Patent · US Active

Rotor blade for a turbomachine and turbomachine

US9482099B2 · kind B2 · utility

0Cited by

12References

15Claims

0Family size

Assignee

MTU Aero Engines AG · DE

Inventors

Markus Schlemmer · Mainburg, DE
Bartlomiej Pikul · Tarnów, PL

Key dates

Filing date	Jan 14, 2011
Grant date	Nov 1, 2016
Priority date	—
Expiry date	Apr 3, 2033

Classification

Technology area (CPC Y)Emerging Cross-Sectional Technologies
CPC primaryY02T50/60
WIPO fieldEngines, pumps, turbines
WIPO sectorMechanical engineering

Abstract

The invention relates to a blade (2) of a turbomachine, in particular a rotor blade of a gas turbine, which has a variable transition radius (Rv1) in the vicinity of at least one platform overhang (16), and to a turbomachine having at least one such blade (2).

Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.