Invention Grant
- Patent Title: Axial turbo engine with low gap losses
- Patent Title (中): 具有低间隙损失的轴流涡轮发动机
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Application No.: US13054190Application Date: 2009-07-08
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Publication No.: US08647054B2Publication Date: 2014-02-11
- Inventor: Marcel Aulich , Christian Cornelius , Georg Kröger
- Applicant: Marcel Aulich , Christian Cornelius , Georg Kröger
- Applicant Address: DE Munich
- Assignee: Siemens Aktiengesellschaft
- Current Assignee: Siemens Aktiengesellschaft
- Current Assignee Address: DE Munich
- Priority: EP08012959 20080717
- International Application: PCT/EP2009/058681 WO 20090708
- International Announcement: WO2010/006975 WO 20100121
- Main IPC: F01D5/20
- IPC: F01D5/20

Abstract:
An axial turbomachine including a rotor blade cascade is provided. The rotor blade cascade includes rotor blades each including front edge, a radially outer free blade tip and an annular enclosure enclosing the rotor blade cascade with an annulus inner side by means of which the annular enclosure is arranged directly adjacent to the blade tips to give a radial gap between the enveloping ends of the blade tips and the annulus inner side. The rotor blades include a radial projection in the region of the front edge on the blade tip and the annular enclosure has an annular radial recess in the annulus inner side, arranged at a radial distance from the ends of the blade tips, such that in the main flow direction of the axial turbomachine the line of the radial projections on the side facing the radial gap matches the line of the radial recess.
Public/Granted literature
- US20110189020A1 Axial turbo engine with low gap losses Public/Granted day:2011-08-04
Information query
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