Patent · US Active

Intermittent spigot joint for gas turbine engine casing connection

US11009039B2 · kind B2 · utility

0Cited by
14References
7Claims
0Family size

Assignee

Inventors

Key dates

Filing dateDec 20, 2018
Grant dateMay 18, 2021
Priority date
Expiry dateFeb 15, 2039

Classification

  • Technology area (CPC Y)Emerging Cross-Sectional Technologies
  • CPC primaryY10T403/7069
  • WIPO fieldEngines, pumps, turbines
  • WIPO sectorMechanical engineering

Abstract

A gas turbine engine casing apparatus includes annular first and second annular cases connected by a spigot joint. The spigot joint includes an annular projection of the first annular case fitted into an annular recess of the second annular case. A plurality of circumferentially spaced apart scallops are formed on one of surfaces of the annular projection or of the annular recess, and are located in selective circumferential locations adjacent respective enhanced stiff areas of the first and second annular cases.

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