SOLID-LIQUID COMPOSITE STRUCTURES

• US 20170320559A1
• Filed: 11/19/2015
• Published: 11/09/2017
• Est. Priority Date: 11/20/2014
• Status: Active Grant

• Current Assignee: TECHNION RESEARCH AND DEVELOPMENT FOUNDATION, LTD.
• Original Assignee: TECHNION RESEARCH AND DEVELOPMENT FOUNDATION, LTD.
• Inventors: GAT, Amir, ELBAZ, Shai, MATIA, Yoav
• Granted Patent: US 10,450,051 B2
• Time in Patent Office: Days
• CPC Class Codes: B29L 2031/3085 Wings
• CPC Class Codes: B64C 1/34 comprising inflatable structural components
• CPC Class Codes: B64C 3/185 Spars
• CPC Class Codes: B64C 3/38 Adjustment of complete wings or parts thereof

Abstract

A pressurized, fluid-filled channel network embedded in an elastic structure, asymmetrically to the neutral plane, is used to create a deformation field within the structure by the pressurization of the embedded fluidic network, which can be applied in accordance with external forces acting on the structure. The deformation of the structure resulting from the liquid pressure and geometry of the network is related to a continuous deformation-field function. This enables the design of networks creating steady arbitrary deformation fields as well as to eliminate deformation created by external time varying forces, thus increasing the effective rigidity of the beam. By including the effects of the deformation created by the channel network on the beam inertia, the response of the beam to oscillating forces can be modified, enabling the design of channel networks which create pre-defined oscillating deformation patterns in response to external oscillating forces.

Claims

1. A structural element comprising:

a base material having a predetermined stiffness; and

a set of channels configured to be filled with fluid and embedded within said base material such that at least some of said channels are spatially asymmetric relative to the neutral plane of said structural element,

wherein at least the positions of said set of channels within said base material, the dimensions of said set of channels and the pressure of the fluid within said channels are designated such that a deformation field generated by said pressure applied to said fluid within said set of channels is adapted to offset deformations caused to the element by the application of externally applied forces.

2. The structural element of claim 1 wherein at least some of said channels are located in a position offset from the midline of said element.

3. The structural element of claim 1 wherein the cross sectional geometric shapes of at least some of said set of channels are selected in determining said deformation field.

4. The structural element of claim 1 wherein said deformation field generated by said pressure applied to said fluid within said set of channels is determined by integration of the products of the channel density at points along said structural element with the geometric deflection generated by said pressure applied to said fluid in a single channel at said points along said structural element.

5. The structural element of claim 4 wherein said geometric deflection generated by said pressure applied to said fluid in a single channel at a point along said structural element, is determined as a function of at least:

(i) the level of the pressure within said channel,

(ii) Young'"'"'s modulus of said material of said structural element,

(iii) Poisson'"'"'s ratio of said material of said structural element,

(iv) the offset of said channel from the centerline of said structural element, and

(v) the size of the channel relative to the dimension of said structural element in the direction of said deflection.

7. The structural element of claim 1 wherein said level of pressure is generated by a signal derived from the level of said externally applied force.

8. The structural element of claim 1 wherein said level of pressure is generated by direct application of said externally applied force to a piston generating said pressure.

9. The structural element of claim 1, wherein said pressure is changed dynamically such that the vibrational response of said element to time dependent applied forces is reduced.

10. The structural element of claim 1, wherein the effective stiffness of said structural element is higher than said predetermined stiffness of said base material when said pressure is applied to said fluid within said channels.

12. The structural element of claim 1, wherein said structural element is part of an aircraft wing, and said externally applied forces are aerodynamic forces operating on said wing.

13. A system for reducing the effect of deformation of a structural element by external forces, said system comprising:

a structural element constructed according to claim 1;

a sensing element actuated by said external forces; and

a compressor generating the pressure for application to said fluid within said channels according to the output of said sensing element.

14. The system of claim 13 wherein said sensing element is a mechanical element actuated by said external forces and connected to a piston compressing said fluid within said channels.

27. The structural element of claim 1 wherein said fluid contained in said set of channels has a viscosity sufficiently high that the pressure within said set of channels varies spatially along said set of channels.

6. (canceled)

11. (canceled)

15. (canceled)

16. (canceled)

17. A method of increasing the effective stiffness of a structural element, comprising:

providing a base material constituting the basis of said structural element, said base material having embedded therein a set of channels containing a fluid, at least some of said channels being spatially asymmetric relative to the neutral plane of said structural element; and

applying pressure to said fluid in accordance with the configuration of an external force field incident on said structural element,

wherein at least the positions of said set of channels within said base material, the dimensions of said set of channels and the pressure of the fluid within said set of channels are configured so that a deformation field generated by said pressure is adapted to offset deformations that would be caused to said structural element by said externally applied force field, such that the effective stiffness of said structural element is increased.

18. The method of claim 17 wherein at least some of said channels are located in a position offset from the midline of said element.

19. The method of claim 17 wherein the cross sectional geometric shapes of at least some of said set of channels are suitably configured in determining said deformation field.

20. The method of claim 17 wherein said deformation field generated by said pressure applied to said fluid within said set of channels is determined by integration of the products of the channel density at points along said structural element with the geometric deflection generated by said pressure applied to said fluid in a single channel at said points along said structural element.

21. The method of claim 20 wherein said geometric deflection generated by said pressure applied to said fluid in a single channel at a point along said structural element, is determined as a function of at least:

(i) the level of the pressure within said channel,

(ii) Young'"'"'s modulus of said material of said structural element,

(iii) Poisson'"'"'s ratio of said material of said structural element,

(iv) the offset of said channel from the centerline of said structural element, and

(v) the size of the channel relative to the dimension of said structural element in the direction of said deflection.

23. The method of claim 17 wherein the level of said pressure is generated by a signal derived from the level of said externally applied force field.

24. The method of claim 17 wherein the level of said pressure is generated by direct application of said externally applied force field to a piston generating said pressure.

25. The method of claim 17, further comprising changing said pressure dynamically such that the vibrational response of said element to time dependent applied forces is reduced.

28. The method of claim 17, wherein said fluid contained in said set of channels has a viscosity sufficiently high that the pressure within said set of channels varies spatially along said set of channels.

22. (canceled)

26. (canceled)