US4730453A
Expired / Lapsed
US
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Afterburner fuel injection system
Assignee: Safran Aircraft Engines SAS
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Filing: 1986-10-20
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Granted: 1988-03-15
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Expires: 2006-10-20
Abstract
Abstract An afterburner fuel injection system is disclosed which utilizes a plurality of individual fuel injectors displayed in a radial array around the periphery of a turbojet afterburner. An atomizing chamber is associated with each fuel injection conduit to achieve a homogeneous atomization of the fuel with the exhaust gases passing through the afterburner. Each fuel injector is individually connected to a fuel supply source and a source of purging air to minimize the delay in afterburner ignition and to prevent coking of the injector nozzles.
Inventors
- 👤 Rene A. Benoist
- 👤 Guy J. Lapergue
- 👤 Jacques A. Legueux
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-28 21:34
CPC Classifications
F; F23; F23R; F23R3/00; F23R3/02; F23R3/16; F23R3/18; F23R3/20; F05; F05B; F05B2260/00; F05B2260/60; F05B2260/602
Claims Analysis
Total Claims: 9
Claim 1
Independent Claim
223 words
In a gas turbine engine having at least one turbine wheel, an afterburner and a flame holder located in the afterburner such that exhaust gases pass through the turbine wheel into the afterburner from an upstream direction toward a downstream direction generally parallel to a longitudinal axis of the turbojet engine, the improved system for injecting fuel into the exhaust gas stream in the afterburner comprising: (a) a plurality of individual tubular injectors regularly distributed about the periphery of the afterburner and extending into the afterburner generally perpendicularly to the flow of gases therethrough; (b) fuel supply means to supply fuel to each of the tubular injectors independently of the other tubular injectors; (c) atomizing chamber means, one atomizing chamber associated with each tubular injector each atomizing chamber means defining at least one intake orifice to allow exhaust gas to pass into the chamber, and further defining a plurality of exit orifices, such that (i) the number of exit orifices is greater than the number of intake orifices, and (ii) the size of each exit orifice is smaller then the size of the at least one intake orifice; and, (d) nozzle means associated with each tubular injector to spray fuel into the associated atomizing chamber so as to create a finely atomized fuel mixture which passes through the exit orifices into the afterburner.
Claim 2
Dependent Claim
223 words
In a gas turbine engine having at least one turbine wheel, an afterburner and a flame holder located in the afterburner such that exhaust gases pass through the turbine wheel into the afterburner from an upstream direction toward a downstream direction generally parallel to a longitudinal axis of the turbojet engine, the improved system for injecting fuel into the exhaust gas stream in the afterburner comprising: (a) a plurality of individual tubular injectors regularly distributed about the periphery of the afterburner and extending into the afterburner generally perpendicularly to the flow of gases therethrough; (b) fuel supply means to supply fuel to each of the tubular injectors independently of the other tubular injectors; (c) atomizing chamber means, one atomizing chamber associated with each tubular injector each atomizing chamber means defining at least one intake orifice to allow exhaust gas to pass into the chamber, and further defining a plurality of exit orifices, such that (i) the number of exit orifices is greater than the number of intake orifices, and (ii) the size of each exit orifice is smaller then the size of the at least one intake orifice; and, (d) nozzle means associated with each tubular injector to spray fuel into the associated atomizing chamber so as to create a finely atomized fuel mixture which passes through the exit orifices into the afterburner.
Claim 3
Dependent Claim
42 words
The improved system according to claim 1 wherein the at least one intake orifice is defined by the atomizing chamber means so as to face in the upstream direction and wherein the at least one exit orifice faces in a downstream direction.
Claim 4
Dependent Claim
67 words
The improved system according to claim 2 wherein a radially innermost end of the individual tubular injector defines the nozzle means and wherein the atomizing chamber means further comprises a wall spaced from and aligned with the nozzle means, the wall defining a generally spherical, concave indentation to cause splattering of the fuel impinging thereon from the nozzle means to assist in the atomization of the fuel.
Claim 5
Dependent Claim
94 words
The improved system according to claim 2 wherein the atomizing chamber means comprises a cylindrical sleeve disposed about the individual tubular injectors, the cylindrical sleeve defining at least one intake orifice and at least one exit orifice, the orifices having axes extending substantially parallel to each other and substantially parallel to the direction of gas flow through the afterburner; and wherein each tubular injector defines at least two nozzle means within the cylindrical sleeve, the nozzle means having axes extending generally perpendicular to a plane containing the axes of the intake and exit orifices.
Claim 6
Dependent Claim
75 words
The improved system according to claim 4 wherein the cylindrical sleeve defines a pair of intake orifices and three rows of exit orifices, a first row of exit orifices having axes extending substantially parallel to the axes of the intake orifices, the second and third rows of exit orifices having axes extending at an angle of between 30° and 50° with respect to a plane containing the axes of the first row of exit orifices.
Claim 7
Dependent Claim
75 words
The improved system according to claim 4 wherein the cylindrical sleeve defines a pair of intake orifices and three rows of exit orifices, a first row of exit orifices having axes extending substantially parallel to the axes of the intake orifices, the second and third rows of exit orifices having axes extending at an angle of between 30° and 50° with respect to a plane containing the axes of the first row of exit orifices.
Claim 8
Dependent Claim
69 words
The improved system according to claim 1 further comprising: (a) air supply means associated with each tubular injector to supply purging air to the fuel circuit; (b) a control valve interposed between the air supply means and each tubular injector to control the flow of purging air to each tubular injector; and, (c) means to actuate each control valve so as to simultaneously purge all of the tubular injectors.
Claim 9
Dependent Claim
77 words
The improved system according to claim 1 further comprising: (a) an outer wall concentrically disposed about the afterburner so as to define a secondary air passage therebetween; (b) a plurality of fastening braces extending generally radially between the outer wall and the afterburner; and, (c) means to attach individual tubular injectors to the outer wall such that each is diametrically opposite a fastening brace and such that the atomizing chamber means is disposed entirely within the afterburner.
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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) | 1991-03-15 | 1991-09-14 | 1992-03-15 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1995-03-15 | 1995-09-14 | 1996-03-15 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1999-03-15 | 1999-09-14 | 2000-03-15 | $7700.00 | Window Closed / Lapsed |