Invention Grant
US08403629B2 Stator for a jet engine, a jet engine comprising such a stator, and an aircraft comprising the jet engine
失效
用于喷气发动机的定子,包括这种定子的喷气发动机和包括喷气发动机的飞行器
- Patent Title: Stator for a jet engine, a jet engine comprising such a stator, and an aircraft comprising the jet engine
- Patent Title (中): 用于喷气发动机的定子,包括这种定子的喷气发动机和包括喷气发动机的飞行器
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Application No.: US11718727Application Date: 2005-10-20
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Publication No.: US08403629B2Publication Date: 2013-03-26
- Inventor: Anders Lundbladh
- Applicant: Anders Lundbladh
- Applicant Address: SE Trollhättan
- Assignee: Volvo Aero Corporation
- Current Assignee: Volvo Aero Corporation
- Current Assignee Address: SE Trollhättan
- Agency: WRB-IP LLP
- Priority: SE0402714 20041105
- International Application: PCT/SE2005/001572 WO 20051020
- International Announcement: WO2006/049551 WO 20060511
- Main IPC: F01D5/14
- IPC: F01D5/14

Abstract:
A stator for installation in a rear section of a jet engine includes a plurality of guide vanes which extend in the radial direction of the stator and between them define ducts for leading a gas. A first side of the stator in its axial direction defines an inlet for the gas and a second side, opposite the first side, defines an outlet for the gas. The guide vanes have such a shape that together they at least substantially cover the gas inlet viewed in the axial direction of the stator from the outlet side thereof.
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