US4802337A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Flameholder for a turbojet engine afterburner
Assignee: Safran Aircraft Engines SAS
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Filing: 1987-02-27
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Granted: 1989-02-07
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Expires: 2007-02-27
Abstract
Abstract A flameholder structure for a turbojet engine afterburner is disclosed in which a generally "V" shaped flameholder ring has a plurality of substantially radially extending fins attached to and extending radially outwardly from its outer surface. A portion of each of the fins is disposed at an angle to the gas flow so as to impart a cylindrical rotation to that portion of the flow passing over the fins. The cylindrical rotation of the flow increases the shear effect to thereby improve the stability of the flame front and increase the efficiency of the afterburner.
Inventors
- 👤 Jacques E. J. Caruel
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-31 17:28
CPC Classifications
F; F23; F23R; F23R3/00; F23R3/02; F23R3/16; F23R3/18
Claims Analysis
Total Claims: 7
Claim 1
Independent Claim
167 words
A flameholder structure for a turbojet engine afterburner having an afterburner duct to direct turbojet engine gases from an upstream portion toward a downstream portion, the flameholder structure comprising: (a) an annular flameholder ring having a substantially "V"-shaped cross-section defined by a radially outer leg portion and a radially inner leg portion interconnected at upstream ends by a base portion such that the "V" shape opens in a downstream direction; and (b) a plurality of substantially radially extending fins regularly distributed about the periphery of the annular flameholder ring and extending radially outwardly therefrom into the turbojet engine gas flow from only the radially outer leg portion of the flameholder ring, each fin having at least a downstream portion attached to the radially outer leg portion and in contact therewith along substantially its entire length, each downstream portion disposed at an angle to the direction of the gas flow so as to impart a circumferential rotation to that portion of the gas flow passing across the fins.
Claim 2
Dependent Claim
167 words
A flameholder structure for a turbojet engine afterburner having an afterburner duct to direct turbojet engine gases from an upstream portion toward a downstream portion, the flameholder structure comprising: (a) an annular flameholder ring having a substantially "V"-shaped cross-section defined by a radially outer leg portion and a radially inner leg portion interconnected at upstream ends by a base portion such that the "V" shape opens in a downstream direction; and (b) a plurality of substantially radially extending fins regularly distributed about the periphery of the annular flameholder ring and extending radially outwardly therefrom into the turbojet engine gas flow from only the radially outer leg portion of the flameholder ring, each fin having at least a downstream portion attached to the radially outer leg portion and in contact therewith along substantially its entire length, each downstream portion disposed at an angle to the direction of the gas flow so as to impart a circumferential rotation to that portion of the gas flow passing across the fins.
Claim 3
Dependent Claim
32 words
The flameholder structure according to claim 1 wherein each of the fins has a portion extending from the base portion in an upstream direction substantially parallel to the direction of gas flow.
Claim 4
Dependent Claim
23 words
The flameholder structure according to claim 2 further comprising a generally cylindrical continuous sleeve interconnecting radially outermost edges of the plurality of fins.
Claim 5
Dependent Claim
38 words
The flameholder structure according to claim 3 further comprising a flange formed on the cylindrical sleeve and extending therefrom in an upstream direction such that a distal edge of the flange extends beyond upstream edges of the fins.
Claim 6
Dependent Claim
23 words
The flameholder structure according to claim 1 further comprising a generally cylindrical continuous sleeve interconnecting radially outermost edges of the plurality of fins.
Claim 7
Dependent Claim
38 words
The flameholder structure according to claim 5 further comprising a flange formed on the cylindrical sleeve and extending therefrom in an upstream direction such that a distal edge of the flange extends beyond upstream edges of the fins.
References Cited (Backward Citations)
GB706698A
Cited
US2935847A
Cited
US3056261A
Cited
US3154920A
Cited
US3176465A
Cited
US3153324A
Cited
US3931707A
Cited
US4064691A
Cited
US4259839A
Cited
US4445339A
Cited
US4418531A
Cited
US4490973A
Cited
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1992-02-07 | 1992-08-08 | 1993-02-07 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1996-02-07 | 1996-08-08 | 1997-02-07 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 2000-02-07 | 2000-08-08 | 2001-02-07 | $7700.00 | Window Closed / Lapsed |