US4101712A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Method of producing a material with locally different properties and applications of the method
Assignee: BBC Brown Boveri AG Switzerland
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Filing: 1975-12-02
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Granted: 1978-07-18
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Expires: 1995-12-02
Abstract
Abstract A method of producing a material with locally different properties comprises filling a form with at least two different component powders such that the ratio of contents of said powders in the mixture continuously varies over at least some spatial extent, compacting the mixed powders in the form, and subsequently sintering the compacted powders.
Inventors
- 👤 Michael J. Bomford
- 👤 Gernot Gessinger
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-23 12:09
CPC Classifications
B; B22; B22F; B22F7/00; B22F7/06; B22F2999/00; Y; Y10; Y10T; Y10T29/00; Y10T29/49; Y10T29/49316; Y10T29/49336; Y10T29/49337; Y10T428/00; Y10T428/12; Y10T428/12014; Y10T428/12021
Claims Analysis
Total Claims: 7
Claim 1
Independent Claim
167 words
A method of producing a turbine blade with locally different properties, comprising: filling a form with two different component powders such that the ratio of contents of said powders in the mixture continuously varies over the spatial extent of the form; wherein each of the powdered components to be mixed together is introduced in the desired proportion by a conveyer proportioning screw into another mixing screw and therefrom is deposited in the mixed state into said form; and wherein one of said powders is a high strength super-alloy and is the predominant ingredient of said mixture in the portion of the workpiece intended for the blade foot, and the other powder is a non-corrosive Co- or Ni-base alloy and is the predominant ingredient of said mixture in the portion of the workpiece intended for the blade tip, and the transition from one powder to the other along the length of the workpiece is continuous; compacting the mixed powders in the form; and subsequently sintering the compacted powders.
Claim 2
Independent Claim
167 words
A method of producing a turbine blade with locally different properties, comprising: filling a form with two different component powders such that the ratio of contents of said powders in the mixture continuously varies over the spatial extent of the form; wherein each of the powdered components to be mixed together is introduced in the desired proportion by a conveyer proportioning screw into another mixing screw and therefrom is deposited in the mixed state into said form; and wherein one of said powders is a high strength super-alloy and is the predominant ingredient of said mixture in the portion of the workpiece intended for the blade foot, and the other powder is a non-corrosive Co- or Ni-base alloy and is the predominant ingredient of said mixture in the portion of the workpiece intended for the blade tip, and the transition from one powder to the other along the length of the workpiece is continuous; compacting the mixed powders in the form; and subsequently sintering the compacted powders.
Claim 3
Dependent Claim
30 words
The method of claim 1 wherein said high strength super alloy is IN 700 and said non-corrosive alloy consists essentially of 25% Cr, 4% Al, 1% Y, and balance Ni.
Claim 4
Dependent Claim
111 words
The method of claim 1, for producing a material for use in turbine blades wherein the powders which are the predominant ingredient of said mixture in the portion of the workpiece intended for the blade tip is a material having a higher heat- and creep-strength then is possessed by the powder which is the predominant ingredient of said mixture in the blade foot, and wherein said latter powder is a material having a greater toughness than said former powder and wherein the transition from predominance of the powder appropriate for the blade foot to the predominance of the powder appropriate for the blade tip is continuous along the workpiece being fabricated.
Claim 5
Dependent Claim
28 words
The method of claim 3 wherein said higher heat- and creep strength powder is made of alloy IN-853 and said higher toughness powder is made of alloy IN-100.
Claim 6
Dependent Claim
10 words
A turbine blade made by the method of claim 1.
Claim 7
Dependent Claim
10 words
A turbine blade made by the method of claim 3.
References Cited (Backward Citations)
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1981-07-17 | 1982-01-16 | 1982-07-18 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1985-07-17 | 1986-01-16 | 1986-07-18 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1989-07-17 | 1990-01-16 | 1990-07-18 | $7700.00 | Window Closed / Lapsed |