Method of determining dynamic strains in composite structures

• US 3,934,452 A
• Filed: 12/02/1974
• Issued: 01/27/1976
• Est. Priority Date: 12/02/1974
• Status: Expired due to Term

• Current Assignee: Allied Chemical Corporation (Honeywell International Inc.)
• Original Assignee: Allied Chemical Corporation (Honeywell International Inc.)
• Inventors: Kwon, Young Doo, Sharma, Raj Kumar, Prevorsek, Dusan Cyril
• Primary Examiner(s): Gill, James J.
• Assistant Examiner(s): Ciarlante, Anthony V.
• Application Number:
  US05/528,610
• Time in Patent Office: 421 Days
• Field of Search: 73/15.6, 73/146, 73/92, 73/99
• US Class Current: 374/47
• CPC Class Codes: G01M 17/02 Tyres
• CPC Class Codes: G01N 2203/0094 Visco-elasticity
• CPC Class Codes: G01N 2203/0222 Temperature
• CPC Class Codes: G01N 3/32 by applying repeated or pulsating forces

Abstract

A method for determining strain amplitudes in each component, during cyclic straining of a 2-component structure in which at least one component shows non-linear viscoelastic behavior. The heat generation rates of each component are determined experimentally, at various temperatures, as functions of the experimentally imposed strain amplitudes. These functions are used to solve, by computer, a heat balance equation involving temperature values through the structure. To find pairs of strain amplitudes which produce observed temperatures, the value of strain amplitude entering into the equations for one component is varied (for each value of a set of strain amplitudes of the other component) until the temperature at a selected point of the structure, thus calculated, matches the temperature determined experimentally; and likewise for a second selected point. The desired pair of strain amplitudes is thus identified as being a pair which produces a match of calculated vs. measured temperature at both selected points.

Claims

1. Method of determining the strain amplitudes of the two principal components of a structure composed principally of two viscoelastic materials A and B at least one of which shows non-linear viscoelastic behavior under strain, due to cyclic straining of the structure with heat generation, comprising the following steps:

1. Experimentally determining rates of heat generation, Q, per unit volume of each material, due to cyclic straining, for each material at a series of temperatures by hysteresis measurements at various strain amplitudes (ε

_A) for material (A) and (ε

_B) for material (B);

2. calculating by computer for each pair of a set of pairs of strain amplitudes (ε

_A, ε

_B), the steady-state temperatures at two positions (P) and (P'"'"') in the structure, using finite difference approximations at successive positions through the structure, to solve the heat balance equation appropriate for the particular structure, having as its simplest form;

space="preserve" listing-type="equation">σ

C.sub.p ∂

T/∂

t = K ∂

.sup.2 T/∂

q.sup.2 + Q

where ∂

/∂

t indicates partial differentiation by time;

∂

/∂

q indicates partial differentiation by the space coordinate;

σ

= density

C_p = heat capacity per unit volume

T = temperature

K = coefficient of thermal conductivity

Q = heat generation rate per unit volume, at the temperature calculated for each volume element dV and at the value of strain amplitude (ε

_A) or (ε

_B) imposed upon the material (A) or (B);

3. Method of claim 1 wherein said structure is the side wall of a vehicular pneumatic tire composed principally of material showing linear viscoelastic behavior under strain, and of reinforcing material.

4. Method of determining the strain amplitudes for each of the two constituent materials of a structure in accordance with claim 1, wherein more than one pair of strain amplitudes (ε

_A, ε

_B) corresponds to an intersection of the curves determined at step (5) of claim 1, which method comprises determining such curves for two such structures having a difference in heat generation rates of one of their components but being otherwise closely similar; and

observing the intersection which applies to both structures.

5. Method of claim 3 wherein said structure is the sidewall of a vehicular pneumatic tire composed of a reinforced zone of plies of material showing non-viscoelastic behavior embedded in rubber and separated by interply rubber layers, the whole being between an inner and an outer layer of rubber.

6. Method of claim 1 wherein said structure is the shoulder region of a vehicular pneumatic tire composed principally of material showing linear viscoelastic behavior under strain, and of reinforcing material.

2. representing the calculated set of temperatures at (P) as a function of strain amplitudes, ε

, of one of the materials for each value of the other ε

, and likewise representing the calculated set of temperatures at (P'"'"');

4. experimentally determining steady-state temperatures TP and T_P '"'"' at positions (P) and (P'"'"') of the structure as it undergoes the specified straining cycle;

5. Representing the curve of ε

_A vs. ε

_B at the temperature T_P and an likewise the ε

_A vs. ε

_B curve at the temperature T_P '"'"' using the data revealed by step (3) above;

6. Observing the intersections of the two curves revealed by step (5) above, thereby determining a pair of strain amplitudes ( ε

_A, ε

_B) imposed by the cyclic straining, which pair of amplitudes will give rise to the experimentally determined temperatures T_P and T_P '"'"'.