Combustion chamber construction

• US 4,614,082 A
• Filed: 12/19/1972
• Issued: 09/30/1986
• Est. Priority Date: 12/19/1972
• Status: Expired due to Term

• Current Assignee: General Electric Company
• Original Assignee: General Electric Company
• Inventors: Williams, Jesse J., Wakeman, Thomas G., Sterman, Albert P.
• Primary Examiner(s): ECHOLS, PERCY W
• Application Number:
  US06/316,530
• Time in Patent Office: 5,033 Days
• Field of Search: 60/39.65, 60/39.66, 60/39.69, 60/39.32, 60/39.36, 60/752, 60/753, 60/754, 60/755, 60/756, 60/757, 60/758, 60/759, 60/760
• US Class Current: 60/796
• CPC Class Codes: F23R 3/002 Wall structures F23R3/02 and F23R3/007 take precedence

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 the material mounted by means of a slideable friction 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 liner panels in the circumferential, axial, and radial directions with respect to the frame as well as circumferentially with respect to other liner panels. The individual liner panels may be easily removed for repair or replacement without disassembling the frame and associated components. For the purpose of cooling, a cooling fluid is passed into a plenum to cool the radially outward side of the panels by convection. Means are also provided for directing the same fluid from the plenum to the liner inner surfaces in a cooling film.

Claims

1. 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 and defining a combustion zone, said liner means including a plurality of panels of high temperature materials;

circumferential mounting means for positioning said panels laterally with respect to one another;

axial mounting means for positioning said panels axially with respect to said frame means;

wherein said circumferential mounting means includes frictionally slideable engaging means cooperating with adjacent pairs of said panels;

wherein said frictionally slideable engaging means includes a projection disposed on one lateral edge of preselected first of said panels, and a mating slot disposed on an opposed edge of preselected second of said panels disposed adjacent said first panels;

wherein said axial mounting means includes;

first radially extending shoulder means cooperating with preselected of said panels,

second radially extending shoulder means cooperating with said frame means, and engaging said first shoulder means, and

a first axially extending flange carried by said first shoulder means; and

a second axially extending flange carried by said second shoulder means, said second flange underlying and interlocking with said first flange.

2. The combustion chamber of claim 1 wherein said axial mounting means further includes:

a third flange cooperating with preselected first of said panels; and

a fourth flange cooperating with preselected second of said panels, said third and fourth flanges engaging and cooperating with one another.

3. The combustion chamber of claim 1 further including:

circumferential securing means for securing said panels circumferentially with respect to said frame means.

4. The combustion chamber of claim 3 wherein said circumferential securing means includes a plurality of radially extending protrusions cooperating with preselected of said panels and said frame means.

5. The combustion chamber of claim 1 wherein individuals of said panels and portions of said frame combine to define a plurality of plena, and wherein said combustion chamber includes inlet apertures opening into said plena for directing a cooling fluid thereto, and said combustion chamber further includes exit apertures for directing cooling fluid from said plena in a film upon said panels.

6. The combustion chamber of claim 1 wherein said first shoulder means includes a radial gap, and said second shoulder means includes a radial extension, said gap and said extension being dimensioned so that the extension may pass freely axially through the gap when the shoulders are in a first relative circumferential orientation, and said extension is restrained from axial movement through the gap when the shoulders are in a second relative circumferential orientation.

7. The combustion chamber of claim 6 wherein:

said frame and preselected of said panels define a plurality of plena;

said frame includes inlet apertures opening into said plena for directing a cooling fluid thereto; and

said panels include exit apertures for directing cooling fluid from said plena in a film upon predetermined of said panels.

8. The combustion chamber of claim 6 wherein:

said exit apertures are disposed so as to direct said film upon the same panel in which the aperture is disposed.

9. The combustion chamber of claim 1 wherein said projection and said slot are dimensioned so as to provide a slideable, frictional tongue and groove cooperation.

10. 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 and defining a combustion zone, said liner means including a plurality of panels of high temperature material;

circumferential mounting means for positioning said panels laterally with respect to one another;

axial mounting means for positioning said panels axially with respect to said frame means;

and further including;

radial securing means for securing said panels radially with respect to said frame means, said radial securing means including a circumferentially extending damping spring disposed between and engaging said panels and said frame, whereby said panels are restrained from approaching said frame, and are maintained at a predetermined radial distance from said frame.

11. The combustion chamber of claim 10 wherein said radial securing means further includes a circumferentially extending retainer in the form of a segmented cylindrical hoop, and wherein said damping spring comprises a corrugated, segmented generally cylindrical band.

12. The combustion chamber of claim 11 wherein said retainer and said damping spring are positioned between said frame and individuals of said panels.