GB2227965A - Method and apparatus for drilling a shaped hole in a workpiece - Google Patents

Method and apparatus for drilling a shaped hole in a workpiece Download PDF

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Publication number
GB2227965A
GB2227965A GB8823874A GB8823874A GB2227965A GB 2227965 A GB2227965 A GB 2227965A GB 8823874 A GB8823874 A GB 8823874A GB 8823874 A GB8823874 A GB 8823874A GB 2227965 A GB2227965 A GB 2227965A
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GB
United Kingdom
Prior art keywords
workpiece
lens
axis
hole
mirror
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.)
Granted
Application number
GB8823874A
Other versions
GB2227965B (en
GB8823874D0 (en
Inventor
Arthur George Corfe
David Stroud
Jonathan Paul William Towill
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Rolls Royce PLC filed Critical Rolls Royce PLC
Priority to GB8823874A priority Critical patent/GB2227965B/en
Publication of GB8823874D0 publication Critical patent/GB8823874D0/en
Priority to US07/417,083 priority patent/US5043553A/en
Priority to DE3933448A priority patent/DE3933448C2/en
Priority to DE68926014T priority patent/DE68926014T2/en
Priority to EP89310322A priority patent/EP0365195B1/en
Priority to US07/417,971 priority patent/US4992025A/en
Priority to FR8913257A priority patent/FR2637524B1/en
Priority to JP1266086A priority patent/JPH02192890A/en
Publication of GB2227965A publication Critical patent/GB2227965A/en
Priority to US07/568,781 priority patent/US5096379A/en
Application granted granted Critical
Publication of GB2227965B publication Critical patent/GB2227965B/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • F01D5/22—Blade-to-blade connections, e.g. for damping vibrations
    • F01D5/225—Blade-to-blade connections, e.g. for damping vibrations by shrouding
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K26/00—Working by laser beam, e.g. welding, cutting or boring
    • B23K26/36—Removing material
    • B23K26/38—Removing material by boring or cutting
    • B23K26/382—Removing material by boring or cutting by boring
    • B23K26/384—Removing material by boring or cutting by boring of specially shaped holes
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K26/00—Working by laser beam, e.g. welding, cutting or boring
    • B23K26/36—Removing material
    • B23K26/38—Removing material by boring or cutting
    • B23K26/382—Removing material by boring or cutting by boring
    • B23K26/389—Removing material by boring or cutting by boring of fluid openings, e.g. nozzles, jets
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • F01D5/14—Form or construction
    • F01D5/18—Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
    • F01D5/186—Film cooling
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49316—Impeller making
    • Y10T29/49336—Blade making
    • Y10T29/49339—Hollow blade
    • Y10T29/49341—Hollow blade with cooling passage

Description

1 METHOD AND APPARATUS FOR DRILLING A SHAPED HOLE IN A WORKPIECE This
invention relates to a method and apparatus for drilling a shaped hole in a workpiece, in particular a f ilm-cooling hole in a blade or nozzle guide vane of a gas turbine engine. - The thermodynamic efficiency of a gas turbine engine increases with increased running temperature of the turbine. The known technique of f ilm-cooling permits a turbine to be run at a temperature (and hence at a high thermodynamic efficiency in excess of the maximum permissible operating temperature of the blades and nozzle guide vanes.
The technique of film-cooling works as follows. The turbine blade or nozzle guide vane is hollow in section and is provided with a large number of holes drilled through at the leading edge and at various positions along the chord. Cool air is forced into the root of the blade or nozzle guide vane and bleeds out through the cooling holes to form a thin film of cool air over the surface of the blade or nozzle guide. This thin film of cool air enables the surface of the blade or vane to remain at a temperature substantially below that of the ambient turbine gases. A gas turbine may therefore run at a temperature about 2000 above the melting temperature of the blades or vanes within the engine.
There are three principal methods of drilling cylindrical film-cooling holes, as follows, Electron discharge machining (EDM) uses an electrode with a low-voltage, high current power source to cut through the workpiece by spark erosion. Roles of 0.2 2 mm. diameter and larger can be produced, but the rate of cutting can be slow and tooling costs are very high.
Capillary drilling uses an electrode surrounded by a concentric glass capillary tube. An electrolyte is forced down the annular gap between the electrode and the capillary tube -so that when a voltage is applied across the electrode and workpiece, material is removed from the workpiece. Again, holes of 0.2 =m. diameter and larger can be produced, but the rate of cutting can be slow.
Since both EDM and capillary drilling involve electrical conduction through the workpiece it is only possible to drill metallic materials by means of these processes.
Laser machining uses a laser machine tool to focus a beam of high energy coherent radiation (laser light) at the workpiece surface, hence causing material to be vaporized and expelled. Through holes can be drilled either by focusing a stationary laser beam at a spot on the workpiece, or by trepanning. In trepanning, a continuous beam of laser light is passed through an optical system which causes the beam to describe a cylinder, typically in about one second. Hence the beam cuts out the hole around its edge rather than drilling through in one go. Holes with a diameter of 0. 25 mm. and larger can be drilled with the laser at much higher speeds than can be attained with the two previously described methods. Non- metallic materials may also be readily drilled with a laser beam.
The cylindrical cooling holes described above have disadvantages: it is difficult to arrange the cooling holes to provide an adequate flow of air without a risk of the film separating from the surface of the turbine 3 blade, and some cooling holes tend to become blocked. Both these effects reduce the efficiency of the cooling.
The disadvantages of cylindrical cooling holes may be overcome by providing a cooling hole that has a shaped exit. In particular, this type of hole has an exit area greater than the inlet area in oilder to diffuse the cooling air smoothly into an effective boundary layer.
Figure 1 is a section through a portion of a turbine blade 10 showing, in section, a cooling hole that has a cylindrical inlet 11 and a conical (fan-shaped in section) exit 12. The fan-shaped exit 12 enables the cooling air to diffuse smoothly into an effective boundary layer. The inlet 11 of the hole determines the flow rate through the hole. Since there is a tolerance on the wall thickness of the turbine blade it is not possible to define accurately the inlet area of a hole that is entirely conical from one side of the blade to the other.
Although the exit portion of the cooling hole may have any shape that has a larger exit area than the inlet area it is usually a cone or combination of a number of cones. Two suitable hole shapes are shown in perspective view in Figures.2 and 3. The hole of Figure 2 has an exit 12 which is a flattened cone (a "2-D" hole) and the hole of Figure 3 has an exit 12 which is a regular cone (a "3-W' hole).
Hitherto, the only techniques available for producing shaped exit holes as described herein are those based on EDM.
In one EDM technique a standard cylindrical electrode is oscillated lateraily during drilling, at an amplitude 1 4 which decreases towards the bottom of the hole. Clearly, this is a slow process.
In another technique an electrode is used which is nominally the same shape as that required for the hole. The electrode is moved linearly into the workpiece during drilling. Again, this is a slow process and each shaped electrode must be discarded after it has been used to drill a hole. A further disadvantage of EDM techniques is that they cannot be used to drill ceramic materials per se.
According- to a first aspect of the present invention there is provided a method of drilling a shaped hole in a workpiece by means of a laser beam, comprising, (a) directing the beam onto the workpiece, (b)-controlling the angle of the beam striking the workpiece relative to the axis of the hole, and (c) controlling the distance between the intersection of the beam with the surface of the workpiece and the axis of the hole.
Preferably, the method further comprises rotating the direction of the beam about the axis of the hole so as to describe at least part of the curved surface of a cone that has its vertex within. the body of the workpiece.
According to a second aspect of the present invention there is provided an apparatus for drilling a shaped hole in a workpiece by means of a laser beam emanating from a laser source, comprising, (a) means for directing the beam onto the workpiece, (b) means for controlling the angle of the beam -I striking the workpiece relative to the axis of the hole, and, (c) means for controlling the distance between the intersection of the beam with the surface of the workpiece and the axis of the hole, whereby the combination of the means for controlling the angle and the means for controlling the distance enables a shaped hole to be drilled in the workpiece by the laser beam.
Preferably, the apparatus further comprises means for rotating the direction of the beam about the axis of the hole so as to describe at least part of the curved surface of a cone that has its vertex within the body-of the workpiece.
The invention will now be described by way of example with reference to Figures 4 to 9 of the accompanying drawings, in which, Figure 4 is a schematic diagram of a first embodiment of an apparatus, including a lens, for drilling a shaped hole in a workpiece by means of a laser; Figure 5 is a diagrammatic perspective layout of components of the apparatus of Figure 4, excluding the lens and workpiece; Figures 6 to 8 are schematic diagrams of second, third and fourth embodiments, respectively, of apparatus for drilling a shaped hole in a workpiece by means of a laser; and Figure 9 shows a "double-cone" hole drilled in a workpiece by means of the invention.
6 Referring to the first embodiment of the invention in Figures 4 and 5 there is shown an apparatus 20 for drilling a shaped hole in a workpiece 22. The apparatus 20 comprises a source 24 to generate a beam 26 of highenergy coherent radiation (laser light), a convex lens 28 arranged to direct the beam onto the workpiece, the optical axis of the lens beingin alignment with the beam as it leaves the source, a set of mirrors 30, 32, 34, 36 in the light path of the beam between the source and the lens arranged to direct the beam onto the lens off-centre from and parallel to the optical axis. A protective cover slide 38 is located between the lens 28 and the workpiece 22 to piotect the lens from vapour or burning material given off by the workpiece when it is being drilled by the laser. The distance between the lens 28 and the workpiece 22 is controlled by motor means (not shown). The- workpiece 22 is positioned laterally so that the axis of the hole to be drilled is substantially in alignment with the laser beam 26 as it leaves the source 24.
Mirrors 30, 32 and 34 are fixed relative to each other and are arranged so as to turn the laser beam 26 through an angle of 90 0 relative to the optical axis of the lens 28, and to direc the beam towards the optical axis so as to strike mirror 36. Mirror 36 is arranged so to be movable to and from mirror 34 by motor means 40 in a direction orthogonal to the optical axis of the lens 28, and is angled relative to the optical axis of the lens so as to direct the beam 26 onto the lens in a direction parallel to the optical axis. On passing through the lens 28 the beam 26 is directed onto the workpiece 22, where the energy of the laser beam burns away or otherwise vaporizes the material of the workpiece.
k 1 t 7 A second position of mirror 36 along the direction orthogonal to the optical axis of the lens 28 is indicated by dashed lines 361, and the path of the laser beam from mirror position 361 through the lens onto the workpiece 22 is indicated by dashed lines 261. This second position of the mirror 36 is reached by actuating motor 40 so as to move the mirror 36 in a plane orthogonal to the optical axis of the lens. In the ncond position 361 the mirror directs the laser beam onto the lens at a different position (but still parallel to the optical axis of the lens) so that the beam is deflected by the lens and strikes the workpiece at a different angle and distance from the axis of the hole. The second position 361 is one of an infinite number of positions determined by control of the motor 40.
As shown in Figure 5, there is provided an aluminium base plate 42 of an inverted "L" section which carries on its top horizontal surface 46 bearings 44. The bearings 44 are coaxial with the beam 26 emanating from the laser source 24 and are clamped to the laser source by means of brackets (not shown). On the inside vertical face 48 of the "L" are attached the mirrors 30 - 36 and the motor 40 controlling lateral movement of mirror 36. The base plate 42 is able to rotate about the laser beam 26 emanating from the source 24 by means of the bearings 44. The rotation is controlled by a motor (not shown).
Mirror 36 is thus able to orbit about the axis of the hole to be drilled in a controlled f ashion and at a distance from the axis determined by motor 40. The laser beam 26 is consequently able to rotate about the axis of the hole, describing at least part of the curved surf ace of an imaginary cone the apex of which lies on or within the surface of the workpiece 22, and to drill 8 out a conical hole of predetermined angle in the workpiece.
Hence, by controlling (a) the lateral offset of mirror 36 from the optical axis of the lens, and therefore the angle at which the laser beam strikes the workpiece, (b) the distance between the lens and the workpiece, and therefore the depth of the hole to be drilled, and (c) the angle through which mirror 36 orbits about the axis of the hole, it is possible to drill in the workpiece a conical hole of controllable angle and size. By causing the mirror 36 to orbit through 360 0 a complete trepanning motion can be achieved.
The distance between the lens 28 and the workpiece- 22 may be varied by moving either the lens or the workpiece along their mutual axis.
If the mirror 36 is not orbited about the axis of the hole a "2-D" conical hole may be provided if required.
After a conical hole has been drilled it may be drilled through at its apex to provide a hole as shown in Figure 2 or 3. Further control of the laser beam by the mirrors 30 - 36 and the motors may provide a hole having an exit cone opposed to the entrance cone, as shown in Figure-9.
In a variant embodiment (not illustrated) of the invention of Figures 4 and 5 it may be preferred to move the lens by means of an X-Y table laterally relative to the axis of the hole, while keeping mirror 36 fixed relative to mirrors 30 - 34 and directly in alignment with the beam emanating from the source. It is also possible in this variant to dispense with the mirrors and to direct the beam from the source directly onto the lens. Thus cylindrical trepanning can be achieved.
9 It will be understood that throughout the description of this invention the term "mirror" includes not only a reflective surface but a prism designed to act as a reflective surface. Also, "convex lens" includes not only a double convex shape but also a plano-convex shape, and other lens shapes, or combinations of lens shapes, which have an overall convex effect. The lens may even be anamorphic or may consist of a finite number af prismatic elements. The lens may be designed to minimize astigmatism and spherical aberrations.
The embodiment of Figure 6 shows an arrangement whereby the laser beam 26 passes through a convex lens 6Q onto a fixed first prism 62 on the optical axis of the lens. The prism 62 reflects the beam onto a second prism 64 located laterally of the optical axis (the Z-axis) of the lens. The second prism 64 is arranged to translate along the X-axis (towards the optical axis) to alter cone depth, and to rotate about the Y-axis (to alter cone angle), whilst both prisms 62, 64 are coupled to rotate about the Z-axis to produce a trepanning motion. The beam then passes through a protective cover slide 66 onto the workpiece 22.
The embodiment of Figure 7 shows an arrangement of a convex lens 70, a hollow cylindrical mirror 76- and a prism 72. The cylindrical mirror 76 has its reflective surface on the inside and is coaxial with the optical axis (Z-axis) of the lens 70 which is positioned between the laser source 24 and the mirror. The prism 72 is located on the optical axis of the cylindrical mirror 76 (ie on the Z-axis). In operation the laser beam 26 emanating from the laser source 24 passes through the lens 70 along the Zaxis of the cylindrical mirror 76 and onto the prism 72. The prism 72 directs the beam 26 onto the reflective inside surface of the cylindrical mirror 76 from where it is reflected at an angle to the Z-axis through a protective cover slide 74 onto the workpiece 22. The prism 72 Ls able to rotate about the Z-axis to provide a trepanning motion, about a Y-axis to vary the approach angle, and to translate along the Z-axis to alter the cone depth.
The embodiment of Figure 8 shows an arrangement whereby the laser beam 26 passes through a convex lens 80 onto a prism 82 which deflects the beam through 90 0 to a second prism 84. The second prism 84 is able to translate along the X-axis and to rotate a limited amount (about 20 0) about its own X,Y-axes. Prisms 82, 84 are coupled to rotate a limited amount (about 200) about the Z-axis of the lens. The beam leaves prism 84 to pass through a cover slide 86 onto the workpiece 22. The axis of the hole and the lens 80 are parallel but not coincident.
Although the embodiments of Figures 6, 7 and 8 may be useful in specific circumstances it will be understood that they have individual disadvantages which make it difficult for them to have the general applicability of the embodiment of Figures 4 and 5.
The invention thus enables shaped holes to be drilled to very fine tolerances in metals and refractory materials, as are used in the manufacture of gas turbine components, using a high-energy laser beam, both economically and speedily.
z

Claims (22)

1. A method of drilling a shaped hole in a workpiece by means of a laser beam, comprising, (a) directing the beam onto the workpiece, (b) controlling the angle of the beam striking the workpiece relative to the axis of the hole, and (c) controlling the distance between the intersection of the beam with the surface of the workpiece and the axis of the hole.
2. A method as claimed in Claim 1 further comprising rotating the direction of the beam about the axis of the hole so as to describe at least part of the curved surface of a cone that has its vertex within the body of the workpiece.
3. A method as claimed in Claim 1 or 2 comprising controlling the angle of the beam striking the workpiece by passing the beam through a convex lens at a linear offset to the optical axis of the lens, and controlling the amount of offset.
4. A method as claimed in Claim 3 comprising controlling the distance between the intersection of the beam with the surface of the workpiece and the axis of the hole by controlling the distance between the lens and the workpiece.
5. A method as claimed in Claim 3 comprising first directing the beam onto a mirror and thence through the lens, and controlling the amount of offset by relative parallel movement between the lens and the mirror orthogonal to the axis of the lens.
12
6. A method as claimed in Claim 5 comprising providing said relative parallel movement by moving the mirror under control in a plane orthogonal to the axis of the lens.
7. A method as claimed in Claim 5 comprising providing said relative parallel movement by miving the lens under control in a plane orthogonal to the axis of the lens.
8. A method as claimed in Claim 3 comprising using the lens to focus the beam onto the workpiece by controlling the distance between the lens and the workpiece.
9. An apparatus for drilling a shaped hole in a workpiece by means of a laser beam emanating from a laser source, comprising, (a) means'for directing the beam onto the workpiece, (b) means for controlling the angle of the beam striking the workpiece relative to the axis of the hole, and, (c) means for controlling the distance between the intersection of the beam with the surface of the workpiece and the axis of the hole, whereby the combination of the means for controlling the angle and the means for c6ntrolling the distance enables a shaped hole to be drilled in the workpiece by the laser beam.
10. Apparatus as claimed in Claim 9 further comprising means for rotating the direction of the beam about the axis of the hole so as to describe at least part of the curved surface of a cone that has its vertex on or within the body of the workpiece.
11. Apparatus as claimed in Claim 9 or 10 wherein the means for controlling the angle of the beam striking the 1 -1 i workpiece relative to the axis of the hole and the means for controlling the distance between the intersection of the beam with the surface of the workpiece and the axis of the hole is provided by, (a) a convex lens, being also the means for directing the beam onto the workpiece, (b) means directing the beam onto the lens parallel to the optical axis of the lens, and (c) means for effecting lateral displacement between the point where the beam strikes the lens and the axis of the lens in a plane orthogonal to the optical axis of the lens so that the beam is thereby directed onto the workpiece at an angle determined by said lateral displacement.
12. Apparatus as claimed in Claim 11 wherein the means directing the beam onto the lens is a first mirror means.
13. Apparatus as claimed in Claim 12 wherein the laser beam emanating from the source is substantially coaxial with the optical axis of the lens, there being provided second mirror means arranged to provide a light path for the beam from the source to the first mirror means, said second mirror means being fixed relative to the beam emanating from the source.
14. Apparatus as claimed in Claim 13 wherein the second mirror means comprises an arrangeME!nt of at least one mirror arranged to direct the beam in a direction orthogonal to said optical axis.
15. Apparatus as claimed in Claim 14 wherein the arrangement comprises three mirrors fixed relative to each other.
14
16. Apparatus as claimed in Claim 11 wherein the means for effecting relative linear displacement is a motor arranged to move the first mirror means in said plane.
17. Apparatus as claimed in Claim 11 wherein the means for effecting relative linear displacement is a motor arranged to move the lens in said plane independently of any movement of the first mirror means.
18. Apparatus as claimed in Claim 11 as dependent on claim 10 wherein the first mirror means is arranged to orbit under control about the axis of the lens.
19. Apparatus as claimed in Claim 18 wherein a motor means is provided to enable the first mirror means to orbit about the axis of the lens.
20. A method of drilling a shaped hole in a workpiece by means of a laser beam, substantially as hereinbefore described with reference to Figures 4 to 8 of the accompanying drawings.
21. An apparatus for drilling a shaped hole in a workpiece by means of a laser beam, substantially as hereinbefore described with reference to Figures 4 and 5 of the accompanying drawings.
22. An apparatus for drilling a shaped hole in a workpiece by means of a laser beam, substantially as hereinbefore described with reference to any one of Figures 6 to 8 of the accompanying drawings.
Published 1990 at The Patent Office. State House. 66 71 High Holborn. London WC1R 4TP. Further copies mkvbe obtained from The Patent OfficeSales Branch. St Mary Cray. Orpington, Kent BR5 3RD- Printed by Multiplex techniques ltd. St MarY Cray. Kent. Con. 1,87
GB8823874A 1988-10-12 1988-10-12 Apparatus for drilling a shaped hole in a workpiece Expired - Fee Related GB2227965B (en)

Priority Applications (9)

Application Number Priority Date Filing Date Title
GB8823874A GB2227965B (en) 1988-10-12 1988-10-12 Apparatus for drilling a shaped hole in a workpiece
US07/417,083 US5043553A (en) 1988-10-12 1989-10-04 Method and apparatus for drilling a shaped hole in a workpiece
DE3933448A DE3933448C2 (en) 1988-10-12 1989-10-06 Method and device for drilling a specially shaped hole in a workpiece
DE68926014T DE68926014T2 (en) 1988-10-12 1989-10-09 Laser processing processes
EP89310322A EP0365195B1 (en) 1988-10-12 1989-10-09 Laser machining method
US07/417,971 US4992025A (en) 1988-10-12 1989-10-10 Film cooled components
FR8913257A FR2637524B1 (en) 1988-10-12 1989-10-11 METHOD AND DEVICE FOR DRILLING A PARTICULAR HOLE IN A FACTORY PART
JP1266086A JPH02192890A (en) 1988-10-12 1989-10-12 Method and apparatus for drilling work by laser beam
US07/568,781 US5096379A (en) 1988-10-12 1990-08-17 Film cooled components

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB8823874A GB2227965B (en) 1988-10-12 1988-10-12 Apparatus for drilling a shaped hole in a workpiece

Publications (3)

Publication Number Publication Date
GB8823874D0 GB8823874D0 (en) 1988-11-16
GB2227965A true GB2227965A (en) 1990-08-15
GB2227965B GB2227965B (en) 1993-02-10

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Family Applications (1)

Application Number Title Priority Date Filing Date
GB8823874A Expired - Fee Related GB2227965B (en) 1988-10-12 1988-10-12 Apparatus for drilling a shaped hole in a workpiece

Country Status (6)

Country Link
US (3) US5043553A (en)
EP (1) EP0365195B1 (en)
JP (1) JPH02192890A (en)
DE (2) DE3933448C2 (en)
FR (1) FR2637524B1 (en)
GB (1) GB2227965B (en)

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DE102007051408A1 (en) 2007-10-25 2009-05-28 Prelatec Gmbh Method for drilling holes of defined geometries by means of laser radiation
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DE68926014T2 (en) 1996-08-22
FR2637524B1 (en) 1993-12-10
EP0365195B1 (en) 1996-03-20
DE68926014D1 (en) 1996-04-25
US4992025A (en) 1991-02-12
US5096379A (en) 1992-03-17
EP0365195A2 (en) 1990-04-25
GB2227965B (en) 1993-02-10
EP0365195A3 (en) 1991-04-17
GB8823874D0 (en) 1988-11-16
US5043553A (en) 1991-08-27
DE3933448C2 (en) 1998-10-22
DE3933448A1 (en) 1990-05-03
FR2637524A1 (en) 1990-04-13
JPH02192890A (en) 1990-07-30

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