Combustor heat shield with carbon avoidance feature

Patent metadata

Field	Value
Publication number	US-9518739-B2
Application number	US-201313790451-A
Country	US
Kind code	B2
Filing date	Mar 8, 2013
Priority date	Mar 8, 2013
Publication date	Dec 13, 2016
Grant date	Dec 13, 2016

Abstract

The build-up of carbon deposition on the front face of a combustor heat shield is discouraged by jetting air out from the front face of the heat shield with sufficient momentum to push approaching fuel droplets or rich fuel-air mixture way from the heat shield.

First claim

What is claimed is:

1. A gas turbine engine combustor comprising:
a combustor shell defining a combustion chamber;
a heat shield mounted to an inner surface of the combustor shell, the heat shield having a back face facing the inner surface of the combustor shell and being spaced therefrom to define an air gap, the heat shield having localized areas on an opposed front face thereof where carbon residues tend to build-up during engine operation; and
an airflow path extending along a generally straight line across the combustor shell, the air gap and the heat shield at each of said localized areas;
each airflow path comprising an impingement hole defined in the combustor shell and disposed directly on top of a group of carbon purge air holes defined in the heat shield so that an axial projection of the impingement hole onto the back face of the heat shield captures the group of carbon purge air holes, wherein the axial projection is taken along a longitudinal axis of the combustor, the carbon purge air holes having respective axes extending in a direction generally parallel to an axis of the impingement hole and generally normal to the front face of the heat shield, the impingement holes and the carbon purge air holes being sized to preserve enough air momentum at the exit of the purge air holes to deflect fuel droplets away from the front face of the heat shield to impede carbon build-up on said front face,
wherein rails extend from the back face of the heat shield in sealing engagement with the inner surface of the combustor shell to seal the air gap, and wherein effusion film cooling holes are defined in the heat shield, the cross-sectional area of the carbon purge air holes being greater than that of the of the effusion film cooling holes.

2. The gas turbine engine combustor defined in claim 1 , wherein the carbon purge air holes have a cross-sectional area which is smaller than the cross-sectional area of the impingement hole, the impingement hole directing an air impingement jet on an impingement zone on the back face of the heat shield, at least a plurality of said carbon purge air holes being disposed within the confines of said impingement zone.

3. The gas turbine engine combustor defined in claim 1 , wherein the carbon purge air holes have a diameter which is smaller than that of dilution holes defined in the combustor shell.

4. The gas turbine engine combustor defined in claim 1 , wherein the carbon purge air holes have a cross-sectional area greater than that of effusion-type cooling holes used for forming a cooling film over the front face of the heat shield.

5. The gas turbine engine combustor defined in claim 1 , further comprising impingement cooling holes defined in the combustor shell for directing impingement cooling jets against the back face of the heat shield, the impingement cooling holes having a smaller cross-sectional area than the impingement holes of the airflow path extending through the localized areas subject to carbon deposition.

6. The gas turbine engine combustor defined in claim 1 , wherein the localized areas subject to carbon deposition are located in a primary zone of the combustor near fuel injection points thereof.

7. The gas turbine engine combustor defined in claim 1 , wherein the airflow path defines a flow direction which is generally parallel to the axis of the impingement hole and the respective axes of the carbon purge air holes.

8. The gas turbine engine combustor defined in claim 1 , wherein the rails sealingly engage the combustor shell on opposed sides of the impingement hole and the group of carbon purge air holes.

Assignees

• Pratt & Whitney Canada

Inventors

• Hu Tin Cheung John
• Sze Robert
• Stastny Honza

Classifications

• F23R3/007

  constructed mainly of ceramic components · CPC title

• F23R3/005

  Combined with pressure or heat exchangers · CPC title

• F23R2900/00004

  Preventing formation of deposits on surfaces of gas turbine components, e.g. coke deposits · CPC title

• F23R3/10

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

• F23R3/06

  Arrangement of apertures along the flame tube · CPC title