Patent · US Active

Tangential blade root neck conic

US10982555B2 · kind B2 · utility

0Cited by
6References
17Claims
0Family size

Assignee

Inventors

Key dates

Filing dateFeb 27, 2014
Grant dateApr 20, 2021
Priority date
Expiry dateJan 17, 2038

Classification

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

Abstract

A root extending from a platform of an airfoil is disclosed. The root may include a first portion having a generally cylindrical shape, and a second portion extending from the first portion to the platform. The second portion may have a circumference larger than a circumference of the first portion.

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