Invention Grant
- Patent Title: Trailing edge core compartment vent for an aircraft engine
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Application No.: US14870401Application Date: 2015-09-30
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Publication No.: US10040560B2Publication Date: 2018-08-07
- Inventor: Robert H. Willie , Paul R. Tretow , David F. Cerra
- Applicant: The Boeing Company
- Applicant Address: US IL Chicago
- Assignee: THE BOEING COMPANY
- Current Assignee: THE BOEING COMPANY
- Current Assignee Address: US IL Chicago
- Agency: MH2 Technology Law Group LLP
- Main IPC: B64D33/04
- IPC: B64D33/04 ; B64D27/12 ; B64D29/00 ; F02K1/82 ; F02K3/04 ; F01D25/26 ; F02K1/38 ; F02C7/18

Abstract:
A turbine engine nozzle can include a primary outer wall extending from an engine core area to an annular wall terminus that surrounds an engine tail cone, to form a core nozzle. The turbine engine nozzle also includes a single engine core cowl extending from the engine core area to an annular cowl terminus to form a core compartment vent nozzle. The core compartment vent nozzle exhausts air from a core compartment in a trailing edge between the single engine core cowl and the primary outer wall.
Public/Granted literature
- US20170088275A1 TRAILING EDGE CORE COMPARTMENT VENT FOR AN AIRCRAFT ENGINE Public/Granted day:2017-03-30
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