Nova Patents
EP2093384A3

Filter system for blade outer air seal

Abstract

A gas turbine engine component (54) has a filter (86) mounted adjacent an impingement cavity (80) to filter particles out of a secondary cooling airflow outboard of a cooling channel (84) in communication with the secondary cooling airflow.

EP2093384A3, drawing sheet 1
Sheet 1 of 1

Term

2.2 yearsto projected expiry

Projected expiry 11 December 2028, counted from filing; an application has no term until it is granted.

  1. Priority
  2. Filed
  3. Published
  4. Today
  5. Projected expiry

1 sheet

  1. Sheet 1