Invention Grant
US08769924B2 Gas turbine engine assembly including accessory components within the nacelle
有权
燃气涡轮发动机组件包括在机舱内的附件部件
- Patent Title: Gas turbine engine assembly including accessory components within the nacelle
- Patent Title (中): 燃气涡轮发动机组件包括在机舱内的附件部件
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Application No.: US12129990Application Date: 2008-05-30
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Publication No.: US08769924B2Publication Date: 2014-07-08
- Inventor: Thomas G. Cloft
- Applicant: Thomas G. Cloft
- Applicant Address: US CT Hartford
- Assignee: United Technologies Corporation
- Current Assignee: United Technologies Corporation
- Current Assignee Address: US CT Hartford
- Agency: Carlson, Gaskey & Olds
- Main IPC: F02K3/02
- IPC: F02K3/02
Abstract:
A gas turbine engine assembly includes an inlet lip assembly, a fan containment case, and a front flange. The fan containment case surrounds a fan section and is positioned downstream from the inlet lip assembly. The front flange is mounted between the inlet lip assembly and the fan containment case and is positioned upstream from the fan section.
Public/Granted literature
- US20090293497A1 GAS TURBINE ENGINE ASSEMBLY Public/Granted day:2009-12-03
Information query
