Hole pattern for gas turbine combustor

• US 8,056,342 B2
• Filed: 06/12/2008
• Issued: 11/15/2011
• Est. Priority Date: 06/12/2008
• Status: Active Grant

• Current Assignee: Rtx Corporation
• Original Assignee: United Technologies Corporation (Raytheon Technologies Corporation d/b/a RTX)
• Inventors: Kozola, Stuart L., Shelley, Jonathan K., Cheung, Albert K., Burd, Steven W.
• Primary Examiner(s): Gartenberg; Ehud
• Assistant Examiner(s): SUTHERLAND, STEVEN M
• Application Number:
  US12/137,580
• Publication Number:
  US 20090308077A1
• Time in Patent Office: 1,251 Days
• Field of Search: 607/52, 607/54, 607/66, 607/58, 607/53, 607/60
• US Class Current: 60/752
• CPC Class Codes: F23R 2900/03041 Effusion cooled combustion chamber walls or domes
• CPC Class Codes: F23R 2900/03042 Film cooled combustion chamber walls or domes
• CPC Class Codes: F23R 2900/03044 Impingement cooled combustion chamber walls or subassemblies
• CPC Class Codes: F23R 3/06 Arrangement of apertures along the flame tube
• CPC Class Codes: Y02T 50/60 Efficient propulsion technologies, e.g. for aircraft

Abstract

A combustor for a turbine engine includes an outer liner having a row of circumferentially distributed outer combustion air holes and an inner liner circumscribed by the outer liner and having a row of circumferentially distributed inner combustion air holes. The inner and outer liners each include at least a major air hole having a first hole size, an intermediate air hole having a second hole size, and a minor air hole having a third hole size. The first, second, and third hole sizes are all different from each other.

Claims

1. A combustor for a turbine engine comprising:

an outer liner having a row of circumferentially distributed outer combustion air holes including at least a major outer air hole having a first outer air hole size, an intermediate outer air hole having a second outer air hole size, and a minor outer air hole having a third outer air hole size, wherein said first, said second, and said third outer air hole sizes are all different from each other;

an inner liner circumscribed by said outer liner and having a row of circumferentially distributed inner combustion air holes including at least a major inner air hole having a first inner air hole size, an intermediate inner air hole having a second inner air hole size, and a minor inner air hole having a third inner air hole size, wherein said first, said second, and said third inner air hole sizes are all different from each other; and

wherein said circumferentially distributed outer combustion air holes are radially aligned with said circumferentially distributed inner combustion air holes such that at least one of said major outer, intermediate outer, and minor air holes is aligned with a different hole size of said major inner, intermediate inner, and minor inner air holes.

2. The combustor according to claim 1 wherein said second outer and said second inner air hole sizes are smaller than said first outer and said first inner air hole sizes, and wherein said second outer and said second inner air hole sizes are greater than said third outer and said third inner air hole sizes.

3. The combustor according to claim 2 wherein said intermediate air holes are positioned circumferentially between said major air holes and said minor air holes.

4. The combustor according to claim 3 wherein said row of circumferentially distributed outer combustion air holes is comprised of a plurality of first hole sets, each first hole set including at least one minor air hole that is circumferentially spaced from one intermediate air hole that in turn is circumferentially spaced from one major air hole, and wherein each minor hole of one first hole set is circumferentially spaced from a major air hole of an immediately adjacent first hole set, and wherein said row of circumferentially distributed inner combustion air holes is comprised of a plurality of second hole sets, each second hole set including at least one minor air hole that is circumferentially spaced from one intermediate air hole that is circumferentially spaced from one major air hole, and wherein each minor hole of one second hole set is circumferentially spaced from a major air hole of an immediately adjacent second hole set.

7. The combustor according to claim 2 including a fourth outer air hole having a fourth outer air hole size and a fourth inner air hole having a fourth inner air hole size, said fourth outer and said fourth inner air holes corresponding to one of a major air hole, a minor air hole, or an intermediate air hole.

8. The combustor according to claim 7 wherein at least one of said intermediate air holes is positioned circumferentially between said major air holes and said minor air holes.

11. The combustor assembly according to claim 7 wherein said fourth outer and said fourth inner air holes each comprise intermediate air holes that are larger than said minor air holes and smaller than said major air holes.

12. The combustor according to claim 1 wherein each of said inner and said outer liners comprise a support shell, and including a forward heatshield secured to a forward portion of each support shell and an aft heatshield secured to an aft portion of each support shell.

13. The combustor according to claim 12 including a plurality of impingement cooling holes in each support shell and a plurality of film cooling holes in each heatshield.

14. The combustor according to claim 1 including a combustor front end structure to introduce primary combustion air into a combustion chamber.

15. The combustor according to claim 1 wherein said major outer air hole is at least partially radially aligned with one of said intermediate or minor inner air holes.

16. The combustor according to claim 15 wherein said second outer and said second inner air hole sizes are smaller than said first outer and said first inner air hole sizes, and wherein said second outer and said second inner air hole sizes are greater than said third outer and said third inner air hole sizes.

17. The combustor according to claim 1 wherein said outer liner only includes a single row of circumferentially distributed outer combustion air holes and wherein said inner liner only includes a single row of circumferentially distributed inner combustion air holes that are radially aligned with said single row of circumferentially distributed outer combustion air holes.

18. The combustor according to claim 1 wherein at least one of said inner or outer combustion air holes is not radially aligned with any other combustion air hole.

19. The combustor according to claim 1 at least one of said major outer, intermediate outer, and minor outer air holes is offset from being radially aligned with any of said major inner, intermediate inner, and minor inner air holes.

5. A combustor for a turbine engine comprising:

an outer liner having a row of circumferentially distributed outer combustion air holes including at least a major outer air hole having a first outer air hole size, an intermediate outer air hole having a second outer air hole size, and a minor outer air hole having a third outer air hole size, wherein said first, said second, and said third outer air hole sizes are all different from each other;

an inner liner circumscribed by said outer liner and having a row of circumferentially distributed inner combustion air holes including at least a major inner air hole having a first inner air hole size, an intermediate inner air hole having a second inner air hole size, and a minor inner air hole having a third inner air hole size, wherein said first, said second, and said third inner air hole sizes are all different from each other;

wherein said second outer and said second inner air hole sizes are smaller than said first outer and said first inner air hole sizes, and wherein said second outer and said second inner air hole sizes are greater than said third outer and said third inner air hole sizes;

wherein said intermediate air holes are positioned circumferentially between said major air holes and said minor air holes;

wherein said row of circumferentially distributed outer combustion air holes is comprised of a plurality of first hole sets, each first hole set including at least one minor air hole that is circumferentially spaced from one intermediate air hole that in turn is circumferentially spaced from one major air hole, and wherein each minor hole of one first hole set is circumferentially spaced from a major air hole of an immediately adjacent first hole set, and wherein said row of circumferentially distributed inner combustion air holes is comprised of a plurality of second hole sets, each second hole set including at least one minor air hole that is circumferentially spaced from one intermediate air hole that is circumferentially spaced from one major air hole, and wherein each minor hole of one second hole set is circumferentially spaced from a major air hole of an immediately adjacent second hole set; and

wherein a minor air hole from said first hole set is at least partially aligned in a radial direction with a major air hole from said second hole set, an intermediate air hole from said first hole set is at least partially aligned in a radial direction with an intermediate air hole from said second hole set, and a major air hole from said first hole set is at least partially aligned in a radial direction with a minor air hole from said second hole set.

6. A combustor for a turbine engine comprising:

an outer liner having a row of circumferentially distributed outer combustion air holes including at least a major outer air hole having a first outer air hole size, an intermediate outer air hole having a second outer air hole size, and a minor outer air hole having a third outer air hole size, wherein said first, said second, and said third outer air hole sizes are all different from each other;

an inner liner circumscribed by said outer liner and having a row of circumferentially distributed inner combustion air holes including at least a major inner air hole having a first inner air hole size, an intermediate inner air hole having a second inner air hole size, and a minor inner air hole having a third inner air hole size, wherein said first, said second, and said third inner air hole sizes are all different from each other;

wherein said second outer and said second inner air hole sizes are smaller than said first outer and said first inner air hole sizes, and wherein said second outer and said second inner air hole sizes are greater than said third outer and said third inner air hole sizes;

wherein said intermediate air holes are positioned circumferentially between said major air holes and said minor air holes;

wherein said row of circumferentially distributed outer combustion air holes is comprised of a plurality of first hole sets, each first hole set including at least one minor air hole that is circumferentially spaced from one intermediate air hole that in turn is circumferentially spaced from one major air hole, and wherein each minor hole of one first hole set is circumferentially spaced from a major air hole of an immediately adjacent first hole set, and wherein said row of circumferentially distributed inner combustion air holes is comprised of a plurality of second hole sets, each second hole set including at least one minor air hole that is circumferentially spaced from one intermediate air hole that is circumferentially spaced from one major air hole, and wherein each minor hole of one second hole set is circumferentially spaced from a major air hole of an immediately adjacent second hole set; and

wherein said major air hole from said first hole set is at least partially aligned in a radial direction with an intermediate air hole from said second hole set, an intermediate air hole from said first hole set is at least partially aligned in a radial direction with a major air hole from said second hole set, and a minor air hole from said first hole set is offset from a minor air hole from said second hole set with said intermediate and major air holes of said first and said second hole sets being positioned circumferentially between said minor air holes of said first and said second hole sets.

9. A combustor for a turbine engine comprising:

an outer liner having a row of circumferentially distributed outer combustion air holes including at least a major outer air hole having a first outer air hole size, an intermediate outer air hole having a second outer air hole size, and a minor outer air hole having a third outer air hole size, wherein said first, said second, and said third outer air hole sizes are all different from each other;

an inner liner circumscribed by said outer liner and having a row of circumferentially distributed inner combustion air holes including at least a major inner air hole having a first inner air hole size, an intermediate inner air hole having a second inner air hole size, and a minor inner air hole having a third inner air hole size, wherein said first, said second, and said third inner air hole sizes are all different from each other;

wherein said second outer and said second inner air hole sizes are smaller than said first outer and said first inner air hole sizes, and wherein said second outer and said second inner air hole sizes are greater than said third outer and said third inner air hole sizes;

a fourth outer air hole having a fourth outer air hole size and a fourth inner air hole having a fourth inner air hole size, said fourth outer and said fourth inner air holes corresponding to one of a major air hole, a minor air hole, or an intermediate air hole; and

wherein said row of circumferentially distributed outer combustion air holes is comprised of a plurality of first hole sets, each first hole set including at least one minor air hole that is circumferentially spaced from one intermediate air hole that in turn is circumferentially spaced from one major air hole that in turn is circumferentially spaced from another intermediate air hole, and wherein each minor hole of one first hole set is circumferentially spaced from one intermediate air hole of an immediately adjacent first hole set, and wherein said row of circumferentially distributed inner combustion air holes is comprised of a plurality of second hole sets, each second hole set including at least one minor air hole that is circumferentially spaced from one intermediate air hole that in turn is circumferentially spaced from another intermediate air hole that in turn is circumferentially spaced from one major air hole, and wherein each minor hole of one second hole set is circumferentially spaced from a major air hole of an immediately adjacent second hole set.

10. The combustor according to claim 9 wherein a minor air hole from said first hole set is at least partially aligned in a radial direction with a major air hole from said second hole set, a first intermediate air hole from said first hole set is at least partially in a radial direction aligned with a first intermediate air hole from said second hole set, a major air hole from said first hole set is at least partially aligned in a radial direction with a second intermediate hole from said second hole set, and a second intermediate hole from said first hole set is at least partially aligned in a radial direction with a minor air hole of said second hole set.