US4169355A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Turbocharger wastegate valve
Assignee: Cummins Turbo Technologies Ltd
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Filing: 1977-12-05
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Granted: 1979-10-02
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Expires: 1997-12-05
Abstract
Abstract The disclosure illustrates a turbocharger wastegate valve comprising a cylindrical chamber connected through a radial inlet to the gas stream upstream of the turbine. High pressure air is selectively directed across the inlet through a nozzle to prevent or permit flow into the chamber which is connected to a point downstream of the turbine. The pressure of the air delivered to the nozzle may be varied to proportion the gases bypassed around the turbine.
Inventors
- 👤 Brian E. Walsham
- 👤 William K. Bruffell
- 👤 Howard S. Atkin
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-30 10:29
CPC Classifications
F; F02; F02B; F02B37/00; F02B37/12; F02B37/18; F02B37/183; F05; F05B; F05B2220/00; F05B2220/40; Y; Y02; Y02T; Y02T10/00; Y02T10/10; Y02T10/12; Y10; Y10T; Y10T137/00; Y10T137/9464
Claims Analysis
Total Claims: 10
Claim 1
Independent Claim
138 words
In combination: a turbine rotatable in response to a hot gas stream; means for directing a hot gas stream to and across said turbine; means for selectively bypassing said hot gas stream around said turbine; said bypassing means comprising: means defining a cylindrical chamber having a radially directed inlet from a point upstream of said turbine and an outlet connected to a point down stream of said turbine, means for selectively directing at least one gas stream at high velocity across said radially directed inlet generally at a right angle relative to the gas issuing from said inlet and tangetial to said chamber for selectively preventing flow into said chamber, whereby hot gases are bypassed around said turbine in the absence of said high velocity stream and substantially directed across said turbine when said high velocity stream exists.
Claim 2
Dependent Claim
138 words
In combination: a turbine rotatable in response to a hot gas stream; means for directing a hot gas stream to and across said turbine; means for selectively bypassing said hot gas stream around said turbine; said bypassing means comprising: means defining a cylindrical chamber having a radially directed inlet from a point upstream of said turbine and an outlet connected to a point down stream of said turbine, means for selectively directing at least one gas stream at high velocity across said radially directed inlet generally at a right angle relative to the gas issuing from said inlet and tangetial to said chamber for selectively preventing flow into said chamber, whereby hot gases are bypassed around said turbine in the absence of said high velocity stream and substantially directed across said turbine when said high velocity stream exists.
Claim 3
Dependent Claim
21 words
Apparatus as in claim 1 wherein the outlet to said cylindrical chamber is positioned in line with the central axis thereof.
Claim 4
Dependent Claim
24 words
Apparatus as in claim 1 wherein said selective directing means comprises means for forming a nozzle opening into the curved wall of said chamber.
Claim 5
Dependent Claim
54 words
Apparatus as in claim 3 wherein said nozzle means comprises a base securable to the exterior of said chamber forming means and an elongate portion received in an aperture in said chamber forming means, said elongate portion having a passageway extending to said base and an orifice adjacent said chamber thereby forming said nozzle.
Claim 6
Dependent Claim
30 words
Apparatus as in claim 4 wherein said elongated portion extends to the turned wall of said chamber and has an end face curved to be flush with said curved wall.
Claim 7
Dependent Claim
36 words
Apparatus as in claim 4 wherein said chamber forming means comprises a block having a circular opening therethrough and cover plates secured to opposite sides thereof, said circular opening and cover plates forming said cylindrical chamber.
Claim 8
Dependent Claim
42 words
Apparatus as in claim 6 wherein said inlet is formed through said block in a direction that is generally radial with respect to said cylindrical chamber, said apparatus further comprising a divider for separating the flow in said inlet into two streams.
Claim 9
Dependent Claim
47 words
Apparatus as in claim 1 further comprising: means for pressurizing air to a level substantially higher than the pressure level of the hot gas stream connected to said inlet, means for selectively connecting the output of said air pressurizing means to said high velocity gas stream means.
Claim 10
Dependent Claim
58 words
Apparatus as in claim 8 further comprising: a compressor driven by said turbine to produce a variable pressure output; means for communicating the variable pressure output of said compressor to said selective connecting means being responsive to pressure to permit flow from said high velocity gas stream means only when the compressor pressure is below a given level.
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) | 1982-10-01 | 1983-04-02 | 1983-10-02 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1986-10-01 | 1987-04-02 | 1987-10-02 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1990-10-01 | 1991-04-02 | 1991-10-02 | $7700.00 | Window Closed / Lapsed |