U.S. patents available from 1976 to present.
U.S. patent applications available from 2005 to present.

Process for repair of drive blades such as turbine blades

Patent 5193272 Issued on March 16, 1993. Estimated Expiration Date: Icon_subject December 12, 2011. Estimated Expiration Date is calculated based on simple USPTO term provisions. It does not account for terminal disclaimers, term adjustments, failure to pay maintenance fees, or other factors which might affect the term of a patent.

Patent References

Mold bottom and stool protector construction
Patent #: 4333630
Issued on: 06/08/1982
Inventor: Strange

Turbine engine seal and method for repair thereof
Patent #: 4449714
Issued on: 05/22/1984
Inventor: Meier

Method for restoring a face on the shroud of a rotor blade
Patent #: 4589175
Issued on: 05/20/1986
Inventor: Arrigoni

Alloy and methods of use thereof
Patent #: 4940566
Issued on: 07/10/1990
Inventor: Wood, et al.

Method of rehabilitating propeller hub bodies
Patent #: 4982066
Issued on: 01/01/1991
Inventor: Waring

Method of making and repairing turbine blades
Patent #: 5048183
Issued on: 09/17/1991
Inventor: Cang, et al.

Weld repairable combustor
Patent #: 5086968
Issued on: 02/11/1992
Inventor: Fawley, et al.

Method of repairing or modifying turbine blades
Patent #: 5092942
Issued on: 03/03/1992
Inventor: Fraser, et al.

Integrally bladed rotor fabrication or repair Patent #: 5109606
Issued on: 05/05/1992
Inventor: DeMichael, et al.

Inventors

Assignee

Application

No. 806877 filed on 12/12/1991

US Classes:

29/889.1, Repairing or disassembling29/402.07, And by a metallurgical operation, e.g., welding, diffusion bonding, casting29/402.18, By applying fluent material, e.g., coating, casting164/103Preheating

Examiners

Primary: Cuda, Irene

Attorney, Agent or Firm

Foreign Patent References

  • 2091140 GB 07/12/1982

International Class

B23P 015/02

Foreign Application Priority Data

1990-12-13 DE

Abstract

A process for the repair of single-crystal drive blades, such as turbine blades, in which a sound portion of the blade is inserted into an open bottom of a casting mold in communication with a casting cavity in the mold adopted to the shape of the blade. The molten metal is then cast into the mold to unite with the sound portion and an epitaxial single-crystal solidification of the melt is produced on the sound portion to form the entire blade. A part of the sound portion has an outer surface layer thereof removed to expose a core region which is constituted of substantially pure single crystal material prior to casting. The sound part is secured in a holder which is coupled to the casting mold for only a matter of seconds before the molten metal is cast into the mold.

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