Patent NL70805C successfully refreshed from Google Patents.
Patent US4550004A successfully refreshed from Google Patents.
US4550004A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Method of producing radial type ceramic turbine rotor
Assignee: NGK Insulators Ltd
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Filing: 1983-12-05
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Granted: 1985-10-29
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Expires: 2003-12-05
Abstract
Abstract A method of producing a radial type ceramic turbine rotor having a shaft, a hub connected thereto, a blade portion radially extending from the hub whose end on an air exit side extends from an end of the blade portion on the air exit side, comprises steps of injection molding a ceramic material into a ceramic rotor body and machining extra thicker portions of the molded rotor to a predetermined shaped turbine rotor. According to the invention, the molded rotor is formed by the injection molding so as to be at least 0.5 mm thicker than a predetermined thickness at a fillet between the hub and the blade portion on the air exit side and the molded rotor is then machined by a diamond wheel to remove the extra thicker portions until the thicker fillet becomes to the predetermined thickness to from a predetermined shaped turbine rotor which is free from cracks to have a high strength.
Inventors
- 👤 Takeyuki Mizuno
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-07 00:45
CPC Classifications
C; C04; C04B; C04B35/00; C04B35/622; C04B35/626; C04B35/63; C04B35/632; C04B35/634; C04B35/63404; C04B35/63408; F; F01; F01D; F01D5/00; F01D5/12; F01D5/28; F01D5/284; F02; F02B; F02B1/00; F02B1/02; F02B1/04
Claims Analysis
Total Claims: 8
Claim 1
Independent Claim
166 words
A method of producing a radial type ceramic turbine rotor having a shaft, a hub having an air entrance side and an air exit side and being connected to said shaft, a blade portion radially extending from said hub, said air exit side of said hub axially extending further than said blade portion, said method comprisng the steps of predetermining an appropriate size and shape for a fillet portion which is located on said air exit side of the hub at a connection between said hub and blade portions, injection molding a ceramic rotor body such that it has a thicker fillet portion than said predetermined fillet portion, said thicker fillet portion being at least 0.5 mm thicker than said predetermined fillet portion, heating said injection molded rotor body for removing a plasticizer therefrom, machining said thicker fillet portion of said molded rotor body until said thicker fillet portion becomes the same size and shape of said predetermined fillet portion and sintering said molded rotor body.
Claim 2
Independent Claim
166 words
A method of producing a radial type ceramic turbine rotor having a shaft, a hub having an air entrance side and an air exit side and being connected to said shaft, a blade portion radially extending from said hub, said air exit side of said hub axially extending further than said blade portion, said method comprisng the steps of predetermining an appropriate size and shape for a fillet portion which is located on said air exit side of the hub at a connection between said hub and blade portions, injection molding a ceramic rotor body such that it has a thicker fillet portion than said predetermined fillet portion, said thicker fillet portion being at least 0.5 mm thicker than said predetermined fillet portion, heating said injection molded rotor body for removing a plasticizer therefrom, machining said thicker fillet portion of said molded rotor body until said thicker fillet portion becomes the same size and shape of said predetermined fillet portion and sintering said molded rotor body.
Claim 3
Dependent Claim
25 words
The method of claim 1, wherein said thicker fillet portion is concave in a longitudinal-section passing through a rotating axis of said molded rotor body.
Claim 4
Dependent Claim
39 words
The method of claim 1, wherein a ceramic material to be injection molded comprises at least one material selected from the group of materials consisting of silicon nitride, silicon carbide, sialon and substances which produce these materials when sintered.
Claim 5
Dependent Claim
28 words
The method of claim 1, further comprising pre-sintering said molded rotor body after said machining step and said sintering of said molded body occurs after said pre-sintering step.
Claim 6
Dependent Claim
35 words
The method of claim 1, further comprising pre-sintering said molded rotor body after said heating thereof and prior to said machining step and said sintering of said molded rotor body occurs after said machining step.
Claim 7
Dependent Claim
24 words
The method of claim 1, wherein said sintering of said molded rotor body occurs after said heating step and prior to said machining step.
Claim 8
Dependent Claim
29 words
The method of claim 1, further comprising pre-sintering said molded rotor body after said heating step, and machining said molded rotor body after said sintering of said molded body.
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) | 1988-10-28 | 1989-04-29 | 1989-10-29 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1992-10-28 | 1993-04-29 | 1993-10-29 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1996-10-28 | 1997-04-29 | 1997-10-29 | $7700.00 | Window Closed / Lapsed |