Patent US3978664A successfully refreshed from Google Patents.
US3978664A
Expired / Lapsed
US
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Gas turbine engine diffuser
Assignee: RTX Corp
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Filing: 1975-09-29
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Granted: 1976-09-07
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Expires: 1995-09-29
Abstract
Abstract Apparatus for diffusing the working medium gases which flow from the compression section of a gas turbine engine is disclosed. A controlled diffuser comprising an inner and an outer flow path shroud initially increases the static pressure and decreases the velocity of the medium gases flowing therebetween. The diffusion process is completed downstream of the flow path shrouds in a dump region of rapidly increasing flow area. The inner and outer shrouds of the controlled diffuser are concentrically supported at both the upstream and downstream ends. The inner and outer shrouds support the compressor exit vanes within the path of working medium gases flowing from the compressor and damp vane vibration during operation of the engine.
Inventors
- 👤 Robert W. Parker
- 👤 Bertus Ooms
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-07 07:45
CPC Classifications
F; F04; F04D; F04D29/00; F04D29/40; F04D29/52; F04D29/54; F04D29/541; F04D29/542
Claims Analysis
Total Claims: 11
Claim 1
Independent Claim
190 words
In a gas turbine engine having a compression section which includes a plurality of exit vanes circumferentially disposed within the path of working medium gases flowing from the compression section and having a diffusion section downstream of the compression section which includes an inner wall and an outer wall which are joined by a plurality of radially oriented struts extending between the inner and outer walls, apparatus for diffusing the working medium gases which flow from the compression section to the combustion section during operation of the engine, comprising: an inner flow path shroud having an upstream end which is joined to the exit vanes of the compression section and a downstream end which is located radially outboard of and joined to the inner wall of the diffusion section; and an outer flow path shroud having an upstream end which is attached to the exit guide vanes of the compression section and a downstream end which engages the outer wall of the diffusion section, the inner and outer shrouds forming a controlled diffuser upstream of said struts which is free of protuberances in at least the predominant axial portion thereof
Claim 2
Dependent Claim
190 words
In a gas turbine engine having a compression section which includes a plurality of exit vanes circumferentially disposed within the path of working medium gases flowing from the compression section and having a diffusion section downstream of the compression section which includes an inner wall and an outer wall which are joined by a plurality of radially oriented struts extending between the inner and outer walls, apparatus for diffusing the working medium gases which flow from the compression section to the combustion section during operation of the engine, comprising: an inner flow path shroud having an upstream end which is joined to the exit vanes of the compression section and a downstream end which is located radially outboard of and joined to the inner wall of the diffusion section; and an outer flow path shroud having an upstream end which is attached to the exit guide vanes of the compression section and a downstream end which engages the outer wall of the diffusion section, the inner and outer shrouds forming a controlled diffuser upstream of said struts which is free of protuberances in at least the predominant axial portion thereof
Claim 3
Dependent Claim
28 words
The invention according to claim 1 wherein the inner and outer shrouds terminate at the same downstream axial position with respect to the path of working medium gases.
Claim 4
Dependent Claim
20 words
The invention according to claim 1 wherein the inner and outer shrouds extend into the combustion section of the engine.
Claim 5
Dependent Claim
50 words
The invention according to claim 1 wherein the outer wall has one or more support pads facing in a radially inward direction and the outer flow path shroud has a support surface which faces radially outward and engages one or more of the support pads of the outer annular wall.
Claim 6
Dependent Claim
183 words
In a gas turbine engine having a compression section and a combustion section, a diffusion section which is disposed between the compression and combustion sections and which comprises: an inner annular wall; an outer annular wall having one or more support pads facing in a radially inward direction; a plurality of radially extending struts which join the inner wall to the outer wall; an inner flow path shroud joined to the inner annular wall and extending in an upstream axial direction toward the compressor section of the engine; a plurality of stator vanes attached to and extending radially outward from the inner annular shroud; and an outer flow path shroud joined to the outer ends of the plurality of stator vanes and extending axially downstream to the outer wall of the combustion section and having a support surface which faces radially outward to engage one or more of the support pads of the outer annular wall, wherein the inner and outer shrouds form a controlled diffuser upstream of said struts which is free of protuberances in at least the predominant axial portion thereof.
Claim 7
Dependent Claim
183 words
In a gas turbine engine having a compression section and a combustion section, a diffusion section which is disposed between the compression and combustion sections and which comprises: an inner annular wall; an outer annular wall having one or more support pads facing in a radially inward direction; a plurality of radially extending struts which join the inner wall to the outer wall; an inner flow path shroud joined to the inner annular wall and extending in an upstream axial direction toward the compressor section of the engine; a plurality of stator vanes attached to and extending radially outward from the inner annular shroud; and an outer flow path shroud joined to the outer ends of the plurality of stator vanes and extending axially downstream to the outer wall of the combustion section and having a support surface which faces radially outward to engage one or more of the support pads of the outer annular wall, wherein the inner and outer shrouds form a controlled diffuser upstream of said struts which is free of protuberances in at least the predominant axial portion thereof.
Claim 8
Dependent Claim
23 words
The invention according to claim 5 wherein said plurality of stator vanes are attached to said inner annular shroud by mechanical attaching means.
Claim 9
Dependent Claim
13 words
The invention according to claim 6 wherein said mechanical attaching means are rivets.
Claim 10
Dependent Claim
17 words
The invention according to claim 1 wherein the controlled diffuser is mechanically detachable from the diffusion section.
Claim 11
Dependent Claim
40 words
The invention according to claim 1 wherein the inner and outer walls of the diffusion section define downstream of the controlled diffuser a dump diffuser region into which the medium gases are flowed prior to distribution about the combustion section.
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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) | 1979-09-07 | 1980-03-08 | 1980-09-07 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1983-09-07 | 1984-03-08 | 1984-09-07 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1987-09-07 | 1988-03-08 | 1988-09-07 | $7700.00 | Window Closed / Lapsed |