Invention Grant
- Patent Title: One-piece bladed drum of an axial turbomachine compressor
- Patent Title (中): 轴向涡轮机压缩机的单件叶片滚筒
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Application No.: US12580070Application Date: 2009-10-15
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Publication No.: US08414256B2Publication Date: 2013-04-09
- Inventor: Jean-François Cortequisse , André Lhoest
- Applicant: Jean-François Cortequisse , André Lhoest
- Applicant Address: BE Herstal (Milmort)
- Assignee: Techspace Aero, S.A.
- Current Assignee: Techspace Aero, S.A.
- Current Assignee Address: BE Herstal (Milmort)
- Agent James E. Walton; Richard G. Eldredge
- Priority: EP08172923 20081224
- Main IPC: F04D29/52
- IPC: F04D29/52

Abstract:
A compressor drum for an axial turbo-machine includes a hollow body generally symmetrical in revolution about its axis of rotation and forming a shell at the periphery of which are arranged a plurality of parallel rows of vanes, each row corresponding to one stage of the compressor. Each vane includes at its root an attachment platform housed in a corresponding opening made in the shell of the hollow body. The outer surface of each platform is flush with the outer surface of the shell at the edge of the opening and each platform is attached to the hollow body by welding between the outer edge of the platform and the inner edge of the corresponding opening. The platform has the general shape of a parallelogram, a bisector of which corresponds approximately to the main axis of the profile of the vane at the platform.
Public/Granted literature
- US20100158690A1 One-Piece Bladed Drum of an Axial Turbomachine Compressor Public/Granted day:2010-06-24
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