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US4843825A Expired / Lapsed US ⏱️ 0.0 years remaining

Combustor dome heat shield

Assignee: RTX Corp
•
Filing: 1988-05-16
•
Granted: 1989-07-04
•
Expires: 2008-05-16
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Abstract

Abstract An annular combustor has a plurality of fuel injectors 14, each supporting a heat shield 30. Each shield has an overlap portion 42 deflecting cooling air passing between the shields, thereby avoiding a curtain of air between the flames of adjacent fuel injectors.

Inventors

  • 👤 Jim A. Clark

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-27 21:55
CPC Classifications
F; F23; F23R; F23R3/00; F23R3/02; F23R3/04; F23R3/10; F23R3/002; F05; F05B; F05B2260/00; F05B2260/20; F05B2260/201

Claims Analysis

Total Claims: 7
Claim 1
Independent Claim 149 words
An annular combustor for a gas turbine engine comprising: an annular combustion chamber having an inner circumference and an outer circumference; a plurality of circumferentially spaced fuel injectors in said combustion chamber; swirl means for introducing fuel and primary air to said combustion chamber in a swirl around the axis of each of said injectors; at least one ignitor extending from one circumference of said combustion chamber; an annular support dome structure for supporting said plurality of fuel injectors and for passing secondary air therethrough; a plurality of circumferentially spaced heat shields interposed between said dome structure and said combustion chamber, each one of said heat shields secured to one of said fuel injectors; and an overlap portion on each of said heat shields axially overlapping an adjacent heat shield, whereby secondary air passing between said heat shields is deflected away from the axial direction toward the circumferential direction.
Claim 2
Dependent Claim 149 words
An annular combustor for a gas turbine engine comprising: an annular combustion chamber having an inner circumference and an outer circumference; a plurality of circumferentially spaced fuel injectors in said combustion chamber; swirl means for introducing fuel and primary air to said combustion chamber in a swirl around the axis of each of said injectors; at least one ignitor extending from one circumference of said combustion chamber; an annular support dome structure for supporting said plurality of fuel injectors and for passing secondary air therethrough; a plurality of circumferentially spaced heat shields interposed between said dome structure and said combustion chamber, each one of said heat shields secured to one of said fuel injectors; and an overlap portion on each of said heat shields axially overlapping an adjacent heat shield, whereby secondary air passing between said heat shields is deflected away from the axial direction toward the circumferential direction.
Claim 3
Dependent Claim 54 words
A combustor as in claim 1: said swirl means establishing a common circumferential flow direction on each radial side of said plurality of fuel injectors; and said overlap portion of each heat shield overlapping the adjacent heat shield to deflect secondary air passing therebetween in the same circumferential direction as said common flow direction.
Claim 4
Dependent Claim 29 words
A combustor as in claim 2: said overlap portion of each heat shield overlapping the adjacent heat shield only on one radial side of said plurality of fuel injectors.
Claim 5
Dependent Claim 21 words
A combustor as in claim 3: said one radial side being the radial side contiguous with the circumference containing said ignitor.
Claim 6
Dependent Claim 28 words
A combustor as in claim 2: said overlap portion of each heat shield overlapping the adjacent heat shield on both radial sides of said plurality of fuel injectors.
Claim 7
Dependent Claim 12 words
A combustor as in claim 4: said circumference being the outer circumference.

References Cited (Backward Citations)

US2768497A Cited
CA994115A Cited
US4085581A Cited
US4180974A Cited
US4222230A Cited
US4356693A Cited
US4567730A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1992-07-03 1993-01-02 1993-07-04 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1996-07-03 1997-01-02 1997-07-04 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 2000-07-03 2001-01-02 2001-07-04 $7700.00 Window Closed / Lapsed

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