Invention Grant
US09341121B2 Gas turbine engine with intercooling turbine section and intercooling turbine section bypass
有权
具有中间冷却涡轮部分和中间冷却涡轮部分旁路的燃气涡轮发动机
- Patent Title: Gas turbine engine with intercooling turbine section and intercooling turbine section bypass
- Patent Title (中): 具有中间冷却涡轮部分和中间冷却涡轮部分旁路的燃气涡轮发动机
-
Application No.: US14569282Application Date: 2014-12-12
-
Publication No.: US09341121B2Publication Date: 2016-05-17
- Inventor: Daniel B. Kupratis
- Applicant: UNITED TECHNOLOGIES CORPORATION
- Applicant Address: US CT Farmington
- Assignee: United Technologies Corporation
- Current Assignee: United Technologies Corporation
- Current Assignee Address: US CT Farmington
- Agency: Cantor Colburn LLP
- Main IPC: F02K3/02
- IPC: F02K3/02 ; F02C9/18 ; F02K3/075 ; F02K3/077 ; F02C7/143
Abstract:
A gas turbine engine includes an intercooling turbine section to selectively cool the core flow. An intercooling turbine section bypass is also included to selectively bypass at least a portion of a core flow through an intercooling turbine section bypass path around the intercooling turbine section.
Public/Granted literature
- US20150252732A1 GAS TURBINE ENGINE WITH INTERCOOLING TURBINE SECTION AND INTERCOOLING TURBINE SECTION BYPASS Public/Granted day:2015-09-10
Information query
