Patent US4555901A successfully refreshed from Google Patents.
US4555901A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Combustion chamber construction
Assignee: General Electric Co
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Filing: 1972-12-19
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Granted: 1985-12-03
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Expires: 1992-12-19
Abstract
Abstract A combustion chamber for use in gas turbine engines is provided with a liner formed of a high temperature material. The liner includes a plurality of panels of material mounted by means of a slideable, frictional mounting arrangement upon a high strength structural frame. As a result of this mounting arrangement, the liner is substantially isolated from structural forces associated with the combustion chamber, while the frame is substantially isolated from thermal stresses associated with the liner. Means are provided for positioning and securing individual panel members axially relative to the frame. The panels may be continuous annular bodies, or may be circumferentially segmented. In the latter case, means are provided for mounting individual panels in a slideable, frictional cooperation with laterally adjacent panels, as well as for sealing the abutting junctions. The individual liner panels may be easily removed for repair or replacement without disassembling the frame and associated components.
Inventors
- 👤 Thomas G. Wakeman
- 👤 Harvey M. Maclin
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-26 09:52
CPC Classifications
F; F23; F23R; F23R3/00; F23R3/02; F23R3/04; F23R3/06; F23R3/08; F23R3/002; F05; F05B; F05B2230/00; F05B2230/70; F05B2230/80
Claims Analysis
Total Claims: 13
Claim 1
Independent Claim
167 words
A combustion chamber for use in gas turbine engines, the chamber comprising: an inlet for receiving air and fuel to be burned; an outlet for expelling products of combustion; high strength structural frame means disposed between the inlet and the outlet for supporting mechanical forces associated with the chamber; liner means cooperating with the frame means and defining a combustion zone, said liner means including a plurality of panels of high temperature material; axial mounting means for positioning said panels axially with respect to said frame means, said axial mounting means including: first shoulder means cooperating with preselected of said panels, and partially defining a circumferential slot of first predetermined axial width therein; second shoulder means cooperating with the frame means; a flange of predetermined second axial width less than said first width, said flange formed upon said second shoulder means for disposition within the slot; and a circumferentially extending retainer ring of predetermined third axial width suitable for disposition, together with said flange, within said slot.
Claim 2
Dependent Claim
167 words
A combustion chamber for use in gas turbine engines, the chamber comprising: an inlet for receiving air and fuel to be burned; an outlet for expelling products of combustion; high strength structural frame means disposed between the inlet and the outlet for supporting mechanical forces associated with the chamber; liner means cooperating with the frame means and defining a combustion zone, said liner means including a plurality of panels of high temperature material; axial mounting means for positioning said panels axially with respect to said frame means, said axial mounting means including: first shoulder means cooperating with preselected of said panels, and partially defining a circumferential slot of first predetermined axial width therein; second shoulder means cooperating with the frame means; a flange of predetermined second axial width less than said first width, said flange formed upon said second shoulder means for disposition within the slot; and a circumferentially extending retainer ring of predetermined third axial width suitable for disposition, together with said flange, within said slot.
Claim 3
Dependent Claim
25 words
The combustion chamber of claim 1 wherein said third width is such that said flange is retained within the slot in a frictionally slideable cooperation.
Claim 4
Dependent Claim
25 words
The combustion chamber of claim 1 wherein said third width is such that said flange is retained within the slot in a substantially rigid cooperation.
Claim 5
Dependent Claim
13 words
The combustion chamber of claim 1 wherein said retainer ring comprises circumferential segments.
Claim 6
Dependent Claim
170 words
A combustion chamber for use in gas turbines engines, the chamber comprising: an inlet for receiving air and fuel to be burned; an outlet for expelling products of combustion; high strength structural frame means disposed between the inlet and the outlet for supporting mechanical forces associated with the chamber; liner means cooperating with the frame means and defining a combustion zone, said liner means including a plurality of panels of high temperature material; and axial mounting means for positioning said panels axially with respect to said frame means, said axial mounting means including: first shoulder means cooperating with preselected of said panels and partially defining a circumferential slot of first predetermined axial width therein; and second shoulder means cooperating with the frame means, wherein: said second shoulder means includes a first flange for disposition within said slot, said first flange having a predetermined second axial width less than said first width; and said first shoulder means includes a second flange for overlying and retaining the first flange within the slot.
Claim 7
Dependent Claim
170 words
A combustion chamber for use in gas turbines engines, the chamber comprising: an inlet for receiving air and fuel to be burned; an outlet for expelling products of combustion; high strength structural frame means disposed between the inlet and the outlet for supporting mechanical forces associated with the chamber; liner means cooperating with the frame means and defining a combustion zone, said liner means including a plurality of panels of high temperature material; and axial mounting means for positioning said panels axially with respect to said frame means, said axial mounting means including: first shoulder means cooperating with preselected of said panels and partially defining a circumferential slot of first predetermined axial width therein; and second shoulder means cooperating with the frame means, wherein: said second shoulder means includes a first flange for disposition within said slot, said first flange having a predetermined second axial width less than said first width; and said first shoulder means includes a second flange for overlying and retaining the first flange within the slot.
Claim 8
Dependent Claim
148 words
A combustion chamber for use in gas turbine engines, the chamber comprising: an inlet for receiving air and fuel to be burned; an outlet for expelling products of combustion; high strength structural frame means disposed between the inlet and the outlet for supporting mechanical forces associated with the chamber; liner means cooperating with the frame means and defining a combustion zone, said liner means including a plurality of panels of high temperature material; and axial mounting means for positioning said panels axially with respect to said frame means, said axial mounting means including: first shoulder means cooperating with preselected of said panels; and second shoulder means cooperating with the frame means and engaging the first shoulder means, wherein: said panels include leading and trailing edges, and preselected of said panels include edge flanges proximate their trailing edges for retaining cooperation with the leading edges of other preselected panels.
Claim 9
Dependent Claim
148 words
A combustion chamber for use in gas turbine engines, the chamber comprising: an inlet for receiving air and fuel to be burned; an outlet for expelling products of combustion; high strength structural frame means disposed between the inlet and the outlet for supporting mechanical forces associated with the chamber; liner means cooperating with the frame means and defining a combustion zone, said liner means including a plurality of panels of high temperature material; and axial mounting means for positioning said panels axially with respect to said frame means, said axial mounting means including: first shoulder means cooperating with preselected of said panels; and second shoulder means cooperating with the frame means and engaging the first shoulder means, wherein: said panels include leading and trailing edges, and preselected of said panels include edge flanges proximate their trailing edges for retaining cooperation with the leading edges of other preselected panels.
Claim 10
Dependent Claim
16 words
The combustion chamber of claim 6 wherein said panels cooperate telescopically to form said liner means.
Claim 11
Dependent Claim
122 words
A combustion chamber for use in gas turbine engines, the chamber comprising: an inlet for receiving air and fuel to be burned; an outlet for expelling products of combustion; high strength structural frame means disposed between the inlet and outlet for supporting mechanical forces associated with the chamber; liner means cooperating with the frame means and defining a combustion zone, said liner means including a plurality of circumferentially segmented panels, said panels adapted for disposition in lateral cooperation to form an annular body; axial mounting mans for positioning said panels axially with respect to said frame means; and a plurality of seals disposed between preselected laterally adjacent panels; and wherein said preselected panels include recesses along opposed edges for receiving said seals.
Claim 12
Dependent Claim
122 words
A combustion chamber for use in gas turbine engines, the chamber comprising: an inlet for receiving air and fuel to be burned; an outlet for expelling products of combustion; high strength structural frame means disposed between the inlet and outlet for supporting mechanical forces associated with the chamber; liner means cooperating with the frame means and defining a combustion zone, said liner means including a plurality of circumferentially segmented panels, said panels adapted for disposition in lateral cooperation to form an annular body; axial mounting mans for positioning said panels axially with respect to said frame means; and a plurality of seals disposed between preselected laterally adjacent panels; and wherein said preselected panels include recesses along opposed edges for receiving said seals.
Claim 13
Dependent Claim
20 words
The combustion chamber of claim 8 wherein said recesses and said seals are dimensioned to provide a frictionally slideable cooperation.
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) | 1988-12-02 | 1989-06-03 | 1989-12-03 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1992-12-02 | 1993-06-03 | 1993-12-03 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1996-12-02 | 1997-06-03 | 1997-12-03 | $7700.00 | Window Closed / Lapsed |