System and method for performing a visual inspection of a gas turbine engine
First Claim
1. A system for performing a visual inspection of a gas turbine engine, the system comprising:
- a plurality of optical probes to be installed through a plurality of access ports that are spaced apart axially along a longitudinal axis of the gas turbine engine to be inspected, the plurality of optical probes being configured to provide internal views of the gas turbine engine from a plurality of different axial locations associated with the plurality of access ports;
a rotating device configured to rotate the gas turbine engine about the longitudinal axis as the plurality of optical probes are used to simultaneously obtain images of an interior of the gas turbine engine at the plurality of different axial locations; and
a computing device communicatively coupled to each of the plurality of optical probes, the computing device being configured to receive image data associated with the images obtained by each of the plurality of optical probes at the plurality of different axial locations;
wherein the rotating device is communicatively coupled to the computing device, the computing device being configured to transmit control signals to the rotating device such that the rotating device rotates the gas turbine engine at a controlled speed about the longitudinal axis.
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Accused Products
Abstract
A method for performing a visual inspection of a gas turbine engine may generally include inserting a plurality of optical probes through a plurality of access ports of the gas turbine engine. The access ports may be spaced apart axially along a longitudinal axis of the gas turbine engine such that the optical probes provide internal views of the gas turbine engine from a plurality of different axial locations along the gas turbine engine. The method may also include coupling the optical probes to a computing device, rotating the gas turbine engine about the longitudinal axis as the optical probes are used to simultaneously obtain images of an interior of the gas turbine engine at the different axial locations and receiving, with the computing device, image data associated with the images obtained by each of the optical probes at the different axial locations.
50 Citations
20 Claims
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1. A system for performing a visual inspection of a gas turbine engine, the system comprising:
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a plurality of optical probes to be installed through a plurality of access ports that are spaced apart axially along a longitudinal axis of the gas turbine engine to be inspected, the plurality of optical probes being configured to provide internal views of the gas turbine engine from a plurality of different axial locations associated with the plurality of access ports; a rotating device configured to rotate the gas turbine engine about the longitudinal axis as the plurality of optical probes are used to simultaneously obtain images of an interior of the gas turbine engine at the plurality of different axial locations; and a computing device communicatively coupled to each of the plurality of optical probes, the computing device being configured to receive image data associated with the images obtained by each of the plurality of optical probes at the plurality of different axial locations; wherein the rotating device is communicatively coupled to the computing device, the computing device being configured to transmit control signals to the rotating device such that the rotating device rotates the gas turbine engine at a controlled speed about the longitudinal axis. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14, 15, 16, 17, 18, 19, 20)
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Specification