Invention Application
US20130170950A1 VARIABLE SHAPE INLET SECTION FOR A NACELLE ASSEMBLY OF A GAS TURBINE ENGINE
审中-公开
燃气轮机发动机组件的变形形状入口部分
- Patent Title: VARIABLE SHAPE INLET SECTION FOR A NACELLE ASSEMBLY OF A GAS TURBINE ENGINE
- Patent Title (中): 燃气轮机发动机组件的变形形状入口部分
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Application No.: US13777300Application Date: 2013-02-26
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Publication No.: US20130170950A1Publication Date: 2013-07-04
- Inventor: Ashok K. Jain , Zaffir A. Chaudhry
- Applicant: United Technologies Corporation
- Applicant Address: US CT Hartford
- Assignee: UNITED TECHNOLOGIES CORPORATION
- Current Assignee: UNITED TECHNOLOGIES CORPORATION
- Current Assignee Address: US CT Hartford
- Main IPC: F01D17/00
- IPC: F01D17/00
Abstract:
A method of improving the aerodynamic performance of an inlet section of a nacelle assembly of a gas turbine engine, according to an exemplary aspect of the present disclosure includes, among other things, (a) sensing an operability condition, (b) adjusting a leading edge of the inlet section in response to the step (a), and (c) adjusting a thickness of the inlet section in response to the step (a).
Information query
