Optical apparatus and sight tube for inspecting turbine engine components

Patent metadata

Field	Value
Publication number	US-10473528-B2
Application number	US-201615043508-A
Country	US
Kind code	B2
Filing date	Feb 13, 2016
Priority date	Feb 13, 2016
Publication date	Nov 12, 2019
Grant date	Nov 12, 2019

Abstract

An apparatus for insertion through an opening in an outer casing of a gas turbine engine and inspection of internal turbine components at elevated temperatures having an optical sight tube configured to optically communicate with an interior of gas turbine engine via a distal end disposed at the interior and a proximal end disposed exterior of the internal turbine components and defined by a first longitudinal wall, at least one lens at the distal end of the optical sight tube adjacent to the longitudinal wall; and at least one longitudinal cooling groove in the longitudinal wall for flowing a cooling medium from a location external to the turbine to cool the optical sight tube at a location at least adjacent the distal end.

First claim

What is claimed is:

1. An apparatus for insertion through an opening in an outer casing of a turbine engine and inspection of internal turbine components at elevated temperatures comprising:
a hollow optical sight tube configured to optically communicate with an interior of a gas turbine engine via a distal end disposed at the interior of the gas turbine engine and a proximal end disposed exterior of the internal turbine components and defined by a first longitudinal wall defining a continuous, even, and concentric interior surface; and
at least two lenses received within the hollow optical sight tube, the at least two lenses fixed to a first portion of the interior surface of the first longitudinal wall at the distal end of the optical sight tube, and not fully contacting a second portion of the longitudinal wall, wherein a space between the second portion and the at least two lenses defines a longitudinal lens cooling groove of each of the at least two lenses, and wherein the cooling groove of each of the at least two lenses are axially aligned along the first longitudinal wall, the lens cooling groove arranged for flowing a cooling medium from a location external to the turbine to cool the hollow optical sight tube at a location at least adjacent the distal end.

2. The apparatus of claim 1 further comprising a plurality of holes in the longitudinal wall, the plurality of holes adjacent the lens to direct cooling medium from the respective groove toward the lens to purge the lens.

3. The apparatus of claim 1 comprising a plurality of longitudinal cooling grooves.

4. The apparatus of claim 1 further including an inlet nozzle removably secured to the optical sight tube to supply the cooling medium.

5. The apparatus of claim 1 further including a plurality of lenses located in spaced arrangement across the extent of the optical sight tube.

6. The apparatus of claim 1 wherein the distal end of the optical sight tube defines a radial aperture receiving of the at least two lenses, and wherein the respective lens cooling groove is defined by a portion of the radial aperture between the lens and the distal end.

7. The apparatus of claim 1 wherein the optical sight tube is an elongated cylinder.

8. The apparatus of claim 7 wherein the optical sight tube is hollow except for the at least two lenses.

9. The apparatus of claim 1 wherein the at least two lenses are received at an axial location, and wherein the first portion and the second portion of the first longitudinal wall are axially aligned with the axial location.

10. An optical sight tube for viewing internal components of a turbine engine, comprising:
a first elongated wall defining a continuous, even, and concentric interior surface; and
at least two lenses proximate to an interior distal end of the first elongated wall, each of the at least two lenses fixed at a relative first portion of the interior surface of the first elongated wall and not fully contacting a relative second portion of the interior surface of the first elongated wall, wherein a space between the second portion and the at least two lenses defines a lens cooling groove of each of the at least two lenses, and wherein the cooling groove of each of the at least two lenses are axially aligned along the first elongated wall such that the lens cooling groove is configured for flowing a cooling medium from a location external to the turbine to cool the optical sight tube at a location at least adjacent the distal end.

11. The optical sight tube of claim 10 comprising a plurality of longitudinal cooling grooves.

12. The optical sight tube of claim 10 further including a connection for removably securing an inlet nozzle to supply the cooling medium.

13. The optical sight tube of claim 10 further including a plurality of lenses located in spaced arrangement across the extent of the optical sight tube.

14. The apparatus of claim 10 wherein the optical sight tube is an elongated cylinder.

15. The apparatus of claim 10 wherein the optical sight tube is hollow except for the at least two lenses.

16. The apparatus of claim 10 wherein the at least two lenses is received at an axial location of the first elongated wall, and wherein the first portion and the second portion of the first elongated wall are axially aligned with the axial location.

Assignees

• Gen Electric

Inventors

• Sakami Mohamed
• Nirmalan Nirm Velumylum
• Bailey Jeremy Clyde

Classifications

• G01N2021/9542

  using a probe · CPC title

• G01N21/954 Primary

  Inspecting the inner surface of hollow bodies, e.g. bores · CPC title

• F02D41/1451

  the sensor being an optical sensor · CPC title

• G01N25/72

  Investigating presence of flaws · CPC title

• G01N2021/151

  Gas blown · CPC title