APPARATUS AND METHOD FOR FORMING A VARIABLE DIAMETER HOLE IN A CONDUCTIVE WORKPIECE
Assignee
General Electric
Filed as: GENERAL ELECTRIC COMPANY A CORP. OF NEW YORK
Filed
Sep 30, 1991
Granted
Nov 11, 1997
Location
FT. THOMAS KY US
Abstract
A method and apparatus for forming a passage with a variable diameter along its length in a conductive workpiece are disclosed. The workpiece is mounted in a fixture and an externally insulated hollow electrode is positioned proximate to a surface location of the workpiece into which the passage is to be formed. A first selected voltage is connected between the electrode and the workplace with the voltage being connected to cause the electrode to act as a cathode and the workpiece to act as an anode. A pump causes an acidic electrolyte to flow through the electrode at a chosen pressure and onto the workpiece surface. The electrode is moved toward the workpiece at a first selected feed rate by a CNC controller to cause a portion of the passage to be formed at a first predetermined diameter. The CNC controller causes at least one of the first selected DC voltage to switch to a different selected DC voltage or the first selected feed rate to switch to a different selected feed rate when a predetermined depth is sensed by an encoder to cause another portion of the passage to be drilled at a second predetermined diameter.
Source: Google Patents
35 USC §181 Secrecy Order
Imposed
Jun 19, 1992
Rescinded
Apr 9, 1997
Duration
4 years, 9 months
Inventor
- 1LAWRENCE J. SCHRODER
Record Details
- Patent number
- US 5685971
- Application
- 07768131
- Aerospace match
- No
- Dataset source
- 35 USC §181 SO records
Browse by Assignee
General ElectricMore from this assignee
ADAPTIVE DIGITAL BEAMFORMING ARCHITECTURE AND ALGORITHM FOR NULLING MAINLOBE AND MULTIPLE SIDELOBE RADAR JAMMERS WHILE PRESERVING MONOPULSE RATIO ANGLE ESTIMATION ACCURACY
General Electric
TURBINE BLADE HAVING VARIABLE CONFIGURATION TURBULATORS
General Electric
TURBINE BLADE HAVING OPPOSING WALL TURBULATORS
General Electric
SETTABLE ELECTRONIC FUZING SYSTEM FOR CANNON AMMUNITION
General Electric
COOLING APPARATUS FOR AIRCRAFT GAS TURBINE ENGINE EXHAUST NOZZLES
General Electric
STAGGERED FAN BLADE ASSEMBLY FOR A TURBOFAN ENGINE
General Electric