Invention Grant
US08539748B2 Segmented inertial particle separators and methods of assembling turbine engines
有权
分段惯性颗粒分离器和组装涡轮发动机的方法
- Patent Title: Segmented inertial particle separators and methods of assembling turbine engines
- Patent Title (中): 分段惯性颗粒分离器和组装涡轮发动机的方法
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Application No.: US11611652Application Date: 2006-12-15
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Publication No.: US08539748B2Publication Date: 2013-09-24
- Inventor: John Paul Petrowicz , Timothy Joseph Higgins , Walter Jackson Tingle
- Applicant: John Paul Petrowicz , Timothy Joseph Higgins , Walter Jackson Tingle
- Applicant Address: US NY Schenectady
- Assignee: General Electric Company
- Current Assignee: General Electric Company
- Current Assignee Address: US NY Schenectady
- Agency: General Electric Company
- Agent William Scott Andes; Matthew P. Hayden
- Main IPC: F02G3/00
- IPC: F02G3/00
Abstract:
A method for assembling a turbine engine including a compressor is disclosed. The method includes coupling an inlet including an inertial particle separator (IPS) and a first surface that is defined using a segment angle, to a gas turbine engine, and coupling the first surface substantially flush against a fuselage of an aircraft to reduce drag.
Public/Granted literature
- US20080141649A1 SEGMENTED INERTIAL PARTICLE SEPARATORS AND METHODS OF ASSEMBLING TURBINE ENGINES Public/Granted day:2008-06-19
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