← Back to Patent Explorer
US4183208A Expired / Lapsed US ⏱️ 0.0 years remaining

Fluidized bed gasifier

Assignee: RTX Corp
•
Filing: 1977-12-15
•
Granted: 1980-01-15
•
Expires: 1997-12-15
📄 Original PDF 🌐 Google Patents 🔄 Sync Now

Abstract

Abstract An increase in the temperature of the gaseous working medium in a gas turbine engine fueled with coal-fired gasifier having a rotating fluidized bed, where the coal is fed radially inwardly through the bed toward the axis of rotation is obtained by including a secondary combustor. The gasifier is fed with compressor discharge air and is operated fuel rich by limiting the amount of compressor discharge air fed to the fluidized bed. The excess compressor discharge air mixes with the exhaust from the gasifier for further combustion resulting in an increase in the temperature of the gaseous working medium that is ultimately utilized for driving the turbine of the engine.

Inventors

  • 👤 John J. Horgan
  • 👤 Stuart Hamilton

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-28 15:33
CPC Classifications
F; F02; F02B; F02B43/00; F02B43/08; C; C10; C10J; C10J3/00; C10J3/46; C10J3/48; C10J3/485; C10J3/487; C10J3/54; C10J3/56; C10J3/72; C10J3/74; F02C; F02C3/00; F02C3/20; F02C3/26; F02C3/28; C10J2300/00; C10J2300/09; C10J2300/0913; C10J2300/093; C10J2300/0953; C10J2300/0956; Y; Y02; Y02T; Y02T10/00; Y02T10/10; Y02T10/30

Claims Analysis

Total Claims: 2
Claim 1
Independent Claim 201 words
A gas turbine engine having a compressor, a turbine driving said compressor and a centrifugal coal-burning gasifier defining a first combustor generating hot gases for powering said turbine, means to rotate said gasifier means for generating a fluidized bed formed in a cylindrical wall in said gasifier, means for admitting coal into said gasifier through openings in said cylindrical wall and directing the coal from the outer diameter of said cylindrical wall toward its center, connection means supplying a portion of compressor discharge air to said first combustor for fluidizing said fluidized bed and supporting combustion centrally within said cylinder to combust said coal, means for increasing the temperature of the hot gases admitted to said turbine, said means including a secondary combustor interposed between said centrifugal gasifier and said turbine for receiving the hot gases generated thereby, and means for limiting the amount of compressor air to said fluidized bed so that the hot gases generated in said gasifier have a content of combustible gases and means for burning said combustible gases in said secondary combustor, and connection means interconnecting said compressor and said secondary combustor for supplying the remaining portion of compressor discharge air for supporting said combustion therein.
Claim 2
Dependent Claim 201 words
A gas turbine engine having a compressor, a turbine driving said compressor and a centrifugal coal-burning gasifier defining a first combustor generating hot gases for powering said turbine, means to rotate said gasifier means for generating a fluidized bed formed in a cylindrical wall in said gasifier, means for admitting coal into said gasifier through openings in said cylindrical wall and directing the coal from the outer diameter of said cylindrical wall toward its center, connection means supplying a portion of compressor discharge air to said first combustor for fluidizing said fluidized bed and supporting combustion centrally within said cylinder to combust said coal, means for increasing the temperature of the hot gases admitted to said turbine, said means including a secondary combustor interposed between said centrifugal gasifier and said turbine for receiving the hot gases generated thereby, and means for limiting the amount of compressor air to said fluidized bed so that the hot gases generated in said gasifier have a content of combustible gases and means for burning said combustible gases in said secondary combustor, and connection means interconnecting said compressor and said secondary combustor for supplying the remaining portion of compressor discharge air for supporting said combustion therein.

References Cited (Backward Citations)

US3446012A Cited
US4039272A Cited
US4148186A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1983-01-14 1983-07-16 1984-01-15 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1987-01-14 1987-07-16 1988-01-15 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1991-01-14 1991-07-16 1992-01-15 $7700.00 Window Closed / Lapsed

Assigned Categories & Tags

No categories assigned to this patent yet.

Assign Category Tag