Invention Grant
- Patent Title: Low noise aeroengine inlet system
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Application No.: US14463031Application Date: 2014-08-19
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Publication No.: US09957889B2Publication Date: 2018-05-01
- Inventor: Michel Labrecque , Vincent Couture-Gagnon , Richard Ullyott
- Applicant: PRATT & WHITNEY CANADA CORP.
- Applicant Address: unknown Longueuil, Quebec
- Assignee: PRATT & WHITNEY CANADA CORP.
- Current Assignee: PRATT & WHITNEY CANADA CORP.
- Current Assignee Address: unknown Longueuil, Quebec
- Agency: Norton Rose Fulbright Canada
- Main IPC: F02C7/045
- IPC: F02C7/045 ; F02C7/042 ; F02K3/06
Abstract:
An aeroengine is provided with a splitter apparatus disposed in a section of an inlet duct. The splitter apparatus can be actuated from a stowed position to a deployed position to allow splitter(s) to selectively move from out of the inlet flow to a position extending into the inlet duct to divide the inlet flow into multiple passages.
Public/Granted literature
- US20160053684A1 LOW NOISE AEROENGINE INLET SYSTEM Public/Granted day:2016-02-25
Information query
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