发明名称 INDUSTRIAL GAS TURBINE EXHAUST SYSTEM DIFFUSER INLET LIP
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.
申请公布号 US2015143810(A1) 申请公布日期 2015.05.28
申请号 US201314087042 申请日期 2013.11.22
申请人 Salunkhe Anil L.;Orosa John A.;Shteyman Yevgeniy;Han Lijuan;Delisa, III Matthew J.;Riveros Daniel F. 发明人 Salunkhe Anil L.;Orosa John A.;Shteyman Yevgeniy;Han Lijuan;Delisa, III Matthew J.;Riveros Daniel F.
分类号 F01D25/30 主分类号 F01D25/30
代理机构 代理人
主权项 1. An industrial gas turbine exhaust system, comprising: an inner case; an outer case circumscribing the inner case in spaced relationship relative to a centerline defined by the exhaust system; a plurality of struts interposed between the outer and inner cases; a turbine exhaust path defined between the outer and inner cases; and the outer case defining an outer diameter ring with a lip extending radially inwardly therefrom into the turbine exhaust path on an inlet side of the outer case.
地址 Charlotte NC US