Autonomous inspection of a surface topology of an airfoil of a gas turbine engine

Patent metadata

Field	Value
Publication number	US-12529551-B2
Application number	US-202418592181-A
Country	US
Kind code	B2
Filing date	Feb 29, 2024
Priority date	Feb 29, 2024
Publication date	Jan 20, 2026
Grant date	Jan 20, 2026

Abstract

Apparatus and associated methods relate to autonomous devices configured to inspect surface topologies of airfoils of a gas turbine engine. The autonomous device moves across the airfoil while remaining coupled thereto while sensing the surface topology of the airfoil using a plurality of topological sensors. Each of the plurality of topological sensors includes a piezoelectric sensor that generates an electrical signal indicative of a loading to the piezoelectric sensor, as well as an airfoil contacting member. The airfoil contacting member extends between the piezoelectric sensor and the airfoil when the body is coupled thereto. The airfoil contacting member provides changes to the loading to the piezoelectric sensor in response to changes in the surface topology of the airfoil as the body moves thereacross.

First claim

The invention claimed is:

1 . An autonomous device for inspecting surface topology of an airfoil of a gas turbine engine, the autonomous device comprising:
a body; means for coupling the body to the airfoil in a manner that permits movement of the body across the airfoil while remaining coupled thereto; means for moving the body across the airfoil while remaining coupled thereto; a plurality of topological sensors extending from the body to the airfoil when the body is coupled thereto, each of the plurality of topological sensors including:
a piezoelectric sensor that generates an electrical signal indicative of a loading to the piezoelectric sensor;
an airfoil contacting member extending between the piezoelectric sensor and the airfoil when the body is coupled thereto, thereby providing changes to the loading to the piezoelectric sensor in response to changes in the surface topology of the airfoil as the body moves thereacross; and
a surface topology calculator attached to the body and electrically connected to the plurality of piezoelectric sensors and configured to locate defects in the surface topology of the airfoil based on the electrical signals generated by the plurality of piezoelectric sensors.

2 . The autonomous device of claim 1 , wherein the surface topology calculator determines the surface topology of the airfoil along each of a plurality of paths across the airfoil taken by the plurality of topological sensors.

3 . The autonomous device of claim 1 , wherein the means for coupling the body to the airfoil includes:
a device coupling member that couples the body to the airfoil using van der Waals force.

4 . The autonomous device of claim 1 , wherein the means for coupling the body to the airfoil includes:
a sealing element circumscribing an evacuation chamber, the sealing element configured to engage the surface of the airfoil; and a vacuum pump configured to evacuate the evacuation chamber, thereby causing the autonomous device to adhere to the surface of the airfoil.

5 . The autonomous device of claim 1 , wherein the means for moving the body across the airfoil includes:
a wheel extending from the body so as to engage the airfoil when the body is coupled thereto; and a motor configured to rotate the wheel, thereby moving the body across the airfoil when coupled thereto.

6 . The autonomous device of claim 1 , wherein the means for moving the body across the airfoil includes:
an arm or leg that sequentially positions itself so as to engage the airfoil and pushes or pulls the body across the airfoil when coupled thereto.

7 . The autonomous device of claim 1 , further comprising:
means for steering the body as it moves across the airfoil.

8 . The autonomous device of claim 7 , further comprising:
edge sensors that sense the edge of the airfoil.

9 . The autonomous device of claim 8 , further comprising:
a navigation computer configured to control the means for steering the body and the means for moving the body across the airfoil so as to map surface topology of a plurality of portions of the airfoil.

10 . The autonomous device of claim 9 , wherein the navigation computer is configured to cause the body to move across the airfoil in a serpentine fashion.

11 . The autonomous device of claim 1 , wherein each of the plurality of topological sensors further includes:
a linkage assembly mechanically coupling the airfoil contacting member to the piezoelectric sensor, the linkage assembly having:
a spring member; and
a damping member.

12 . The autonomous device of claim 1 , wherein each of the plurality of airfoil contacting members has a pointed tip configured to contact the airfoil.

13 . The autonomous device of claim 1 , wherein each of the contact arms has a wheel configured to contact the airfoil, the wheel coupled to the contact arm via a castor.

14 . The autonomous device of claim 1 , wherein each of the plurality of topological sensors includes:
a piezoelectric actuator configured to superimpose, to the piezoelectric sensor, a sinusoidal loading to the loading provided by the airfoil contacting member.

15 . A method for inspecting surface topology of an airfoil of a gas turbine engine, the method comprising:
adhering a body of an autonomous device to the airfoil in a manner that permits movement of the body across the airfoil while remaining coupled thereto; moving the body of the autonomous device across the airfoil while remaining coupled thereto; extending a plurality of topological sensors from the body to the airfoil when the body is coupled thereto, each of the plurality of topological sensors:
providing changes to a loading to a piezoelectric sensor in response to changes in the surface topology of the airfoil as the body moves thereacross; and
generating, via the piezoelectric sensor, an electrical signal indicative of a loading to the piezoelectric sensor; and
locating, via a surface topology calculator, defects in the surface topology of the airfoil based on the electrical signals generated by the plurality of piezoelectric sensors.

16 . The method of claim 15 , further comprising:
superimposing, via a piezoelectric actuator and to the piezoelectric sensor, a sinusoidal loading upon the loading provided by the airfoil contacting member.

17 . The method of claim 15 , further comprising:
determining for each of the plurality of topological sensors, via the surface topology calculator, the surface topology of the airfoil along the path traversed thereby, based on the resonant frequency of topological sensor.

18 . The method of claim 15 , wherein the coupling the body to the airfoil includes:
circumscribing an evacuation chamber via a sealing element circumscribing, the sealing element configured to engage the surface of the airfoil; and evacuating the evacuation chamber via a vacuum pump, thereby causing the autonomous device to adhere to the surface of the airfoil.

19 . The method of claim 15 , wherein moving the body across the airfoil includes:
engaging, via a wheel extending from the body, the airfoil when the body is coupled thereto; and rotating the wheel via a motor, thereby moving the body across the airfoil when coupled thereto.

20 . The method of claim 15 , wherein the moving the body across the airfoil includes:
sequentially positioning an arm or leg so as to engage the airfoil, thereby pushing or pulling the body across the airfoil when coupled thereto.

Assignees

• Rtx Corp

Inventors

• Haye Sheridon
• Lee Jeremiah

Classifications

• G01M5/0016

  of aircraft wings or blades · CPC title

• G01N29/28

  providing acoustic coupling {, e.g. water (impedance matching G10K11/02)} · CPC title

• G01N2291/106

  one or more transducer arrays · CPC title

• G01N2291/2693

  Rotor or turbine parts · CPC title

• G01N29/225

  Supports, positioning or alignment in moving situation · CPC title