US4327154A
Expired / Lapsed
US
⏱️ 0.0 years remaining
High-strength components of complex geometric shape and method for their manufacture
Assignee: MTU Aero Engines AG
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Filing: 1978-08-07
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Granted: 1982-04-27
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Expires: 1998-08-07
Abstract
Abstract A high-strength component of complex geometric shape is formed by a core of hollow spheres of metallic particles surrounded by a shell of homogeneous metallic material. The hollow spheres are intimately bonded to each other and to the inner walls of the surrounding shell by hot isostatic pressing. The pressing procedure is enhanced by the use of elements such as boron which lower the melting point of the hollow spheres, for example, when said spheres are coated by said boron.
Inventors
- 👤 Axel Rossmann
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-03 22:51
CPC Classifications
B; B22; B22F; B22F7/00; B22F7/06; B22F7/08; B22F5/00; B22F5/04; F; F01; F01D; F01D25/00; F01D25/005; B22F2999/00; Y; Y10; Y10T; Y10T428/00; Y10T428/12; Y10T428/12007
Claims Analysis
Total Claims: 12
Claim 1
Independent Claim
105 words
A high strength component comprising a shell of the desired final shape and a core having a given shape fitting into said shell, said core being made of atomized metallic particles which are initially of substantially spherical shape having hollow spaces therein, said particles being pressed into said given shape to form said core directly in said shell whereby said metallic particles are bonded at their outer surfaces to one another and to said shell, while said hollow spaces remain separated from one another, said shell of homogeneous metallic material permanently surrounding said core, whereby strength as well as complex geometric shapes may be attained.
Claim 2
Dependent Claim
105 words
A high strength component comprising a shell of the desired final shape and a core having a given shape fitting into said shell, said core being made of atomized metallic particles which are initially of substantially spherical shape having hollow spaces therein, said particles being pressed into said given shape to form said core directly in said shell whereby said metallic particles are bonded at their outer surfaces to one another and to said shell, while said hollow spaces remain separated from one another, said shell of homogeneous metallic material permanently surrounding said core, whereby strength as well as complex geometric shapes may be attained.
Claim 3
Dependent Claim
25 words
The component of claim 1, wherein said core and said shell are made of metal selected from the group consisting of titanium and super alloys.
Claim 4
Independent Claim
166 words
A method of manufacturing a high strength component having a core and a shell intimately and permanently bonded to said core, comprising the following steps: (a) manufacturing a homogeneous metallic shell substantially with a shape corresponding to the final shape of the component; (b) filling said shell with atomized metallic particles which are initially of substantially spherical shape having hollow spaces therein; (c) evacuating said shell and hermetically sealing said atomized metallic particles in said shell; and (d) subjecting said evacuated and sealed shell to hot isostatic pressing by adjusting the temperature and pressure so that the atomized metallic particles of the core deform until all the interstices between said particles themselves and between the particles and the inner wall of the shell have substantially disappeared and the particles become intimately bonded to one another and to the inside of the shell, whereby said core becomes intimately bonded to said shell and whereby said hollow spaces remain separated from one another in the high strength component.
Claim 5
Independent Claim
166 words
A method of manufacturing a high strength component having a core and a shell intimately and permanently bonded to said core, comprising the following steps: (a) manufacturing a homogeneous metallic shell substantially with a shape corresponding to the final shape of the component; (b) filling said shell with atomized metallic particles which are initially of substantially spherical shape having hollow spaces therein; (c) evacuating said shell and hermetically sealing said atomized metallic particles in said shell; and (d) subjecting said evacuated and sealed shell to hot isostatic pressing by adjusting the temperature and pressure so that the atomized metallic particles of the core deform until all the interstices between said particles themselves and between the particles and the inner wall of the shell have substantially disappeared and the particles become intimately bonded to one another and to the inside of the shell, whereby said core becomes intimately bonded to said shell and whereby said hollow spaces remain separated from one another in the high strength component.
Claim 6
Dependent Claim
25 words
The method of claim 3, wherein said shell and said core are made of metal selected from the group consisting of titanium and super alloys.
Claim 7
Dependent Claim
19 words
The method of claim 3 or 4 further comprising providing said atomized metallic particles with melting point lowering means.
Claim 8
Dependent Claim
20 words
The method of claim 5, comprising coating said atomized metallic particles with boron acting as a melting point lowering agent.
Claim 9
Dependent Claim
17 words
The method of claim 3, further mechanically or electromechanically finishing said component after completing said isostatic pressing.
Claim 10
Independent Claim
21 words
A method for manufacturing atomized metallic particles having hollow spherical shapes, comprising atomizing a metal melt in an inert gaseous atmosphere.
Claim 11
Independent Claim
21 words
A method for manufacturing atomized metallic particles having hollow spherical shapes, comprising atomizing a metal melt in an inert gaseous atmosphere.
Claim 12
Dependent Claim
12 words
The method of claim 8, wherein said inert gaseous atmosphere includes argon.
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) | 1985-04-26 | 1985-10-26 | 1986-04-27 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1989-04-26 | 1989-10-26 | 1990-04-27 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1993-04-26 | 1993-10-26 | 1994-04-27 | $7700.00 | Window Closed / Lapsed |