Magnetic sensor system for detecting abnormal movement in a gas turbine shaft

Abstract

The present invention relates to a system (100, 300, 400) for detecting abnormal movement of a gas turbine shaft. The system comprises: a magnetic circuit (104, 302, 402) comprising a first magnetic portion (110, 304) and a second portion (112, 404), and including at least one air gap between the first portion and the second portion; and a detection coil (106) wound around the first magnetic portion. The second portion is coupled to or moveable with the shaft to reduce the air gap, on axial movement of the shaft to change the reluctance of the magnetic circuit and thereby induce a voltage in the coil. The system may comprise a controller (108) for shutting off power to the gas turbine when the induced voltage exceeds a threshold voltage.

Claims

1. A system for detecting breakage of a gas turbine shaft comprising: a magnetic circuit, forming one or more closed loop paths containing a magnetic flux, comprising a first magnetic portion and a second portion, and including at least one air gap between the first portion and the second portion; and a detection coil wound around the first magnetic portion; wherein, the second portion is coupled to or moveable with the gas turbine shaft to reduce the at least one air gap, on axial movement of the gas turbine shaft, to change the reluctance of the magnetic circuit and thereby induce a voltage in the detection coil.

2. The system according to claim 1, wherein the first magnetic portion comprises a permanent magnet.

3. The system according to claim 1, wherein the first magnetic portion comprises an electromagnet.

4. The system according to claim 3, wherein the first magnetic portion comprises a further coil wound around a soft magnetic material to form the electromagnet.

5. The system according to claim 4, wherein a constant current is applied to the further coil.

6. The system according to claim 4 wherein an alternating current is applied to the further coil.

7. The system according to claim 3, wherein a constant current is applied to the detection coil to power the electromagnet.

8. The system according to claim 1, wherein the first magnetic portion comprises a base portion, and two arm portions, the detection coil being wound around the base portion.

9. The system according to claim 3, wherein the base portion is formed of a soft magnetic material.

10. The system according to claim 8, wherein the second portion of the magnetic circuits sized to fit between the two arm portions with clearance.

11. The system according to claim 1, wherein the second portion is formed of a soft magnetic material.

12. The system according to claim 1, wherein the second portion of the magnetic circuit is fixed to a plunger, the plunger being coupled to or moveable with the gas turbine shaft.

13. The system according to claim 1, wherein the second portion of the magnetic circuit is fixed to a last stage of a turbine disc of a gas turbine.

14. The system according to claim 13 wherein the second portion is a disc or a ring.

15. The system according to claim 1, further comprising a controller coupled to the detection coil, the controller being configured to shut off power to a gas turbine when the induced voltage in the detection coil exceeds a threshold voltage.

16. The system according to claim 15, wherein the controller is further configured to filter the induced voltage output of the detection coil.

17. The system according to claim 1, wherein the gas turbine shaft is part of a gas turbine engine.

18. The system according to claim 17, wherein the gas turbine engine is a jet engine.

Description

(1) FIG. 1a shows a schematic illustration of a system for detecting abnormal movement of a gas turbine shaft according to a first embodiment of the present invention;

(2) FIG. 1b shows the system of FIG. 1 in a configuration when the shaft is in an abnormal position;

(3) FIG. 2 shows a plot of a representative voltage output of the sensing system;

(4) FIG. 3 shows a schematic illustration of a system for detecting abnormal movement of a gas turbine shaft according to a second embodiment of the present invention; and

(5) FIG. 4 shows a schematic illustration of a system for detecting abnormal movement of a gas turbine shaft according to a third embodiment of the present invention.

(6) The system of the present invention for detecting abnormal movement in a gas turbine finds particular application in jet engines. A typical two spool turbo fan, jet engine comprises an intake, a fan, a nacelle, compressors, a combustion chamber, a fan nozzle, turbines, and a core nozzle. The engine also comprises an engine control unit (ECU), which, among other operations, is configured to control the flow of fuel to the engine.

(7) The engine may include a fan across the air intake. The fan is mounted on a shaft on which are also mounted the compressor rotors or blades and the turbine rotors or blades. The system of the present invention is configured to be mounted adjacent the downstream end of the shaft.

(8) The term axial, as used herein, refers to the direction of the axis of rotation of the shaft. The term transverse as used herein, refers to the direction perpendicular to the axis of rotation of the shaft. The term downstream, as used herein, refers to the direction from the intake of the engine towards the exhaust. The term upstream as used herein, refers to the direction opposite to the downstream direction.

(9) The portion of the turbine in which the system is located is, when the jet engine is in use, a high temperature environment. Temperatures in the engine can exceed 800 C. which means that the environment is an aggressive one.

(10) FIGS. 1a and 1b are schematic illustrations of a system for detecting abnormal movement of a gas turbine in accordance with an embodiment of the invention. The system comprises a plunger 102 mountable within a gas turbine engine (not shown). The system further comprises a magnetic circuit, represented by dashed line 104, a detection coil 106 and a controller 108.

(11) As used herein, the term magnetic circuit refers to a circuit of one or more closed loop paths containing a magnetic flux. The flux may be generated by permanent magnets or electromagnets and the flux is confined to the path by magnetic cores consisting of soft magnetic materials. The path may include one or more air gaps or other materials.

(12) The magnetic circuit 104 comprises a first portion 110, and a second portion 112. The first portion 110 comprises a base portion 114 and two arm portions 116 and 118. Each arm portion 116 and 118 has a proximal end, adjacent the base portion 114 and a free distal end. The first portion 110 of the magnetic circuit is thereby provided with a C-shape, or a U-shape. The second portion 112 is coupled to the plunger 102. In normal operation of the gas turbine, the system is configured to have an air gap, L.sub.g, between the free distal ends of the arm portions 116 and 118 and the second portion 112.

(13) The base portion 114 of the first portion of the magnetic circuit is formed of a magnetic material. As discussed above, the system operates in harsh and high temperature environments, and the materials used to form the various components of the system are chosen accordingly. The magnetic material is preferably a soft magnetic material, and preferably has a relatively high Curie temperature. Particularly appropriate materials are Cobalt, which has a Curie temperature of about 1128 degrees C., and Iron which has a Curie temperature of about 771 degrees C.

(14) In the embodiment of FIGS. 1a and 1b, the arm portion 116 is a permanent magnet. The arm portion 116 is also preferably formed from a soft magnetic material, and again preferably has a high Curie temperature. A particularly appropriate permanent magnet is AlNiCo formed from iron Aluminium, Nickel and Cobalt AlNiCo has a Curie temperature of about 860 degrees C.

(15) The arm portion 118 is formed of a magnetic material as described above with reference to the base portion 114. Preferably, the arm portion 118 and the base portion 114 are formed of the same material.

(16) As shown in FIG. 1a, the base portion 114 and the arm portions 116 and 118 are separate components. However, as will be appreciated, the base portion 114, and arm portions 116 and 118 may be integral. In this case, the whole of the first portion 110 may be formed of a permanent magnet, or a section of the first portion 110 may be formed of a permanent magnet. In either case, the arm portions 116 and 118 and the base portion 114 are elongate, and may have a square, or any other suitable, cross-sectional shape.

(17) In the embodiment shown in FIGS. 1a and 1b, the second portion 112 of the magnetic circuit 104 is configured to fit within the arm portions 116 and 118 with a clearance to prevent the second portion 112 from contacting the arm portions during an abnormal movement. Such a configuration enables the air gap, L.sub.g, to be minimised. The clearance provided is such that, even under abnormal transverse movement of the plunger, the second portion 112 does not contact the first portion 110.

(18) However, the system 100 may be configured such that the second portion 112 does not fit within the arm portions but rather is configured such that the distal ends of the second portion 112 overlap the distal ends of the arm portions 16 and 118. In this alternative, the system is configured such that, even under abnormal axial movement, the second portion does not contact the arm portions.

(19) The detection coil 106 is wound around the base portion 114. The coil is preferably formed of high temperature wires such as platinum wires with ceramic insulation or mineral insulated cables which can operate up to 1100 degrees C. The coil is electrically coupled to the controller 108. The controller 108 is discussed in detail below.

(20) As discussed above, during normal operation of the gas turbine, the second portion 112 of the magnetic circuit 104 is separated from the first portion 110 by the air gap L.sub.g. Providing the air gap results in a magnetic circuit having a high reluctance, R. The reluctance, R, of the circuit is given by the following formula:
R=L.sub.m/.sub.mA.sub.c+L.sub.g/.sub.gA.sub.c

(21) where, L.sub.m is the magnetic path length, L.sub.g is the length of the air gap, .sub.m is the magnetic permeability of the material forming the circuit, .sub.g is the magnetic permeability of air, and A.sub.c, is the core area of the circuit. In this case, the core area is the cross-sectional area of the first and second portions 116, 118 of the magnetic circuit 104.

(22) FIG. 1b shows the system 100 during an abnormal movement of the gas turbine shaft. For example, such an abnormal movement may occur when the shaft fails, separating the compressor from the turbine, whereby the loads acting on the turbine are such that it moves axially downstream. The abnormal shaft movement may be between about 5 mm and about 7 mm, in a particular example the abnormal shaft movement is about 7 mm.

(23) When the shaft fails it acts on the plunger 102 and pushes it axially towards the first portion 110 of the magnetic circuit 104 and therefore reduces the air gap L.sub.g between the distal ends of the arm portions 116 and 118 and the second portion 112. Under this condition the reluctance, R, of the magnetic circuit 104 is significantly reduced causing a rapid increase of the magnetic flux, , in the circuit. The change in magnetic flux generates an electric signal in the detection coil 106 wound around the base portion 114.

(24) The voltage amplitude of the induced signal is proportional to the change of flux and is given by the formula:
V=d/dtK

(25) where K is a constant, is the magnetic flux in the circuit, and t is time.

(26) The magnetic flux is given by the formula.
=F/R=F/(L.sub.m/.sub.mA.sub.c+L.sub.g/.sub.gA.sub.c)

(27) where F is the magnetomotive force (MMF) and R is the reluctance.

(28) In the embodiment of FIGS. 1a and 1b, and as discussed above the MMF is generated by permanent magnet 116.

(29) The induced voltage signal in the detection coil 106 is in the form of a short pulse, for example a short pulse as shown in FIG. 2. This pulse is detected by the controller and compared to a threshold voltage. The threshold voltage is pre-set during configuration of the system at a level which is crossed when an abnormal movement of the shaft occurs. It is important that the threshold voltage is set at a level which does not result in false positives but also at a level which does not fail to determine when an abnormal movement occurs. On determining that the induced voltage in the detection coil has crossed the threshold voltage, the controller may send a signal to the ECU to shut off the engine. In one example, the controller bypasses the normal operation of the ECU and directly shuts off fuel supply to the engine.

(30) Abnormal movement caused by shaft failure occurs very rapidly, and must be controlled very quickly, within 1 or 2 ms, to prevent catastrophic damage to the gas turbine. As shown above, the voltage pulse generated in the detection coil is dependent on the rate of change of magnetic flux in the magnetic circuit. As such, the voltage generated by abnormal movement, which occurs over a shorter time period, and over a greater distance than normal movements during normal operation, is significantly larger than the voltage induced during normal operation. Unlike known abnormal movement detection systems, the present system is therefore sensitive to the rate of change of movement, and not to the absolute movement.

(31) The system of the present invention may therefore compensate for movements caused by wear on the turbine components during use. As will be appreciated, the maintenance period between bearing replacement may be 30,000 hours or more of engine running time, during which time the bearings will wear, enabling the shaft to move in the downstream direction when under load. The slow absolute movement of the shaft caused by wear will occur over a relatively long time period which, although resulting in a decrease in the reluctance, R, of the magnetic circuit, will not induce a voltage in the detection coil sufficient to cross the threshold voltage. Known abnormal movement detection systems, such as that of U.S. Pat. No. 6,607,349, may not compensate for such movements, and thus are more likely to produce false positives towards the end of the maintenance period when the distance that the shaft must move to break the link is reduced. Periods of increased, but normal movement, for example during acceleration and deceleration, may be particularly problematic.

(32) As discussed above, the environment in which the detection system is used is harsh, and may vibrations and other interferences can result in noise in the voltage signal induced in the detection coil. The controller 108 may therefore amplify the voltage signal, which may only be of the order or millivolts, and filter the signal before comparing the signal to the voltage threshold. Such amplification and filtering are well-known to those skilled in the art, and the specific configuration of such amplifiers and filters will be dependent on the design of the particular abnormal movement detection system, for example dependent on the physical size of the magnetic circuit. Any suitable voltage threshold detector may be used and are known to those skilled in the art.

(33) FIG. 3 is a schematic illustration of a system 300 for detecting abnormal movement of a gas turbine in accordance with a further embodiment of the invention. The system 300 is similar to that described with reference to FIGS. 1a and 1b, and like reference numerals refer to like components. The system 300 again comprises a plunger 102 mountable within a gas turbine engine (not shown). The system 300 further comprises a magnetic circuit, represented by dashed line 302, a detection coil 106 and a controller 108. In FIG. 3, the system is shown in the normal operating condition.

(34) The magnetic circuit 302 comprises a first portion 304, and the second portion 112. The first portion 304 comprises a base portion 114 and two arm portions 118 and 306. Each arm portion 118 and 306 has a proximal end, adjacent the base portion 114 and a free distal end. The second portion 112 is coupled to the plunger 102. In normal operation of the gas turbine, the system is configured to have an air gap, L.sub.g, between the free distal ends of the arm portions 118 and 306 and the second portion 112. In this respect, the system 300 is the same as system 100 as described above.

(35) The base portion 114 of the first portion of the magnetic circuit is formed of a magnetic material. As discussed above, the system operates in harsh and high temperature environments, and the materials used to form the various components of the system are chosen accordingly. The magnetic material is preferably a soft magnetic material, and preferably has a relatively high Curie temperature. Particularly appropriate materials are Cobalt, which has a Curie temperature of about 1128 degrees C., and Iron which has a Curie temperature of about 771 degrees C.

(36) The arm portion 118 is the same as described above with reference to FIGS. 1a and 1b. However, in the system 300 shown in FIG. 3, the MMF of the magnetic circuit 302 is provided by an electromagnet, and not by a permanent magnet. As such, arm portion 306 is formed from a magnetic material, which is preferably the same as the magnetic material used to form base portion 114 and arm portion 118. A coil 308 is wound around arm portion 306 to form the electromagnet. A power supply 310 is electrically coupled to the coil 308 for providing a current source to the coil to power the electromagnet, and thereby provide the MMF of the magnetic circuit 302.

(37) The coil 308 may be formed of the same or similar material to that described above as being suitable for the detection coil 108.

(38) The MMF, F, of the magnetic circuit 302 is therefore given by the formula:
F=ni

(39) where, n is the number of turns of the coil 308, and i is the current supplied by the power supply 310. In the embodiment shown in FIG. 3, the power supply 310 is configured to supply a constant current.

(40) The operation of the system 300 is the same as that of system 100 described above. Therefore, during an abnormal movement of the gas turbine shaft, the air gap L.sub.g between the distal ends of the arm portions 118 and 306 and the second portion 112 is reduced. Again, the reluctance, R, of the magnetic circuit 104 is significantly reduced causing a rapid increase of the magnetic flux, , in the circuit. The change in magnetic flux generates an electric signal in the detection coil 106 wound around the base portion 114. When the voltage of the electric signal crosses a pre-set threshold, an alarm is triggered, which as described above is used to initiate engine shut-down, for example by shutting off the fuel supply.

(41) In an alternative, yet similar, embodiment a system is provided where the MMF is provided by supplying a constant current to the detection coil 106 in this embodiment, as will be appreciated, the power supply 310 is preferably incorporated into the controller 108 and the coil 308 is not provided. All other components of the system, and the operation thereof, are the same as for system 300 described above with reference to FIG. 3. In this alternative embodiment, a filter, such as an electronic filter, may be used to filter out the induced voltage signal.

(42) A yet further embodiment of the invention utilises an alternating current source in the system 300, instead of the constant current source 310 described above. As such, the induced voltage signal in the detection coil 106 is given by the formula:
V=d/dtK=d{(ni)/(L.sub.m/.sub.mA.sub.c+L.sub.g/.sub.gA.sub.c)}/dtK

(43) where, i=i.sub.0 cos(t).

(44) The induced voltage signal in the detection coil 108 may be filtered to remove noise. The alternating current may have a frequency between about 50 Hz and around 20 kHz, and in one example the frequency is about 1 kHz. In this example a narrow band-pass filter is used centred about 1 kHz to remove noise induced by the harsh environment of the engine.

(45) FIG. 4 illustrates a system 400 for detecting abnormal movement in a gas turbine shaft of a yet further embodiment of the invention. The system 400 is similar to that of system 100 shown in FIGS. 1a and 1b, and like reference numerals refer to like components. As can be seen, the system 400 comprises a magnetic circuit 402 formed from the first portion 110, and a second portion 404. The second portion 404 is directly coupled to a last stage of the gas turbine disc 406. For example, the second portion 404 may be welded to the last stage of the gas turbine disc 406. The second portion 404 is balanced, and coupled to the turbine disc such that vibrations induced by the additional mass of the second portion 404 are minimised.

(46) The second portion 404 may be in the form of a circular disc, or a circular ring. The disc or ring preferably has an outer diameter substantially the same as the transverse width of the first portion 110 of the magnetic circuit. The second portion 404 is formed of a magnetic material and is similar to the second portion 112 described above.

(47) The detection coil 106, and controller are the same as those described above.

(48) The air gap, L.sub.g, in the magnetic circuit 402 ensures that the reluctance, R, of the circuit is high under normal operating conditions. When an abnormal movement of the shaft, or turbine disc, occurs, the air gap reduces, and as described above the reluctance significantly increases over a short period of time inducing a voltage in the coil 106.

(49) The system 400 is configured such that, even when an abnormal movement occurs, there is always an air gap between the distal ends of the arm portions 116 and 118 and the second portion 404 to prevent damage to the system.

(50) The above described systems may be compact, and may have overall axial length of between about 15 mm about 50 mm, preferably between about 20 mm and about 30 mm. As such, the compact system may be particularly suited to smaller engines, such as gas turbines for helicopters.

(51) The features of the embodiments described above with reference to the accompanying figures may be combined in any suitable manner. For example, the use of an electromagnet to provide the MMF in the magnetic circuit of system 400 is envisaged. Any other suitable combination of the above described features is also envisaged.