Determining the ballistic threshold velocity for a composite structure using multiple failure models

Patent metadata

Field	Value
Publication number	US-10691848-B2
Application number	US-201815898984-A
Country	US
Kind code	B2
Filing date	Feb 19, 2018
Priority date	Feb 19, 2018
Publication date	Jun 23, 2020
Grant date	Jun 23, 2020

Abstract

A composite structure, such as a laminated composite panel, for example, comprises one or more layers or “plies” embedded in a matrix material or otherwise fixed together in an arrangement, commonly referred to as a “stack up.” Each material in the structure has a corresponding material failure model (MFM) defining the physical characteristics of that material. A ballistic threshold velocity computing device obtains the MFMs for each material in the composite structure, generates a predicted ballistic velocity threshold velocity for each MFM, and then generates a parametric model to compute a composite ballistic velocity threshold velocity for the composite structure.

First claim

What is claimed is:

1. A computing device comprising:
a communication interface circuit configured to communicate data with one or more devices over a communications network; and
one or more processing circuits operatively connected to the communication interface circuit and configured to:
generate a parametric model configured to aggregate predicted ballistic threshold velocities of a plurality of material failure models (MFMs) associated with a composite structure, wherein each predicted ballistic threshold velocity in the parametric model has a corresponding weighting coefficient to be applied to the predicted ballistic threshold velocity;
determine a value for each weighting coefficient in the parametric model;
generate a composite ballistic threshold velocity for the composite structure from the parametric model;
generate a structural design for the composite structure according to the composite ballistic threshold velocity; and
create the composite structure according to the structural design generated for the composite structure.

2. The computing device of claim 1 wherein each MFM comprises data defining one or both of a characteristic and a physical property of materials comprising the composite structure.

3. The computing device of claim 2 wherein the one or more processing circuits are further configured to generate the predicted ballistic threshold velocity for each MFM according to a selected finite element solving algorithm.

4. The computing device of claim 3 wherein the finite element solving algorithm used to generate the predicted ballistic threshold velocity for a first MFM is different than the finite element solving algorithm used to generate the predicted ballistic threshold velocity for a second MFM.

5. The computing device of claim 3 wherein the one or more processing circuits are further configured to generate at least one predicted ballistic threshold velocity using a stress-based failure analysis of the composite structure.

6. The computing device of claim 3 wherein the one or more processing circuits are further configured to generate at least one predicted ballistic threshold velocity using a fracture-based failure analysis of the composite structure.

7. The computing device of claim 3 wherein the one or more processing circuits are further configured to generate at least one predicted ballistic threshold velocity using a continuum damage failure analysis of the composite structure.

8. The computing device of claim 1 wherein to determine a value for each weighting coefficient, the one or more processing circuits are further configured to:
fit the parametric model to empirical test data for the composite structure responsive to determining that the empirical test data is accessible; and
obtain weighting coefficients from a previously generated parametric model responsive to determining that the empirical test data is not accessible.

9. The computing device of claim 1 wherein the one or more processing circuits are further configured to determine whether the composite ballistic threshold velocity is within a predetermined range of a reference ballistic threshold velocity.

10. A method of determining a ballistic threshold velocity for a composite structure, the method comprising:
generating a parametric model configured to aggregate predicted ballistic threshold velocities of a plurality of material failure models (MFMs) associated with the composite structure, wherein each predicted ballistic threshold velocity in the parametric model has a corresponding weighting coefficient to be applied to the predicted ballistic threshold velocity;
determining a value for each weighting coefficient in the parametric model;
generating a composite ballistic threshold velocity for the composite structure from the parametric model;
generating a structural design for the composite structure according to the composite ballistic threshold velocity; and
creating the composite structure according to the structural design generated for the composite structure.

11. The method of claim 10 further comprising generating the predicted ballistic threshold velocity for each MFM using a corresponding different finite element analysis solving algorithm.

12. The method of claim 11 wherein generating the predicted ballistic threshold velocity for each MFM comprises generating at least one predicted ballistic threshold velocity using a stress-based failure analysis of the composite structure.

13. The method of claim 11 wherein generating the predicted ballistic threshold velocity for each MFM comprises generating at least one predicted ballistic threshold velocity using a fracture-based failure analysis of the composite structure.

14. The method of claim 11 wherein generating the predicted ballistic threshold velocity for each MFM comprises generating at least one predicted ballistic threshold velocity using a continuum damage failure analysis of the composite structure.

15. The method of claim 10 wherein determining a value for each weighting coefficient in the parametric model comprises fitting the parametric model to empirical test data for the composite structure responsive to determining that the empirical test data is accessible.

16. The method of claim 15 wherein determining a value for each weighting coefficient in the parametric model comprises obtaining weighting coefficients from a previously generated parametric model responsive to determining that the empirical test data is not accessible.

17. The method of claim 10 further comprising determining whether the composite ballistic threshold velocity is within a predetermined range of a reference ballistic threshold velocity.

18. The method of claim 10 wherein the composite structure comprises part of a vehicle.

19. The method of claim 10 wherein the composite structure comprises part of a protective article of clothing worn by a user.

20. A non-transitory computer-readable medium storing a computer program product configured to control a programmable computing device, the computer program product comprising software instructions that, when executed by processing circuitry of the programmable computing device, cause the processing circuitry to:
generate a parametric model configured to aggregate predicted ballistic threshold velocities of a plurality of material failure models (MFMs) associated with a composite structure, wherein each predicted ballistic threshold velocity has a corresponding weighting coefficient to be applied to the predicted ballistic threshold velocity;
fit the parametric model to empirical test data to determine a value for each weighting coefficient in the parametric model;
generate a predicted composite ballistic threshold velocity for the composite structure from the parametric model; and
generate a structural design for the composite structure according to the composite ballistic threshold velocity; and
create the composite structure according to the structural design generated for the composite structure.

Assignees

• Boeing Co

Inventors

• Hunziker Kenneth Joseph
• Iqbal Jaffar Sher
• Pang Jenna Kristin
• Rassaian Mostafa

Classifications

• G06F30/20 Primary

  Design optimisation, verification or simulation (optimisation, verification or simulation of circuit designs G06F30/30) · CPC title

• G06F7/544

  for evaluating functions by calculation {(G06F7/4824 takes precedence)} · CPC title

• G06F2113/26

  Composites · CPC title

• F41H5/00

  Armour; Armour plates (processes for manufacturing or treating B21, C21, {heat treatment C21D9/42; wall or panel structure for safes E05G1/024}) · CPC title

• G06F30/17

  Mechanical parametric or variational design · CPC title