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

Turbine engine seal and method for repair thereof

Patent 4449714 Issued on May 22, 1984. Estimated Expiration Date: Icon_subject March 22, 2003. 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

2285583

3046648

3918925

Rotor seal element with heat resistant alloy coating
Patent #: 4060250
Issued on: 11/29/1977
Inventor: Davis ,   et al.

Rotary labyrinth seal member
Patent #: 4148494
Issued on: 04/10/1979
Inventor: Zelahy ,   et al.

Method of restoring the shrouds of turbine blades
Patent #: 4291448
Issued on: 09/29/1981
Inventor: Cretella ,   et al.

Fully plasma-sprayed compliant backed ceramic turbine seal Patent #: 4336276
Issued on: 06/22/1982
Inventor: Bill ,   et al.

Inventor

Assignee

Application

No. 06/477717 filed on 03/22/1983

US Classes:

277/414, Formed by cellular pockets (e.g., honeycomb, etc.)277/922, BONDING OR JOINING FOR MANUFACTURE OF SEAL29/402.02, Seal or element thereof29/402.07, And by a metallurgical operation, e.g., welding, diffusion bonding, casting415/170.1, BEARING, SEAL, OR LINER BETWEEN RUNNER PORTION AND STATIC PART415/230, Seal427/451, Additionally containing nickel, cobalt, or iron as free metal or alloy427/456Aluminum, nickel, cobalt, or iron metal or alloy containing coating

Examiners

Primary: Warden, Robert J.

Attorney, Agent or Firm

International Class

B23P 6/00 (20060101)

Abstract

A method for repairing turbine engine seals and a product manufactured in accordance with the method are provided. A worn or damaged honeycomb seal is removed from a backing plate together with a portion of the surface of the plate. The plate is restored to substantially its original thickness by a low pressure plasma spraying operation which may be followed by further machining to arrive at the required plate thickness. A new seal is then brazed thereon. The finished product will include the backing plate, a low pressure plasma sprayed coated surface, and a honeycomb seal brazed to the coated surface.

Other References

  • Elektrie, vol. 32, No. 4, 1978, E. Kranz et al., "Verfahren der Plasmatechnologie", pp. 194-199
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