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US3739576A Expired / Lapsed US ⏱️ 0.0 years remaining

Combustion system

Assignee: RTX Corp
•
Filing: 1969-08-11
•
Granted: 1973-06-19
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Expires: 1989-08-11
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Abstract

Abstract A combustion system for turbine engines wherein a plurality of ejector units are placed around the circumference of an annular burner. The airflow enters the inlet pipes of the ejector units and the air flow passing through these inlet pipes pumps fuel from an annular manifold in proportion to the local air flow thereby attempting to maintain a constant fuel-air ratio around the entire annular burner where ignition occurs.

Inventors

  • 👤 J Chamberlain

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-04 10:47
CPC Classifications
F; F23; F23R; F23R3/00; F23R3/02; F23R3/04; F23R3/10

Claims Analysis

Total Claims: 2
Claim 1
Independent Claim 191 words
An engine having in combination, air supply means, fuel supply means, a combustion section, said combustion section having burner means, said combustion section having an inlet area for air from said air supply means, said fuel supply means including a metering control for providing a desired overall fuel flow to said burner means, said metering control directing its flow to a fuel manifold, said fuel manifold having a plurality of conduit means extending therefrom, each conduit means being connected to said burner means by an ejector unit, each ejector unit having a driving fluid inlet which receives air flow from one point in said inlet area, each ejector unit having a suction inlet connected directly to its cooperating conduit means, each ejector unit having an outlet for the mixture of said air and fuel, the amount of metered overall fuel flow being sucked into each ejector unit being dependent on the air flowing through its cooperating driving fluid inlet to maintain a substantially constant fuel-air ratio throughout, said driving fluid inlet being a cylindrical member having swirl vanes therearound to produce the low pressure for acting on the cooperating suction inlet.
Claim 2
Dependent Claim 191 words
An engine having in combination, air supply means, fuel supply means, a combustion section, said combustion section having burner means, said combustion section having an inlet area for air from said air supply means, said fuel supply means including a metering control for providing a desired overall fuel flow to said burner means, said metering control directing its flow to a fuel manifold, said fuel manifold having a plurality of conduit means extending therefrom, each conduit means being connected to said burner means by an ejector unit, each ejector unit having a driving fluid inlet which receives air flow from one point in said inlet area, each ejector unit having a suction inlet connected directly to its cooperating conduit means, each ejector unit having an outlet for the mixture of said air and fuel, the amount of metered overall fuel flow being sucked into each ejector unit being dependent on the air flowing through its cooperating driving fluid inlet to maintain a substantially constant fuel-air ratio throughout, said driving fluid inlet being a cylindrical member having swirl vanes therearound to produce the low pressure for acting on the cooperating suction inlet.

References Cited (Backward Citations)

US1612838A Cited
US1893533A Cited
US1918326A Cited
US2592748A Cited
US2727358A Cited
US2948117A Cited
US3020717A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1976-06-18 1976-12-18 1977-06-19 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1980-06-18 1980-12-18 1981-06-19 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1984-06-18 1984-12-18 1985-06-19 $7700.00 Window Closed / Lapsed

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