Nova Patents
EP1801351A3

Turbine blade tip cooling

Abstract

A turbine engine blade (20) has an attachment root (42), a platform (40) outboard of the attachment root (42), and an airfoil (22) extending from the platform (40). The airfoil (22) has pressure and suction sides (34, 36) extending between leading and trailing edges (30, 32). An internal cooling passageway network includes at least one inlet (44) in the root (42) and a plurality of outlets (334, 376) along the airfoil. The passageway network includes a leading spanwise cavity (310) fed by a first trunk (323). A streamwise cavity (324) is inboard of a tip (26) of the airfoil. A spanwise feed cavity (326) feeds the streamwise cavity (324) absent down-pass. A second trunk (327) feeds the spanwise feed cavity (326).

EP1801351A3, drawing sheet 1
Sheet 1 of 2

Term

0.2 yearsto projected expiry

Projected expiry 18 December 2026, counted from filing; an application has no term until it is granted.

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

2 sheets

  1. Sheet 1
  2. Sheet 2