Patent US5418869A successfully refreshed from Google Patents.
Patent US3739576A successfully refreshed from Google Patents.
US3739576A
Expired / Lapsed
US
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Combustion system
Assignee: RTX Corp
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Filing: 1969-08-11
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Granted: 1973-06-19
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Expires: 1989-08-11
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)
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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 |