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US4677828A
Expired / Lapsed
US
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Circumferentially area ruled duct
Assignee: RTX Corp
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Filing: 1984-11-13
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Granted: 1987-07-07
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Expires: 2004-11-13
Abstract
Abstract The area ruling of an annular diffuser disposed between the compressor and burner of a gas turbine engine is proportioned in a circumferential direction so that the maximum area ruling is adjacent the struts supporting the diffuser walls and the minimum is mid-way between the struts so as to achieve a substantial uniform velocity profile of the exiting air in the circumferential direction.
Inventors
- 👤 John A. Matthews
- 👤 Edmund E. Striebel
- 👤 Domingo Sepulveda
- 👤 Francis C. Pane, Jr.
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-07 07:30
CPC Classifications
F; F01; F01D; F01D5/00; F01D5/12; F01D5/14; F01D5/141; F01D5/142; F01D5/143; F01D9/00; F01D9/02; F01D9/04; F01D9/047; F04; F04D; F04D29/00; F04D29/40; F04D29/52; F04D29/54; F04D29/541; F23; F23R; F23R3/00; F23R3/02; Y; Y02; Y02T; Y02T50/00; Y02T50/60; Y10; Y10S; Y10S415/00; Y10S415/914
Claims Analysis
Total Claims: 4
Claim 1
Independent Claim
173 words
In combination, a gas turbine engine having a burner for receiving a working medium, an annular diffuser having an inner conically shaped wall and an outer conically shaped wall diverging relative to each other for diffusing said working medium prior to entering said burner, at least eight, but less then 20, equally spaced struts between said inner wall and outer wall supporting said walls in spaced relationship, said struts defining with said inner and outer walls open-ended passageways within said diffuser and being an obstruction to the flow passing therethrough, means for compensating for said obstruction to obtain a relatively uniform velocity profile in the circumferential direction, said means including a circumferential increase in cross sectional flow area of each of the diffuser passageways formed by each of said inner and outer walls on either side of each of said struts, and said inner and outer walls having a displaced portion of concave shape merging with an adjacent strut and further including convex wall portions disposed between each pair of adjacent concave portions.
Claim 2
Dependent Claim
173 words
In combination, a gas turbine engine having a burner for receiving a working medium, an annular diffuser having an inner conically shaped wall and an outer conically shaped wall diverging relative to each other for diffusing said working medium prior to entering said burner, at least eight, but less then 20, equally spaced struts between said inner wall and outer wall supporting said walls in spaced relationship, said struts defining with said inner and outer walls open-ended passageways within said diffuser and being an obstruction to the flow passing therethrough, means for compensating for said obstruction to obtain a relatively uniform velocity profile in the circumferential direction, said means including a circumferential increase in cross sectional flow area of each of the diffuser passageways formed by each of said inner and outer walls on either side of each of said struts, and said inner and outer walls having a displaced portion of concave shape merging with an adjacent strut and further including convex wall portions disposed between each pair of adjacent concave portions.
Claim 3
Dependent Claim
141 words
In combination, a gas turbine engine, a diffuser in said engine having a pair of diverging annular walls for flowing fluid from an upstream to a downstream direction, at least eight, but less than 20, equally spaced strut-like elements in said diffuser uniformly spaced around the circumference thereof defining open-ended passageways and being an obstruction to the flow passing therethrough, means for compensating for said obstruction to obtain a relatively uniform velocity profile in the circumferential direction, said means including a circumferential increase in cross sectional flow area of each of the diffuser passageways formed by each of said annular walls on either side of each of said strut-like elements and said annular walls having a displaced portion of concave shape merging with an adjacent strut-like element and further including convex wall portions disposed between each pair of adjacent concave portions.
Claim 4
Dependent Claim
141 words
In combination, a gas turbine engine, a diffuser in said engine having a pair of diverging annular walls for flowing fluid from an upstream to a downstream direction, at least eight, but less than 20, equally spaced strut-like elements in said diffuser uniformly spaced around the circumference thereof defining open-ended passageways and being an obstruction to the flow passing therethrough, means for compensating for said obstruction to obtain a relatively uniform velocity profile in the circumferential direction, said means including a circumferential increase in cross sectional flow area of each of the diffuser passageways formed by each of said annular walls on either side of each of said strut-like elements and said annular walls having a displaced portion of concave shape merging with an adjacent strut-like element and further including convex wall portions disposed between each pair of adjacent concave portions.
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) | 1990-07-06 | 1991-01-05 | 1991-07-07 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1994-07-06 | 1995-01-05 | 1995-07-07 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1998-07-06 | 1999-01-05 | 1999-07-07 | $7700.00 | Window Closed / Lapsed |