Patent US4527386A successfully refreshed from Google Patents.
US4527386A
Expired / Lapsed
US
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Diffuser for gas turbine engine
Assignee: RTX Corp
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Filing: 1983-02-28
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Granted: 1985-07-09
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Expires: 2003-02-28
Abstract
Abstract A diffuser system for a gas turbine engine includes a prediffuser and a piping system that diverts the flow into two streams. One stream captures the prediffuser discharge air at the center of the gas path where the total pressure is at its highest level and provides an additional stage of diffusing before dumping it around the burner to supply liner cooling air, turbine cooling air and if necessary, small amounts of dilution air to trim radial temperature profile. The other stream is ducted directly into the burner avoiding the typical dump diffuser losses.
Inventors
- 👤 Stanley J. Markowski
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-07 19:18
CPC Classifications
F; F02; F02C; F02C7/00; F02C7/12; F02C7/16; F02C7/18; F23; F23R; F23R3/00; F23R3/02; Y; Y02; Y02T; Y02T50/00; Y02T50/60
Claims Analysis
Total Claims: 3
Claim 1
Independent Claim
229 words
In combination with an annular burner having an inner and outer liner defining an annular combustion chamber, a dome interconnecting said inner and outer liner for covering the front end of said annular combustion chamber, a plurality of air injectors mounted on apertures circumferentially formed around the front end of said dome, each of said air injectors having a first straight through central passageway for leading compressor discharge air in the central portion of the annular space of said annular combustion chamber for defining the secondary flow of combustion and dilution air, an annular straight through passage defining a second passageway concentric with said first passageway for leading the compressor discharge air into the annular space of said annular combustion chamber, a diffuser feed system having an annular prediffuser, a plurality of first pipes having a conical portion flaring from a smaller to larger diameter in the direction of flow for effectuating diffusion of the air stream for leading high total pressure diffused air in a cavity surrounding said annular combustion chamber, and a straight through pipe collecting air adjacent the boundary of said prediffuser connected to the front of each of said air injector and said first pipes connected to the discharge end of said prediffuser but spaced from said boundary layer to deliver solely the air with the higher total pressure of the air in said prediffuser.
Claim 2
Dependent Claim
229 words
In combination with an annular burner having an inner and outer liner defining an annular combustion chamber, a dome interconnecting said inner and outer liner for covering the front end of said annular combustion chamber, a plurality of air injectors mounted on apertures circumferentially formed around the front end of said dome, each of said air injectors having a first straight through central passageway for leading compressor discharge air in the central portion of the annular space of said annular combustion chamber for defining the secondary flow of combustion and dilution air, an annular straight through passage defining a second passageway concentric with said first passageway for leading the compressor discharge air into the annular space of said annular combustion chamber, a diffuser feed system having an annular prediffuser, a plurality of first pipes having a conical portion flaring from a smaller to larger diameter in the direction of flow for effectuating diffusion of the air stream for leading high total pressure diffused air in a cavity surrounding said annular combustion chamber, and a straight through pipe collecting air adjacent the boundary of said prediffuser connected to the front of each of said air injector and said first pipes connected to the discharge end of said prediffuser but spaced from said boundary layer to deliver solely the air with the higher total pressure of the air in said prediffuser.
Claim 3
Dependent Claim
24 words
In combination as in claim 1 including means for admitting fuel in each of said air injectors to mix with the air flowing therethrough.
References Cited (Backward Citations)
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1988-07-08 | 1989-01-07 | 1989-07-09 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1992-07-08 | 1993-01-07 | 1993-07-09 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1996-07-08 | 1997-01-07 | 1997-07-09 | $7700.00 | Window Closed / Lapsed |