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

Parts for and methods of repairing turbine blades

Patent 4832252 Issued on May 23, 1989. Estimated Expiration Date: Icon_subject December 16, 2007. 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

3564689

3854189

Method of refurbishing turbine vane or blade components
Patent #: 4141127
Issued on: 02/27/1979
Inventor: Cretella ,   et al.

Method for repairing a turbomachinery blade tip
Patent #: 4214355
Issued on: 07/29/1980
Inventor: Zelahy

Method of manufacturing rotor blade
Patent #: 4241110
Issued on: 12/23/1980
Inventor: Ueda ,   et al.

Turbine blade repair Patent #: 4611744
Issued on: 09/16/1986
Inventor: Fraser ,   et al.

Inventor

Assignee

Application

No. 07/133527 filed on 12/16/1987

US Classes:

228/119, Repairing, restoring, or renewing product for reuse228/226, Diverse fillers228/231, Including post-heating228/232, Including preheating29/402.13, Metallurgically attaching preform29/402.16, Metallurgically attaching preform29/889.1, Repairing or disassembling416/224, Having wear liner, sheathing or insert416/241RCoating, specific composition or characteristic

Examiners

Primary: Godici, Nicholas P.
Assistant: Heinrich, Samuel M.

Attorney, Agent or Firm

International Classes

B23P 6/00 (20060101)
B23P 15/04 (20060101)
F01D 5/00 (20060101)

Foreign Application Priority Data

1986-12-20 GB

Abstract

A part and method for repairing a high velocity fluid flow machine part, for example a turbine blade comprises an insert which may be made from a piece of material the same as the turbine blade and prior to attachment to the blade has an edge region hardened by any suitable means, for example induction hardening, the insert then being secured to the blade by welding or brazing, the weld or braze material being of a relatively soft nature to provide a cushion between the insert and the blade so as to minimize the occurrence of stress corrosion cracking.

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