Patent · US Active

Engine component assembly with ceramic matrix composite component and connection pin

US12196100B1 · kind B1 · utility

0Cited by
14References
20Claims
0Family size

Assignee

Inventors

Key dates

Filing dateMay 17, 2024
Grant dateJan 14, 2025
Priority date
Expiry dateMay 17, 2044

Classification

  • Technology area (CPC F)Mechanical Engineering; Lighting; Heating
  • CPC primaryF05D2300/6033
  • WIPO fieldEngines, pumps, turbines
  • WIPO sectorMechanical engineering

Abstract

A turbine engine component assembly includes a first part comprising a ceramic matrix composite material and having a first flange defining a first borehole, a second part defining a second borehole, and a pin inserted, in an axial direction, through the first borehole and the second borehole to connect the first part to the second part. The pin includes a first contact portion positioned at a first axial location of the pin corresponding to the first borehole and an elongated portion extending axially from the first contact portion. The first contact portion includes a first chamfered section, a second chamfered section, and a first contact surface between the first chamfered section and the second chamfered section. The first chamfered section and the second chamfered section slope away from the first contact surface with decreasing diameters.

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