Invention Grant
- Patent Title: Gas turbine engine with 2.5 bleed duct core case section
- Patent Title (中): 燃气涡轮发动机带有2.5排放管芯芯部分
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Application No.: US12411452Application Date: 2009-03-26
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Publication No.: US08167551B2Publication Date: 2012-05-01
- Inventor: Brian D. Merry , Gabriel L. Suciu
- Applicant: Brian D. Merry , Gabriel L. Suciu
- Applicant Address: US CT Hartford
- Assignee: United Technologies Corporation
- Current Assignee: United Technologies Corporation
- Current Assignee Address: US CT Hartford
- Agency: Carlson Gaskey & Olds, P.C.
- Main IPC: F01D1/02
- IPC: F01D1/02
Abstract:
A core case section for a gas turbine engine a multitude of discreet radial extending 2.5 bleed ducts defined in part by a rear structural wall.
Public/Granted literature
- US20100247306A1 GAS TURBINE ENGINE WITH 2.5 BLEED DUCT CORE CASE SECTION Public/Granted day:2010-09-30
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