifreeze, or a combination of antifreeze and lubricant.

6. The power plant according to claim 5, wherein the reserve is provided with one transfer pump per bottle.

7. The power plant according to claim 1, wherein the at least one main closure means is distinct from the at least one secondary closure means.

8. The power plant according to claim 1, wherein the heat engine is a turbine engine having a free turbine and a gas generator.

9. The power plant according to claim 1 wherein the main and secondary closure means are provided by a hydraulic distributor, the hydraulic distributor with an inlet orifice hydraulically connected to the reserve, a first outlet orifice hydraulically connected to the heat engine, and a second outlet orifice hydraulically connected to the gearbox.

10. A power plant for a rotorcraft comprising: a gearbox for driving a rotary wing; a heat engine connected to the gearbox to drive the gearbox; a fluid reserve comprising a first bottle configured to contain pure water and a second bottle configured to contain an intermediate solution; a main valve positioned between and hydraulically connecting the fluid reserve and the heat engine; a secondary valve positioned between and hydraulically connecting the fluid reserve to the gearbox; a mixer, and a controller configured to control the main valve to control injecting a fluid from the fluid reserve into the heat engine and the secondary valve to control injecting the fluid from the fluid reserve into gearbox; wherein the controller is configured to control the mixer to only inject fluid from the first bottle into the heat engine; and wherein the controller is configured to control the mixer to inject fluid from the first bottle and the second bottle as a fluid mixture into the gearbox.

11. The power plant according to claim 10, wherein the heat engine is a turbine engine having a free turbine and a gas generator.

12. The power plant according to claim 11, further comprising an injection pipe hydraulically connected to the fluid reserve and the main valve to inject the fluid from the fluid reserve into the heat engine, the injection pipe positioned in one of a fuel feed pipe of the heat engine, a combustion chamber of the heat engine, and an air inlet of the heat engine.

13. The power plant according to claim 10 further comprising a transfer pump; wherein the transfer pump is hydraulically connected to one of the first bottle and the second bottle to pump the fluid therefrom.

14. The power plant according to claim 10 further comprising a duct fluidly connected to the fluid reserve, the duct opening out into an injection nozzle directed towards at least one member to be lubricated within the gearbox, the injection nozzle is configured to inject the fluid from the fluid reserve in the form of a jet or a mist.

15. The power plant according to claim 10 wherein the main and secondary valves are integrated into a hydraulic distributor, the hydraulic distributor with an inlet orifice hydraulically connected to the fluid reserve, a first outlet orifice hydraulically connected to the heat engine, and a second outlet orifice hydraulically connected to the gearbox.

16. The power plant according to claim 12, wherein for the injection pipe positioned in the fuel feed pipe of the heat engine, the fluid from the fluid reserve is injected together with a fuel; and wherein for the injection pipe positioned in the combustion chamber of the heat engine, the fluid from the fluid reserve is injected independently of the fuel.

17. The power plant according to claim 10, wherein the intermediate solution comprises one of an antifreeze, and an antifreeze and a lubricant.

18. The power plant according to claim 10, wherein the fluid from the fluid reserve is injected into the heat engine to increase a power of the heat engine without increasing a temperature of the heat engine or to reduce the temperature of the heat engine without reducing the power of the heat engine.

19. The power plant according to claim 10 further comprising a selector switch in communication with the controller, the selector switch configured to receive an order from a pilot regarding injection of the fluid into the heat engine.

20. The power plant according to claim 10, wherein the controller has a memory containing preprogrammed relationships to determine injection of the fluid into the heat engine.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

(1) The invention and its advantages appear in greater detail in the context of the following description with embodiments given by way of illustration and with reference to the accompanying figures, in which:

(2) FIG. 1 is a diagram explaining the method of the invention;

(3) FIG. 2 shows a first embodiment provided with a reserve fitted with a bottle;

(4) FIG. 3 shows a second embodiment provided with a reserve fitted with two bottles;

(5) FIG. 4 shows a variant of the first and second embodiments fitted with a hydraulic distributor.

(6) Elements that are present in more than one of the figures are given the same references in each of them.

DETAILED DESCRIPTION

(7) The present invention relates to a method of making safe a power plant 10, the power plant 10 including at least one heat engine 1 driving a power transmission gearbox BTP.

(8) In a rotorcraft, and in particular a helicopter, the gearbox BTP drives a rotor mast 5 in rotation about an axis of rotation AX, the rotor mast 5 being secured to a hub 6 carrying a plurality of blades 7. Such a gearbox BTP is known as a main gearbox.

(9) According to the invention, the power plant includes a reserve 30 filled with a fluid comprising water connected to the main gearbox BTP and to the heat engine 1. Thus, the reserve is filled with a fluid that is suitable for being injected into the heat engine 1 and/or into the main gearbox BTP.

(10) The fluid may be selected from a list referred to as the second predetermined list, this list including at least one of the following aqueous solutions: pure water; a first mixture of pure water and antifreeze of the ethylene glycol type; and a second mixture of pure water with at least an antifreeze and a lubricant.

(11) The reserve 30 may include a single bottle filled with such fluid, or a plurality of bottles 33, 34 serving to contain the various ingredients of the fluid.

(12) Under such circumstances, in compliance with the method of the invention, the fluid is injected into the heat engine 1 in order to achieve at least one situation contained in the catalog of predetermined situations. This catalog comprises at least one of the following situations: an increase in the power developed by the heat engine 1 without increasing the temperature of a member of the heat engine, e.g. the inlet to the free turbine stage; a decrease in the temperature of a member of the heat engine without modifying the power developed by the heat engine, e.g. the temperature T4 at the inlet to the free turbine stage of a turbine engine.

(13) In addition, the catalog may also comprise one or more of the following additional situations: for a moving member that is to be set into movement at a speed limited by a given maximum speed at each instant, the fluid is injected when the moving member moves at a speed that is faster than said given maximum speed; for a moving member that is to be set into movement at a speed limited by a given minimum speed at each instant, said fluid is injected when said moving member is moving at a speed slower than said given minimum speed; for the heat engine 1 being a turbine engine having a free turbine and a gas generator, said fluid is injected when a monitored parameter crosses a predetermined threshold, i.e. on going below a minimum threshold or above a maximum threshold, the monitored parameter forming part of a first list including at least one of the following parameters: the speed of rotation Ng of said gas generator; the speed of rotation NTL of the free turbine; the temperature T4 of the gas at the inlet to the free turbine; and the flow rate Q of fuel feeding the heat engine; and for a power plant having two heat engines suitable for operating at at least a first rating when neither of the heat engines is inoperative and at least one emergency rating when one of the engines is inoperative, with the working engine developing super-emergency power PSU for a predetermined duration D1 during said emergency, the fluid is injected in order to increase the super-emergency power PSU and to lengthen the predetermined duration D1.

(14) Furthermore, in the method, when the heat engine is a turbine engine having a free turbine and a gas generator, the gas generator including an air inlet and a combustion chamber into which a fuel is injected, the fluid is injected using an injection process selected from a third list comprising at least one of the following injection processes: the fluid is injected into a fuel feed pipe of the heat engine 1 so as to be delivered into the combustion chamber together with the fuel; the fluid is injected into the combustion chamber in order to be injected into said combustion chamber independently of the fuel; and said fluid is injected into the air inlet.

(15) FIG. 2 shows a first embodiment provided with a reserve having one bottle, this embodiment being an embodiment that is preferred by virtue of its simplicity.

(16) The power plant shown comprises first and second heat engines 1, 2 of the turbine engine type. These first and second heat engines 1, 2 are fed with fuel from a fuel tank 8 via respective first and second fuel feed pipes 8 and 8.

(17) Thus, the first heat engine 1 is provided with a first gas generator comprising in succession a first air inlet 11, a first compressor 12, with a first combustion chamber 13, a first turbine connected to the first compressor 12 optionally being located at the outlet from the first combustion chamber 13. A first free turbine stage 14 is located downstream from the first gas generator, i.e. after the first combustion chamber 13 or the first turbine, as appropriate.

(18) Similarly, the second heat engine 2 is provided with a second gas generator comprising in succession a second air inlet 21, a second compressor 22 with a second combustion chamber 23, a turbine connected to the second compressor 22 possibly being located at the outlet from the second combustion chamber 23. A second free turbine stage 24 is located downstream from the second gas generator, i.e. after the second combustion chamber 23 or after the second turbine, where appropriate.

(19) Furthermore, the power plant 10 possesses a reserve 30 containing a water-based fluid suitable for being injected into each heat engine 1, 2 via at least one injection zone, and optionally into the inside of the gearbox BTP via at least one injection zone.

(20) Thus, the power plant 10 includes a hydraulic connection connecting the reserve 30 to each injection zone Z1, Z2, Z3, Z4, Z5, Z6, and Z7, main closure means being arranged between each injection zone Z1, Z2, Z3, Z4, Z5, and Z6, of the heat engines and the reserve 30, and secondary closure means being arranged between each injection zone Z7 of the gearbox BTP and the reserve 30.

(21) With reference to FIGS. 2 and 3 in a first variant, the hydraulic connection includes a first intermediate connection 91 leaving the reserve 30 and leading towards the first heat engine 1, this first intermediate connection 91 being a pipe, for example.

(22) Since the first heat engine is a turbine engine, the first intermediate connection 91 is advantageously extended by a first injection pipe 50 having a main admission valve 51 of main closure means opening out into an injection zone Z3 of the first fuel feed pipe 8 feeding the first combustion chamber 13. In addition, the first intermediate connection 91 is also connected to a second injection pipe 70 provided with a main admission valve 71 of main closure means opening out directly into an injection zone Z2 of the first combustion chamber 13. Finally, the first intermediate connection 91 is connected to a third injection pipe 60 provided with a main admission valve 61 of main closure means opening out into an injection zone Z1 of the first air inlet 11.

(23) Under such circumstances, each injection zone Z1, Z2, Z3 of the first heat engine is thus separated from the reserve 30 by main closure means suitable for preventing or allowing fluid to pass from the reserve to the first heat engine 1.

(24) Similarly, the hydraulic connection includes a second intermediate connection 92 going from the reserve 30 towards the second heat engine 2, this second intermediate connection 92 being a pipe, for example. Since the second heat engine 2 is a turbine engine, the second intermediate connection 92 is advantageously extended by a second injection pipe 150 provided with a main admission valve 151 of main closure means opening out into an injection zone Z6 of a second fuel feed pipe 8 feeding the second combustion chamber 23. In addition, the second intermediate connection 92 is connected to a second injection pipe 160 provided with a main admission valve 161 of main closure means opening out directly into an injection zone Z5 of the second combustion chamber 23. Finally, the second intermediate connection 92 is connected to a third injection pipe 170 provided with a main admission valve 171 of main closure means opening out into an injection zone Z4 of the second air inlet 21.

(25) Under such circumstances, each injection zone Z4, Z5, and Z6 of the second heat engine is thus separated from the reserve 30 by main closure means suitable for preventing or allowing a fluid to pass from the reserve to the second heat engine 2.

(26) Finally, the hydraulic connection includes a third intermediate connection 93 going from the reserve 30 and extended by a duct 40 and secondary closure means opening out into an injection zone Z7 of the gearbox BTP provided with at least one fluid injection nozzle. The duct 40 is then provided with secondary closure means 41.

(27) Each injection zone is thus separated from the reserve by an admission valve of closure means, two different valves being physically distinct and constituting two different pieces of equipment.

(28) It is possible to implement only one or two of the above-described three injection pipes 50, 60, 70, for example.

(29) In the first embodiment of FIG. 1, the reserve 30 includes a single bottle 31 filled with a fluid and possibly a transfer pump 32 or some other pressurizing system, in particular systems as described in document FR 2 826 094, for example.

(30) Furthermore, the power plant 10 is provided with a control member 80 including a processor 81 connected to a memory 82.

(31) The control member 80 is electrically connected to the main admission valves 51, 61, 71, 151, 161, and 171, to the secondary admission valve 41, and to the pump 32 in order to control them so as to deliver fluid to the associated injection zone.

(32) It should be observed that the electrical connections between the control member 80 and the main admission valves 51, 61, 71, 151, 161, and 171, the secondary admission valve 41, and the pump 32 are not shown in the figures in order to simplify them. By way of example, these electrical connections may be of the wired or of the non-wired type.

(33) The main admission valves 51, 61, 71, 151, 161, and 171 and the secondary admission valve 41 are in a closed mode when in a normal configuration so as to prevent fluid from flowing from the reserve 30 to the associated injection zone.

(34) In an automatic mode of operation, the processor 81 makes use of preprogrammed regulation relationships contained in the memory 82 in order to determine whether or not a valve ought to be opened.

(35) For example, if the processor is advised that the first stage of the free turbine 14 of the first heat engine 1 is rotating at a speed higher than a maximum speed programmed in the memory 82, by means of sensors dedicated to this purpose, then the processor 81 opens the admission valve 51 of the first injection pipe 50 and activates the pump 32 to inject the fluid into the first combustion chamber 13 together with the fuel, at a pressure that is preprogrammed in said memory 82.

(36) Conversely, if the processor is advised that the first stage of the free turbine 14 of the first heat engine 1 is rotating at a speed slower than a minimum speed programmed in the memory 82, by means of sensors dedicated for this purpose, then the processor 81 opens the admission valve 61 of the third injection pipe 60 and activates the pump 32 to inject the fluid into the second combustion chamber independently of the fuel, and at a pressure that is preprogrammed in said memory 82.

(37) In a manual mode of operation, the pilot has control means 83 provided with a rotary knob 83. When the rotary knob is in the OFF position, all of the valves are closed.

(38) In contrast, when the knob is positioned in some other position one or more of the valves are opened. For example, the positions 51, 61, 71, 151, 161, 171, and 41 open the valves 51, 61, 71, 151, 161, 171, and 41 respectively.

(39) With reference to FIG. 3, in a second embodiment, the reserve 30 includes a plurality of bottles, each provided with a pump leading to a mixer 37.

(40) For example, the reserve 30 includes a first bottle 33 of pure water associated with a first pump 35, and a second bottle 33 associated with a second pump 36 and containing an intermediate solution comprising either antifreeze or a third mixture of at least an antifreeze and a lubricant.

(41) Thus, when it is necessary to feed fluid to a heat engine, the processor 81 requests the mixer 37 to block the liquid coming from the second bottle. In contrast, when it is necessary to feed fluid to the gearbox, the processor requests the mixer 37 to mix the pure water of the first bottle 33 to the intermediate solution of the second bottle 34.

(42) It should be observed that the control member 80 may be a dedicated control member, or that it may be incorporated in existing means, e.g. the member for regulating the heat engines 1 and 2.

(43) FIGS. 2 and 3 show a variant having a plurality of main and secondary closure means that are physically distinct from one another.

(44) Nevertheless, with reference to FIG. 4, these main and secondary closure means could form parts of a single piece of equipment, a hydraulic distributor 94.

(45) The hydraulic distributor may include a slide, an inlet orifice, and a plurality of outlet orifices representing the main admission valves 51, 61, 71, 151, 161, and 171, and the secondary admission valve 41. By moving the slide, the control member 80 then causes one or more of the valves to be opened, as appropriate.

(46) The hydraulic distributor is then controlled by the control member 80 via an electrical connection, not shown.

(47) Each main closure means is thus distinct from each secondary closure means, even if the valves all form part of a single assembly.

(48) Naturally, the present invention may be subjected to numerous variations as to its implementation. Although several embodiments are described, it will readily be understood that it is not conceivable to identify exhaustively all possible embodiments. It is naturally possible to envisage replacing any of the means described by equipment means without going beyond the ambit of the present invention.