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US4389845A Expired / Lapsed US ⏱️ 0.0 years remaining

Turbine casing for turbochargers

Assignee: IHI Corp
•
Filing: 1980-09-22
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Granted: 1983-06-28
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Expires: 2000-09-22
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Abstract

Abstract A turbine casing for turbochargers adapted for use with reciprocating internal combustion engines, in which in response to the flow rate of the exhaust gases from an engine, the exhaust gases are directed to flow through a first or radially inward scroll divided into two or more exhaust gas passages in the axial direction of a turbine wheel or through said first or radially inward scroll and a second or radially outward scroll, whereby regardless of the variations in flow rate an optimum supercharging efficiency can be maintained over the whole region of operating conditions of the engine.

Inventors

  • 👤 Takaaki Koike

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-27 21:40
CPC Classifications
F; F01; F01D; F01D17/00; F01D17/10; F01D17/12; F01D17/14; F01D17/146; F01D9/00; F01D9/02; F01D9/026; F02; F02B; F02B37/00; F02B37/02; F02B37/025; F02B37/12; F02B37/22; Y; Y02; Y02T; Y02T10/00; Y02T10/10; Y02T10/12

Claims Analysis

Total Claims: 2
Claim 1
Independent Claim 312 words
A turbine casing for turbochargers having a turbine wheel, comprising: (a) a first radially inward casing wall having an appended integral centrally positioned partition wall extending radially inward therefrom, said casing wall with said partition wall being formed to establish a first radially inward partially divided scroll surrounding substantially half of the periphery of the turbine wheel for service as first and second side-by-side exhaust passages in the axial direction of the shaft of said turbine wheel so that separate flows of exhaust gases from an engine may be directed through respective said passages to the portion of said turbine wheel surrounded by said first scroll; (b) a second radially outward casing wall formed integral with and surrounding the entirety of said first casing wall, said second casing wall being formed to establish a second scroll located radially outward from said first scroll and utilizing said first casing wall as a portion of the boundary thereof, said second scroll being separated from and surrounding a major portion of said first scroll and having a terminal portion surrounding a further minor portion of the periphery of said turbine wheel additional to the portion surrounded by said first scroll, said second scroll thereby being adapted for service as a third exhaust passage surrounding and separated from said first and second exhaust passages so that a separate flow of exhaust gases from an engine may be directed through said third passage to said minor portion of said turbine wheel surrounded by said second scroll; (c) casing structure formed integral with said first and second casing walls and providing a common inlet to said first and second scrolls for exhaust gases from an engine; and (d) control valve means for selectively controlling the flow of the exhaust gases from said inlet to said second scroll while maintaining the flow of such gases to said first scroll.
Claim 2
Dependent Claim 312 words
A turbine casing for turbochargers having a turbine wheel, comprising: (a) a first radially inward casing wall having an appended integral centrally positioned partition wall extending radially inward therefrom, said casing wall with said partition wall being formed to establish a first radially inward partially divided scroll surrounding substantially half of the periphery of the turbine wheel for service as first and second side-by-side exhaust passages in the axial direction of the shaft of said turbine wheel so that separate flows of exhaust gases from an engine may be directed through respective said passages to the portion of said turbine wheel surrounded by said first scroll; (b) a second radially outward casing wall formed integral with and surrounding the entirety of said first casing wall, said second casing wall being formed to establish a second scroll located radially outward from said first scroll and utilizing said first casing wall as a portion of the boundary thereof, said second scroll being separated from and surrounding a major portion of said first scroll and having a terminal portion surrounding a further minor portion of the periphery of said turbine wheel additional to the portion surrounded by said first scroll, said second scroll thereby being adapted for service as a third exhaust passage surrounding and separated from said first and second exhaust passages so that a separate flow of exhaust gases from an engine may be directed through said third passage to said minor portion of said turbine wheel surrounded by said second scroll; (c) casing structure formed integral with said first and second casing walls and providing a common inlet to said first and second scrolls for exhaust gases from an engine; and (d) control valve means for selectively controlling the flow of the exhaust gases from said inlet to said second scroll while maintaining the flow of such gases to said first scroll.

References Cited (Backward Citations)

GB1044176A Cited
US3313518A Cited
US3557549A Cited
DE1949484A1 Cited
GB1426554A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1986-06-27 1986-12-27 1987-06-28 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1990-06-27 1990-12-27 1991-06-28 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1994-06-27 1994-12-27 1995-06-28 $7700.00 Window Closed / Lapsed

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