US4008568A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Combustor support
Assignee: Rolls Royce Corp
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Filing: 1976-03-01
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Granted: 1977-02-22
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Expires: 1996-03-01
Abstract
Abstract A combustor assembly includes a porous, laminated metal dome and an elongated tubular body portion disposed vertically within an air supply plenum. The dome and body portion are joined by a yieldable ring and a plurality of radially inwardly directed convolutions on one end of the body portion. A load support member is telescoped over the upper end of the dome and includes a tubular axial extension with a plurality of radially inwardly directed convolutions connected to the body portion and wherein the support member includes a plurality of radially outwardly directed spider arms extending from a support flange on the upper end of the support member secured to a fixed fuel nozzle pad whereby the porous laminated metal dome is supported for free flex movement with respect to the pad during combustor operation.
Inventors
- 👤 Esten W. Spears, Jr.
- 👤 Eugene R. Young
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-05 07:30
CPC Classifications
F; F23; F23R; F23R3/00; F23R3/42; F23R3/60
Claims Analysis
Total Claims: 4
Claim 1
Independent Claim
242 words
A combustor support assembly for vertically supporting axially aligned combustor dome and liner segments on nozzle support pad comprising a spider support member having a top flange at one end thereof with a central opening adapted to receive a fuel distribution nozzle and a peripheral flange of the other end thereof, means on said top flange for fixedly securing it to the nozzle support pad, said spider support member having a plurality of circumferentially spaced radially outwardly formed spider arms extending from said top flange to said peripheral flange, an annular support plate having opposite ends thereon with one end thereof secured to said peripheral flange, a combustor liner having one end telescoped into the opposite end of said support plate in radially inward spaced relationship therewith, convoluted spacer elements interposed between said combustor liner and said support plate having circumferentially spaced segments thereon secured to said combustor liner and support plate and flex segments between said fixed segments for yieldably supporting said liner on said support plate, a dome of porous material located concentrically within said support plate and having an inclined top in spaced parallelism with said spider arms, means for supporting said dome on said one end of said liner for free axial and radial movement with respect to said spider support plate with said spider support plate assuming the full vertical weight of said liner and dome and said dome being unloaded vertically to reduce stress loading thereof.
Claim 2
Dependent Claim
242 words
A combustor support assembly for vertically supporting axially aligned combustor dome and liner segments on nozzle support pad comprising a spider support member having a top flange at one end thereof with a central opening adapted to receive a fuel distribution nozzle and a peripheral flange of the other end thereof, means on said top flange for fixedly securing it to the nozzle support pad, said spider support member having a plurality of circumferentially spaced radially outwardly formed spider arms extending from said top flange to said peripheral flange, an annular support plate having opposite ends thereon with one end thereof secured to said peripheral flange, a combustor liner having one end telescoped into the opposite end of said support plate in radially inward spaced relationship therewith, convoluted spacer elements interposed between said combustor liner and said support plate having circumferentially spaced segments thereon secured to said combustor liner and support plate and flex segments between said fixed segments for yieldably supporting said liner on said support plate, a dome of porous material located concentrically within said support plate and having an inclined top in spaced parallelism with said spider arms, means for supporting said dome on said one end of said liner for free axial and radial movement with respect to said spider support plate with said spider support plate assuming the full vertical weight of said liner and dome and said dome being unloaded vertically to reduce stress loading thereof.
Claim 3
Dependent Claim
201 words
A combustor support assembly for vertically supporting axially aligned combustor dome and liner segments within an air supply plenum casing comprising a support member having a top flange with an opening adapted to receive a fuel distribution nozzle, means on said flange for securing it to the casing, said support having an inclined top and a peripheral side wall, a combustor liner having one end telescoped into the support, convoluted spacer element interposed between said combustion liner and said side wall having circumferentially spaced segments thereon secured to said combustor liner and said side wall and flex segments between said fixed segments for yieldably supporting said liner on said side wall, a dome of porous material located concentrically within said support member and having an inclined inlet end in spaced parallelism with said inclined top, means including a float ring on said dome for receiving a fuel nozzle secured to the casing and for supporting said dome on said one end of said liner for free axial and radial movement with respect to said support member with said support member assuming the full vertical weight of said liner and dome and said dome being unloaded vertically to reduce stress loading thereof.
Claim 4
Dependent Claim
201 words
A combustor support assembly for vertically supporting axially aligned combustor dome and liner segments within an air supply plenum casing comprising a support member having a top flange with an opening adapted to receive a fuel distribution nozzle, means on said flange for securing it to the casing, said support having an inclined top and a peripheral side wall, a combustor liner having one end telescoped into the support, convoluted spacer element interposed between said combustion liner and said side wall having circumferentially spaced segments thereon secured to said combustor liner and said side wall and flex segments between said fixed segments for yieldably supporting said liner on said side wall, a dome of porous material located concentrically within said support member and having an inclined inlet end in spaced parallelism with said inclined top, means including a float ring on said dome for receiving a fuel nozzle secured to the casing and for supporting said dome on said one end of said liner for free axial and radial movement with respect to said support member with said support member assuming the full vertical weight of said liner and dome and said dome being unloaded vertically to reduce stress loading thereof.
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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) | 1980-02-22 | 1980-08-23 | 1981-02-22 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1984-02-22 | 1984-08-23 | 1985-02-22 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1988-02-22 | 1988-08-23 | 1989-02-22 | $7700.00 | Window Closed / Lapsed |