There are many methods to take a force vector in one direction as an input and split it into a force in multiple directions, however, most of the mechanisms that do so either have many parts which can make them difficult to manufacture (for example, but without limitation, Hoberman Linkages), the mechanisms rely on rotational components which make implementation unintuitive, they do not provide precise movements, or they do not provide an even and linear splitting of the input force between the output directions.
The majority of these force splitting mechanisms are not planar, as the input force is perpendicular to the output forces, which can limit the miniaturization of the mechanisms and limit the space into which the mechanisms can fit, particularly with regard to converting a uni-axial test frame into a bi-axial and/or multi-axial test frame.
Force splitting can be more easily imagined as a symmetric movement of the end effectors (i.e. grips, probes), so when one end effector is moved, the other end effectors move in tandem, and vice versa, so that the motion of all of the end effectors are constrained to each other. It is the constrained motion that splits the applied force.
A force splitting mechanism can be actuated from one or multiple directions by any force generating entity, whether it is by, but without limitation, human hand, beast of burden, simple machine, falling weight, electric motor, fluid pressure, or combustion engine. Force splitting mechanisms have applications in a wide variety of fields, from mechanical material property test fixtures, to robotic grips, expandable structures and antenna, expanding sails, tooling apparatuses (e.g. framing jigs), apertures, valves, and furniture (e.g. expanding tables), and can be created on vastly different scales from the very small, as in microelectrical mechanical systems (MEMS), to the very large, as in expandable space structures (solar arrays, antennas, and solar sails).
The present invention is directed to a mechanical material property test fixture for testing a material that includes a plurality of beams disposed on one geometrical plane, each beam having substantially equal angles between adjacent beams; a plurality of linear bearings, each linear bearing disposed on a corresponding beam, the linear bearings attachable to the material; a plurality of hinged linkage bars, each linkage bar communicating with two adjacent linear bearings such that the linear bearings can freely slide along the corresponding beam, the linkage bars are substantially the same length such that a symmetric multi-axial movement in the linear bearings is created, and allows for equal force to be applied to the material; and, an apparatus that applies force on the plurality of linear bearings such that the material being tested has a uniform force applied on it by the fixture.
It is a feature of the present invention to provide a mechanical material property test fixture for testing a material that takes an input force and splits it into multiple components, so that the force is applied along the direction of the input force and some other direction (or directions).
It is a feature of the present invention to provide a mechanical material property test fixture for testing a material that can be used as a bi-axial material mechanical property test fixture either in compression or in tension.
These and other features, aspects, and advantages of the present invention will become better understood with reference to the following description and appended claims, and accompanying drawings wherein:
The preferred embodiments of the present invention are illustrated by way of example below and in
In the description of the present invention, the invention will be discussed in a military aircraft environment; however, this invention can be utilized for any type of application that requires use of a test fixture.
The test fixture 10 is a combination of a variable geometry mechanism (made up of linear bearings 200 and hinged linkage bars 300) that can slide freely on the beams 100 of a fixed geometry frame in a linear fashion. In the preferred embodiment, as shown in
The mechanism of this invention is coupled with grips for holding a material or structure to create a material test fixture. When the mechanism is actuated, the grips pull on the test article along at least two axes. This is particularly useful for testing tensile properties of fabrics, coated fabrics, leather, rubber, and other soft materials, which are often used in inflatable and load bearing applications that produce a bi- or multi-axial strain state in the material. The grips may be replaced with probes to apply compression to a test article, which is useful for cylindrical test articles.
Materials react differently depending on the rate at which a force is applied, so a quasi-static force deforms (or yields) a material in a different manner than a dynamic (i.e. high strain rate) force. For many polymers and metals, a dynamic force will be more likely to cause brittle failure as opposed to ductile yielding. In the preferred embodiment, this bi-axial test fixture applies a force at a high strain rate through the use of a weight that drops and jerks the mechanism apart (generally shown in
When introducing elements of the present invention or the preferred embodiment(s) thereof, the articles “a,” “an,” “the,” and “said” are intended to mean there are one or more of the elements. The terms “comprising,” “including,” and “having” are intended to be inclusive and mean that there may be additional elements other than the listed elements.
Although the present invention has been described in considerable detail with reference to certain preferred embodiments thereof, other embodiments are possible. Therefore, the spirit and scope of the appended claims should not be limited to the description of the preferred embodiment(s) contained herein.
The invention described herein may be manufactured and used by or for the Government of the United States of America for governmental purposes without payment of any royalties thereon or therefor.