Light source and optical sensor packaging

Patent metadata

Field	Value
Publication number	US-2026056088-A1
Application number	US-202418810173-A
Country	US
Kind code	A1
Filing date	Aug 20, 2024
Priority date	Aug 20, 2024
Publication date	Feb 26, 2026
Grant date	—

Abstract

An apparatus may include a fan case and an optical pipe. The fan case may define a gas flow path. The optical pipe may have a portion extending through the fan case into the gas flow path. The optical pipe may include a lens, a beamsplitter, a light source, and an optical sensor. The lens may be positioned within the fan case. The beam splitter may be aligned with the lens. The light source may be positioned on a first side of the beam splitter. The optical sensor may be positioned on a second side of the beam splitter in a manner that an optical axis of the optical sensor is colinear with an optical axis of the light source at the lens.

First claim

What is claimed is:

1 . An apparatus comprising:
a fan case defining a gas flow path; and an optical pipe comprising a portion extending through the fan case into the gas flow path, the optical pipe including:
a lens positioned within the fan case;
a beam splitter aligned with the lens;
a light source positioned on a first side of the beam splitter; and
an optical sensor positioned on a second side of the beam splitter in a manner that an optical axis of the optical sensor is colinear with an optical axis of the light source at the lens.

2 . The apparatus of claim 1 , wherein the beam splitter is a dichroic mirror.

3 . The apparatus of claim 1 , wherein the light source is positioned to project light through the beam splitter.

4 . The apparatus of claim 1 , wherein the optical sensor is positioned to capture an image reflected by the beam splitter.

5 . The apparatus of claim 1 , wherein the optical pipe further comprises a mirror positioned between the beam splitter and the light source.

6 . The apparatus of claim 1 , wherein the optical pipe further comprises a pivot configured to rotate the portion of the optical pipe extending into the gas flow path to be flush with the fan case.

7 . The apparatus of claim 1 , wherein the optical pipe further comprises a shutter for the lens.

8 . A gas turbine engine comprising:
a fan case defining a gas flow path; a plurality of blades; and an optical pipe including a portion extending through the fan case into the gas flow path, the optical pipe including:
a lens positioned within the fan case;
a beam splitter aligned with the lens;
a light source positioned on a first side of the beam splitter; and
an optical sensor positioned on a second side of the beam splitter in a manner that an optical axis of the optical sensor is colinear with an optical axis of the light source at the lens.

9 . The gas turbine engine of claim 8 , wherein the beam splitter is a dichroic mirror.

10 . The gas turbine engine of claim 8 , wherein the light source is positioned to project light through the beam splitter.

11 . The gas turbine engine of claim 8 , wherein the optical sensor is positioned to capture an image reflected by the beam splitter.

12 . The gas turbine engine of claim 8 , wherein the optical pipe further comprises a mirror positioned between the beam splitter and the light source.

13 . The gas turbine engine of claim 8 , wherein the optical pipe further comprises a pivot to rotate the portion of the optical pipe extending into the gas flow path to be flush with the fan case.

14 . The gas turbine engine of claim 8 , wherein the optical pipe further comprises a shutter for the lens.

15 . A method for an optical pipe comprising a portion extending through a fan case into a gas flow path, the method comprising:
positioning, in the optical pipe, a lens within the fan case; aligning, in the optical pipe, a beam splitter with the lens; positioning, in the optical pipe, a light source on a first side of the beam splitter; and positioning, in the optical pipe, an optical sensor on a second side of the beam splitter in a manner that an optical axis of the optical sensor is colinear with an optical axis of the light source at the lens.

16 . The method of claim 15 , wherein the beam splitter is a dichroic mirror.

17 . The method of claim 15 , wherein positioning the light source comprises positioning the light source to project light through the beam splitter.

18 . The method of claim 15 , wherein positioning the optical sensor comprises positioning the optical sensor to capture an image reflected by the beam splitter.

19 . The method of claim 15 , further comprising:
positioning, in the optical pipe, a mirror between the beam splitter and the light source.

20 . The method of claim 15 , further comprising:
rotating, using a pivot of the optical pipe, the portion of the optical pipe extending through the fan case so that the portion of the optical pipe extending into the gas flow path is flush with the fan case.

Assignees

• Rtx Corp

Inventors

• Ahmadian Shayan

Classifications

• F05D2260/83

  Testing, e.g. methods, components or tools therefor · CPC title

• F05D2220/32

  in gas turbines · CPC title

• F01D21/003 Primary

  Arrangements for testing or measuring (for measuring vibrations G01H) · CPC title

• F05D2270/804

  Optical devices · CPC title

• F01D1/00

  Non-positive-displacement machines or engines, e.g. steam turbines (wit working-fluid flows in opposite axial directions for balancing axial thrust F01D3/02; with other than pure rotation F01D23/00; turbines characterised by their use in special steam systems, cycles, or processes, regulating devices therefor F01K) · CPC title