发明申请
- 专利标题: INDUSTRIAL GAS TURBINE EXHAUST SYSTEM DIFFUSER INLET LIP
- 专利标题(中): 工业气体涡轮排气系统扩散器进样口
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申请号: US14087042申请日: 2013-11-22
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公开(公告)号: US20150143810A1公开(公告)日: 2015-05-28
- 发明人: Anil L. Salunkhe , John A. Orosa , Yevgeniy Shteyman , Lijuan Han , Matthew J. Delisa, III , Daniel F. Riveros
- 申请人: Anil L. Salunkhe , John A. Orosa , Yevgeniy Shteyman , Lijuan Han , Matthew J. Delisa, III , Daniel F. Riveros
- 主分类号: F01D25/30
- IPC分类号: F01D25/30
摘要:
An integrated single-piece exhaust system (SPEX) with modular construction that facilitates design changes for enhanced aerodynamics, structural integrity or serviceability. The SPEX defines splined or curved exhaust path surfaces, such as a series of cylindrical and frusto-conical sections that mimic curves. The constructed sections may include: (i) a tail cone assembly fabricated from conical sections that taper downstream to a reduced diameter; or (ii) an area-ruled cross section axially aligned with one or more rows of turbine struts; or both features. Modular inner and outer diameter inlet lips enhance transitional flow between the last row blades and the SPEX, as well as enhance structural integrity. Modular strut collars have large radius profiles between the SPEX annular inner diameter and outer diameter flow surfaces, for enhanced airflow and constant thickness walls for uniform heat transfer and thermal expansion. Scalloped mounting flanges enhance structural integrity and longevity.
公开/授权文献
- US09598981B2 Industrial gas turbine exhaust system diffuser inlet lip 公开/授权日:2017-03-21
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