Patent · US Active

Method to pilot using flexible profile

US10422238B2 · kind B2 · utility

2Cited by
22References
27Claims
0Family size

Assignee

Inventors

Key dates

Filing dateNov 9, 2015
Grant dateSep 24, 2019
Priority date
Expiry dateApr 30, 2038

Classification

  • Technology area (CPC F)Mechanical Engineering; Lighting; Heating
  • CPC primaryF05D2260/97
  • WIPO fieldEngines, pumps, turbines
  • WIPO sectorMechanical engineering

Abstract

A gas turbine engine according to the present disclosure includes a first component, a second component coupled to the first component, and a pilot unit. The pilot unit provides means for maintaining a pilot-setting force between the first and second component to retain alignment of the first component with the second component.

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