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US4151713A Expired / Lapsed US ⏱️ 0.0 years remaining

Burner for gas turbine engine

Assignee: RTX Corp
•
Filing: 1977-03-15
•
Granted: 1979-05-01
•
Expires: 1997-03-15
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Abstract

Abstract This invention relates to means for minimizing the smoke emitted from the exhaust of a gas turbine engine by judiciously adding air to the primary burning zone of a combustor at discrete locations. This invention contemplates retrofitting existing burners by substituting the improvement for existing can burner components to obviate the necessity of replacing the entire combustor.

Inventors

  • 👤 Joseph J. Faitani
  • 👤 William E. Woodburn, Jr.

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-26 00:02
CPC Classifications
F; F23; F23R; F23R3/00; F23R3/42; F23R3/50; F23R3/02; F23R3/04; F23R3/045; F23R3/06; Y; Y02; Y02T; Y02T50/00; Y02T50/60

Claims Analysis

Total Claims: 6
Claim 1
Independent Claim 160 words
Means for reducing the smoke density of a combustor having an outer liner having a plurality of cooling and combustion holes defining a primary and secondary combustion zone, being closed at one end and opened at the opposite end, a centrally disposed tube extending inwardly from said closed end, opened at its upstream end for feeding air to a plurality of cooling and combustion holes, and closed at its downstream end, said smoke density reducing means including a first and second bank of a plurality of circumferentially spaced holes disposed in the wall of said tube in proximity to said primary combustion zone and being dimensioned for ingressing air in the range of 1.5 to 2.5 percentage relative to the total amount of air ingested by said combustor, the holes in said downstream bank of holes being disposed in out of phase relationship with the holes in the upstream bank of holes and defines therewith a cluster of three holes.
Claim 2
Dependent Claim 160 words
Means for reducing the smoke density of a combustor having an outer liner having a plurality of cooling and combustion holes defining a primary and secondary combustion zone, being closed at one end and opened at the opposite end, a centrally disposed tube extending inwardly from said closed end, opened at its upstream end for feeding air to a plurality of cooling and combustion holes, and closed at its downstream end, said smoke density reducing means including a first and second bank of a plurality of circumferentially spaced holes disposed in the wall of said tube in proximity to said primary combustion zone and being dimensioned for ingressing air in the range of 1.5 to 2.5 percentage relative to the total amount of air ingested by said combustor, the holes in said downstream bank of holes being disposed in out of phase relationship with the holes in the upstream bank of holes and defines therewith a cluster of three holes.
Claim 3
Dependent Claim 53 words
Means as in claim 1 including a plurality of holes circumferentially spaced about the combustor center line formed in said outer line in proximity to said primary combustion zone and being dimensioned for ingressing air in the range of 2.0 to 3.5 percentage of the total amount of air ingested by said combustor.
Claim 4
Dependent Claim 66 words
Means as in claim 1 wherein said outer wall of said combustor and said tube wall is fabricated from a plurality of circular louver elements extending in each adjacent louver element being attached to each other to define said combustion zone, said first bank of circumferentially mounted holes in an upstream louver and said second bank of circumferentially mounted holes formed in a downstream adjacent louver.
Claim 5
Dependent Claim 39 words
Means as in claim 3 wherein the number of said downstream bank of holes are sized so as to ingress air in the range of 0.5 to 1.0 percentage of air relative to the total air in said combustor.
Claim 6
Dependent Claim 48 words
Means as in claim 3 wherein the number of said upstream bank of holes is twice the number of said holes in the downstream bank of holes and ingresses air in the range of 1.0 to 1.5 percentage of air relative to the total air in said combustor.

References Cited (Backward Citations)

GB948128A Cited
GB892949A Cited
US3430443A Cited
US3498055A Cited
US3643430A Cited
DE2145891A1 Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1982-04-30 1982-10-30 1983-05-01 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1986-04-30 1986-10-30 1987-05-01 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1990-04-30 1990-10-30 1991-05-01 $7700.00 Window Closed / Lapsed

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