CANTILEVERED INTEGRAL AIRFOIL CASTING AND METHOD
Assignee
CHROMALLOY CASTINGS MIAMI CORPORATION, A CORP. OF DE
Filed
Jan 27, 1987
Granted
Nov 13, 1990
Location
CORAL GABLES FL US
Abstract
An outer stabilizing band or bands at the unsupported end portion of the air foils changes the configuration from an unsupported cantilevered airfoil to a baband supported airfoil during the forming of the mold and casting of the product. Such band or bands, which are later shaved away, permit dimensional stabilization and provide an outer wall for venting, fill-out, and inclusion trapping. The stabilizing band or bands are extremely thin, normally in the range of 20 to 60 one thousandths of an inch, which avoids the need for gating and minimizes the amount of machining required to remove such stabilizing band or bands from the integral airfoil and hub casting. The bands may be outside the end of the airfoil or flush with the ends of the airfoil. The procedure and method for incorporating the outer band or bands into the casting begins with the process of making the pattern. It also aids in the stabilizing of the configuration of the pattern thereby achieving more dimensional accuracy. This is applicable whether soluble patterns, one piece wax patterns, or patterns made of assembled parts are involved.
Source: Google Patents
35 USC §181 Secrecy Order
Imposed
Jul 2, 1987
Rescinded
Nov 2, 1988
Duration
1 year, 4 months
Inventor
- 1DAVID F. JANNEY
Record Details
- Patent number
- US 4970125
- Application
- 07006957
- Aerospace match
- Yes
- Dataset source
- 35 USC §181 SO records
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