Burner seal of a gas turbine and method for manufacturing the same

Patent metadata

Field	Value
Publication number	US-10330204-B2
Application number	US-201715809155-A
Country	US
Kind code	B2
Filing date	Nov 10, 2017
Priority date	Nov 10, 2017
Publication date	Jun 25, 2019
Grant date	Jun 25, 2019

Abstract

A burner seal of a gas turbine with a substantially tubular base body, which has a ring-shaped inlet lip on the inflow side and a funnel at its outflow side, wherein an inner diameter of the inflow side is embodied to be larger than an inner diameter of a sealing surface that is arranged axially in front of the funnel, wherein cooling channels are formed in the base body distributed about the circumference, wherein the cooling channels are formed respectively in the base body in the area of the sealing surface and of the funnel, and respectively open into an end area of the funnel in an exit hole.

First claim

The invention claimed is:

1. A burner seal of a gas turbine comprising:
a tubular base body including an inflow side and an outflow side;
a ring-shaped inlet lip on the inflow side;
a funnel on the outflow side;
a sealing surface arranged axially upstream of the funnel, wherein an inner diameter of the inflow side is larger than an inner diameter of the sealing surface;
an entry hole located in an inner surface of the burner seal;
an exit hole positioned in the funnel; and
a cooling channel formed in the base body and extending from the entry hole to the exit hole.

2. The burner seal according to claim 1 , wherein the exit hole opens into an outermost end area of the funnel.

3. The burner seal according to claim 1 , wherein a central axis of the exit hole is positioned at an angle of 70° to 90° with respect to a central axis of the burner seal.

4. The burner seal according to claim 1 , wherein the entry hole is arranged in an area of the inner diameter of the inflow side.

5. The burner seal according to claim 1 , wherein the entry hole is arranged in an area of the sealing surface.

6. The burner seal according to claim 1 , wherein the cooling channel has at least one chosen from a circular, elliptic, diamond-shaped and drop-shaped cross section.

7. The burner seal according to claim 1 , wherein a cross section of the cooling channel is variable along a length of the cooling channel.

8. The burner seal according to claim 1 , wherein the cooling channel is at least one chosen from curved, bent and linear along a length of the cooling channel.

9. The burner seal according to claim 1 , wherein a surface of the entry hole and a surface of the exit hole have same dimensions.

10. The burner seal according to claim 1 , wherein a central axis of the exit hole is positioned at an angle of 70° to 80° with respect to a central axis of the burner seal.

11. The burner seal according to claim 10 , wherein a central axis of the exit hole is positioned at an angle of 75° with respect to a central axis of the burner seal.

12. The burner seal according to claim 1 , wherein a surface of the entry hole and a surface of the exit hole have different dimensions.

13. A method for manufacturing a burner seal, comprising:
providing:
a tubular base body including an inflow side and an outflow side;
a ring-shaped inlet lip on the inflow side;
a funnel on the outflow side;
a sealing surface arranged axially upstream of the funnel, wherein an inner diameter of the inflow side is larger than an inner diameter of the sealing surface;
an entry hole located in an inner surface of the burner seal;
an exit hole positioned in the funnel; and
a cooling channel formed in the base body and extending from the entry hole to the exit hole;

manufacturing the burner seal using an additive process.

Assignees

• Rolls Royce Deutschland Ltd & Co Kg

Inventors

• Clemen Carsten

Classifications

• F02C7/28

  Arrangement of seals · CPC title

• F16J15/4472 Primary

  with axial path · CPC title

• F02C7/18

  the medium being gaseous, e.g. air {(F02C7/125 takes precedence)} · CPC title

• F23R3/10 Primary

  for primary air (F23R3/06, F23R3/045 take precedence) · CPC title

• F16J15/44

  Free-space packings · CPC title