Invention Grant
- Patent Title: Bypass turbojet
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Application No.: US13978047Application Date: 2012-01-05
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Publication No.: US09611865B2Publication Date: 2017-04-04
- Inventor: Cedric Morel , Alexandre Alfred Gaston Vuillemin
- Applicant: Cedric Morel , Alexandre Alfred Gaston Vuillemin
- Applicant Address: FR Paris
- Assignee: SNECMA
- Current Assignee: SNECMA
- Current Assignee Address: FR Paris
- Agency: Oblon, McClelland, Maier & Neustadt, L.L.P.
- Priority: FR1150224 20110111
- International Application: PCT/FR2012/050027 WO 20120105
- International Announcement: WO2012/095592 WO 20120719
- Main IPC: F04D29/66
- IPC: F04D29/66 ; F02C6/08 ; F02C7/045 ; F02K3/06 ; F04D29/52 ; F04D29/68

Abstract:
A bypass turbojet including a fan wheel carrying blades and surrounded by an annular casing, the casing including an air suction mechanism sucking air from an annular clearance formed between the casing and radially outer ends of the blades of the fan wheel. The air suction mechanism includes an inlet including at least one inlet slot formed in an inside wall of the casing and connected to a suction channel extending downstream. The inlet slot of the suction mechanism is situated axially in register solely with upstream portions of chords of the blades of the fan wheel at their radially outer ends.
Public/Granted literature
- US20130280046A1 BYPASS TURBOJET Public/Granted day:2013-10-24
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