Invention Grant
- Patent Title: Translating core cowl having aerodynamic flap sections
- Patent Title (中): 具有气动翼片的翻转核心罩
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Application No.: US12443887Application Date: 2006-10-12
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Publication No.: US08434309B2Publication Date: 2013-05-07
- Inventor: Glenn Levasseur
- Applicant: Glenn Levasseur
- Applicant Address: US CT Hartford
- Assignee: United Technologies Corporation
- Current Assignee: United Technologies Corporation
- Current Assignee Address: US CT Hartford
- Agency: Carlson, Gaskey & Olds PC
- International Application: PCT/US2006/039951 WO 20061012
- International Announcement: WO2008/045067 WO 20080417
- Main IPC: F02K1/00
- IPC: F02K1/00
Abstract:
An example core nacelle for a gas turbine engine includes a core cowl positioned adjacent an inner duct boundary of a fan bypass passage having an associated discharge airflow cross-sectional area. The core cowl includes at least one translating section and at least one flap section. The translating section of the core cowl is selectively moveable to vary the discharge airflow cross-sectional area.
Public/Granted literature
- US20100115914A1 TRANSLATING CORE COWL HAVING AERODYNAMIC FLAP SECTIONS Public/Granted day:2010-05-13
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