Turbine blade repair

Abstract: A method of repairing turbine blades (13, 14, 15) where it is required to repair a blade whilst it is in situ on a rotor involves the movement of a lacing wire (20) out of engagement with the blade to be repaired so that the blade may be repaired. The lacing wire may be completely removed from the array and replaced, or a new lacing wire member inserted by providing elongate holes or slots in the blade to enable the lacing wire member or members to be inserted into the blade array.

Description: The present invention relates to the repair of turbine blades and is particularly concerned with repair of turbine blades in which the turbine blade assembly has a plurality of blades interconnected by means of lacing wires, the lacing wires being wires or rods or other members that interconnect a plurality of blades by passing through holes in the blades, the purpose of the lacing wires being to prevent excessive relative movement between the blades and to generally dampen any vibration during operation of the turbine. As aforementioned, the lacing wires may be wires, rods, tubes or other members and will hereinafter be referred to for the sake of convenience as lacing wires. In use of turbines the blades are subjected to wear from contact with steam or particles carried by the steam which leads to erosion, particularly on the leading edge of the blade. In view of the extremely high forces to which the blades are subjected, other damage may occur in the form of cracks which may, necessitate complete removal and replacement of the turbine blade, or where the damage is not too severe, the damage can sometimes be rectified by repair to the blade. British patent specification No. 2,091,139 discloses a method of repairing a turbine blade, the method including the step of filling, a lacing wire hole with weld material prior to carrying out any welding or brazing operation, in the vicinity of the lacing wire hole. When the blade was subsequently subjected to a stress relieving heat treatment, the discontinuity afforded by the lacing wire holes had been eliminated, thereby preventing inbuilt stress being caused by the heat treatment process around the discontinuity of the lacing wire holes. Such a method of repair has been found highly satisfactory. However, problems occur when through improved techniques and equipment enabling repair of a turbine blade while the blade is still in position on the rotor, that in view of the proximity of adjacent blades, removal of the lacing wire from the lacing wire hole to enable the hole to be filled has been found to be impossible unless the lacing wire is cut out completely and then it is not possible, without removing the blades from the rotor, to insert new lacing wire. In practice, the lacing wire is made up of a plurality of pieces of material and in some cases the ends of the lacing wire pieces may be formed so as to overlap each other so as to permit of some relative movement between the lacing wire pieces. In other examples the lacing wire may be secured, for example by a tack weld or braze material, to each blade through which it passes and a small gap may be left between the ends of adjacent lacing wires so that the turbine blades are effectively laced in groups. In some cases it will not be necessary to fill the lacing wire hole. However, it may still be necessary to remove the lacing wire from the blade to enable a satisfactory repair to be carried out since, for example, access to the blade with the lacing wire in position may not be possible. It is an object of the present invention to provide a new method of repair of turbine blades. According to the present invention, we provide a method of repairing a turbine blade in a turbine blade array, said method comprising the steps of:- (a) removing the lacing wire from the or each blade to be repaired in the array; (b) carrying out a repair step on the or each blade to be repaired; (c) forming a hole in at least one turbine blade of a size enabling insertion of a new lacing wire member to said turbine blade array; (d) moving said lacing wire member around the array to a position out of contact with said blade in which said hole had been formed; (e) filling said hole; (f) moving said lacing wire member to its proper position; (g) remaking any connection between said lacing wire members with each other and with said blades. Preferably, where the repair step involves a welding or brazing operation, the blade is subjected to a heat treatment process to relieve stress in the blade caused by the welding or brazing operation carried out on the blade. In some cases it will be required to carry out repairs to more than one turbine blade and in these cases once a single blade has been repaired, and the lacing wires moved in a clockwise or anti-clockwise direction around the turbine blade array so that they are moved out of register with an adjacent turbine blade which may then be repaired and then each of the blades requiring repair may be repaired in turn. After all the blades have been repaired a new lacing wire member may be inserted. Preferably said hole is of elongate form and conveniently may comprise a slot extending from the lacing wire hole to either the leading edge or the trailing edge of a turbine blade. In some cases a blade adjacent to the blade which has been formed with a slot may be provided with an elongate hole or slot to assist in the insertion of a lacing wire member into said turbine blade array. Once an individual lacing wire member has been inserted into the array, it maybe moved around the array and further lacing wire members inserted until the lacing wire is complete. The lacing wire members will be moved into a position wherein they are initially out of contact with the blade or blades in which the slots have been formed to enable the filling of said slots and/or holes wherever the lacing wire members may be placed in their correct position and any required connections between individual lacing wire members and/or blades in the array may then be made. In some cases where the turbine blades in an array are in close proximity to each other, a combination of said holes or slots may be necessary to enable the removal of a lacing wire member. Preferably, if the repair to be carried out involves the application of considerable thermal energy, such as may occur during a welding or brazing operation for example, the blade must be subjected to a heat treatment process to relieve stress in the blade after said welding or brazing operation and prior to said welding or brazing operation said lacing wire hole will be filled with material so as to eliminate discontinuities in the blade to ameliorate said stress relieving heat treatment process. In some instances it is possible that only one or two blades, in an array of fifty or sixty blades for example, may need repair and it is envisaged that in such cases the work and time involved in disconnecting all the members forming the lacing wire so as to enable one or two blades to be freed from the lacing wire may be unnecessarily time consuming. It will be appreciated that in some cases in order to replace the lacing wire, some circumferential movement of the members forming the lacing wire will be necessary and it is also envisaged that in some cases it will be necessary to replace the lacing wire member in more than one piece to enable insertion through the lacing wire holes, after which such members will have to be joined in any suitable manner and could, for example, be joined by welding, brazing or the inclusion of a sleeve which may be welded Or brazed to the ends of the lacing wire member, or alternatively crimped in position. It has been found that removal of the lacing wire from an array of turbine blades can in many cases considerably facilitate repair in that it provides better access to the blades being repaired which is of considerable benefit when repairs in situ are carried out since the space available is very limited due to the presence of adjacent blades, and furthermore, removal of the lacing wire may permit Of more than one blade to be repaired at the same time and enables, for example, one person to repair a blade on one side of the array whilst another person is repairing a blade on the other side of the array. Since down time of the turbine is often important, it is essential to carry out the repair as quickly as possible which has considerable benefit in speeding up the repair process. The method of repair of the present invention will now be described in more detail with reference to the accompanying drawings, wherein:- FIGURE 1 is a schematic view of part of a turbine array; FIGURE 2 is a cross-section through the lacing wire shown in Figure 1; FIGURE 3 is a schematic view of the turbine blade array in which the lacing wires have been removed; FIGURE 4 is a schematic view of a turbine blade array with an alternative form of lacing wire; FIGURE 5 is a schematic view of a turbine blade array with a still further alternative lacing wire; FIGURE 6 is a view of a lacing wire in which a part has been removed; FIGURE 7 is a view of a joint to a lacing wire following removal of a piece thereof; FIGURE 8 is a perspective schematic view of three turbine blades, the lacing wire passing therethrough; FIGURE 9 is a view of the blades shown in Figure 8 following the formation of slots into the blades to enable release of the lacing wire. Referring first to Figure 1, the turbine blade array shown schematically comprises a rotor 10 having a shaft 11 with an axis of rotation 12. A series of turbine blades, three of which are shown at 13, 14 and 15 are attached to the shaft 11 by a root part 16, 17, 18. A lacing wire generally indicated at 20 is made from a plurality of different lacing wire members, e.g. 21, 22, 23, 24 etc., each of which may comprise D-section tube or rod as shown in Figure 2. The ends of each member of lacing wire are usually slightly bent so that any relative movement causes engagement of the end with a turbine blade to provent undue "rotation" of the lacing wire members. In order to remove the lacing wires from one of the blades, e.g. the blade 15 as shown in Figure 3, any connection between the lacing wire 20 or individual members forming the lacing wire 20 and the turbine blades is freed, for example if it was a tack weld the tack weld could be ground away, and the members forming the lacing wire are moved around the turbine blade array in a direction towards a position diametrically opposite to the rotational axis 12 from the blade 15. Since a small distance exists between the bent end portions of adjacent wires, by closing said gaps a much bigger gap can be created so that the lacing wires may be cleared from one blade 15. In some cases it will not be possible for there to be sufficient movement available to enable the lacing wire 20 to be clear of one blade and in such cases one or more of the members forming the lacing wire 20 may be cut to remove a piece thereof, which piece may be subsequently replaced or another piece inserted therefor which will be later described. Once the lacing wire 20 has been removed from a blade, for example the blade 15, to be repaired the blade may if required be removed from the rotor and if it is not required to be removed from the rotor, it may remain in place and the repair may be carried out in situ. The removal of the lacing wire in such manner enables the lacing wire hole to be filled prior to any stress relieving heat treatment of the blade. After the repair step has been carried out and the heat treatment process is over, the lacing wire hole may be re-drilled and the lacing wires moved in an opposite direction towards the blade 15 to take up their normal position, and any securing of the lacing wire members to the blades of the array may then take place. Referring now to Figure 4, an alternative lacing wire is shown in which the blades, e.g. 30, 31, 32, 33 of an array are secured in groups, in the example illustrated in groups of two. However, in practice they may be groups having a considerable number of turbine blades secured by a single lacing wire member, e.g. the blades 31 and 32 are secured relative to each other by lacing wire member 35. The lacing wire member 35 may be in the form of a rod or tube and may be secured to one, several or even all of the blades in the group for example by a tack weld securing the lacing wire to each blade. Such a weld is shown on the blades 31 and 32 at 36 and 37 respectively. In the example shown, gaps 38 and 39 are present between the ends of the lacing wire member 35 and adjacent lacing wire members 40 and 41 respectively, and in this case the gaps are sufficiently large and the total number of gaps around the array sufficient to enable movement of the lacing wire members in a direction diametrically opposite a blade to be repaired to enable at least one blade to have the lacing wire member removed completely therefrom to enable the repair to be carried out. In the example illustrated, since the lacing wires are secured to the blades, it will be necessary for such securement to be removed before movement of the lacing wire members can take place. Figure 5 shows a similar arrangement. However, in this case the gaps 50 and 51 between adjacent groups of blades tied by a respective lacing wire member 52, 53 and 54 are too small to permit one of the blades to have the lacing wire member completely removed therefrom even when all the members, for example those shown at 52, 53 and 54 forming the lacing wire are moved around the turbine blade array towards a position diametrically opposite to the blade to be repaired. In such cases, as shown in Figure 6, it will be necessary to remove a piece of lacing wire such as the piece 60 removed from lacing wire member 53, and the provision of an addition gap will enable movement of the lacing wire members so that a blade to be repaired may have the lacing wire removed completely therefrom and subsequent to the repair of the blade, and indeed any other blades that have to be repaired, a joining piece such as that shown at 61 may be secured to the lacing wire member 53 and welded thereto or brazed, crimped or in any other suitable way connected to the lacing wire 53 to bridge the gap formed by the piece that has been removed. It is further envisaged that by a slight increase in the gap between adjacent lacing wire members, it may not be necessary to provide a joining piece 61 and where this is the intention, the piece would be removed from the end of a lacing wire member rather than a position between its ends. It will be appreciated that the size of the piece removed would ensure that the lacing wire member is still of sufficient length to span the required number of blades. It is further envisaged that a small piece may be removed from more than one lacing wire so as to enable sufficient movement of the lacing wire members to enable one of the blades to be freed from the lacing wire so that repair may be effected. Referring now to Figure 8, three blades 60, 61 and 62 are shown, all being interconnected by a lacing wire member 63. Each of the blades 60, 61 and 62 has a hard metal shield 64 to 66 respectively, the hard metal shield being to minimise the effects of erosion and is commonly made of Stellite. The replacement of an erosion shield, such as those shown at 64, 65 and 66 is a not infrequent repair and it is usual to cut out the piece of material of the blade carrying the shield since usually, not only the shield but also part of the blade surrounding the shield, is also eroded and Figure 9 illustrates the blades 60, 61 and 62 in which the erosion shields have been removed. In order to also remove the lacing wire 63 so that the hole may be filled prior to heat treatment, a slot 67 and an oval hole 68 are formed in blades 60 and 61 respectively to enable some lateral movement of the lacing wire member 63 once the end 69 has been freed and by a combination of lateral movement and some deformation of the lacing wire member 63, it may be removed from the blades 60, 61 and 62 and others in the array through which it may extend. In the example shown, if it is only required to remove one lacing wire member, then since it is required to carry out heat treatment of any repaired blade while the lacing wire hole member is filled and obviously the slot 67 and oval hole 68 also filled, it is envisaged that the lacing wire member 63 will be replaced in more than one part to enable insertion into the re-formed lacing wire holes followed by joining of the parts to complete the lacing wire member 63. Apart from enabling a proper repair to be made once the lacing wire has been removed, a further very significant advantage is gained in that once the lacing wire is free of the blade, the blade may be set by the application of physical force into its correct position, or any other desired position without any force applied to the blade being transmitted either to the lacing wire or to adjacent blades.

Claims: A method of repairing a turbine blade in a turbine blade array, said method comprising the steps of:- (a) removing the lacing wire (63) from the or each blade (60,62) to be repaired in the array; (b) carrying out a repair step on the or each blade (60,62) to be repaired; (c) forming a hole (68) in at least one turbine blade (61) of a size enabling insertion of a new lacing wire member (63) to said turbine blade array; (d) moving said lacing wire member (63) around the array to a position out of contact with said blade in which said hole had been formed; (e) filling said hole (68); (f) moving said lacing wire member (63) to its proper position; (g) remaking any connection between said lacing wire members with each other and with said blades. A method according to claim 1 wherein said hole comprises a slot (67) extending either to the leading edge or the trailing edge of said turbine blade. A method of repairing a turbine blade according to claim 1 or claim 2 wherein said repair on the or each turbine blade is carried out while said turbine blade array (13-15) is connected to said rotor (20). A method of repairing a turbine blade according to any one of the preceding claims wherein the repair step involves a welding or brazing operation on the blade and further comprising the step of subjecting the blade (15) to a heat treatment process to relieve stress in the blade (15) caused by the welding or brazing operation.

Inventors: FRASER MICHAEL JAMES, FRASER, MICHAEL JAMES
Applicants: REFURBISHED TURBINE COMPONENTS, REFURBISHED TURBINE COMPONENTS LIMITED
Application year: 1989
Main classification: B23P6
IPC codes: F01D5, B23P6