T.O. 33B-1-15-78maximum flexure in the layer being tested, is chosen for the inspection. A typical fixed frequency is 25 kHz. The lowfrequencies eliminate the need for liquid couplant between the transducer and the test part. On some instruments, avariable time gate is used to select the part of the received pulse that has the greatest change in amplitude when theprobe is scanned from a bonded area to an unbonded area. The amplitude will be larger over the unbond versus abonded area because the motion of the layer is restricted over a bonded area and energy is lost into the second layer.The pitch/catch modes work on composite delaminations, skin-to-core unbonds, metal-to-metal unbonds and skin-to-core disbonds. The method tends to lose its effectiveness if the material thickness between the probe and thedisbond/delamination exceeds 0.08 inch of aluminum or 0.30 inch of nonmetallic composite. In addition, theminimum dimension of a detectectable flaw is greater than or equal to the probe tip spacing.5.4.6.3 Pitch/CatchSweptFrequencyMethod.Instead of a single frequency, each pulse contains a range of frequencies, for example, 20 to 40 kHz or 30 to 50 kHz.Ultrasonic plate or Lamb waves are generated in the part. These waves are attenuated by coupling into the second layerin well bonded joints. In an unbond region the waves travel with very little attenuation or leakage into the second layerand produce larger indications. Both the swept and impulse techniques will find similar types of defects. However,with the swept technique, calibration interpretation of the signals may be easier because both the amplitude and phasesignals are simultaneously displayed in the form of circular patterns on one X-Y active screen. Figure 5-78 showsinstrument displays corresponding to three situations detected with the Pitch/Catch Swept-Frequency Method.Figure 5-78. Pitch/Catch Swept-Frequency Signal Patterns.5.4.6.4 MechanicalImpedanceAnalysis(MIA)Method.The driver portion of a single-tip dual-element probe generates low-frequency sound waves that transfer to mechanicalmovements in the test material. The stiffness and mass of the material are measured by the receiving sensor anddisplayed in terms of both phase and amplitude values. The receiver element at the bottom of the probe has its loadingaffected by the part stiffness which changes from very high over bonded regions to low over unbonded regions. Sincethe measurements are a comparison of stiffness, results are better on stiff structures. Flexible composites would nothave much change in stiffness from bonded to unbonded areas. The MIA mode does not require couplant and has asmall contact area so it can be used on irregular or curved surfaces. The MIA technique seems most suitable fordetecting damage associated with honeycomb core such as skin-to-core disbonds severely corroded aluminum core, andbuckled or crushed core. However, disbonds and delaminations also can be detected with this method. Figure 5-79shows typical positions of indications produced with the MIA method. During an inspection only the "flying" spotwould be present on the display. The gate box can be positioned anywhere on the display; the appropriate position isdetermined during calibration. Figure 5-80 illustrates an instrument that is capable of operating in all four modes(resonance, pitch/catch impulse, pitch/catch swept-frequency and mechanical impedance). The alignment problem isnormally solved be gridding off the inspection area and keeping the inspection area down to a manageable size. If thearea is very large special fixtures are normally manufactured to hold both transducers and keep them aligned.
Integrated Publishing, Inc. - A (SDVOSB) Service Disabled Veteran Owned Small Business