Patent · US Active

Maintenance assembly adaptable within gas turbine engine

US9540829B2 · kind B2 · utility

1Cited by
51References
10Claims
0Family size

Assignee

Inventors

Key dates

Filing dateJul 18, 2014
Grant dateJan 10, 2017
Priority date
Expiry dateJul 18, 2034

Classification

  • Technology area (CPC F)Mechanical Engineering; Lighting; Heating
  • CPC primaryF05D2230/72
  • WIPO fieldEngines, pumps, turbines
  • WIPO sectorMechanical engineering

Abstract

The maintenance assembly, for workers to perform maintenance activities within a gas turbine engine, is capable of being arranged within a cavity, generally around a combustor, accessible from a manhole of the gas turbine engine. The maintenance assembly includes a platform, and an inflatable member cooperatively configured to the platform. The inflatable member is at a normal condition, when placed outside of the cavity, being at a deflated position and is at a working condition, when arranged within the cavity, being at inflated position so as to accommodate a shape coordinating the cavity in such a manner that the platform is advance within the cavity up to a predetermined level to enable the workers on the platform to reach at a predetermined position within the cavity to perform the maintenance activities.

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