Transition support system for combustion transition ducts for turbine engines

• US 9,328,664 B2
• Filed: 11/08/2013
• Issued: 05/03/2016
• Est. Priority Date: 11/08/2013
• Status: Expired due to Fees

• Current Assignee: Siemens Energy Incorporated (Siemens AG)
• Original Assignee: Siemens Energy Incorporated (Siemens AG)
• Inventors: Piersall, Keith W., Shteyman, Yevgeniy, Angel, Robert, Girdich, Ashley N., Brooks, Robert T., Alfonso, James, Marshall, James
• Primary Examiner(s): Gartenberg, Ehud
• Assistant Examiner(s): MANFREDI, FILIPPO C.
• Application Number:
  US14/074,911
• Publication Number:
  US 20150128609A1
• Time in Patent Office: 907 Days
• Field of Search: 607/96, 607/99
• US Class Current: 1/1
• CPC Class Codes: F01D 25/04 Antivibration arrangements
• CPC Class Codes: F01D 9/023 Transition ducts between combustor cans and first stage of the turbine in gas-turbine engines; their cooling or sealings
• CPC Class Codes: F02C 7/20 Mounting or supporting of plant; Accommodating heat expansion or creep
• CPC Class Codes: F02C 9/16 Control of working fluid flow F02C9/48 takes precedence; control of air-intake flow F02C7/057
• CPC Class Codes: F05D 2260/30 Retaining components in desired mutual position
• CPC Class Codes: F05D 2260/96 Preventing, counteracting or reducing vibration or noise
• CPC Class Codes: F23R 2900/00014 Reducing thermo-acoustic vibrations by passive means, e.g. by Helmholtz resonators
• CPC Class Codes: F23R 3/46 Combustion chambers comprising an annular arrangement of several essentially tubular flame tubes within a common annular casing or within individual casings
• CPC Class Codes: F23R 3/60 Support structures; Attaching or mounting means

Abstract

An adjustable transition duct support system for a transition duct that channels hot gases from a combustor exit to a gas turbine inlet of a turbine engine. The adjustable transition duct support system includes an adjustable forward transition flexible support assembly in contact with a transition duct body, whereby the forward transition flexible support assembly may be formed from a base extending toward the transition duct body and first and second side support arms extending from the base to the transition duct body. The first and second side support arms may be formed from a plurality of flex plates spaced from each other with spacers that provide rigidity in circumferential and radial directions and flexibility in an axial direction. The number of flex plates used may be varied to accommodate different turbine engines. The adjustable transition duct support system may have natural frequencies for circumferential and radial modes above two engine orders.

Claims

1. An adjustable transition duct support system for a transition duct that channels hot gases from a combustor exit to a gas turbine inlet of a turbine engine, comprising:

a transition duct body formed from an outer wall that forms an internal passage extending between an inlet and an outlet of the transition duct body;

an adjustable forward transition flexible support assembly in contact with the transition duct body, wherein the forward transition flexible support assembly is formed from a base extending toward the transition duct body, and a first side support arm and a second side support arm extending from the base to the transition duct body;

wherein the first side support arm is formed from a plurality of first side flex plates spaced from each other with spacers, wherein the first side flex plates provide rigidity in circumferential and radial directions and flexibility in an axial direction; and

wherein the second side support arm is formed from a plurality of second side flex plates spaced from each other with spacers, wherein the second side flex plates provide rigidity in circumferential and radial directions and flexibility in the axial direction.

2. The transition duct support system of claim 1, wherein the first side flex plates are formed from between two and eighteen flex plates between 0.5 millimeters and 2.5 millimeters in thickness.

3. The transition duct support system of claim 2, wherein the first side flex plates are formed from between eight and twelve flex plates between 1.0 millimeters and 2.0 millimeters in thickness.

4. The transition duct support system of claim 1, wherein the second side flex plates are formed from between two and eighteen flex plates between 0.5 millimeters and 2.5 millimeters in thickness.

5. The transition duct support system of claim 4, wherein the second side flex plates are formed from between eight and twelve flex plates between 1.0 millimeters and 2.0 millimeters in thickness.

6. The transition duct support system of claim 1, wherein the base is formed from a top beam and a bottom beam that are coupled together via first and second outer columns separated by a middle column.

7. The transition duct support system of claim 6, wherein the first and second columns have thicknesses less than a thickness of the middle column.

8. The transition duct support system of claim 1, wherein the first side support arm includes a first outer bracket and a second outer bracket at an outer end adjacent the transition duct body, wherein the first and second outer brackets are subject to a compressive force towards each other, thereby placing outer ends of the first side flex plates under compression, and wherein the first side support arm includes a first inner bracket and a second inner bracket at an inner end adjacent the transition duct body, wherein the first and second inner brackets are subject to a compressive force towards each other, thereby placing inner ends of the first side flex plates under compression.

9. The transition duct support system of claim 8, wherein the first and second outer brackets are placed under compression via one or more bolts and further comprising a first pin and a second pin extending from the first outer bracket, through the first side flex plates, to the second outer bracket to reduce loads other than compressive loads in the one or more bolts extending from the first outer bracket to the second outer bracket, and wherein the first and second inner brackets are placed under compression via one or more bolts and further comprising a first pin and a second pin extending from the first inner bracket, through the first side flex plates, to the second inner bracket to reduce loads other than compressive loads in the one or more bolts extending from the first inner bracket to the second inner bracket.

10. The transition duct support system of claim 1, wherein the second side support arm includes a first outer bracket and a second outer bracket at an outer end adjacent the transition duct body, wherein the first and second outer brackets are subject to a compressive force towards each other, thereby placing outer ends of the second side flex plates under compression, and wherein the second side support arm includes a first inner bracket and a second inner bracket at an inner end adjacent the transition duct body, wherein the first and second inner brackets are subject to a compressive force towards each other, thereby placing inner ends of the second side flex plates under compression.

11. The transition duct support system of claim 10, wherein the first and second outer brackets are placed under compression via one or more bolts and further comprising a first pin and a second pin extending from the first outer bracket, through the second side flex plates, to the second outer bracket to reduce loads other than compressive loads in the one or more bolts extending from the first outer bracket to the second outer bracket, and wherein the first and second inner brackets are placed under compression via one or more bolts and further comprising a first pin and a second pin extending from the first inner bracket, through the second side flex plates, to the second inner bracket to reduce loads other than compressive loads in the one or more bolts extending from the first inner bracket to the second outer bracket.

12. The transition duct support system of claim 1, wherein the first side flex plates are formed from an outer attachment section and an inner attachment section separated by a transition section having linear sides that are nonlinear with sides forming the outer and inner attachment sections, thereby positioning the outer attachment section offset laterally from the inner attachment section.

13. The transition duct support system of claim 1, wherein the second side flex plates are formed from an outer attachment section and an inner attachment section separated by a transition section having linear sides that are nonlinear with sides forming the outer and inner attachment sections, thereby positioning the outer attachment section offset laterally from the inner attachment section.

14. The transition duct support system of claim 1, wherein first and second outer brackets of the first and second side support arms include at least one orifice with a racetrack configuration enabling axial adjustment;

wherein first and second inner brackets of the first and second side support arms include at least one orifice with a racetrack configuration further enabling the axial adjustment; and

further comprising at least one shim positioned between the first and second side support arms and the base for radial adjustment.

15. The transition duct support system of claim 1, wherein the adjustable forward transition flexible support assembly has a natural frequency in the radial mode greater than 150 Hertz, in the circumferential mode greater than 100 Hertz, in the torsional mode greater than 150 Hertz and in the axial mode greater than 100 Hertz.

16. An adjustable transition duct support system for a transition duct that channels hot gases from a combustor exit to a gas turbine inlet of a turbine engine, comprising:

a transition duct body formed from an outer wall that forms an internal passage extending between an inlet and an outlet of the transition duct body;

an adjustable forward transition flexible support assembly in contact with the transition duct body, wherein the forward transition flexible support assembly is formed from a base extending toward the transition duct body, and a first side support arm and a second side support arm extending from the base to the transition duct body;

wherein the first side support arm is formed from a plurality of first side flex plates spaced from each other with spacers, wherein the first side flex plates provide rigidity in circumferential and radial directions and flexibility in an axial direction;

wherein the second side support arm is formed from a plurality of second side flex plates spaced from each other with spacers, wherein the second side flex plates provide rigidity in circumferential and radial directions and flexibility in the axial direction;

wherein the first side flex plates are formed from an outer attachment section and an inner attachment section separated by a transition section having linear sides that are nonlinear with sides forming the outer and inner attachment sections, thereby positioning the outer attachment section offset laterally from the inner attachment section;

wherein the first side and second side support arms are formed from the plurality of first and second side flex plates that are aligned with each other within each arm, wherein each side support arm has their larger, outer planar surfaces aligned with a longitudinal axis of a top beam of the base;

wherein first and second outer brackets of the first and second side support arms include at least one orifice with a racetrack configuration enabling axial adjustment;

wherein first and second inner brackets of the first and second side support arms include at least one orifice with a racetrack configuration further enabling the axial adjustment; and

further comprising at least one shim positioned between the first and second side support arms and the base for radial adjustment; and

wherein the base is formed from a top beam and a bottom beam that are coupled together via first and second outer columns separated by a middle column and wherein the first and second columns have thicknesses less than a thickness of the middle column.

17. The transition duct support system of claim 16, wherein the first side flex plates are formed from between two and eighteen flex plates between 0.5 millimeters and 2.5 millimeters and the first side flex plates are formed from between eight and twelve flex plates between 1.0 millimeters and 2.0 millimeters in thickness.

18. The transition duct support system of claim 16, wherein the first side support arm includes a first outer bracket and a second outer bracket at an outer end adjacent the transition duct body, wherein the first and second outer brackets are subject to a compressive force towards each other, thereby placing outer ends of the first side flex plates under compression, and wherein the first side support arm includes a first inner bracket and a second inner bracket at an inner end adjacent the transition duct body, wherein the first and second inner brackets are subject to a compressive force towards each other, thereby placing inner ends of the first side flex plates under compression,

wherein the first and second outer brackets are placed under compression via one or more bolts and further comprising a first pin and a second pin extending from the first outer bracket, through the first side flex plates, to the second outer bracket to reduce loads other than compressive loads in the one or more bolts extending from the first outer bracket to the second outer bracket, and wherein the first and second inner brackets are placed under compression via one or more bolts and further comprising a first pin and a second pin extending from the first inner bracket, through the first side flex plates, to the second inner bracket to reduce loads other than compressive loads in the one or more bolts extending from the first inner bracket to the second inner bracket,

wherein the second side support arm includes a first outer bracket and a second outer bracket at an outer end adjacent the transition duct body, wherein the first and second outer brackets are subject to a compressive force towards each other, thereby placing outer ends of the second side flex plates under compression, and wherein the second side support arm includes a first inner bracket and a second inner bracket at an inner end adjacent the transition duct body, wherein the first and second inner brackets are subject to a compressive force towards each other, thereby placing inner ends of the second side flex plates under compression,

wherein the first and second outer brackets are placed under compression via one or more bolts and further comprising a first pin and a second pin extending from the first outer bracket, through the second side flex plates, to the second outer bracket to reduce loads other than compressive loads in the one or more bolts extending from the first outer bracket to the second outer bracket, and wherein the first and second inner brackets are placed under compression via one or more bolts and further comprising a first pin and a second pin extending from the first inner bracket, through the second side flex plates, to the second inner bracket to reduce loads other than compressive loads in the one or more bolts extending from the first inner bracket to the second outer bracket.

19. The transition duct support system of claim 16, wherein the base has a width, as measured orthogonal to a direction of flow of hot gas through the transition duct body, that is at least 80 percent of a width of the transition duct body measured orthogonal to a direction of flow of hot gas through the transition duct body.

20. The transition duct support system of claim 16, wherein the adjustable forward transition flexible support assembly has a natural frequency in the radial mode greater than 150 Hertz, in the circumferential mode greater than 100 Hertz, in the torsional mode greater than 150 Hertz and in the axial mode greater than 100 Hertz.