Invention Grant
- Patent Title: Fluid cooling systems for a gas turbine engine
-
Application No.: US15424021Application Date: 2017-02-03
-
Publication No.: US10830056B2Publication Date: 2020-11-10
- Inventor: Daniel Jason Erno , Narendra Digamber Joshi , William Dwight Gerstler
- Applicant: General Electric Company
- Applicant Address: US NY Schenectady
- Assignee: General Electric Company
- Current Assignee: General Electric Company
- Current Assignee Address: US NY Schenectady
- Agency: Armstrong Teasdale LLP
- Main IPC: F01D5/18
- IPC: F01D5/18 ; F02K3/06 ; F01D9/06 ; F01D25/18 ; F02C7/14 ; F16N39/02 ; F01D25/16

Abstract:
A heat exchanger includes an airfoil configured to be positioned in a coolant stream. The airfoil includes a pressure sidewall and a suction sidewall coupled to the pressure sidewall. The suction sidewall and the pressure sidewall define a leading edge and a trailing edge opposite the leading edge. The leading edge defines an impingement zone wherein the coolant stream is configured to impinge the airfoil. The heat exchanger also includes at least one channel defined within the airfoil between the pressure sidewall and the suction sidewall. The at least one channel is at least partially defined within the impingement zone proximate the leading edge.
Public/Granted literature
- US20190003315A1 FLUID COOLING SYSTEMS FOR A GAS TURBINE ENGINE Public/Granted day:2019-01-03
Information query