Fiber optic sensing for variable area fan nozzles

Patent metadata

Field	Value
Publication number	US-10184425-B2
Application number	US-201615009298-A
Country	US
Kind code	B2
Filing date	Jan 28, 2016
Priority date	Jan 28, 2016
Publication date	Jan 22, 2019
Grant date	Jan 22, 2019

Abstract

A control system for a variable area fan nozzle (VAFN) having a plurality of petals is disclosed. The control system may include at least one fiber optic shape sensor extending along at least one of the plurality of petals, and a light source operatively connected to the at least one fiber optic shape sensor. The control system may further include a receiver operatively connected to the at least one fiber optic shape sensor. The control system may further include a VAFN control unit in operative communication with the plurality of petals and the receiver. The VAFN control unit may be configured to receive a signal from the receiver indicative of the measured strain along the at least one fiber optic shape sensor, and calculate a nozzle area of the VAFN based on the measured strain.

First claim

What is claimed is:

1. A control system for a variable area fan nozzle (VAFN) having a plurality of petals, the control system comprising:
a fiber optic shape sensor forming a continuous loop around the perimeter of each petal of the plurality of petals;
a respective light source operatively connected to, and configured to direct a light through, each of the fiber optic shape sensors;
a respective receiver operatively connected to each of the fiber optic shape sensors, each respective receiver configured to receive a reflected light from an associated fiber optic shape sensor and measure a strain along the associated fiber optic shape sensor based on the reflected light; and
a VAFN control unit in operative communication with the plurality of petals and the respective receivers, the VAFN control unit configured to receive a first signal from each respective receiver indicative of the measured strain along each of the associated fiber optic shape sensors, and calculate an actual nozzle area of the VAFN based on the measured strain.

2. The control system of claim 1 , wherein each respective receiver is further configured to determine a displacement of the associated fiber optic shape sensor based on the measured strain.

3. The control system of claim 1 , wherein each fiber optic shape sensor includes an optical fiber having a plurality of Fiber Bragg gratings configured to reflect predetermined wavelengths of light.

4. The control system of claim 1 , wherein each fiber optic shape sensor includes Optical Frequency Domain Reflectometry (OFDR) technology configured to provide a fully distributed sensing fiber.

5. The control system of claim 4 , wherein each respective light source comprises a wavelength tunable laser.

6. The control system of claim 1 , wherein each fiber optic shape sensor comprises three optical fibers with fiber optic sensing devices bundled together, and wherein each respective receiver is further configured to determine a three-dimensional displacement of the associated fiber optic shape sensor based on the measured strain from the three optical fibers bundled together.

7. The control system of claim 6 , wherein the VAFN control unit is further configured to determine a three-dimensional position of each petal of the plurality of petals based on the determined three-dimensional displacement from each respective receiver.

8. The control system of claim 1 , further comprising an engine electronic control in communication with the VAFN control unit, the engine electronic control configured to generate a command nozzle area for the VAFN and send a second signal to the VAFN control unit indicative of the command nozzle area.

9. The control system of claim 8 , wherein the VAFN control unit is further configured to determine a difference between the actual nozzle area and the command nozzle area.

10. The control system of claim 9 , wherein the VAFN control unit is further configured to generate an actuator command for the plurality of petals based on the determined difference between the actual nozzle area and the command nozzle area.

11. The control system of claim 10 , wherein the VAFN control unit uses one of proportional integral differential, linear quadratic regression, or bang-bang control to generate the actuator command.

12. The control system of claim 11 , wherein the engine electronic control is configured to generate the command nozzle area based on an engine operating condition.

13. A variable area fan nozzle (VAFN) comprising:
a plurality of petals disposed along a circumference of a fan duct, wherein each petal of the plurality of petals includes a first side and an opposite second side that extend in a longitudinal direction from a supported end to a free end that forms an opening of the VAFN;
each respective petal of the plurality of petals having an associated pair of first and second fiber optic shape sensors, wherein the first fiber optic shape sensor extends along at least the first side of the respective petal of the plurality of petals and the second fiber optic shape sensor extends along the opposite second side of the respective petal of the plurality of petals;
respective first and second light sources configured to direct light through the first and second fiber optic shape sensors of each associated pair of first and second fiber optic shape sensors;
respective first and second receivers configured to receive reflected light from the first and second fiber optic shape sensors of each associated pair of first and second fiber optic shape sensors and determine displacement of the first and second fiber optic shape sensors of each associated pair of first and second fiber optic shape sensors based on the reflected light;
an engine electronic control configured to generate a command nozzle area of the opening of the VAFN based on an engine operating condition; and
a VAFN control unit in operative communication with the plurality of petals, each respective first and second receiver, and the engine electronic control, the VAFN control unit configured to receive a sensor displacement signal indicative of the determined displacement from each respective first and second receiver, calculate an actual nozzle area of the VAFN based on the determined displacement from each respective first and second receiver, receive a command nozzle area signal indicative of the command nozzle area from the engine electronic control, determine a difference between the actual nozzle area and the command nozzle area, and generate an actuator command based on the determined difference between the actual nozzle area and the command nozzle area.

14. The VAFN of claim 13 , wherein the first and second fiber optic shape sensors of each associated pair of first and second fiber optic shape sensors are embedded inside the respective petal of the plurality of petals.

15. The VAFN of claim 13 , wherein the first and second fiber optic shape sensors of each associated pair of first and second fiber optic shape sensors are attached to a surface of the respective petal of the plurality of petals.

16. A method of controlling a nozzle area of a variable area fan nozzle (VAFN) having a plurality of petals, each petal of the plurality of petals having an associated fiber optic shape sensor, the method comprising:
transmitting light through each associated fiber optic shape sensor, wherein each associated fiber optic shape sensor forms a continuous loop around the perimeter of a respective petal of the plurality of petals;
receiving reflected light from each associated fiber optic shape sensor;
measuring strain based on the received reflected light from each associated fiber optic shape sensor;
determining a displacement of each associated fiber optic shape sensor based on the measured strain, the receiving, measuring, and determining being performed by a respective receiver operably coupled to each associated fiber optic shape sensor;
calculating an actual nozzle area of an opening defined by the plurality of petals based on the determined displacement of each associated fiber optic shape sensor; and
generating an actuator command based at least in part on the actual nozzle area, the calculating and generating being performed by a VAFN control unit.

17. The method of claim 16 , wherein each associated fiber optic shape sensor includes three bundled optical fibers with fiber optic sensing devices to form each associated fiber optic shape sensor, the method further comprising determining a three-dimensional shape of each petal of the plurality of petals.

18. The

Assignees

• Boeing Co

Inventors

• Jackowski Jason J
• Karnofski Kent E

Classifications

• F05D2270/804

  Optical devices · CPC title

• F02K1/15 Primary

  Control or regulation · CPC title

• F02K1/18 Primary

  automatic · CPC title

• F02K1/06

  Varying effective area of jet pipe or nozzle (by using fluid jets to influence the jet flow F02K1/30) · CPC title

• F02K1/12

  by means of pivoted flaps · CPC title