GB2428608A - A method for production of a set of holes by monitoring fluid flow - Google Patents

A method for production of a set of holes by monitoring fluid flow Download PDF

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Publication number
GB2428608A
GB2428608A GB0515772A GB0515772A GB2428608A GB 2428608 A GB2428608 A GB 2428608A GB 0515772 A GB0515772 A GB 0515772A GB 0515772 A GB0515772 A GB 0515772A GB 2428608 A GB2428608 A GB 2428608A
Authority
GB
United Kingdom
Prior art keywords
holes
fluid
flow
wall
treatment
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.)
Withdrawn
Application number
GB0515772A
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GB0515772D0 (en
Inventor
Ian Glendinning
Robin Mcmillan
Senior Peter
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.)
Siemens AG
Original Assignee
Siemens AG
Siemens Industrial Turbomachinery Ltd
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 Siemens AG, Siemens Industrial Turbomachinery Ltd filed Critical Siemens AG
Priority to GB0515772A priority Critical patent/GB2428608A/en
Publication of GB0515772D0 publication Critical patent/GB0515772D0/en
Priority to PCT/EP2006/064157 priority patent/WO2007014828A1/en
Priority to RU2008107947/02A priority patent/RU2008107947A/en
Priority to CNA2006800364459A priority patent/CN101277783A/en
Priority to EP06764150A priority patent/EP1910018A1/en
Publication of GB2428608A publication Critical patent/GB2428608A/en
Withdrawn legal-status Critical Current

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K37/00Auxiliary devices or processes, not specially adapted to a procedure covered by only one of the preceding main groups
    • B23K37/04Auxiliary devices or processes, not specially adapted to a procedure covered by only one of the preceding main groups for holding or positioning work
    • B23K37/053Auxiliary devices or processes, not specially adapted to a procedure covered by only one of the preceding main groups for holding or positioning work aligning cylindrical work; Clamping devices therefor
    • B23K37/0531Auxiliary devices or processes, not specially adapted to a procedure covered by only one of the preceding main groups for holding or positioning work aligning cylindrical work; Clamping devices therefor internal pipe alignment clamps
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23HWORKING OF METAL BY THE ACTION OF A HIGH CONCENTRATION OF ELECTRIC CURRENT ON A WORKPIECE USING AN ELECTRODE WHICH TAKES THE PLACE OF A TOOL; SUCH WORKING COMBINED WITH OTHER FORMS OF WORKING OF METAL
    • B23H9/00Machining specially adapted for treating particular metal objects or for obtaining special effects or results on metal objects
    • B23H9/14Making holes
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K26/00Working by laser beam, e.g. welding, cutting or boring
    • B23K26/02Positioning or observing the workpiece, e.g. with respect to the point of impact; Aligning, aiming or focusing the laser beam
    • B23K26/03Observing, e.g. monitoring, the workpiece
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K26/00Working by laser beam, e.g. welding, cutting or boring
    • B23K26/14Working by laser beam, e.g. welding, cutting or boring using a fluid stream, e.g. a jet of gas, in conjunction with the laser beam; Nozzles therefor
    • B23K26/142Working by laser beam, e.g. welding, cutting or boring using a fluid stream, e.g. a jet of gas, in conjunction with the laser beam; Nozzles therefor for the removal of by-products
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K26/00Working by laser beam, e.g. welding, cutting or boring
    • B23K26/36Removing material
    • B23K26/38Removing material by boring or cutting
    • B23K26/382Removing material by boring or cutting by boring
    • B23K26/389Removing material by boring or cutting by boring of fluid openings, e.g. nozzles, jets
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23PMETAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P13/00Making metal objects by operations essentially involving machining but not covered by a single other subclass
    • B23P13/02Making metal objects by operations essentially involving machining but not covered by a single other subclass in which only the machining operations are important
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23PMETAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P15/00Making specific metal objects by operations not covered by a single other subclass or a group in this subclass
    • B23P15/16Making specific metal objects by operations not covered by a single other subclass or a group in this subclass plates with holes of very small diameter, e.g. for spinning or burner nozzles
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23QDETAILS, COMPONENTS, OR ACCESSORIES FOR MACHINE TOOLS, e.g. ARRANGEMENTS FOR COPYING OR CONTROLLING; MACHINE TOOLS IN GENERAL CHARACTERISED BY THE CONSTRUCTION OF PARTICULAR DETAILS OR COMPONENTS; COMBINATIONS OR ASSOCIATIONS OF METAL-WORKING MACHINES, NOT DIRECTED TO A PARTICULAR RESULT
    • B23Q15/00Automatic control or regulation of feed movement, cutting velocity or position of tool or work
    • B23Q15/007Automatic control or regulation of feed movement, cutting velocity or position of tool or work while the tool acts upon the workpiece
    • B23Q15/12Adaptive control, i.e. adjusting itself to have a performance which is optimum according to a preassigned criterion
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23PMETAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P2700/00Indexing scheme relating to the articles being treated, e.g. manufactured, repaired, assembled, connected or other operations covered in the subgroups
    • B23P2700/06Cooling passages of turbine components, e.g. unblocking or preventing blocking of cooling passages of turbine components
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R2900/00Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
    • F23R2900/00018Manufacturing combustion chamber liners or subparts
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R2900/00Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
    • F23R2900/03041Effusion cooled combustion chamber walls or domes

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Optics & Photonics (AREA)
  • Mechanical Engineering (AREA)
  • Plasma & Fusion (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Thermal Sciences (AREA)
  • Laser Beam Processing (AREA)

Abstract

A method for production of a set of holes 10 through a wall 12 by treatment of the wall by forming and/or changing the cross-section of said holes, the holes having as a set a predetermined characteristic, comprises the steps of arranging for a fluid to flow through said holes at least during the last phase of said production while keeping said wall on the location for said treatment, monitoring said flow through the holes at least during the last phase of said production to monitor the progress of the production of said set of holes, and adapting said treatment to the result of said monitoring for obtaining said set of holes with said predetermined characteristic. The predetermined characteristic may be the total cross-sectional area of the holes, or a specific pressure drop for a specific mass flow at a certain feed pressure. The holes may be effusion cooling holes in a combustor can of a gas turbine. Preferably the holes may be formed by conventional drilling, laser burning, piercing, or other material converging/diverging measures. The method may also be applied to pre-existing holes, eg via coating. Sealing means 14,15 are also disclosed.

Description

A method and a device for production of a set of holes
TECHNICAL FIELD OF THE INVENTION AND PRIOR ART
The present invention relates to a method for production of a set of holes through a wall by treatment of the wall by forming and/or changing the cross-section of said holes, said holes having as a set a predetermined characteristic, as well as a de- vice for such a production.
"Production of a set of holes" is to be interpreted broadly and covers the formation of a set of holes through a wall by material diverging measures, i.e. by removing material, such as through conventional drilling or by laser burning, or material conserving measures such as displacing material by piercing, changing of the cross-section of already existing holes by increasing the cross-section thereof through diverging and/or conserving ma- chining or material converging measures decreasing the cross- section thereof by for instance partially coating the holes as well as all possible combinations of these types of treatments of the wall for obtaining a set of holes having a predetermined char- acteristic. Thus, some of the holes may for instance already be there and the production only consist of the formation of addi- tional holes for obtaining said set having a predetermined char- acteristic. "Predetermined characteristic" may for example be a predetermined total cross-section area of said holes or an effec- tive cross-section experienced by a flow through those holes.
The characteristic may also be a specific pressure drop for a specific mass flow at a certain feed pressure.
Furthermore, "wall" is also to be interpreted broadly and refers to any "wall-like" element and has not to be a real wall, but it may for instance be a turbine blade in a gas turbine.
The production of a set of holes in the form of effusion cooling holes in a combustor can for a gas turbine will now be described for illuminating the invention but not in any way limiting the scope thereof. The result of this production has a significant im- pact on cooling, operating temperature and emissions of the combustor of the gas turbine and the lifetime of downstream components in the turbine. It is known to produce such a set of holes by so-called laser drilling, which means mainly material diverging machining of the wall material by laser beam burning.
It is very important that these holes as a set has a predeter- mined characteristic, such as a predetermined total cross-sec- tion area, but also other parameters may be included in said predetermined characteristic, so as to obtain an optimum opera- tion of the combustor and the turbine. This issue is handled by taking the completed part to which said wall belongs to a sepa- rate test stand after it has been removed from the laser ma- chining centre and carrying out measurements thereon. When these measurements show a deviation from said predetermined characteristic of said set of holes correction of for instance the whole combustor assembly flow rate then takes place by for in- stance drilling trimming holes in adjacent parts such as the im- pingement sleeve.
A number of disadvantages are inherent in this way of proceed- ing. At least two operations are required with separate fixtures, which slows down the manufacturing process. There will be a significant variation between individual sub-parts having a said wall, since the set of holes of each sub-part will have different characteristics, so that inter-changeability is compromised. Ac- cordingly, one such sub-part may not be replaced by another, since said measurements have not been carried out on a sepa- rate such sub-part, but only for the entire combustor assembly.
Furthermore, as such sub-parts have to be trimmed and matched, there is an opportunity for mistaken assembly. Since the matching is for the assembly as a whole at a given test con- dition, there will still be flow split variation at conditions away from this condition, such as those which are experienced in the operation of the gas turbine.
A method of the type defined in the introduction is already known through US patent No. 6 408 610 disclosing a "method of adjusting gas turbine component cooling air flow", in which the production of a set of holes in a wall takes place by coating an area of the wall including existing holes, so that said holes are then partially coated and the cross-section thereof is changed.
After this has been done, the component having said set of holes is brought to a pressure flow stand, which is used to flow check the component. It is then checked whether the air flow is within a preselected range of desired cooling hole airflows.
When this is the case, the component is accepted for use and otherwise it is returned to a chamber for said coating procedure and subjected to further coating, whereupon it is flow checked again in said pressure flow stand. This method solves some of the problems mentioned above, but the production of said set of holes is still time consuming, rather complicated and in some situations not reliable enough.
SUMMARY OF THE INVENTION
The object of the present invention is to provide a method and a device of the type defined in the introduction solving the above problems of such methods and devices already known.
With respect to the method this object is according to the inven- tion obtained by providing such a method comprising the steps of arranging for a fluid to flow through said holes at least during the last phase of said production while keeping said wall on the location for said treatment, monitoring said flow through the holes at least during the last phase of said production to monitor the progress of the production of said set of holes, and adapting said treatment to the result of said monitoring for obtaining said set of holes with said predetermined characteristic.
By arranging for said flow through said holes and the monitoring thereof during the production of a set of holes while keeping the wall on the location for said treatment two operations, i.e. pro- duction and checking, are combined in one and no separate fix- tures are needed. This shortens the time for the production of said set of holes. The treatment will directly be adapted to the result of the monitoring so that a set of holes with said prede- termined characteristic will efficiently and reliably be obtained.
Furthermore, combining two operations into one will narrow the necessary tolerance band during production, and an analysis has shown a strong correlation between hardware temperatures and the width of the tolerance band in the case of combustor can cooling flow area.
It is pointed out that it may be arranged for said fluid flow during the entire phase of said production, while the monitoring only takes place during said last phase, which also includes the case of carrying out said monitoring as of a moment in which it is as- sumed that the set of holes has said predetermined characteris- tic, and when the assumption is correct, the adaption of said treatment will then simply mean that the treatment is stopped.
Other combinations of said arranging for the fluid flow and said monitoring thereof are also possible, and the invention also in- cludes the case of intermittently arranging for such a flow and/or monitoring such a flow as long as said wall is kept on the loca- tion for said treatment.
According to an embodiment of the invention said treatment is continued until one or more parameters of said flow substantially has assumed a predetermined value. Such parameters may for instance be pressure or mass flowrate of said flow.
According to a further embodiment it is arranged for a fluid to flow through said holes by applying a fluid to said holes with a substantially constant pressure, and said flow is monitored by measuring the mass flowrate of said fluid through said holes.
This way of proceeding is especially suitable when using a liq- uid, such as water, as said fluid.
According to another embodiment of the invention it is arranged for a fluid to flow through said holes by applying a fluid to said holes with a substantially constant mass flowrate, and said flow is monitored by measuring the pressure by which said fluid is applied to said holes, which advantageously may be carried out when using a gas, such as air, as said fluid.
According to another embodiment of the invention said treat- ment of the wall comprises material diverging and/or material conserving machining, such as drilling and piercing, respec- tivety. It has turned out that it may mostly be arranged for a fluid to flow through said holes during the actual treatment in the form of such machining for facilitating the control of the opera- tion for said production of the set of holes.
According to another embodiment of the invention the pressure by which said fluid is applied to said holes is selected so as to be able to eject possible debris, such as drilling debris, from the holes. This means that said flow being there for ensuring that a set of holes with said predetermined characteristic is obtained is also utilised for removing debris trapped in the holes, so that no extra operation is needed therefor.
According to another embodiment of the invention the mass flowrate by which said fluid is applied to said holes is selected so as to be able to eject possible debris, such as drilling debris, from the holes, which is a suitable way to proceed when using a liquid as said fluid.
According to another embodiment of the invention said fluid is applied to said holes in a pulsating manner so as to eject possi- ble debris, such as drilling debris, from the holes. This is a way of further improving the debris removing features of said fluid flow.
According to another embodiment of the invention said fluid is applied to said holes in alternating directions so as to eject pos- sible debris, such as drilling debris, from said holes.
According to another embodiment of the invention it is arranged for a fluid to flow through said holes during substantially the en- tire production of said set of holes for removing waste, such as drilling debris, from the holes formed and/or changed.
According to another embodiment of the invention it is arranged for a fluid to flow through said holes only during the last phase of the production of said set of holes, which is advantageous should there be a desire to avoid fluid flow through said holes earlier in the production process for instance to conserve fluid but not limited to this objective.
According to another embodiment of the invention before the step of arranging for a fluid to flow through said holes a de- burring or polishing of sharp edges in at least some of the holes formed or changed is carried out. This further improves the reli- ability of the method, since that treatment of the sharp edges will give the holes their final shape, and this is particularly ad- vantageous when this is carried out for the majority of the holes before the step of arranging for a fluid to flow through said holes.
According to another embodiment of the invention the method comprises a step of coating at least a portion of an area of said wall including existing said holes. It is then possible to let this coating step be a part of said treatment while partially coating at least some of existing holes for reducing the cross-section thereof. The coating may for example be metal and ceramic coating, but it also includes application of thermal paint or other paint.
According to another embodiment of the invention it is arranged for a fluid to flow through said holes during at least a part of said coating step. The flow of fluid may in this way be used for controlling the crosssection area of the holes thus coated, and it may even be controlled so that there will be no coating of the holes and the coating step will then not be a part of said treat- ment for the production of said set of holes. However, in the first case the arranging for a fluid to flow through said holes will in- fluence the result of the changing of the cross-section of the holes by said coating and accordingly itself be a part of said treatment.
According to another embodiment of. the invention a set of holes is produced in a wall in a component of a turbomachine. This component may for instance be a combustor can, a guide vane, a turbine blade, a heat shield, a burner or a cooling insert. The method is particularly advantageous for such components with respect to the problems discussed in the introduction of known methods for producing such components.
According to another embodiment of the invention a set of holes is produced in a wall of a component part of a combustor of a gas turbine, and this component part may for instance be a combustor can of a gas turbine, but quite different parts are con- ceivable, such as a burner. In the case of a can-like shape of said component part this may have any desired cross-section, such as circular and rectangular. However, the component part may just as well be an annular combustor.
According to another embodiment of the invention a set of holes is produced in a wall to be used for impingement cooling by flow of cooling fluid through said holes onto another component.
According to another embodiment of the invention a set of holes is produced through a wall of a member to be cooled by a flow of cooling fluid through said holes. The cooling may for this member be intended to be mainly obtained by the flow through said holes (effusion cooling) or by the passage of the cooling fluid along said wall before passing through said holes while providing a shield against hot fluid (film cooling).
According to another embodiment of the invention a set of holes is produced in a wall for later supply of a component, such as fuel, needed for a combustion in a space at least partially de- limited by said wall. This component may for instance be a burner and said space have an arbitrary cross-section.
According to another embodiment of the invention it is arranged for a fluid to flow through said holes by sealing a space on one side of said wall partially delimited by an area of said wall in which said set of holes is intended to be located and said flow is created through said holes by feeding said fluid into said space and through said holes out of said space or by feeding said fluid into said space through said holes. "Feeding" is intended to cover extracting, such as through suction, as well as supplying, such as blowing (in the case of a gas). By sealing a space and carry out said feeding in this way the monitoring of said feed flow for determining whether said set of holes has said prede- termined property may be easily and reliably carried out.
With respect to the device the object of the present invention is obtained by providing a device for production of a set of holes through a wall, said holes having as a set a predetermined characteristic, said device comprising an arrangement adapted to subject said wall to a treatment by forming and/or changing the cross-section of said holes, which is further characterized in that it comprises means for supplying a fluid to flow through said holes at least during the last phase of said production with said wall being on the location for said treatment, means adapted to monitor said flow through the holes at least during the last phase of said production by measuring at least one parameter thereof, means adapted to compare the results of said meas- urement of said monitoring means with a parameter indicative of said predetermined characteristic, and means adapted to control said arrangement for said treatment of the wall in dependence of the result of said comparison for obtaining said set of holes with said predetermined characteristic.
The function, results and advantages of such a device appear from the description above of the method according to the in- vention.
According to an embodiment of the invention said control means is adapted to control said arrangement to continue to carry out said treatment until one or more parameters of said flow sub- stantially has assumed.a predetermined value, in which these parameters may for instance be the pressure by which the fluid is applied to said holes or the mass flow of the fluid through said holes.
According to an embodiment of the invention the device com- prises means for sealing a space on one side of said wall par- tially delimited by an area of said wall in which said set of holes is intended to be located and including sealing members adapted to sealingly bear against said wall for creating said sealed space, and said supplying means is adapted to create a flow through said holes by feeding said fluid into said space and through said holes out of said space or by feeding said fluid into said space through said holes. Through such a device said set of holes may efficiently and reliably be created in any compo- nent having a said wall irrespectively of the shape of said com- ponent or wall.
According to a further embodiment of the invention constituting a further development of the embodiment last mentioned said arrangement is adapted to produce a said set of holes through walls forming an envelope surface of a can-like member, and said sealing means is adapted to create said sealed space by bearing circumferentially against the envelope surface of the can at both ends thereof by sealing members. The space may in this way be created either inside the can-like member by having the sealing members adapted to press against the inner enve- lope surface of the can-like member or externally thereof by having the sealing members adapted to press against the outer envelope surface of the can-like member.
According to another embodiment of the invention said ar- rangement is adapted to produce a said set of holes through walls forming an envelope surface of a can-like member, the de- vice also comprises holding means adapted to hold said can-like member fixed in place during said treatment by the action of in- flatable members upon said can-like member, and said holding means comprises means adapted to inflate said inflatable mem- bers and let gas out thereof for holding and releasing, respec- tively, said can-like member. By using this type of inflatable members as holding means an accurate geometrical location of said can-like member with an adequate resistance to machining forces may be obtained without damaging the can-like member and facilitating quick and easy fixing and releasing of the can- like member.
According to another embodiment of the invention said sealing members of said sealing means are formed by said inflatable members adapted to circumferentially press against the enve- lope surface of said can-like member when inflated. By combin- ing the inflatable members of the holding means and the sealing members the design and the operation of the device is simpli- fied.
According to another embodiment of the invention said inflatable members have leakage holes opening into said sealed space, and said supplying means is adapted to also act as said inflating means. This design combining the supplying means and the holding means simplifies the device by only requiring one supply line for both holding (fixing) said can-like member and supplying said fluid flow for monitoring the progress of the production of said set of holes.
Further advantages as well as advantageous features of the in- vention appear from the following description and the other de- pendent claims.
BRIEF DESCRIPTION OF THE DRAWINGS
With reference to the appended drawings, below follows a spe- cific description of embodiments of the invention cited as exam- ples.
In the drawings: Fig 1 is a schematic cross-section view through a part of a known gas turbine having components during the manufacture of which the method and the device ac- cording to the present invention may be applied, Fig 2 is a sketch very schematically illustrating a device ac- cording to a first embodiment of the invention, and Fig 3 is a view corresponding to that of fig 2 of a device ac- cording to a second embodiment of the invention.
DETAILED DESCRIPTION OF EMBODIMENTS OF THE INVEN-
TION
A known gas turbine as used in for instance a power plant is schematically illustrated in fig 1. The gas turbine has an air inlet 1 at one end followed by a compressor 2 for compressing the air from said inlet. Combustors 3 having a can-like shell are distrib- uted around the turbine shaft 4. Fuel is introduced into the re- spective combustor at 5 and is there mixed with a part of said air from the air inlet 1 for the combustion. Hot gases resulting from the combustion are driving the turbine blades 6 of the tur- bine part of the gas turbine and guided through guide vanes 7.
Parts of the gas turbine may be provided with a set of holes having as a set a predetermined characteristic, such as a pre- determined total cross-section area. These holes may be ap- plied for different reasons, such as for cooling. Thus, cooling air may for instance be introduced as a layer along the interior walls of each combustor can and escape through such holes for protecting the wall of the combustor can through so-called effu- sion cooling. Similar hotes may be arranged for use for film cooling in for instance some or all turbine blades 6 and/or guide vanes 7. A set of holes may also be arranged in an impingement sleeve very schematically indicated at 8 used for so-called im- pingement cooling of the outer walls of the combustors 3.
A device and a method for production of a said set of holes will now be described with reference to fig 2. It is illustrated how a combustor can 9 having a substantially circular cross-section is provided with a set of holes 10 having a predetermined charac- teristic by a device according to a first embodiment of the inven- tion. This device comprises an arrangement 11 in the form of a laser beam for treatment of the wall 12 of the combustor can 9 by substantially material diverging machining in the form of laser burning, so-called laser drilling. The device further comprises means for sealing a space 13 inside the combustor can partially delimited by an area of the wall 12 in which said set of holes is intended to be located. This sealing means comprises inflatable tyre-like members 14, 15 arranged at both ends of the combus- tor can 9 and adapted to circumferentially press against the in- ner envelope surface thereof when inflated as shown in fig 2.
The sealing means also comprises means 16 for supplying com- pressed air to said inflatable members. The inflatable members 14, 15 and the means 16 for supplying compressed air also con- stitutes a holding means adapted to hold said can-like member fixed in place during said treatment. The combustor can 9 is in this way fixed on a machine table 17 by being pressed down thereonto by said inflatable members. Release of the combustor can may easily be achieved by letting the air out of said inflat- able members.
The device further comprises means in the form of compressed air supplying means 18 for supplying a fluid to flow through said holes at least during the last phase of said production of the set of holes. In this case the fluid is air and is fed to the interior of the sealed space 13 for escaping through the holes 10. Another alternative would be to suck air from the exterior and into the space 13 through said holes 10. The device also comprises means schematically indicated at 19 adapted to monitor said fluid through the holes at least during the last phase of said production by measuring at least one parameter thereof, such as the pressure of the air inside said space 13. It is for instance possible to supply a fixed mass flow, preferably after a certain portion of the holes have been drilled, and then stop drilling when the pressure measured by the monitoring means 19 has changed to a correct fixed value. The mass flow may for a gas be established by measuring pressure differences and for a Iiq- uid by measuring the velocity of the liquid. Thus, 19 may stand for more than one sensor arranged on separate locations. The device comprises for this sake means 20 adapted to compare the results of said measurement of said monitoring means with a parameter indicative of said predetermined characteristic as well as means 21 adapted to control the arrangement 11 for said treatment of the wall in dependence of the result of this comparison for obtaining a set of holes with said predetermined characteristic.
The supplying means 18 may be adapted to supply said fluid to the space 13 and by that the holes in a pulsating manner so as to eject possible debris, such as drilling debris, from the holes.
The method for production of a set of holes having a predeter- mined property may through the use of this device be altered in many different ways as appear from the above discussion of the method according to the invention. One advantageous way to proceed is to drill so-called trimming holes, i.e. holes being less critical for the proper function of the set of holes for the later intended use thereof, during said last phase of the production of said set of holes. These holes may primarily be located close to the ends of the combustor can 9 as indicated by the holes 22 and 23. Sufficient cooling during the later use of the combustor can is in this way ensured where the component are most sensi- tive, whereas the number of holes in the end regions is not criti- cal and may be adapted to the result of said comparison.
It is shown how a shield 24 is arranged for preventing the laser beams from damaging the fixture part 25 therebehind intercon- necting the inflatable members 14, 15.
The air connections to the inflatable members and said space are preferably flexible, so that the machine table 17 can tray- erse/swivel past a fixed laser head of the arrangement 11.
Moreover, leaving the supply of fluid to said space flowing as the "holding fluid" is removed would pre-release or eject the can 9 for even easier handling.
Fig 3 schematically illustrates a device according to a second embodiment of the invention differing from that according to fig 2 only with respect to the holding means and the means for sup- plying fluid to flow through said set of holes, why only these parts will be further described here and the other parts have been provided with the same reference numerals as used for the embodiment according to fig 2. Said supplying means and holding means are here combined in one member 16' adapted to supply compressed air to the inflatable members 14, 15. How- ever, these members are provided with leakage holes 26, 27 through holes in the structure 25 holding said inflatable mem- bers. These holes 26, 27 allow a flow of fluid into the space 13 and out thereof through the holes 10 of said set of holes under production. The holes 26, 27 have to be dimensioned to ensure a higher holding pressure inside the inflatable members than the pressure resulting inside the space 13. The supply of fluid for said flow through the holes 10 and for holding the combustor can fixed in place and sealing the inner space thereof is in this way combined, which results in a simplified construction, i.e. a cheaper tooling fixture. The device according to this embodi- ment only works in blow-mode, with pressure and not mass flow control and imposes continuous operation throughout the machining through the arrangement 11. The leakage holes 26, 27 are in fact applied through a member connected to the inflatable members and enclosing a volume together therewith. The ex- pression "said inflatable members having leakage holes" does accordingly in this context also include such an arrangement of the leakage holes as shown in fig 3. "Inflatable" is in this disclo- sure to be interpreted to not only include inflating a member by a gas but also by a liquid for creating a volume change of said member.
The invention is of course not in any way restricted to the em- bodiments described above, but many possibilities to modifica- lions thereof would be apparent to a person with ordinary skill in the art without departingfrom the basic idea of the invention as defined in the appended claims.
As already mentioned, a set of holes may according to the in- vention be produced in the most different components for having various function in the later use of the respective component.
The number of holes in said set of holes may be arbitrary, which also apply to the pattern and size of said holes, and said set of holes may very well include holes of different sizes and shapes.
The holes may for instance have a square or conical shape.

Claims (48)

  1. Claims 1. A method for production of a set of holes (10) through a wall
    (12) by treatment of the wall by forming and/or chang- ing the cross-section of said holes, said holes having as a set a predetermined characteristic, the method comprising the steps of arranging for a fluid to flow through said holes at least during the last phase of said production while keeping said wall on the location for said treatment, monitoring said flow through the holes at least during the last phase of said production to monitor the progress of the production of said set of holes, and adapt- ing said treatment to the result of said monitoring for ob- taining said set of holes with said predetermined character- istic.
  2. 2. A method according to claim 1, in which said treatment is continued until one or more parameters of said flow sub- stantially has assumed a predetermined value.
  3. 3. A method according to claim 1 or 2, in which it is arranged for a fluid to flow through said holes by applying a fluid to said holes with a substantially constant pressure, and said flow is monitored by measuring the mass flowrate of said fluid through said holes.
  4. 4. A method according to claim 1 or 2, in which it is arranged for a fluid to flow through said holes by applying a fluid to said holes with a substantially constant mass flowrate, and said flow is monitored by measuring the pressure by which said fluid is applied to said holes.
  5. 5. A method according to any of the preceding claims, in which said treatment of the wall comprises material diverging and/or material conserving machining, such as drilling and piercing, respectively.
  6. 6. A method according to claim 5, in which said treatment comprises formation of holes through the wall by drilling.
  7. 7. A method according to claim 5 or 6, in which said treatment comprises said machining for increasing the cross-section of already existing holes.
  8. 8. A method according to any of claims 5-7, in which the pres- sure by which said fluid is applied to said holes is selected so as to be able to eject possible debris, such as drilling debris, from the holes.
  9. 9. A method according to any of claims 5-8, in which the mass flow by which said fluid is applied to said holes is selected so as to be able to eject possible debris, such as drilling debris, from the holes.
  10. 10. A method according to any of claims 5-9, in which said fluid is applied to said holes in a pulsating manner so as to eject possible debris, such as drilling debris, from the holes.
  11. 11. A method according to any of claims 5-10, in which said fluid is applied to said holes in alternating directions so as to eject possible debris, such as drilling debris, from said holes.
  12. 12. A method according to any of the preceding claims, in which it is arranged for a fluid to flow through said holes during substantially the entire production of said set of holes for removing waste, such as drilling debris, from the holes formed and/or changed.
  13. 13. A method according to any of claims 1-11, in which it is ar- ranged for a fluid to flow through said holes only during the last phase of the production of said set of holes.
  14. 14. A method according to claim 13, in which before the step of arranging for a fluid to flow through said holes a deburring or polishing of sharp edges in at least some of the holes formed or changed is carried out.
  15. 15. A method according to any of the preceding claims, in which it comprises a step of coating at least a portion of an area of said wall including existing said holes.
  16. 16. A method according to claim 15, in which it is arranged for a fluid to flow through said holes during at least a part of said coating step.
  17. 17. A method according to claim 15 or 16, in which said treat- ment comprises the step of partially coating at least some of existing holes by said coating step for reducing the cross- section thereof.
  18. 18. A method according to any of the preceding claims, in which holes being less critical for the proper function of the set of holes for the later intended use thereof are formed and/or changed with respect to the cross-section during said last phase.
  19. 19. A method according to any of the preceding claims, in which it is arranged for a fluid in the form of a gas to flow through said holes.
  20. 20. A method according to claim 19, in which said gas is air.
  21. 21. A method according to any of claims 1-18, in which it is ar- ranged for a fluid in the form of a liquid to flow through said holes.
  22. 22. A method according to claim 21, in which said liquid is wa- ter.
  23. 23. A method according to any of the preceding claims, in which a set of holes is produced in a wall in a component of a tur- bomachine.
  24. 24. A method according to claim 23, in which a set of holes is produced in a wall in a component of a gas turbine.
  25. 25. A method according to claim 24, in which a set of holes is produced in a wall of a component part of a combustor of a gas turbine.
  26. 26. A method according to claim 25, in which a set of holes is produced in a wall of a combustor can of a gas turbine.
  27. 27. A method according to claim 24, in which a set of holes is produced in a wall to be used for impingement cooling by a flow of cooling fluid through said holes onto another com- ponent.
  28. 28. A method according to any of the preceding claims, in which a set of holes is produced through a wall of a member to be cooled by a flow of a cooling fluid through said holes.
  29. 29. A method according to any of the preceding claims, in which a set of holes is produced in a wall for later supply of a component, such as fuel, needed for a combustion in a space at least partially delimited by said wall.
  30. 30. A method according to any of the preceding claims, in which it is arranged for a fluid to flow through said holes (10) by sealing a space (13) on one side of said wall partially de- limited by an area of said wall in which said set of holes is intended to be located, and said flow is created through said holes by feeding said fluid into said space and through said holes out of said space or by feeding said fluid into said space through said holes.
  31. 31. A device for production of a set of holes through a wall, said holes having as a set a predetermined characteristic, said device comprising an arrangement (11) adapted to subject said wall (12) to a treatment by forming and/or changing the cross-section of said holes (10), characterized in that the device further comprises means (18, 16') for supplying a fluid to flow through said holes at least during the last phase of said production with said wall being on the loca- tion for said treatment, means (19) adapted to monitor said flow through the holes at least during the last phase of said production by measuring at least one parameter thereof, means (20) adapted to compare the results of said measurement of said monitoring means with a parameter indica- tive of said predetermined characteristic, and means (21) adapted to control said arrangement (11) for said treatment of the wall in dependence of the result of said comparison for obtaining said set of holes with said predetermined characteristic.
  32. 32. A device according to claim 31, characterized in that said control means (21) is adapted to control said arrangement (11) to continue to carry out said treatment until one or more parameters of said flow substantially has assumed a predetermined value.
  33. 33. A device according to claim 31 or 32, characterized in that said supplying means (16', 18) is adapted to supply a fluid to said holes with a substantially constant pressure, and that said monitoring means (19) is adapted to measure the mass flow of said fluid through said holes.
  34. 34. A device according to claim 31 or 32, characterized in that said supplying means (16', 18) is adapted to supply a fluid to said holes with a substantially constant mass flow, and that said monitoring means (19) is adapted to measure the pressure by which said fluid is supplied to said holes.
  35. 35. A device according to any of claims 31-34, characterized in that said arrangement (11) comprises material diverging and/or material conserving machining means, such as drill- ing means and piercing means, respectively.
  36. 36. A device according to claim 35, characterized in that said supplying means (16', 18) is adapted to apply said fluid to said holes with a pressure able to eject possible debris, such as drilling debris, from the holes.
  37. 37. A device according to claim 35, characterized in that said supplying means (16', 18) is adapted to supply said fluid to said holes with a mass flow able to eject possible debris, such as drilling debris, from the holes.
  38. 38. A device according to any of claims 35-37, characterized in that said supplying means (16', 18) is adapted to supply said fluid to said holes in a pulsating manner so as to eject possible debris, such as drilling debris, from the holes.
  39. 39. A device according to any of claims 35-38, characterized in that said supplying means (18) is adapted to supply said fluid to said holes in alternating directions so as to eject possible debris, such as drilling debris, from said holes.
  40. 40. A device according to any of claims 31-39, characterized in that said arrangement comprises means adapted to apply a material for coating purposes to at least a portion of an area of said wall including existing said holes.
  41. 41. A device according to claim 40, characterized in that said supplying means (16', 18) is adapted to supply a fluid to flow through said holes during at least a part said coating step.
  42. 42. A device according to claim 40 or 41, characterized in that said material applying means is adapted to partially coat at least some of existing holes for reducing the cross-section thereof.
  43. 43. A device according to any of claims 31-42, characterized in that it comprises means (14, 15) for sealing a space (13) on one side of said wall partially delimited by an area of said wall in which said set of holes is intended to be located and including sealing members (14, 15) adapted to sealingly bear against said wall for creating said sealed space, and that said supplying means (16', 18) is adapted to create a flow through said holes by feeding said fluid into said space and through said holes out of said space or by feeding said fluid into said space through said holes.
  44. 44. A device according to claim 43, characterized in that said arrangement (11) is adapted to produce a said set of holes through walls forming an envelope surface of a can-like member (9), and that said sealing means is adapted to cre- ate said sealed space by bearing circumferentially against the envelope surface of the can at both ends thereof by sealing members (14, 15).
  45. 45. A device according to claim 43 or 44, characterized in that said arrangement (11) is adapted to produce a said set of holes through walls forming an envelope surface of a can- like member (9), that the device also comprises holding means (14-16) adapted to hold said can-like member fixed in place during said treatment by the action of inflatable members (14, 15) upon said can-like member, and that said holding means comprises means (16, 16') adapted to inflate said inflatable members and let gas out thereof for holding and releasing, respectively, said can-like member.
  46. 46. A device according to claims 44 and 45, characterized in that said sealing members of said sealing means are formed by said inflatable members (14, 15) adapted to circumferen- tially press against the envelope surface of said can-like member (9) when inflated.
  47. 47. A device according to claim 46, characterized in that said inflatable members (14, 15) have leakage holes (26, 27) opening into said sealed space (13), and that said supplying means (16') is adapted to also act as said inflating means.
  48. 48. A device according to any of claims 44-47, characterized in that said sealing members (14, 15) of the sealing means are adapted to press against the inner envelope surface of the can-like member (9) at both open ends thereof for creating said space (13) inside said can-like member. (J
    48. A device according to any of claims 44-47, characterized in that said sealing members (14, 15) of the sealing means are adapted to press against the inner envelope surface of the can-like member (9) at both open ends thereof for creating said space (13) inside said can-like member.
    Amendments to the claims have been filed as follows Claims 1. A method for production of a set of holes (10) through a waIl (12), said holes having as a set a predetermined characteristic, the method comprising the steps of: (I) treating the wall by forming and/or changing the cross- section of said holes; (ii) in addition to step (i) and at the same time as carrying out step (i), arranging for a fluid to flow through said holes at least during the last phase of said production while keeping said wall in the location for said treatment; (iii) monitoring said flow through the holes at least during the last phase of said production to monitor the progress of the production of said set of holes; and (iv) adapting said treatment to the result of said monitoring for obtaining said set of holes with said predetermined characteristic.
    2. A method according to claim 1, in which said treatment is continued until one or more parameters of said flow sub- stantially has assumed a predetermined value.
    3. A method according to claim I or 2, in which it is arranged for a fluid to flow through said holes by applying a fluid to said holes with a substantially constant pressure, and said flow is monitored by measuring the mass flowrate of said fluid through said holes.
    4. A method according to claim I or 2, in which it is arranged for a fluid to flow through said holes by applying a fluid to said holes with a substantially constant mass flowrate, and said flow is monitored by measuring the pressure by which said fluid is applied to said holes.
    5. A method according to any of the preceding claims, in which said treatment of the wall comprises material diverging 2' and/or material conserving machining, such as drilling and piercing, respectively.
    6. A method according to claim 5, in which said treatment comprises formation of holes through the wall by drilling.
    7. A method according to claim 5 or 6, in which said treatment comprises said machining for increasing the cross-section of already existing holes.
    8. A method according to any of claims 5-7, in which the pres- sure by which said fluid is applied to said holes is selected so as to be able to eject possible debris, such as drilling debris, from the holes.
    9. A method according to any of claims 5-8, in which the mass flow by which said fluid is applied to said holes is selected so as to be able to eject possible debris, such as drilling debris, from the holes.
    10. A method according to any of claims 5-9, in which said fluid is applied to said holes in a pulsating manner so as to eject possible debris, such as drilling debris, from the holes.
    11. A method according to any of claims 5-10, in which said fluid is applied to said holes in alternating directions so as to eject possible debris, such as drilling debris, from said holes.
    12. A method according to any of the preceding claims, in which it is arranged for a fluid to flow through said holes during substantially the entire production of said set of holes for removing waste, such as drilling debris, from the holes formed and/or changed.
    13. A method according to any of claims 1-11, in which it is ar- ranged for a fluid to flow through said holes only during the last phase of the production of said set of holes.
    14. A method according to claim 13, in which before the step of arranging for a fluid to flow through said holes a deburring or polishing of sharp edges in at least some of the holes formed or changed is carried out.
    15. A method according to any of the preceding claims, in which it comprises a step of coating at least a portion of an area of said wall including existing said holes.
    16. A method according to claim 15, in which it is arranged for a fluid to flow through said holes during at least a part of said coating step.
    17. A method according to claim 15 or 16, in which said treat- ment comprises the step of partially coating at least some of existing holes by said coating step for reducing the cross- section thereof.
    18. A method according to any of the preceding claims, in which holes being less critical for the proper function of the set of holes for the later intended use thereof are formed and/or changed with respect to the cross-section during said last phase.
    19. A method according to any of the preceding claims, in which it is arranged for a fluid in the form of a gas to flow through said holes.
    20. A method according to claim 19, in which said gas is air. (((C 25L
    21. A method according to any of claims 1-18, in which it is ar- ranged for a fluid in the form of a liquid to flow through said holes.
    22. A method according to claim 21, in which said liquid is wa- ter.
    23. A method according to any of the preceding claims, in which a set of holes is produced in a wall in a component of a tur- bomachine.
    24. A method according to claim 23, in which a set of holes is produced in a wall in a component of a gas turbine.
    25. A method according to claim 24, in which a set of holes is produced in a wall of a component part of a combustor of a gas turbine.
    26. A method according to claim 25, in which a set of holes is produced in a wall of a combustor can of a gas turbine.
    27. A method according to claim 24, in which a set of holes is produced in a wall to be used for impingement cooling by a flow of cooling fluid through said holes onto another com- ponent.
    28. A method according to any of the preceding claims, in which a set of holes is produced through a wall of a member to be cooled by a flow of a cooling fluid through said holes.
    29. A method according to any of the preceding claims, in which a set of holes is produced in a wall for later supply of a component, such as fuel, needed for a combustion in a space at least partially delimited by said wall.
    30. A method according to any of the preceding claims, in which it is arranged for a fluid to flow through said holes (10) by sealing a space (13) on one side of said wall partially de- limited by an area of said wall in which said set of holes is intended to be located, and said flow is created through said holes by feeding said fluid into said space and through said holes out of said space or by feeding said fluid into said space through said holes.
    31. A device for production of a set of holes through a wall, said holes having as a set a predetermined characteristic, said device comprising: an arrangement (11) adapted to subject said wall (12) to a treatment to form and/or change the cross-section of said holes (10); in addition to said arrangement (11), means (18, 16') for supplying a fluid to flow through said holes at least during the last phase of said production with said wall being in the location for said treatment, said means (18, 16') being configured to supply the fluid at the same time as said arrangement (11) subjects said wall to the treatment; means (19) adapted to monitor said flow through the holes at least during the last phase of said production by measuring at least one parameter thereof; means (20) adapted to compare the results of said measurement of said monitoring means with a parameter in- dicative of said predetermined characteristic; and means (21) adapted to control said arrangement (11) for said treat- ment of the wall in dependence of the result of said com- parison for obtaining said set of holes with said predeter- mined characteristic. 30
    32. A device according to claim 31, characterized in that said control means (21) is adapted to control said arrangement (11) to continue to carry out said treatment until one or more parameters of said flow substantially has assumed a predetermined value.
    33. A device according to claim 31 or 32, characterized in that said supplying means (16', 18) is adapted to supply a fluid to said holes with a substantially constant pressure, and that said monitoring means (19) is adapted to measure the mass flow of said fluid through said holes.
    34. A device according to claim 31 or 32, characterized in that said supplying means (16', 18) is adapted to supply a fluid to said holes with a substantially constant mass flow, and that said monitoring means (19) is adapted to measure the pressure by which said fluid is supplied to said holes.
    35. A device according to any of claims 3 1-34, characterized in that said arrangement (11) comprises material diverging and/or material conserving machining means, such as drill- ing means and piercing means, respectively.
    36. A device according to claim 35, characterized in that said supplying means (16', 18) is adapted to apply said fluid to said holes with a pressure able to eject possible debris, such as drilling debris, from the holes.
    37. A device according to claim 35, characterized in that said supplying means (16', 18) is adapted to supply said fluid to said holes with a mass flow able to eject possible debris, such as drilling debris, from the holes.
    38. A device according to any of claims 35-37, characterized in that said supplying means (16', 18) is adapted to supply said fluid to said holes in a pulsating manner so as to eject possible debris, such as drilling debris, from the holes.
    39. A device according to any of claims 35-38, characterized in that said supplying means (18) is adapted to supply said fluid to said holes in alternating directions so as to eject possible debris, such as drilling debris, from said holes.
    I
    40. A device according to any of claims 31-39, characterized in that said arrangement comprises means adapted to apply a material for coating purposes to at least a portion of an area of said wall including existing said holes.
    41. A device according to claim 40, characterized in that said supplying means (16', 18) is adapted to supply a fluid to flow through said holes during at least a part said coating step.
    42. A device according to claim 40 or 41, characterized in that said material applying means is adapted to partially coat at least some of existing holes for reducing the cross-section thereof.
    43. A device according to any of claims 31-42, characterized in that it comprises means (14, 15) for sealing a space (13) on one side of said wall partially delimited by an area of said wall in which said set of holes is intended to be located and including sealing members (14, 15) adapted to sealingly bear against said wall for creating said sealed space, and that said supplying means (16', 18) is adapted to create a flow through said holes by feeding said fluid into said space and through said holes out of said space or by feeding said fluid into said space through said holes.
    44. A device according to claim 43, characterized in that said arrangement (11) is adapted to produce a said set of holes through walls forming an envelope surface of a can-like member (9), and that said sealing means is adapted to cre- ate said sealed space by bearing circumferentially against the envelope surface of the can at both ends thereof by sealing members (14, 15).
    45. A device according to claim 43 or 44, characterized in that said arrangement (11) is adapted to produce a said set of holes through walls forming an envelope surface of a can- like member (9), that the device also comprises holding means (14-16) adapted to hold said can-like member fixed in place during said treatment by the action of inflatable members (14, 15) upon said can-like member, and that said holding means comprises means (16, 16') adapted to inflate said inflatable members and let gas out thereof for holding and releasing, respectively, said can-like member.
    46. A device according to claims 44 and 45, characterized in that said sealing members of said sealing means are formed by said inflatable members (14, 15) adapted to circumferen- tially press against the envelope surface of said can-like member (9) when inflated.
    47. A device according to claim 46, characterized in that said inflatable members (14, 15) have leakage holes (26, 27) opening into said sealed space (13), and that said supplying means (16') is adapted to also act as said inflating means.
GB0515772A 2005-07-30 2005-07-30 A method for production of a set of holes by monitoring fluid flow Withdrawn GB2428608A (en)

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GB0515772A GB2428608A (en) 2005-07-30 2005-07-30 A method for production of a set of holes by monitoring fluid flow
PCT/EP2006/064157 WO2007014828A1 (en) 2005-07-30 2006-07-12 A method and a device for production of a set of holes
RU2008107947/02A RU2008107947A (en) 2005-07-30 2006-07-12 METHOD AND DEVICE FOR PRODUCING THE HOLE GROUP
CNA2006800364459A CN101277783A (en) 2005-07-30 2006-07-12 A method and a device for production of a set of holes
EP06764150A EP1910018A1 (en) 2005-07-30 2006-07-12 A method and a device for production of a set of holes

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US8764000B2 (en) 2007-06-28 2014-07-01 United Technologies Corporation Tool alignment fixture
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US8710392B2 (en) 2011-06-29 2014-04-29 United Technologies Corporation Electric discharge machining hole drilling
WO2013017319A1 (en) * 2011-08-03 2013-02-07 Robert Bosch Gmbh Method and device for producing a component provided with at least one opening

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EP1910018A1 (en) 2008-04-16
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CN101277783A (en) 2008-10-01
WO2007014828A1 (en) 2007-02-08

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