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US3643431A Expired / Lapsed US ⏱️ 0.0 years remaining

Flow control devices

Assignee: TECHNOLOGY UK
•
Filing: 1969-12-04
•
Granted: 1972-02-22
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Expires: 1989-12-04
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Abstract

Abstract In a venturi having a wide angle divergent section, flow separation can occur near the throat resulting in throttling. Suction is applied through perforations in the venturi surface to cause reattachment with consequent increase in flow rate. Air flowing to primary zones in combustion chambers can be controlled by selective application of suction so as to vary local air/fuel ratios according to operating conditions. A similar arrangement may be applied to fuel injector vaporizing tubes.

Inventors

  • 👤 James Barry Jamieson

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-28 16:33
CPC Classifications
F; F15; F15D; F15D1/00; F15D1/02; F15D1/06; F01; F01D; F01D9/00; F23; F23R; F23R3/00; F23R3/02; F23R3/26; Y; Y10; Y10T; Y10T137/00; Y10T137/206; Y10T137/2273

Claims Analysis

Total Claims: 10
Claim 1
Independent Claim 71 words
Combustion apparatus comprising a combustion chamber and a fuel vaporizing tube defined by an air inlet to the combustion chamber, in which the air inlet incorporates a flow control device comprising a duct, a flow restrictor located within the duct and having a throat and a divergent portion extending downstream from the throat relative to the direction of airflow through the duct, and boundary layer control means associated with the restrictor.
Claim 2
Dependent Claim 71 words
Combustion apparatus comprising a combustion chamber and a fuel vaporizing tube defined by an air inlet to the combustion chamber, in which the air inlet incorporates a flow control device comprising a duct, a flow restrictor located within the duct and having a throat and a divergent portion extending downstream from the throat relative to the direction of airflow through the duct, and boundary layer control means associated with the restrictor.
Claim 3
Dependent Claim 28 words
Combustion apparatus according to claim 1 further comprising a fuel injector arranged to discharge fuel through the restrictor in a downstream direction relative to the direction of airflow.
Claim 4
Dependent Claim 20 words
Combustion apparatus according to claim 2 in which the injector is arranged to discharge fuel immediately upstream of the throat.
Claim 5
Dependent Claim 28 words
Combustion apparatus according to claim 1 in which the boundary layer control means is arranged to be selectively applied to flow passing over a surface of the restrictor.
Claim 6
Dependent Claim 14 words
Combustion apparatus according to claim 1 in which the duct is substantially parallel sided.
Claim 7
Dependent Claim 30 words
Combustion apparatus according to claim 1 in which holes extend through the surface of the divergent portion of the restrictor and the holes are connected to a source of suction.
Claim 8
Dependent Claim 13 words
Combustion apparatus according to claim 6 in which the restrictor is a venturi.
Claim 9
Dependent Claim 34 words
Combustion apparatus according to claim 1 in which the cross-sectional area of the throat of the restrictor is substantially one-third of the cross-sectional area of the duct at the exit plane of the restrictor.
Claim 10
Dependent Claim 22 words
Combustion apparatus according to claim 1 in which the included angle of the divergent portion of the restrictor is substantially 60* .

References Cited (Backward Citations)

US3123285A Cited
US2656096A Cited
GB738006A Cited
US2788719A Cited
US2948148A Cited
US2841182A Cited
US3216455A Cited
US3527052A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1975-02-21 1975-08-23 1976-02-22 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1979-02-21 1979-08-23 1980-02-22 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1983-02-21 1983-08-23 1984-02-22 $7700.00 Window Closed / Lapsed

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