Non-contact strain measurement

Patent metadata

Field	Value
Publication number	US-10402716-B2
Application number	US-201414903919-A
Country	US
Kind code	B2
Filing date	Jul 9, 2014
Priority date	Jul 9, 2013
Publication date	Sep 3, 2019
Grant date	Sep 3, 2019

Abstract

Non-contact strain measurement systems and their method of use to detect strain on rotating components are disclosed. A non-contact strain measurement system comprises magnetic materials plated onto a rotatable component in addition to appropriate encoders and controller. The magnetic materials are spaced apart a first distance D1 when the component is not rotating, and a second distance D2 when the component is rotating. The encoders and controller are utilized to detect strain on the rotating component. A method of using the system to detect strain on a rotating component includes detecting the first distance D1 then detecting the second distance D2, and calculating the strain imparted onto the component from a difference between D1 and D2.

First claim

What is claimed is:

1. A system for determining strain imparted to a rotating fan blade in a gas turbine engine, the system comprising:
a first magnetic target plated onto the fan blade at a first initial position;
a first encoder for detecting a first actual position of the first magnetic target when the fan blade is rotating;
a second magnetic target plated onto the fan blade at a second initial position;
a second encoder for detecting a second actual position of the second magnetic target when the fan blade is rotating;
the first and second initial positions being spaced apart by a first distance when the fan blade is not rotating;
the first and second actual positions being spaced apart by a second distance when the fan blade is rotating at a rotational velocity sufficient to impart a measurable strain to the fan blade;
a controller for receiving first and second signals from the first and second encoders respectively indicative of the first and second actual positions respectively, the controller programmed to calculate the second distance from the first and second signals and programmed with an algorithm to calculate strain imparted onto the fan blade from a difference between the second distance and the first distance, wherein the fan blade is fabricated from a polymer, a reinforced polymer, a polymer matrix composite, a ceramic, or a ceramic matrix composite.

2. The system of claim 1 wherein the first and second encoders are integrated together in a single housing.

3. The system of claim 1 wherein the first and second encoders and the controller are integrated together in a single housing.

4. The system of claim 1 wherein the first and second targets are electroplated onto the fan blade.

5. The system of claim 1 wherein the first and second targets are electroless plated onto the tan blade.

6. The system of claim 1 wherein the first and second targets have thicknesses ranging from about 2.5 to about 20 microns.

7. The system of claim 1 wherein the first encoder includes a Hall effect sensor.

8. The system of claim 1 wherein the second encoder includes a Hall effect sensor.

9. The system of claim 1 wherein the first and second encoders include Hall effect sensors.

10. The system of claim 1 wherein the first and second targets may be removed from the fan blade by peeling.

11. A system for determining strain imparted to a fan blade assembly in a gas turbine engine, the system comprising:
a first magnetic target plated onto the fan blade assembly at a first initial position;
a first encoder for detecting a first actual position of the first magnetic target when the fan blade assembly is rotating;
a second magnetic target plated onto the fan blade assembly at a second initial position;
a second encoder for detecting a second actual position of the second magnetic target when the fan blade assembly is rotating;
the first and second initial positions being spaced apart by a first distance when the fan blade assembly is not rotating;
the first and second actual positions being spaced apart by a second distance when the fan blade assembly is rotating at a rotational velocity sufficient to impart a measurable strain to the fan blade assembly;
a controller for receiving first and second signals from the first and second encoders respectively indicative of the first and second actual positions respectively, the controller programmed to calculate the second distance from the first and second signals and programmed with an algorithm to calculate strain imparted onto the fan blade assembly from a difference between the second distance and the first distance, wherein the fan blade assembly comprises a fan blade fabricated from a polymer, a reinforced polymer, a polymer matrix composite, a ceramic, or a ceramic matrix composite.

12. The system of claim 11 wherein the first and second targets are electroless plated onto the fan blade.

13. The system of claim 11 wherein the first and second targets have thicknesses ranging from about 2.5 to about 20 microns.

14. The system of claim 11 wherein the first encoder, the second encoder or both include a Hall effect sensor.

15. The system of claim 11 wherein the first and second targets are electroplated onto the fan blade.

16. A method for determining strain imparted to a fan blade in a gas turbine engine, the method comprising:
plating a first magnetic target onto the fan blade at a first initial position;
plating a second magnetic target onto the fan blade at a second initial position that is spaced apart from the first initial position by a first distance;
detecting a first actual position of the first magnetic target when the fan blade is rotating;
detecting a second actual position of the second magnetic target when the fan blade is rotating;
calculating a second distance between the first and second actual positions when the fan blade is rotating;
calculating strain imparted onto the fan blade from a difference between the first distance and the second distance, wherein the fan blade assembly comprises a fan blade fabricated from a polymer, a reinforced polymer, a polymer matrix composite, a ceramic, or a ceramic matrix composite.

17. The method of claim 16 wherein the first and second targets are electroplated onto the fan blade.

18. The method of claim 16 wherein the first and second targets are electroless plated onto the fan blade.

19. The method of claim 16 wherein the first and second targets have thicknesses ranging from about 2.5 to about 20 microns.

Assignees

• United Technologies Corp

Inventors

• Cook Iii Grant O
• Twelves Wendell V

Classifications

• B29C64/124

  using layers of liquid which are selectively solidified · CPC title

• C23C18/1653

  Two or more layers with at least one layer obtained by electroless plating and one layer obtained by electroplating · CPC title

• B29L2009/008

  metalized, galvanized · CPC title

• B32B2250/02

  2 layers · CPC title

• G01N2203/0268

  Dumb-bell specimens · CPC title