Patent · US Active

Method of manufacturing heat exchanger cooling passages in aero propulsion structure

US8806747B2 · kind B2 · utility

3Cited by
4References
12Claims
0Family size

Assignee

Inventors

Key dates

Filing dateJul 30, 2009
Grant dateAug 19, 2014
Priority date
Expiry dateAug 2, 2032

Classification

  • Technology area (CPC Y)Emerging Cross-Sectional Technologies
  • CPC primaryY10T29/49996
  • WIPO fieldMachine tools
  • WIPO sectorMechanical engineering

Abstract

Methods and apparatus of an improved cooling structure having cooling passages are provided. A method includes forming pilot holes with an electrical discharge machine (EDM) drill near a heated flow surface. The pilot holes are then shaped with a wire EDM into cooling passages having a desired shape.

Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.