Understanding Material until Failure

The me­chan­i­cal de­scrip­tion of con­tin­u­ous fiber-re­in­forced ther­mo­plas­tic com­pos­ites is chal­leng­ing. On the one hand, the me­chan­i­cal­ly non-lin­ear, or­thotrop­ic ma­te­ri­al be­hav­ior re­quires the char­ac­ter­i­za­tion of a to­tal of five ma­te­ri­al func­tions to ful­ly de­scribe the stress-strain be­hav­ior. On the oth­er hand, the fail­ure be­hav­ior is strong­ly de­pen­dent on the re­spec­tive stress state and the in­ter­ac­tion of in­di­vid­u­al stress com­po­nents, which makes mod­el­ing even more dif­fi­cult.

To fully exploit the immense potential of these materials in practice, we pursue the following approach:

Scanning electron microscope image of a carbon fiber reinforced polyamide 6

Experimental Characterization

The ex­act char­ac­ter­i­za­tion of the me­chan­i­cal ma­te­ri­al be­hav­ior is cru­cial for the ef­fi­cient com­po­nent de­sign of fiber-re­in­forced plas­tic com­pos­ites. The se­lec­tion and ap­pli­ca­tion of suit­able ex­per­i­men­tal meth­ods for de­ter­min­ing the ma­te­ri­al char­ac­ter­is­tics is of par­tic­u­lar im­por­tance. In con­trast to metal­lic ma­te­ri­als such as steel or alu­minum, for which two char­ac­ter­is­tic val­ues (mod­u­lus of elas­tic­i­ty and trans­verse con­trac­tion co­ef­fi­cien­t) are usu­al­ly suf­fi­cien­t, a to­tal of four char­ac­ter­is­tic val­ues must be de­ter­mined for fiber-plas­tic com­pos­ites in the plane stress state and even five in the gen­er­al stress state. This re­quires the use of mul­ti-ax­is test­ing tech­niques in com­bi­na­tion with pre­cise mea­sure­ment meth­od­s, such as op­ti­cal strain mea­sure­men­t.

We im­ple­ment pre­cise­ly this ap­proach for our ma­te­ri­als and thus cre­ate a ba­sis for sys­tem­at­i­cal­ly ex­ploit­ing their full me­chan­i­cal po­ten­tial in the ap­pli­ca­tion.

Biaxial test specimen for testing fiber-reinforced composites
Microscopy of a fiber-reinforced composite
Failure of a fiber-reinforced composite under compression
Failure of a fiber-reinforced composite under shear

Material Modeling Based on Our Own Database

Frac­ture Curve of Car­bon-Fiber Re­in­forced Polyamide 6 (CF­PA6) in In-Plane Stress

Fracture curve of carbon fiber reinforced polyamide-6

The de­ter­mined ma­te­ri­al char­ac­ter­is­tics must be made us­able in prac­tice for en­gi­neers and com­po­nent de­sign­er­s. A par­tic­u­lar chal­lenge lies in the de­scrip­tion of the fail­ure mech­a­nism­s, as fiber-re­in­forced plas­tics can ex­hib­it dif­fer­ent fail­ure modes re­sult­ing from stress in­ter­ac­tion.

To this end, we have de­vel­oped our own ma­te­ri­al mod­el that en­ables a non-lin­ear de­scrip­tion of con­tin­u­ous fiber-re­in­forced plas­tics and in­te­grates a suit­able fail­ure mod­el. This gives us a sim­ple and ef­fec­tive ap­proach to de­sign­ing high­ly stressed com­po­nents based on our ma­te­ri­al­s.

Our mod­el is based on the re­sults of sev­er­al years of re­search by the Leib­niz-In­sti­tute for Com­pos­ite Ma­te­ri­als (leib­niz-ivw.de). In close co­op­er­a­tion with the in­sti­tute, we con­tin­u­ous­ly adapt the mod­el­ing to our new ma­te­ri­al­s.

Composite Specific Component Design

Our ma­te­ri­als have enor­mous po­ten­tial-pro­vid­ed they are used in a tar­get­ed and suit­able man­ner. Due to their di­rec­tion-de­pen­dent me­chan­i­cal be­hav­ior, com­po­nents made from com­pos­ites re­quire spe­cif­ic de­sign prin­ci­ples. Ar­eas where loads are ap­plied and zones where sta­bil­i­ty is at risk are par­tic­u­lar­ly crit­i­cal. Tar­get­ed de­sign ad­just­ments can achieve an eco­nom­i­cal, func­tion­al and ma­te­ri­al-spe­cif­ic de­sign.

Sim­ply sub­sti­tut­ing con­ven­tion­al met­al com­po­nents with com­pos­ite parts does not usu­al­ly lead to the de­sired re­sult­s.

As de­sign­er and pro­duc­er of these ma­te­ri­al­s, we have in-depth ex­per­tise and sup­port you in ex­ploit­ing their full po­ten­tial for your ap­pli­ca­tion in a tar­get-ori­ent­ed way-on re­quest al­so through FEA-sup­port­ed de­sign and anal­y­sis. For this pur­pose, we use our own ma­te­ri­al mod­el, spe­cial­ly de­vel­oped for the non-lin­ear de­scrip­tion and fail­ure be­hav­ior of our fiber ther­mo­plas­tic com­pos­ites.

Manufacturing drawing of a component
Gear made of fiber-reinforced composites
Concepts for load introduction in fibre-reinforced composites
Triaxiality of the material stress of a fibre-reinforced composite under transverse pressure

USE OF COOKIES