Invention Application
US20170003027A1 GAS TURBINE ENGINE COMBUSTOR LINER PANEL WITH SYNERGISTIC COOLING FEATURES
审中-公开
燃气涡轮发动机配备有协同冷却功能的衬板
- Patent Title: GAS TURBINE ENGINE COMBUSTOR LINER PANEL WITH SYNERGISTIC COOLING FEATURES
- Patent Title (中): 燃气涡轮发动机配备有协同冷却功能的衬板
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Application No.: US15106032Application Date: 2015-01-30
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Publication No.: US20170003027A1Publication Date: 2017-01-05
- Inventor: Stanislav Kostka , Frank J. Cunha , James B. Hoke , Timothy S. Snyder , Albert K. Cheung , Christos Adamopoulos
- Applicant: UNITED TECHNOLOGIES CORPORATION
- Applicant Address: US CT Hartford
- Assignee: United Technologies Corporation
- Current Assignee: United Technologies Corporation
- Current Assignee Address: US CT Hartford
- International Application: PCT/US2015/013784 WO 20150130
- Main IPC: F23R3/00
- IPC: F23R3/00 ; F02C7/18 ; F23R3/06
Abstract:
A liner panel for a combustor of a gas turbine engine includes a multiple of heat transfer augmentors. At least one of the multiple of heat transfer augmentors includes a cone shaped pin.
Information query
