Apparatus for simulating operation of fan blades in a gas turbine
AssigneeGeneral Electric Company
InventorsAndrew Thomas Hynous, Brian Ralph Thompson
Life of this patent
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Abstract
This disclosure describes a training apparatus, wherein embodiments of the training apparatus simulate operation of fan blades in a turbine engine. An advantage that practice of some disclosed embodiments of the training apparatus is to provide a platform to train skills for maintaining and servicing turbine engines without placing the individual and/or customer hardware in jeopardy.
Claims15
A training device that replicates operation of a fan blades in a turbine engine, said training device comprising:
- a motor;
- a shaft coupled to the motor, the shaft having a central axis and an array of blade elements disposed radially about the central axis;
- and
- a housing enclosing the array, the housing comprising a plurality of probe mounting members with openings extending through the housing and exposing a top surface of the blade elements in the array, the plurality of probe mounting members comprising,
- a first probe member with a bore surface radially outward of and tangential to the center axis of the shaft, the openings comprising a bore extending normal to the bore surface to receive a first probe inserted therein, and
- a second probe member with an adapter surface extending away from the housing to support an adapter that positions a second probe normal to the top surface of the blades, the openings comprising an adapter opening proximate the adapter surface, the adapter opening exposing the top surface of the blade elements to the second probe.
An apparatus for simulating travel of fan blades of a turbine engine, said apparatus comprising:
- a shaft having a central axis and an array of blade elements disposed radially about the central axis;
- a housing enclosing the array of blade elements, the housing comprising integrated members to position probes proximate a top surface of the blade elements,
- wherein rotation of the shaft, in combination with the number of the blade elements, simulates one or more stages of the turbine engine.
Dependencies are inferred from the claim text.