Patent · US Active

Airfoil blade and method of assembly

US10208982B2 · kind B2 · utility

84Cited by
6References
17Claims
0Family size

Assignee

Inventors

Key dates

Filing dateJan 19, 2016
Grant dateFeb 19, 2019
Priority date
Expiry dateJun 6, 2036

Classification

  • Technology area (CPC F)Mechanical Engineering; Lighting; Heating
  • CPC primaryF24F13/15
  • WIPO fieldThermal processes and apparatus
  • WIPO sectorMechanical engineering

Abstract

An airfoil blade assembly includes a first shell member having a body having a first lock seam formed at one end thereof and a free distal end opposite the first lock seam, and a second shell member having a body having and a second lock seam formed at one end thereof and an a free distal end opposite the second lock seam. The second shell member is inverted with respect to the first shell member. The free distal end of the first shell member is captured within the second lock seam of the second shell member and the free distal end of the second shell member is captured within the first lock seam of the first shell member to lock the blades to one another.

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