Patent · US Active

Engine door with burst seal

US10634060B2 · kind B2 · utility

3Cited by
7References
20Claims
0Family size

Assignee

Inventor

Key dates

Filing dateNov 20, 2016
Grant dateApr 28, 2020
Priority date
Expiry dateOct 21, 2037

Classification

  • Technology area (CPC F)Mechanical Engineering; Lighting; Heating
  • CPC primaryF05D2260/606
  • WIPO fieldEngines, pumps, turbines
  • WIPO sectorMechanical engineering

Abstract

A method and apparatus for a gas turbine engine including a core engine a nacelle surrounding at least a portion of the core engine and defining an interior with an opening. An access door for the opening to provide selective access to the opening where the access door provides pressure relief for the interior.

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