Invention Grant
- Patent Title: Compressor for turbine engine
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Application No.: US16171456Application Date: 2018-10-26
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Publication No.: US10677063B2Publication Date: 2020-06-09
- Inventor: Stéphane Hiernaux
- Applicant: SAFRAN AERO BOOSTERS SA
- Applicant Address: BE Herstal
- Assignee: SAFRAN AERO BOOSTERS SA
- Current Assignee: SAFRAN AERO BOOSTERS SA
- Current Assignee Address: BE Herstal
- Agent James E. Walton
- Priority: com.zzzhc.datahub.patent.etl.us.BibliographicData$PriorityClaim@3b424ad1
- Main IPC: F01D5/02
- IPC: F01D5/02 ; F04D29/32 ; F04D29/68 ; F04D29/54 ; F01D5/14

Abstract:
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.
Public/Granted literature
- US20190128118A1 Compressor for a Turbine Engine Public/Granted day:2019-05-02
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