Electrolysis: processes – compositions used therein – and methods – Electrolytic erosion of a workpiece for shape or surface... – Aperture making
Reexamination Certificate
2000-07-13
2002-05-14
Valentine, Donald R. (Department: 1741)
Electrolysis: processes, compositions used therein, and methods
Electrolytic erosion of a workpiece for shape or surface...
Aperture making
C205S666000, C205S672000, C204S22400M, C204S290010
Reexamination Certificate
active
06387242
ABSTRACT:
BACKGROUND OF THE INVENTION
This invention relates to a tool and a method used for electrochemical machining. More particularly, this invention relates to a tool and method for forming features in predrilled holes using electrochemical machining.
A specialized adaptation of electrochemical machining, known as shaped-tube electrochemical machining (STEM), is used for drilling small, deep holes in electrically conductive materials. STEM is a noncontact electrochemical drilling process that can produce holes with aspect ratios as high as 300:1. It is the only known method which is capable of manufacturing the small, deep holes used for cooling blades of efficient gas turbines.
The efficiency of a gas turbine engine is directly proportional to the temperature of turbine gases channeled from the combustor of the engine and flowing over the turbine blades. For example, for gas turbine engines having relatively large blades, turbine gas temperatures approaching 2,700° F. are typical. To withstand such high temperatures, these large blades are manufactured from advanced materials and typically include state-of-the-art type cooling features.
A turbine blade is typically cooled using a coolant such as compressor discharge air. The blade typically includes a cooling hole through which the air passes. A further design advancement has been the addition of internal ridges in the cooling hole to effect turbulent flow through the hole and increase cooling efficiency. Cooling features within the hole such as turbulence promoting ribs, or turbulators, thus increase the efficiency of the turbine.
The cooling holes commonly have an aspect ratio, or depth to diameter ratio, as large as 300:1, with a diameter as small as a few millimeters. The turbulators extend from sidewalls of the hole into the air passage about 0.2 mm., for example.
The method currently used for drilling the cooling holes in turbine blades is a shaped-tube electrochemical machining (STEM) process. In this process, an electrically conductive workpiece is situated in a fixed position relative to a movable manifold. The manifold supports a plurality of drilling tubes, each of which are utilized to form an aperture in the workpiece. The drilling tubes function as cathodes in the electrochemical machining process, while the workpiece acts as the anode. As the workpiece is flooded with an electrolyte solution from the drilling tubes, material is deplated from the workpiece in the vicinity of the leading edge of the drilling tubes to form holes.
Turbulated ridges are formed in the cooling holes by a modification of the standard shaped-tube electrochemical machining (STEM) process for drilling straight-walled holes. One common method is termed cyclic dwelling. With this technique, the drilling tube is first fed forward, and then the advance is slowed or stopped in a cyclic manner. The dwelling of the tool that occurs when the feed rate is decreased or stopped creates a local enlargement of the hole diameter, or a bulb. The cyclic dwelling, for which cyclical voltage changes may be required, causes ridges to be formed between axially spaced bulbs. These ridges are the turbulators.
The cyclic dwelling method is very low in process efficiency compared to shaped-tube electrochemical machining (STEM) drilling of straight-walled holes because of the lengthy required time for drilling each bulb individually by cyclic tool dwelling. The dwell time required to form a single bulb can be greater than the time for drilling an entire straight-walled hole.
U.S. Pat. No. 5,306,401 describes a method for drilling cooling holes in turbine blades that uses a complex tool resetting cycle for each turbulator in the hole. This method also has low process efficiency, having even longer operating times for drilling the turbulator ridges than the cyclic dwelling method because of the time required to reset the electrode tool.
In addition, both the cyclic dwelling method and the method disclosed in U.S Pat. No. 5,306,401 require that additional equipment be used with a standard STEM machine for control of machine ram accuracy, electrolyte flow and power supply consistency, since these are crucial to hole quality. Failure to control the dimensions of the turbulated holes often leads to part rejection, adding significant manufacturing costs for the machining process.
Accordingly, there is a need in the art for a new and improved method for manufacturing turbulators that has a relatively short machining cycle time. There is an additional need for an improved method of manufacturing more complex features such as spiral or helical ridges and the like. There is an additional need for a method utilizing relatively simple and easily implemented manufacturing techniques. In particular, there is a need for a method that does not require complex lateral or vertical displacement of the electrode.
SUMMARY OF THE INVENTION
A machining process for forming a raised area in a wall of a predrilled hole includes distributing electrolyte via a workpiece internal cavity to a number of predrilled holes. Next, position a template including at least one electrode coated with an insulating material in a pattern defining the raised area to be formed in the wall of the predrilled hole below the workpiece such that the electrode is positioned within a predrilled hole and machining by passing electric current between the electrode and the workpiece wall and circulating electrolyte through the hole.
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Wang Hsin-Pang
Wei Bin
Cabou Christian G.
General Electric Company
Patnode Patrick K.
Valentine Donald R.
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