Thimble assemblies for introducing a cross-flow into a secondary combustion zone

Patent metadata

Field	Value
Publication number	US-10816203-B2
Application number	US-201715838193-A
Country	US
Kind code	B2
Filing date	Dec 11, 2017
Priority date	Dec 11, 2017
Publication date	Oct 27, 2020
Grant date	Oct 27, 2020

Abstract

A thimble assembly, which directs fluid flow through a combustor liner, includes a thimble boss and a thimble. The thimble boss is mounted an outer surface of the liner and surrounds a liner opening, thus defining a thimble boss passage. The thimble is disposed through the passage and the liner opening. The thimble wall extends from an inlet portion to an outlet of the thimble. The inlet portion has a greater diameter than the outlet and defines an inlet plane and a parallel intermediate plane. A terminal plane, parallel to the intermediate plane, includes an array of points most distant from a corresponding array of points defining the intermediate plane. The thimble wall has a non-uniform length, such that the outlet of the thimble is oriented at an oblique angle relative to the terminal plane. The thimble wall may have an arcuate shape defined as one-fourth of an ellipse.

First claim

What is claimed is:

1. A thimble assembly ( 160 ) for directing fluid flow through a combustor liner ( 40 ), the thimble assembly ( 160 ) comprising:
a thimble boss ( 270 ) mounted on an outer surface of the combustor liner ( 40 ), the thimble boss ( 270 ) surrounding a thimble aperture ( 146 ) in the combustor liner ( 40 ) and defining a passage ( 275 ) through the thimble boss ( 270 ); and
a thimble ( 260 ) disposed through the passage ( 275 ) and the thimble aperture ( 146 ) in the combustor liner ( 40 ), the thimble ( 260 ) comprising a thimble wall extending in an axial direction from an inlet portion ( 261 ) to an outlet opening ( 264 ) of the thimble ( 260 ), the inlet portion ( 261 ) having a greater diameter than the outlet opening ( 264 );
wherein an inner surface of the thimble wall defines an arcuate shape ( 400 ) in the axial direction from the inlet portion ( 261 ) to the outlet opening ( 264 ), the arcuate shape ( 400 ) defining one-fourth of an ellipse having a first major axis greater than a first minor axis; and
wherein the inlet portion ( 261 ) of the thimble wall defines, in a direction transverse to the axial direction, an elliptical shape having a center coincident with an injection axis ( 268 ) of the thimble ( 260 ), the elliptical shape having a second major axis greater than a second minor axis; and
wherein the inlet portion ( 261 ) of the thimble ( 260 ) comprises an inlet plane ( 267 ) and an intermediate plane ( 262 ) parallel to and spaced from the inlet plane ( 267 ) in the axial direction, the inlet plane ( 267 ) and the intermediate plane ( 262 ) being perpendicular to the injection axis ( 268 ); and wherein the inlet plane ( 267 ) and the intermediate plane ( 262 ) define therebetween the inlet portion ( 261 ) of the thimble wall, the inlet portion ( 261 ) having a uniform cross-sectional size between the inlet plane ( 267 ) and the intermediate plane ( 262 ).

2. The thimble assembly ( 160 ) of claim 1 , wherein cross-sectional shapes of the thimble wall taken perpendicularly to the injection axis ( 268 ) decrease in size in the axial direction from the intermediate plane ( 262 ) to the outlet opening ( 264 ).

3. The thimble assembly ( 160 ) of claim 1 , wherein the arcuate shape ( 400 ) originates at any point along a cross-sectional shape of the thimble wall residing in the intermediate plane ( 262 ).

4. The thimble assembly ( 160 ) of claim 3 , wherein the arcuate shape ( 400 ) defining one-fourth of an ellipse is defined by a formula

x
2

+

y
2

M
2

=
1

,

where x is a non-zero number, y is greater than zero, and M is a number from 1.5 to 30.

5. The thimble assembly ( 160 ) of claim 4 , wherein each point located along the cross-section of the thimble wall residing in the intermediate plane ( 262 ) of the thimble ( 260 ) defines a first end point of the arcuate shape ( 400 ) defined by the formula.

6. The thimble assembly of claim 4 , wherein a plurality of parallel planes is disposed in the axial direction between the intermediate plane ( 262 ) and a terminal plane ( 266 ) including an array of points disposed on the cross-sectional shape of the thimble wall at a location on the outlet opening ( 264 ) of the thimble ( 260 ) most distant from a corresponding array of points defining the cross-sectional shape of the thimble wall at the intermediate plane ( 262 ), each of the plurality of planes in the axial direction defining an elliptical shape having a center located along the injection axis ( 268 ) of the thimble ( 260 ); and wherein each point of a plurality of points disposed on the cross-sectional shape of the thimble wall in the terminal plane ( 266 ) defines a second end point of the arcuate shape ( 400 ).

7. The thimble assembly of claim 6 , wherein the thimble wall has a non-uniform length, such that the outlet opening ( 264 ) of the thimble ( 260 ) is oriented at an oblique angle relative to the terminal plane ( 266 ).

8. The thimble assembly of claim 1 , wherein the passage ( 275 ) is bounded by a perimeter shelf ( 272 ); and wherein an outer surface of the thimble wall comprises a rib ( 269 ) extending at least partially around a perimeter of the thimble ( 260 ) and projecting outwardly from the outer surface, the rib ( 269 ) engaging the shelf ( 272 ) to secure the thimble ( 260 ) in position within the thimble aperture ( 146 ) defined through the combustor liner ( 40 ).

9. The thimble assembly of claim 1 , wherein the thimble boss ( 270 ) comprises a top surface ( 282 ) and a bottom surface ( 284 ), a portion of the bottom surface ( 284 ) disposed in contact with the combustor liner ( 40 ); and wherein the bottom surface ( 284 ) defines a plurality of air flow passages ( 274 ), the plurality of air flow passages ( 274 ) being in fluid communication with the thimble aperture ( 146 ).

10. A thimble assembly ( 160 ) for directing fluid flow through a combustor liner ( 40 ), the thimble assembly ( 260 ) comprising:
a thimble boss ( 270 ) mounted on an outer surface of the combustor liner ( 40 ), the thimble boss ( 270 ) surrounding a thimble aperture ( 146 ) in the combustor liner ( 40 ) and defining a passage ( 275 ) through the thimble boss ( 270 ); and
a thimble ( 260 ) disposed through the passage ( 275 ) and the thimble aperture ( 146 ) in the combustor liner ( 40 ), the thimble ( 260 ) comprising a thimble wall extending in an axial direction from an inlet portion ( 261 ) to an outlet ( 264 ) of the thimble ( 260 ), the inlet portion ( 261 ) having a greater diameter than the outlet ( 264 ) and defining an inlet plane ( 267 ) and an intermediate plane ( 262 ) parallel to and spaced from the inlet plane in the axial direction, wherein the inlet portion ( 261 ) defines an elliptical shape in a direction transverse to an injection axis ( 268 ) of the thimble, the elliptical shape having a center coincident with the injection axis ( 268 ) of the thimble ( 260 ) and having a first major axis greater than a first minor axis, and wherein the inlet portion has a uniform cross-sectional size between the inlet plane ( 267 ) and the intermediate plane ( 262 );
wherein a terminal plane ( 266 ) is defined parallel to the intermediate plane ( 262 ), the terminal plane ( 266 ) including an array of points disposed on a cross-sectional shape of the thimble wall at a location on the outlet ( 264 ) of the thimble ( 260 ) most distant from a corresponding array of points defining a cross-sectional shape of the thimble wall at the intermediate plane ( 262 );
wherein the thimble wall has a non-uniform length, such that the outlet ( 264 ) of the thimble ( 260 ) is oriented at an oblique angle relative to the terminal plane ( 266 ); and
wherein an interior surface of the thimble wall from the intermediate plane ( 262 ) to the terminal plane ( 266 ) defines an arcuate shape ( 400 ).

11. The thimble assembly of claim 10 , wherein each of the cross-sectional shape of the thimble wall at the intermediate plane ( 262 ) and the cross-sectional shape of the thimble wall at the terminal plane ( 266 ) defines an elliptical shape having a center coincident with the injection axis ( 268 ) of the thimble ( 260 ).

12. The thimble assembly o

Assignees

• Gen Electric

Inventors

• Jones Charlie Edmond
• Harper James
• Wilson Matthew Bernard
• Clifford Robert Wade
• Chong Yon Han
• Kraemer Gilbert Otto

Classifications

• F23R3/045 Primary

  using pipes · CPC title

• F23R2900/03341

  Sequential combustion chambers or burners · CPC title

• F23R3/346

  for staged combustion · CPC title

• F23R3/002

  Wall structures (F23R3/02 and F23R3/007 take precedence) · CPC title

• F23R3/06 Primary

  Arrangement of apertures along the flame tube · CPC title