Patent · US Active

Blade for a turbomachine

US10947850B2 · kind B2 · utility

0Cited by

4References

22Claims

0Family size

Assignee

MTU Aero Engines AG · DE

Inventors

Martin Pernleitner · Dachau, DE
Manfred Dopfer · Unterschleißheim, DE
Daniel Theurich · Munich, DE

Key dates

Filing date	Sep 7, 2018
Grant date	Mar 16, 2021
Priority date	—
Expiry date	Feb 14, 2039

Classification

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

Abstract

A blade (10) for a turbomachine is provided. The blade (10) includes an airfoil (16) having at least one thickening (22) on a pressure side (20) of the airfoil (16). The thickening (22) has a region (B) of constant thickness (D). A turbomachine, a compressor and a turbine having stator vanes and/or rotor blades including at least one such blade (10) is also provided.

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