Invention Grant
- Patent Title: Impingement cooled components having integral thermal transfer features
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Application No.: US15463025Application Date: 2017-03-20
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Publication No.: US10697635B2Publication Date: 2020-06-30
- Inventor: Matthew Robert Pearson
- Applicant: United Technologies Corporation
- Applicant Address: US CT Farmington
- Assignee: RAYTHEON TECHNOLOGIES CORPORATION
- Current Assignee: RAYTHEON TECHNOLOGIES CORPORATION
- Current Assignee Address: US CT Farmington
- Agency: Cantor Colburn LLP
- Main IPC: F23R3/00
- IPC: F23R3/00 ; F02C3/04 ; F23R3/06

Abstract:
Components for gas turbine engines having a hot side surface, a cold side surface, the cold side surface receiving cooling impingement at one or more cold locations, and at least one thermal transfer feature located between the hot side surface and the cold side surface within the component and arranged such that a condenser section of the thermal transfer feature is located proximate at least one of the cold locations and an evaporator section of the thermal transfer feature is located away from the cold location.
Public/Granted literature
- US20180266688A1 IMPINGEMENT COOLED COMPONENTS HAVING INTEGRAL THERMAL TRANSFER FEATURES Public/Granted day:2018-09-20
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