AU682525B2 - Heat treatment apparatus for turbine blades - Google Patents
Heat treatment apparatus for turbine blades Download PDFInfo
- Publication number
- AU682525B2 AU682525B2 AU72328/94A AU7232894A AU682525B2 AU 682525 B2 AU682525 B2 AU 682525B2 AU 72328/94 A AU72328/94 A AU 72328/94A AU 7232894 A AU7232894 A AU 7232894A AU 682525 B2 AU682525 B2 AU 682525B2
- Authority
- AU
- Australia
- Prior art keywords
- support member
- heating
- heating elements
- heating apparatus
- blade
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Ceased
Links
Classifications
-
- H—ELECTRICITY
- H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
- H05B—ELECTRIC HEATING; ELECTRIC LIGHT SOURCES NOT OTHERWISE PROVIDED FOR; CIRCUIT ARRANGEMENTS FOR ELECTRIC LIGHT SOURCES, IN GENERAL
- H05B3/00—Ohmic-resistance heating
- H05B3/20—Heating elements having extended surface area substantially in a two-dimensional plane, e.g. plate-heater
- H05B3/34—Heating elements having extended surface area substantially in a two-dimensional plane, e.g. plate-heater flexible, e.g. heating nets or webs
-
- H—ELECTRICITY
- H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
- H05B—ELECTRIC HEATING; ELECTRIC LIGHT SOURCES NOT OTHERWISE PROVIDED FOR; CIRCUIT ARRANGEMENTS FOR ELECTRIC LIGHT SOURCES, IN GENERAL
- H05B3/00—Ohmic-resistance heating
- H05B3/02—Details
- H05B3/06—Heater elements structurally combined with coupling elements or holders
-
- H—ELECTRICITY
- H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
- H05B—ELECTRIC HEATING; ELECTRIC LIGHT SOURCES NOT OTHERWISE PROVIDED FOR; CIRCUIT ARRANGEMENTS FOR ELECTRIC LIGHT SOURCES, IN GENERAL
- H05B2203/00—Aspects relating to Ohmic resistive heating covered by group H05B3/00
- H05B2203/014—Heaters using resistive wires or cables not provided for in H05B3/54
Landscapes
- Turbine Rotor Nozzle Sealing (AREA)
- Heat Treatment Of Articles (AREA)
- Resistance Heating (AREA)
Description
WO 95/04444 PCT/GB94/01604 Title: "Heat treatment apparatus for turbine blades" The present invention relates to apparatus for the heat treatment of turbine blades.
Heat treatment of turbine blades is necessary for stress relief after repair of the blades, which repair step may involve the input of considerable heat such as occurs during welding or brazing and furthermore it has been found that in some cases where, for example, welding operations are carried out, heat treatment of the blade both prior to the welding operation and during the welding operation can also be advantageous in minimising stress and/or distortion that may occur to the blade during a welding operation.
British patent specification No. 2,144,361 discloses the attachment of electrically heated elements often referred to as heating mats to a turbine blade by means of wires which are used to secure the mats in position.
British patent application No. 9113755.4 discloses a glove type heater comprising two parts which may b'e pivotally connected together, the two parts carrying heating elements and being providing with slots to enable the glove to be slid over the turbine blade from an outer end, the slots accommodating protrusions such as snubbers.
The heater glove permits of a rapid and secure installation of heating elements to the turbine blade to enable stress relieving heat treatment to take place.
It has been found that in some cases, particularly with large free standing turbine blades, i.e. those not tied together by lacing wires, snubbers or the like, a change in the mass of metal per unit length between the tip of the blade and the area of the blade adjacent the root part is so great that a heater glove of the type shown in British application 9113755.4 may not always be entirely suitable.
it has also been found that for successful heat treatment to relieve stress in a repaired blade the temperatures to which various parts of the blade have to be heated and the length of time for which they are held at such temperatures can be very critical and the difference of just a few degrees from a desired temperature may be detrimental to successful stress relief.
It is an object of the present invention to provide a new or improved apparatus for the heat treatment of turbine blades.
According to one aspect of the present invention we provide heating apparatus adapted for the heat treatment of turbine blades, said heating apparatus including: a support member; a plurality of heating elements; connection means connecting the heating elements to said support member; the support member is flexible to enable it to conform to the shape of the part of the turbine blade to be heated.
the connection means permit the heating elements to be attachable and detachable from the support member, the connection means permitting of positional adjustment of said Sheating elements relative to said support member without detaching the heating elements from the support member.
20 Preferably the or each support member comprises a substantially planar member and, for example, may comprise a piece of relatively resilient steel which is capable of being resiliently deformed to a required shape without the application of any great force.
Conveniently said support member is provided with a variety of slots, said 25 heating elements may be provided with a plurality of holes and connection means in the form of pin-like members may be provided, the arrangement being 0 such that each said pin-like member passes through a respective slot in the support member, and through a hole in one of the heating elements, whereby the heating element may be moved relative to said support member whilst in a secured position by sliding the heating element and connection means relative to the support member in a direction longitudinally aligned with said slot.
Said connection means may comprise a pin similar to a cotter pin and washers may be provided at either end, one to prevent the heat passing through the slot and at the other end a washer may be provided and the ends of the cotter pin bent over so as to prevent separation of the heating elements from the support means.
Se *o 0 *e a a *e 0*
S.
_i WO 95/04444 PCT/GB94/01604 3 The relative adjustment provided by the support member and the heating elements enables different heating elements to be provided on different parts of the support member, it enables movement of one heating element relative to another perhaps to provide a gap to permit of access to a work area and in many cases it may be only necessary to have a single support member, heating means constituted by the heating elements collectively extending beyond a lateral edge of the support member whereby it may be folded over, assuming it is of the flexible type, to cover the other side of the turbine blade remote from that on which the heating means and support member is placed.
The support member may be located on one side of the turbine blade by any convenient means and may itself be provided with attachment means whereby it may be attached to the blade.
The attachment means may comprise a length of wire or other material that will not be adversely affected by the heat, a piece of wire passing around the heating means and if the blade is not surrounded by heating means, a surface of the blade, the two ends of the wire being twisted together to hold the heating apparatus in position. Alternatively, wires may be attached to the blade in a manner as described in British patent specification no. 2144361 to secure the heating apparatus to the blade. Alternatively, clips may be provided that have a surface engaging with the heating apparatus and a surface that engages with another heating apparatus or with a blade in a manner similar to that shown in British patent application no. 9113755.4.
The support member, plus the addition of a plurality of heating elements permits of many different combinations of heat input so as to enable different size and thicknesses of blades to be properly heated and whereby various parts of the blade can receive an adequate amount of heat and hence a proper heat treatment irrespective of the variation in thickness imparts to the blade. The provision of a support member only on one side of the blade not only satisfactorily holds and locates the heating means in the desired position but where the heating means extends laterally beyond an edge of the blade enables heat treatment on both sides of the blade whilst, if desired, by modifying the WO 95/04444 PCT/GB94/01604 4 shape of one or more heating means, allowing access for a repair operation to be carried out on the blade.
The present invention will now be described by way of example only with reference to the accompanying drawings, wherein: FIGURE 1 illustrates one embodiment of support member; FIGURE 2 is an illustration of part of a heating means; FIGURE 3 is a cross-sectional view of the heating means attached to the support member; FIGURE 4 is an illustration of a turbine blade on which the heating means has been positioned.
Referring to Figure 1, one embodiment of support member is shown and comprises a substantially planar member 10 which may for example be a piece of resilient steel approximately lmm thickiess and is formed with a series of slots 11 and holes 12.
The planar member 10 will have a certain amount of natural resilience so that it may be bent to conform approximately to fairly complex shapes that are found in turbine blades including concave and convex surfaces, the radii of which change along the length of the blade.
Figure 2 shows a typical heating means which comprises a plurality of ceramic elements 15, 16 for example, the ceramic elements being pivotally connected by connecting means 17, 18, 19 to adjacent ceramic heating means and 21, the ceramic elements 15, 16, 20 and 21 have electrically conductive heating wires passing therethrough, the wires passing through the pivotal connection means 17, 18 through which a current may be passed via a supply to terminals 22 and 23.
The pivotal connections provide a mat which may be easily folded to conform to the complex shapes of turbine blades.
The mats, such as the mat shown in Figure 2, are secured to the support member 10, for example by passing a cotter pin, such as the cotter pin shown at 25, through a slot such as the slot 11 in the support member 10 and through a hole, such as the hole 26 in the ceramic member
I
WO 95104444 PCT/GB94/01604 A washer 27 can be placed at the headed end 28 of the cotter pin and once the pin has been passed through the support member 10 and the ceramic member 15 the ends 30 and 31 can be bent over after a washer 32 has been placed over the ends. Thus the heating mat is secured firmly to the support member 10 but may be moved relative thereto along the direction of the slots by an amount equal to the length of the slots 11 which of course may be made of any desired length.
In addition to the adjustment along the length of the support member the heating mat may be fixed so that it extends only partially across the support member 10, fully across or may have a length whereby it considerably exceeds the width of the support member 10 thereby allowing the heating mat to be doubled over to provide additional heat on one side or possibly after the support member and heating mat has been brought into abutment with a turbine blade, folded over the blade to provide heat on the other side of the blade.
Referring now to Figure 4, a sketch of a heating apparatus in accordance with the present invention is shown around a turbine blade The turbine blade 35 has secured thereto the support member which carries a plurality of different heating mats such as the part of the heating mat shown in Figure 2 and it can be seen that along the length shown by arrow A, the heating mats are only on one side of the blade and not of a length so that they can be folded over the blade. Along the length B the heating mat is of a length whereby it can be folded right across the blade and that both sides of the blade will be provided with approximately equal heat. Along the length C there is no heating mat at all, this might be the case where it is actually desired to work with a welding apparatus, for example in the area C.
Along the length D the heating mats cover the underside of the blade fully but only partially cover the upper surface leaving a part free from any heating means.
The end length E is fully covered with a heating mat.
It will be appreciated that the illustration of Figure 4 is merely an example showing the variations that may be provided by the support means and WO 95/0 44 PCT/GB9401604 6 heating mats of the present invention in combination and which allow an almost universal variation in the heating means applied to the blade and hence the heat input to various parts of the blade so that the blade 35 as a whole may be subjected to a correct heat treatment whereby the various areas of the blade can be heated to a proper temperature and maintained at that temperature for desired lengths of time without variation of temperatures from a predetermined fairly narrow band.
It will be appreciated that whereas in the embodiment shown the support member has been secured to the underside or concave side of the blade, it may equally well be applied to the convex side of the blade and it is also envisaged that the heating mats may be of a length whereby they can be folded over to cover the whole of the blade but in the first preheat operation they may be left in a position whereby they heat one side of the blade only, the other half of the matter being allowed to hang away from the blade and this may continue during a welding operation on the blade and in a subsequent heat treatment operation some or all of the hanging ends of the mats may be brought into contact with the blade to effect proper heat treatment.
It is also envisaged that the support member may be provided with many different heating mats of different shapes and thicknesses and different heat outputs so as to provide for a large range of different heat outputs depending on the thickness and mass of metal of the blade at various positions along its length.
The features disclosed in the foregoing description, or the accompanying drawings, expressed in their specific forms or in the terms of means for performing the desired function, or a method or process for attaining the disclosed result, may, separately or in any combination of such features, be utilised for realising the invention in diverse forms thereof.
Claims (9)
1. Heating apparatus adapted for the heat treatment of turbine blades, said heating apparatus including: a support member; a plurality of heating elements; connection means connecting the heating elements to said support member; the support member is flexible to enable it to conform to the shape of the part of the turbine blade to be heated. the connection means permit the heating elements to be attachable and detachable from the support member, the connection means permitting of positional adjustment of said heating elements relative to said support member without detaching the heating elements from the support member.
2. Heating apparatus as claimed in Claim 1 wherein the support member includes a substantially planar member and is of a resilient material.
S3. Heating apparatus as claimed in Claim 2 wherein the support member includes a resilient steel capable of resilient deformation to a required shape.
4. Heating apparatus as claimed in any one of the preceding claims wherein the support member is provided with a plurality of slots and said heating elements or parts associated with said heating elements are provided with a plurality of holes and said connection means include pin-like members, the arrangement being that a pin-like member passes through a respective slot in the support member and through a hole in one of the heating elements or parts associated therewith enabling the heating elements to be moved relative to said support member whilst secured thereto in a direction aligned with said slot.
Heating apparatus as claimed in any one of the preceding claims 8 wherein said connection means includes a cotter pin and a pair of washers one of said washers provided to prevent the head passing through a slot provided in said support member and the other washer being provided adjacent to said heating elements or part associated therewith, the ends of said cotter pin being bent over in contact with said other washer, said cotter pin thereby maintaining the heating elements connected to said support means.
6. Heating apparatus as claimed in Claim 4 or Claim 5 wherein said pin-like member is of a length enabling a plurality of heating elements to be connected to a respective slot in said support member.
7. Heating apparatus as claimed in any one of the preceding claims wherein said support member is provided with a plurality of slots and a plurality of substantially annular holes.
8. Heating apparatus as claimed in any one of the preceding claims wherein said heating elements each include an electrically conductive element surrounded at least partially by insulating means in the form of a ceramic element.
9. Heating apparatus as claimed in any one of the preceding claims wherein attachment means are provided, the attachment means being adapted to attach the heating apparatus to a turbine blade. *V 9 Heating apparatus substantially as hereinbefore described with reference to and as illustrated in the accompanying drawings. DATED this 2nd day of July, 1997 TURBINE BLADING LIMITED WATERMARK PATENT TRADEMARK ATTORNEYS 4TH FLOOR, 263 ADELAIDE TERF- '1E PERTH, WESTERN AUSTRALIA, %00 AUSTRLAIA *4 a. :o
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB9315502 | 1993-07-27 | ||
GB939315502A GB9315502D0 (en) | 1993-07-27 | 1993-07-27 | Heat treatment apparatus for turbine blades |
PCT/GB1994/001604 WO1995004444A1 (en) | 1993-07-27 | 1994-07-25 | Heat treatment apparatus for turbine blades |
Publications (2)
Publication Number | Publication Date |
---|---|
AU7232894A AU7232894A (en) | 1995-02-28 |
AU682525B2 true AU682525B2 (en) | 1997-10-09 |
Family
ID=10739489
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
AU72328/94A Ceased AU682525B2 (en) | 1993-07-27 | 1994-07-25 | Heat treatment apparatus for turbine blades |
Country Status (6)
Country | Link |
---|---|
EP (1) | EP0711497A1 (en) |
JP (1) | JPH09501008A (en) |
AU (1) | AU682525B2 (en) |
CA (1) | CA2168239A1 (en) |
GB (2) | GB9315502D0 (en) |
WO (1) | WO1995004444A1 (en) |
Families Citing this family (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB9502905D0 (en) * | 1995-02-15 | 1995-04-05 | Dunlop Ltd | Ice protection device |
US20070158388A1 (en) * | 2006-01-06 | 2007-07-12 | Honeywell International, Inc. | Apparatus and method for welding superalloys |
DE102009040324B4 (en) * | 2009-09-05 | 2016-11-17 | MTU Aero Engines AG | Process for heat treatment of gas turbine blades |
US11242588B2 (en) | 2019-12-12 | 2022-02-08 | General Electric Company | System and method to apply multiple thermal treatments to workpiece and related turbomachine components |
US11199101B2 (en) | 2019-12-12 | 2021-12-14 | General Electric Company | System and method to apply multiple thermal treatments to workpiece and related turbomachine components |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0101164A2 (en) * | 1982-06-23 | 1984-02-22 | Refurbished Turbine Components Limited | Turbine blade repair |
GB2144361A (en) * | 1983-08-02 | 1985-03-06 | Refurbished Turbine Components | Improvements in or relating to methods of repair |
GB2257340A (en) * | 1991-06-25 | 1993-01-06 | Turbine Blading Ltd | Heat treating turbine blades |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1312580A (en) * | 1971-10-19 | 1973-04-04 | Electrothermal Eng Ltd | Electrical heating |
DE7235509U (en) * | 1972-09-27 | 1973-04-12 | Daimler Benz Ag | ELECTRICALLY HEATABLE MOTOR VEHICLE SEAT WITH PIPE UPHOLSTERY |
GB2033705B (en) * | 1978-09-29 | 1982-10-20 | Fisher J | Flexible heating elements |
GB2103059A (en) * | 1981-07-27 | 1983-02-09 | Royal Worcester Ind Ceramics L | Bead for a flexible heating assembly |
US5025137A (en) * | 1989-09-18 | 1991-06-18 | Ayrest Robert B | Thermoplastic heating apparatus |
-
1993
- 1993-07-27 GB GB939315502A patent/GB9315502D0/en active Pending
-
1994
- 1994-07-22 GB GB9414804A patent/GB2280580B/en not_active Expired - Fee Related
- 1994-07-25 AU AU72328/94A patent/AU682525B2/en not_active Ceased
- 1994-07-25 EP EP94921724A patent/EP0711497A1/en not_active Withdrawn
- 1994-07-25 JP JP7505643A patent/JPH09501008A/en active Pending
- 1994-07-25 WO PCT/GB1994/001604 patent/WO1995004444A1/en not_active Application Discontinuation
- 1994-07-25 CA CA 2168239 patent/CA2168239A1/en not_active Abandoned
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0101164A2 (en) * | 1982-06-23 | 1984-02-22 | Refurbished Turbine Components Limited | Turbine blade repair |
GB2144361A (en) * | 1983-08-02 | 1985-03-06 | Refurbished Turbine Components | Improvements in or relating to methods of repair |
GB2257340A (en) * | 1991-06-25 | 1993-01-06 | Turbine Blading Ltd | Heat treating turbine blades |
Also Published As
Publication number | Publication date |
---|---|
CA2168239A1 (en) | 1995-02-09 |
GB2280580A (en) | 1995-02-01 |
WO1995004444A1 (en) | 1995-02-09 |
GB9414804D0 (en) | 1994-09-14 |
AU7232894A (en) | 1995-02-28 |
GB9315502D0 (en) | 1993-09-08 |
GB2280580B (en) | 1997-02-26 |
EP0711497A1 (en) | 1996-05-15 |
JPH09501008A (en) | 1997-01-28 |
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