- 专利标题: Compressor for a Turbine Engine
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申请号: US16171456申请日: 2018-10-26
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公开(公告)号: US20190128118A1公开(公告)日: 2019-05-02
- 发明人: Stéphane Hiernaux
- 申请人: SAFRAN AERO BOOSTERS SA
- 申请人地址: BE Herstal
- 专利权人: SAFRAN AERO BOOSTERS SA
- 当前专利权人: SAFRAN AERO BOOSTERS SA
- 当前专利权人地址: BE Herstal
- 优先权: BE2017/5766 20171026
- 主分类号: F01D5/02
- IPC分类号: F01D5/02
摘要:
A compressor for a turbine engine includes an annular row of blades including a first blade with an extrados surface and a second blade with an intrados surface; and a connecting surface joining the intrados surface to the extrados surface, the connecting surface having a bulge of volume VB and a recess of volume VC, the bulge and recess forming a contouring 3D. The volume of the bulge VB is greater than four times the volume VC of the recess, the connecting surface includes a flat or axisymmetric band circumferentially separating the bulge from the recess, and the bottom of the recess being formed against the intrados surface.
公开/授权文献
- US10677063B2 Compressor for turbine engine 公开/授权日:2020-06-09
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