two embodiments of the present invention are comprised of a rectangular solid composite 4 contacting and sandwiched between two or more plates , namely a planar first electrode 6 and a planar second electrode 7 , as shown in fig3 and a planar first electrode 6 and a planar second electrode 7 and two planar pressure plates 18 a , 18 b , as shown in fig4 . a pressure switch 11 is comprised of a composite 4 and electrodes 6 , 7 as shown in fig3 or a composite 4 and pressure plates 18 a , 18 b as shown in fig4 . the composite 4 functionally completes the current path between first electrode 6 and second electrode 7 during acceptable operating conditions and interrupts current flow when a fault condition occurs . the composite 4 is either conductive or resistive based on the pressure state within the composite 4 . for example , the composite 4 may be conductive above and nonconductive below a threshold pressure . alternately , the resistivity of the composite 4 may vary with pressure over a range of resistance values . a typical composite 4 is a pressure dependent conductive material , for example a piezoresistive formulation , comprised of a nonconductive matrix 3 and a conductive filler 2 , as schematically shown in fig1 . preferred mixtures have a volume fraction below the percolation threshold wherein conductive filler 2 is randomly dispersed within the nonconductive matrix 3 . during compression , the nonconductive matrix 3 between conductive filler 2 particles is dimensional reduced thereby crossing the percolation threshold . the nonconductive matrix 3 is a resistive , yet compressible material including but not limited to polymers and elastomers . specific examples include polyethylene , polystyrene , polyvinyldifluoride , polyimide , epoxy , polytetrafluorethylene , silicon rubber , polyvinylchloride , and combinations thereof preferred embodiments are comprised of the elastomer rtv r3145 manufactured by the dow corning company . the conductive filler 2 is an electrically conductive material including but not limited to metals , metal - based oxides , nitrides , carbides , and borides , and carbon black . preferred fillers resist deformation under compressive loads and have a melt temperature sufficiently above the thermal conditions generated during current interrupt . specific metal examples include aluminum , gold , silver , nickel , copper , platinum , tungsten , tantalum , iron , molybdenum , hafnium , combinations and alloys thereof . other example fillers include sr ( fe , mo ) o3 , ( la , ca ) mno3 , ba ( pb , bi ) o3 , vanadium oxide , antimony doped tin oxide , iron oxide , titanium diboride , titanium carbide , titanium nitride , tungsten carbide , and zirconium diboride . [ 0059 ] fig2 describes a fabrication method for various composites 4 . generally , composites 4 are prepared from high - purity feedstock , mixed , formed into a solid , and suffused with oil . one or more plates are adhered to the composite 4 . feedstocks include both powders and liquids . conductive filler 2 feedstock is typically composed of a fine , uniform powder , one example being 325 mesh titanium carbide . nonconductive matrix 3 feedstock may include either a fine , uniform powder or a liquid with sufficiently low - viscosity to achieve adequate dispersion of powder . powder - based formulations are mechanically mixed and compression molded using conventional methods . polytetrafluorethylene formulations may require sintering within an oven to achieve a structurally durable solid . powder - liquid formulations , one example being titanium carbide and a silicone - based elastomer , are vulcanized and hardened within a die under low uniaxial loading at room temperature . the solid composite 4 is placed within a liquid bath thereby allowing infiltration of the additive into the solid . additives are typically inorganic oils , preferably silicone - based . the composite 4 is exposed to the additive bath to insure complete suffusion of the solid , whereby exposure time is determined by dimensions and composition of the composite 4 . for example , a 0 . 125 - inch by 0 . 200 - inch by 0 . 940 - inch composite 4 composed of titanium carbide having a volume fraction of 66 percent and rtv r3145 having a volume fraction of 34 percent was suffused over a 48 hour period . conductive or nonconductive plates are adhered to the composite 4 either before or after suffusion . if prior to suffusion , plates are placed within the die along with the liquid state composite 4 . for example , a silicone elastomer composite 4 is adequately bonded to two 0 . 020 - inch thick brass plates by curing at room temperature typically between 3 to 24 hours or at an elevated temperature between 60 to 120 degrees celcius for 2 to 10 hours . if after suffusion , silicone adhesive is applied between plate and composite 4 and thereafter mechanically pressed to allow for proper bond formation . a porous , nonconductive matrix 3 improves compression and cooling characteristics of the composite 4 without degrading electrical properties . a porous structure is formed by mechanical methods , one example including drilling , after fabrication of the solid composite 4 . another method includes the introduction of pores during mixing of a powder - based conductive filler 2 with a liquid - based nonconductive matrix 3 . an additional method includes the introduction of pores during compression forming the composite 4 . also , pores are formed by heating the composite 4 within an oven resulting in localized heating or phase transitions that result in void formation and growth . furthermore , highly compressible microspheres composed of a low - density , high - temperature foam may be introduced during mixing . pores are either randomly oriented or arranged in a repeating pattern . pore shapes include but are not limited to spheres , cylinders , and various irregular shapes . a single pore may completely traverse the thickness of a composite 4 . [ 0064 ] fig8 - 9 show an embodiment wherein a plurality of holes 40 traverse the cross section of a pressure switch 11 . fig1 shows an embodiment wherein holes traverse the composite 4 within the pressure switch 11 . [ 0065 ] fig1 shows a further embodiment wherein holes 40 are filled with a temperature sensitive material 41 , examples including rods or springs composed of a shape memory alloy . functionally , the temperature sensitive material 41 is typically a rubbery material below , see fig1 a , and hard above , see fig1 b , a phase transition temperature . more importantly , the temperature sensitive material 41 produces a large force above a transition temperature designed within the material as readily understood within the art . this force is sufficiently capable of moving the pressure plates 18 or electrodes 6 , 7 apart and interrupting current flow . the temperature sensitive material 41 is self restoring thereby facilitating current flow after the surrounding composite 4 has cooled . [ 0066 ] fig1 - 13 show two embodiments wherein at least two temperature sensitive actuators 51 apply a compressive force 22 onto a composite 4 thereby allowing current flow . in fig1 , current flows directly through the temperature sensitive actuators 51 a , 51 b , preferably a shape memory alloy . when a fault occurs the temperature sensitive actuators 51 a , 51 b are heated and contract thereby decompressing the composite 4 and interrupting current . the composite 4 is compressed as the temperature sensitive actuator 51 cools . in fig1 , current flows through the first electrode 6 and the second electrode 7 when temperature sensitive actuators 51 a , 51 b are heated by thermal elements 56 a , 56 b . thermal elements 56 a , 56 b are deactivated when a fault condition occurs thereby decreasing the length of the temperature sensitive actuators 51 a , 51 b and reactivated after the fault condition is corrected thereby increasing the length of the temperature sensitive actuators 51 a , 51 b causing compression of the composite 4 and current flow . [ 0067 ] fig5 - 6 show additional embodiments of the present invention comprised of four pressure switches 11 a , 11 b , 11 c , 11 d , a first electrode 6 , a second electrode 7 , two planar conductors 31 a , 31 b , four insulators 32 a , 32 b , 33 a , 33 b , a restoration element 30 , and a pair of actuators 19 a , 19 b . pressure switches 11 a , 11 b , 11 c , 11 d are composed of a pressure conduction composite 4 disposed between and adhered to two electrically conducting plates , as described above . a pair of pressure switches 11 are electrically aligned in a serial arrangement about a single electrode , either the first electrode 6 or the second electrode 7 . one electrically conducting plate from each pressure switch 11 directly contacts the electrode . two such pressure switch 11 and electrode arrangements are thereafter aligned parallel and disposed between , perpendicular to and contacting a pair of conductors 31 a , 31 b so that each pressure switch 11 in a serial arrangement contacts a separate conductor 31 . conductors 31 are composed of materials known within the art and should have sufficient strength to resist deformation when a mechanical load is applied . thereafter , an insulator 32 is placed in contact with and attached or fixed to each conductor 31 . a typical insulator 32 is a planar element composed of an electrically nonconducting material with sufficient strength to resist deformation when a mechanical load is applied . at least one restoration element 30 is disposed between and parallel to the serial arrangement of pressure switches 11 and electrodes 6 or 7 . the restoration element 30 is attached to separate electrically nonconductive insulators 33 a , 33 b . thereafter , insulators 33 a , 33 b are mechanically attached to , perpendicularly disposed and between the conductors 31 a , 31 b . insulators 33 a , 33 b electrically isolate the restoration element 30 from conductors 31 a , 31 b . the restoration element 30 decompresses the composite 4 within each pressure switch 11 , returning it to its original thickness , when the compressive mechanical load is removed from the insulators 32 a , 32 b . a restoration element 30 may be a mechanical spring or coil , a pneumatic device , or any similar device that provides both extension and contraction . in preferred embodiments , an actuator 19 contacts an insulator 32 . in one embodiment , at least one actuator 19 is attached or fixed to each insulator 32 opposite of said conductor 31 , as shown in fig5 . a pair of actively opposed yet equal actuators 19 a , 19 b apply a mechanical load by pushing onto electrically nonconductive insulators 32 a , 32 b to compress the composite 4 within each pressure switch 11 a , 11 b , 11 c , 11 d , as shown in fig5 b . in another embodiment , at least two actuators 19 a , 19 b are mechanically attached or fixed to a pair of insulators 32 a , 32 b , see fig6 . again , a pair of actively opposed yet equal actuators 19 a , 19 b apply a mechanical load by pulling on electrically nonconductive insulators 32 a , 32 b to compress the composite 4 within each pressure switch 11 a , 11 b , 11 c , 11 d , as shown in fig6 b . variations to the described embodiments also include at least two or more actively opposed actuators 19 mechanically compressing one or more current controllers 1 . fig7 describes a three - by - three arrangement of nine current controllers 1 , however not limited to this arrangement . in such embodiments , current controllers 1 are electrically connected parallel thereby providing a total power handling capability equal to the sum of the power handling of individual units . one or more actuators 19 may be employed to drive two or more current controllers 1 . for example , a single actuator 19 or two actively opposed yet equal actuators 19 may apply a mechanically compressive load onto the current controllers 1 so that all are simultaneously compressed and decompressed . alternatively , one or a pair of actuators 19 may apply a mechanically compressive load onto each individual current controller 1 . in this embodiment , it is possible to simultaneously drive all current controllers 1 or to selectively drive a number of units . the embodiments described above may also include a current measuring device electrically coupled before or after the current controller 1 . this device provides real - time sampling of current conditions which are thereafter communicated to the actuators 19 . such monitoring devices are known within the art . an actuator 19 is a rigid beam - like element composed of an active material capable of dimensional variations when electrically activated . for example , the actuator 19 may extend , contract , or extend and contract , as schematically represented by arrows in fig5 - 6 . extension of the actuator 19 increases the overall length of the actuator 19 . actuators 19 are composed of electrically activated devices including piezoelectric , piezoceramic , electrostrictive , and magnetostrictive materials . for example , piezoelectric and piezoceramic materials may be arranged in a planar stack along the actuator 19 . alternatively , an actuator 19 may be a commercially available high - speed piezo - controlled pneumatic element comprised of a pneumatic diaphragm with pilot operated high - bypass value . the description above indicates that a great degree of flexibility is offered in terms of the present invention . although embodiments have been described in considerable detail with reference to certain preferred versions thereof , other versions are possible . therefore , the spirit and scope of the appended claims should not be limited to the description of the preferred versions contained herein .