Method for in-situ nondestructive measurement of Young's modulus of plate structures

• US 6,575,036 B1
• Filed: 06/22/2000
• Issued: 06/10/2003
• Est. Priority Date: 06/22/2000
• Status: Expired due to Fees

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Huang, Jerry Qixin, DeLangis, Leo M., Perez, Robert J.
• Primary Examiner(s): Larkin, Daniel S.
• Assistant Examiner(s): Saint-Surin, Jacques
• Application Number:
  US09/602,173
• Time in Patent Office: 1,083 Days
• Field of Search: 735/97, 735/98, 736/02, 736/09, 735/99, 735/87, 736/29, 736/20, 736/18, 736/33, 736/44
• US Class Current: 73/597
• CPC Class Codes: G01N 2203/0055 using mechanical waves, e.g. acoustic
• CPC Class Codes: G01N 2203/0075 Strain-stress relations or elastic constants
• CPC Class Codes: G01N 2203/0282 Two dimensional, e.g. tapes, webs, sheets, strips, disks or membranes
• CPC Class Codes: G01N 2203/0658 using acoustic or ultrasonic detectors
• CPC Class Codes: G01N 2291/0231 Composite or layered materials
• CPC Class Codes: G01N 2291/0258 Structural degradation, e.g. fatigue of composites, ageing of oils
• CPC Class Codes: G01N 2291/02827 Elastic parameters, strength or force
• CPC Class Codes: G01N 2291/0421 Longitudinal waves
• CPC Class Codes: G01N 3/38 generated by electromagnetic means

Abstract

A method for determining stiffness of a composite laminate plate entails disposing a device for generating an acoustical pulse against a surface of the plate and disposing a detecting device against the same surface spaced a known distance from the pulse-generating device, and using the pulse-generating device to emit a pulse so as to create an extensional wave in the plate. The detecting device is used to determine a time of flight of the wave over the known distance, and the wave velocity is calculated. A Young'"'"'s modulus of the plate is determined based on the wave velocity. Methods for both anisotropic and quasi-isotropic laminates are disclosed.

Claims

1. A nondestructive method for quantitatively evaluating a material stiffness of a composite laminate plate along an in-plane direction, the plate having a plurality of plies arranged in a balanced symmetric ply lay-up and having opposite major surfaces defining a thickness of the plate therebetween, the method comprising:

propagating an elastic extensional-mode wave through the plate along said in-plane direction;

determining a velocity of the extensional-mode wave along said in-plane direction of the plate; and

calculating a material stiffness of the plate along said in-plane direction based on the wave velocity.

2. The method of claim 1, wherein propagating the extensional-mode wave comprises:

imparting energy to the plate at a first point located on a first of the major surfaces of the plate so as to cause the extensional-mode wave to originate at said first point and propagate along the plate.

3. The method of claim 2, wherein determining the wave velocity comprises:

detecting when the extensional-mode wave reaches a second point located on said first major surface and spaced in said in-plane direction from the first point;

determining a distance d between the first and second points along said first major surface of the plane in said in-plane direction;

measuring an elapsed time t required for the extensional-mode wave to travel the distance d from the first point to the second point; and

calculating the wave velocity based on the distance d and the time t.

4. The method of claim 3, wherein calculating the material stiffness comprises calculating a Young'"'"'s modulus along said in-plane direction.

5. The method of claim 4, adapted for evaluating a quasi-isotropic composite laminate plate, wherein the Young'"'"'s modulus E is calculated based on the equation

6. The method of claim 3, wherein detecting when the extensional-mode wave reaches the second point comprises using an acoustic energy detector disposed against the first major surface of the plate at the second point.

7. The method of claim 2, wherein imparting energy to the plate comprises using acoustic energy to create the extensional-mode wave.

8. The method of claim 2, wherein imparting energy to the plate comprises disposing a device for emitting acoustical energy against the first major surface of the plate at the first point and activating the device to emit acoustic energy.

9. A nondestructive method for quantitatively evaluating Young'"'"'s moduli of a composite laminate plate along two orthogonal in-plane x- and y-directions of the plate, comprising:

propagating an extensional wave through the plate;

determining a velocity c_x of the extensional wave along said x-direction;

determining a velocity c_y of the extensional wave along said y-direction;

determining Young'"'"'s moduli E_xx and E_yy respectively along the x- and y-directions by solving a set of simultaneous equations relating the extensional wave velocities, the Young'"'"'s moduli, and Poisson'"'"'s ratios and in-plane stiffness parameters for the plate to one another.

10. The method of claim 9, wherein the Young'"'"'s moduli E_xx and E_yy are determined by solving the set of equations:

11. A nondestructive method for quantitatively evaluating a change in Young'"'"'s modulus of a composite laminate plate along an in-plane direction, the plate having a plurality of plies arranged in a balanced symmetric ply lay-up and having opposite major surfaces defining a thickness of the plate therebetween, the method comprising:

(1) performing a first test including steps (a) through (c) comprising;

(a) imparting energy to the plate at a first point located on a first of the major surfaces of the plate so as to cause an extensional-mode wave to originate at said first point and propagate along the plate in said in-plane direction;

(b) detecting when the extensional-mode wave reaches a second point located on said first major surface and spaced a predetermined distance in said in-plane direction from the first point; and

(c) measuring a first elapsed time t₁ required for the extensional-mode wave to travel from the first point to the second point;

(2) performing a second test including steps (d) through (f) comprising;

(d) imparting energy to the plate at a third point located on a first of the major surfaces of the plate so as to cause an extensional-mode wave to originate at said third point and propagate along the plate in said in-plane direction;

(e) detecting when the extensional-mode wave reaches a fourth point located on said first major surface and spaced from the third point by the same said predetermined distance along said in-plane direction; and

(f) measuring a second elapsed time t₂ required for the extensional-mode wave to travel from the third point to the fourth point; and

(3) calculating a change in Young'"'"'s modulus for the plate along said in-plane direction based on a degree of difference of the times t₁ and t₂.

12. The method of claim 11, wherein the first and second tests are performed at two different times, whereby the change in Young'"'"'s modulus represents a change over time.

13. The method of claim 11, wherein the calculation of change in Young'"'"'s modulus is based on an assumption that density and Poisson'"'"'s ratio for the material of the plate are constant between the first test and the second test.

14. The method of claim 11, wherein calculating the change in Young'"'"'s modulus comprises calculating a ratio of Young'"'"'s moduli for the first and second tests based on a ratio of the times t₁ and t₂.

15. The method of claim 14, wherein the ratio of Young'"'"'s moduli is calculated by the equation

16. A method for quantitatively evaluating a material stiffness of an isotropic or quasi-isotropic plate along an in-plane direction, the method comprising:

disposing a first device for emitting acoustical energy on a first major surface of the plate and activating the device to cause an elastic extensional-mode wave to be propagated through the plate along said in-plane direction;

disposing a second device for detecting the extensional-mode wave on said first major surface of the plate spaced a distance d from the first device along said in-plane direction and using the second device to detect arrival of the extensional-mode wave;

measuring the elapsed time t between initiation of the extensional-mode wave by the first device and detection of the extensional-mode wave by the second device; and

calculating Young'"'"'s modulus E of the plate along said in plane direction based on the equation

17. The method of claim 16, further comprising permanently bonding the first and second devices to said first major surface of the plate, and periodically performing tests with the devices to determine Young'"'"'s modulus at a plurality of sequential times, whereby the spacing between the devices and the devices'"'"' orientation relative to the plate are assured to be fixed from one test to another.