Patent US4356693A successfully refreshed from Google Patents.
US4356693A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Gas turbine engine combustion chambers
Assignee: Rolls Royce PLC
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Filing: 1980-06-27
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Granted: 1982-11-02
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Expires: 2000-06-27
Abstract
Abstract In a gas turbine engine having a can annular combustion system, the diffusion passage between the outlet annulus of the engine compressor and the inlets to the individual combustion chambers located in an annular housing, is partially defined by diffusion control housings, one of each of which is integral with the upstream end of a respective one of the combustion chambers. Each diffusion control housing is wedge-like in planform and increases in circumferential width and radial height in the downstream direction. An opening is provided to receive a fuel injector and an air outlet or inlets is located at the upstream end of each housing. The air inlet can be in the form of a single opening at the apex of the housing or in the form of an opening in each flank of the housing.
Inventors
- 👤 Graham J. Jeffery
- 👤 Richard C. Adkins
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-30 06:19
CPC Classifications
F; F23; F23R; F23R3/00; F23R3/42; F23R3/46; F23R3/02; F23R3/04; F23R2900/00; F23R2900/00002
Claims Analysis
Total Claims: 5
Claim 1
Independent Claim
213 words
A gas turbine engine combustion system comprising: an annular housing defined by inner and outer walls; a plurality of combustion chambers equi-spaced apart and circumferentially arranged within said annular housing, each of said combustion chambers having an upstream end and a downstream end; a diffusion passage upstream of the upstream ends of said combustion chambers, said diffusion passage being defined by upstream inner and outer portions respectively of the inner and outer walls of said annular housing and being arranged to receive a flow of compressed air; and a plurality of diffusion control housings partially defining said diffusion passage, each of said diffusion control housings being axially aligned with and extending from the upstream end of a respective one of said combustion chambers, each of said diffusion control housings being wedge-like in plan form and having a circumferential width and a radial height increasing in a downstream direction, and each of said diffusion control housings comprising radial side walls and circumferential end walls and having an upstream air inlet for receiving at least a portion of the compressed air from said diffusion passage and discharging the same into the respective one of said axially aligned combustion chambers, each of said diffusion control housings further having an opening arranged to receive a fuel injector.
Claim 2
Dependent Claim
213 words
A gas turbine engine combustion system comprising: an annular housing defined by inner and outer walls; a plurality of combustion chambers equi-spaced apart and circumferentially arranged within said annular housing, each of said combustion chambers having an upstream end and a downstream end; a diffusion passage upstream of the upstream ends of said combustion chambers, said diffusion passage being defined by upstream inner and outer portions respectively of the inner and outer walls of said annular housing and being arranged to receive a flow of compressed air; and a plurality of diffusion control housings partially defining said diffusion passage, each of said diffusion control housings being axially aligned with and extending from the upstream end of a respective one of said combustion chambers, each of said diffusion control housings being wedge-like in plan form and having a circumferential width and a radial height increasing in a downstream direction, and each of said diffusion control housings comprising radial side walls and circumferential end walls and having an upstream air inlet for receiving at least a portion of the compressed air from said diffusion passage and discharging the same into the respective one of said axially aligned combustion chambers, each of said diffusion control housings further having an opening arranged to receive a fuel injector.
Claim 3
Dependent Claim
24 words
A combustion system as claimed in claim 1 in which the air inlet to each diffusion control housing is located at its upstream end.
Claim 4
Dependent Claim
31 words
A combustion system as claimed in claim 1 in which the air inlet to each diffusion control housing comprises openings in each of the side walls of the diffusion control housing.
Claim 5
Dependent Claim
46 words
A combustion system as claimed in claim 1, in which each diffusion control housing extends between the upstream inner and outer portions of the inner and outer walls which define the diffusion passage and in cross-section is in the form of a sector of an annulus.
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) | 1985-11-01 | 1986-05-03 | 1986-11-02 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1989-11-01 | 1990-05-03 | 1990-11-02 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1993-11-01 | 1994-05-03 | 1994-11-02 | $7700.00 | Window Closed / Lapsed |