Invention Grant
US09200638B2 Rotor of a turbomachine compressor, with an optimised inner end wall
有权
涡轮机压缩机的转子,具有优化的内端壁
- Patent Title: Rotor of a turbomachine compressor, with an optimised inner end wall
- Patent Title (中): 涡轮机压缩机的转子,具有优化的内端壁
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Application No.: US13498696Application Date: 2010-10-01
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Publication No.: US09200638B2Publication Date: 2015-12-01
- Inventor: Eric Jacques Boston , Alexandre Franck Arnaud Chartoire , Vasiliki Iliopoulou , Ingrid Lepot , Thierry Jean-Jacques Obrecht
- Applicant: Eric Jacques Boston , Alexandre Franck Arnaud Chartoire , Vasiliki Iliopoulou , Ingrid Lepot , Thierry Jean-Jacques Obrecht
- Applicant Address: FR Paris BE Gosselies
- Assignee: SNECMA,CENAERO
- Current Assignee: SNECMA,CENAERO
- Current Assignee Address: FR Paris BE Gosselies
- Agency: Oblon, McClelland, Maier & Neustadt, L.L.P.
- Priority: FR0956891 20091002
- International Application: PCT/EP2010/064652 WO 20101001
- International Announcement: WO2011/039352 WO 20110407
- Main IPC: F04D29/32
- IPC: F04D29/32 ; F01D5/14

Abstract:
A rotor of a turbomachine compressor, including a bladed rotor disk fitted at its radially external end with a wall forming the inner end of an annual flow channel of a primary gas flow, and formed from multiple angular sectors, each of which is delimited between two blades of the disk which are consecutive in a circumferential direction and includes a bulging portion which is convex in the axial direction and in the circumferential direction, together with, upstream from the bulging portion, a troughed portion which is concave in the axial direction and in the circumferential direction and which has a base which is roughly punctiform.
Public/Granted literature
- US20120201692A1 ROTOR OF A TURBOMACHINE COMPRESSOR, WITH AN OPTIMISED INNER END WALL Public/Granted day:2012-08-09
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