AC 43-7

Historical

Advisory circular · Ultrasonic Testing for Aircraft

Approved
September 24, 1974
Last reviewed
October 2, 2024
This change
Canceled by Memo signed by Steven Douglas (AFS-300); dated 12/20/2011.
Family
AC 43-7 · 1 version
14 CFR parts
1
Cited by
2 ADs

Guidance, not mandatory unless a rule or AD requires it. DRS record last changed November 22, 2025.

Show pages 1–2
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TABLE OF CONTENTS Page Chapter 1. INTRODUCTION

1. General

2. Use of Ultrasonics --

3. Limits on Application of Ultrasonics -

4. Ultrasonic Inspection for Corrosion Detection

5.-9. Reserved Chapter 2. TRANSDUCERS (SEARCH UNITS, PROBES, CRYSTALS)

10. General

11. Transducer Materials

12. Piezoelectric Effect

13. Transducer Type Search Units

14. Transducer Groups

15.-20. Reserved Chapter 3. WAVE PROPAGATION

21. Ultrasonic Waves

22. Longitudinal Waves

23. Shear Waves --

24. Surface (Rayleigh) Waves -

25. Plate (Lamb) Waves

26.-30. Reserved Chapter 4. ULTRASONIC VIBRATIONS

31. Testing Methods

32. Reflection of Ultrasonic Waves

33. Refraction and Mode Conversion of Ultrasonic Waves 10

34. Beam Divergence 10

35.-40. Reserved 10 Chapter 5. ULTRASONIC SYSTEMS

41. General 1ł

42. Pulsed 11

43. Reasonance 12

44.-50. Reserved 13 Chapter 6. PRESENTATION

51. Observing and Recording Response Patterns

52. Cathode-Ray Tube (CRT)

53. Scan Presentation 16

54. Indications 16

55.-60. Reserved 19 Chapter 7. RECORDERS

61. Types - 21

62. Deflection Modulation, Conventional Pen-Chart Recorders 21

63. Intensity Modulation, C-Scan Mehod of Facsimile Recording 21

64.-70. Reserved 21

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TABLE OF CONTENTS-Continued Page Chapter 8. ELECTRONIC GATING

71. Functions 23

72. Basic Operating Principles of Gates 23

73.-75. Reserved 24 Chapter 9. DELAY LINE

76. Description 25

77.-80. Reserved 25 Chapter 10. COUPLANT

81. General

82. Description

83.-85. Reserved 27 Chapter 11. ULTRASONIC REFERENCE BLOCKS

86. Introduction

87. Distance-Amplitude Comparison Blocks --.

88. Area-Amplitude Comparison Blocks (Alcoa Blocks)

89. I.I.W. Welding Blocks -

90. ASME Weld Reference Plate

91. Special Reference Standards

92.-95. Reserved 31 Chapter 12. TESTING METHODS

96. Description

97. Contact Testing

98. Immersion Testing

99. Immersed Scanning Technique

100. Water Column Technique (Bubbler, Squirter)

101. Wheel Search Unit

102. Ultrasonic Image Conver

103.-110. Reserved Chapter 13. INSPECTION OF INTEGRAL FUEL TANKS FOR CORRISON

111. General 39

112. Method 39

113. Equipment 39

114. Indications 39

115.-120. Reserved 39 Chapter 14. INSPECTION OF REPRESENTATIVE AIRCRAFT PARTS

121. General

122. Main and Nose Landing Gear Wheels --

123. Main Landing Gear Torsion Link -.

124. Main Landing Gear Torsion Link Lugs ---

125. Main Landing Gear Oleo Outer Cylinder -

126. Main Landing Gear Trunnion Support Structure

127. Nose Landing Gear Outer Cylinder --

128. Inboard and Outboard Nacelle Strut Front Spar Fittings

129. Nose Landing Gear Outer Cylinder

130.-135. Reserved

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LIST OF ILLUSTRATIONS Figure Page

1. Angle Beam Search Unit co co

2. Generation of Ultrasonic Vibration

3. Diagram of an Ultrasonic Search Unit -

4. Natural Quartz Crystal (X and Y Cut)

5. Common Transmitter-Receiver Search Unit .

6. Combined Transmitter-Receiver Search Unit

7. Separate Transmitter-Receiver Search Unit

8. Mechanical Analogy of Wave Propagation

9. Longitudinal Waves

10. Shear Waves _... 11. Transmitting A Wave at a Small Angle - 00 00 00 00 1

12. Surface Waves -.

13. Surface Wave Technique

14. Plate Waves -

15. Reflection of Ultrasound 9

16. Refraction of the Ultrasonic Beam 10

17. Generating Shear Waves 10

18. Generating Surface Waves - 10

19. Beam Divergence of Sound Waves in Steel - 10

20. Diagram of Longitudinal Sound Striking a Surface - 10

21. Block Diagram of Basic Pulse-Echo System - 11

22. Oscilloscope Display in Relationship to Flaw Detection 11

23. Through-Transmission Technique -- 12

24. Conditions of Ultrasonic Resonance in Metal Plate 12

25. Block Diagram of Resonance Thickness Measuring System 12

26. Radio-Frequency Trace and Video Trace - 15

27. Types of Marker Systems - 16

28. A-Scan Presentation 16

29. B-Scan Presentation 16

30. C-Scan Presentation 16

31. Immersion Crystal Focused on Test Block and Indications to be Expected 17

32. Immersion Crystal Focused on Block with Defect and Non-parallel Surface - 17

33. Immersion Crystal Focused on Shaft too Long for Back Reflecion of Return 17

34. Angle Beam Penetrating a Weld Bead -- 18

35. Angle Beam Penetrating a Weld Bead --. 18

36. Angle Beam Penetrating a Flat Plate -- 18

37. Results of a Rough Front and Back Surface ..

38. Evaluating Braze of Carbide Tip to Steel

39. Indication Received from Porous Material

40. Irregular Part

41. Various Recording Charts

42. Ultrasonic Recording of Brazed Honeycomb Panel

43. Controllable Gated Zone in Test Piece -.

44. Threshold Gate Circuit Diagram ..

45. Threshold Gate Wave Form -

46. Ultrasonic Delay Time

47. Couplant (Contact Testing)

48. Couplant (Immersion Testing)

49. Distance-Amplitude Comparison

50. Step Block -

51. Area Amplitude Comparison Blocks .

52. I.I.W. Weld Block --.

53. ASME Weld Reference Plate III

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LIST OF ILLUSTRATIONS-Continued Figure Page

54. Contact Angle-Beam Test into Hidden Weld Region of a Landing Gear Oleo Strut 33

55. Ultrasonic Inspection of a Wing Front Spar - 33

56. Ultrasonic Inspection of a Pylon Structural Member - 33

57. Principle of Ultrasonic Testing (Contact) -- 34

58. Principle of Ultrasonic Testing (Immersion) 34

59. Bubbler Angle-Beam Testing (Pipe) 34

60. Wheel Scanning Method 34

61. Immersed Angle-Beam Technique (Pipe or Tube) 34

62. Immersed Angle-Beam Technique (Plate or Sheet) 35

63. Immersed Through-Transmission Technique 35

64. Removing First Multiple of Interface Indication From Test Area 35

65. Focused Search Unit -- 35

66. Beam Collimator -- 35

67. Bubbler Scanning Method 36

68. Bubbler Angle-Beam Technique (Plate) 36

69. Wheel Search Unit in a Fixed Position -. 36

70. Wheel Search Unit over the Material 36

71. Schematic-Ultrasonic Image Converter System 37

72. Main and Nose Landing Gear Wheels 41

73. Main Landing Gear Torsion Link

74. Main Landing Gear Torsion Link Lugs -----

75. Main Landing Gear Oleo Outer Cyclinder ---

76. Main Landing Gear Trunnion Support Structure

77. Nose Landing Gear Outer Cylinder --

78. Inboard and Outboard Nacelle Strut Front Spar Fitting.

79. Nose Landing Gear Outer Cylinder ----

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Chapter 1. INTRODUCTION

1. GENERAL. Ultrasonic inspection of aircraft plays an important role from both a safety and economic aspect. In order to accomplish the prescribed ultrasonic inspection, only minor aircraft open-up for accessibility is usually required. For example, in the case of the aircraft engine, inspections are performed "on the wing" with the engine still installed in the aircraft. For the airframe, ultrasonics required a minimum of disassembly and removal of interfering equipment. Aircraft inspections with ultrasonics can be performed at the ramp" or "on the line" under circumstances entirely different from total disassembly. It is an extremely sensitive method of nondestructing testing. The limitations are few and when direct coupling (or contact) with the part being checked can be established, the resolving capabilities are excellent. However, interpretation by trained personnel is required.

2. USE OF ULTRASONICS. Ultrasonics employ electronically produced, high-frequency sound waves that will penetrate metals, liquids, composites, and other materials at speeds of several thousand feet per second. This technique can be used to:

d. Detect laps, seams, laminations, inclusions, cracks, corrosion, and other defects in installed

b. Locate porosity, cupping, and nonmetallic inclusions in bar stock.

c. Locate cracks, blow holes, insufficient penetration, lack of fusion, and other discontinuities in

d. Evaluate bond quality in brazed joints and honeycomb composites assemblies.

e. Inspect forgings such as turbine engine shafts, turbine engine discs, and landing gear structural members.

3. LIMITS ON APPLICATION OF ULTRASONIC TESTING. Among the factors which may limit the application of ultrasonic testing are:

a. Sensitivity. The ability of the instrument to detect the small amount of energy reflected from a discontinuity.

b. Resolution. The ability of the instrumentation to detect flaws lying close to the test surface or to separate and distinguish the indications from several defects occurring close together in the specimen.

c. Noise discrimination. The capacity of the instrumentation for differentiating between the signals from defects and the unwanted noise of either electrical or acoustics nature.

d. These factors are affected by others, such as frequency and pulse energy. For example, when frequency is increased, the sensitivity increases.

With the increase in sensitivity, smaller inhomogeneties within the material will become detectable.

This will increase the noise level, thus hindering signal discrimination. With an increase in pulse energy, material noise will increase and resolution

4. ULTRASONIC INSPECTION FOR CORROSION DETECTION. Although ultrasonic inspections have been employed by the aviation industry for several years, it was not until recently that ultrasonics have been used as a means of corrosion detection. Presently, this method of corrosion detection is still in the early stages and certainly not infallible; but it has been demonstrated that, within limitations, ultrasonics can provide a fairly reliable indication of corrosion attack. Highly trained personnel must conduct the examination if any useful information is to be derived from the indicating devices. This is compounded by the fact that the results obtained vary, depending on the model and make of equipment used, and on the techniques used by the individual performing the examination.

5.-9. RESERVED.

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Chapter 2. TRANSDUCERS (SEARCH UNITS, PROBES, CRYSTALS)

10. GENERAL. To understand how inaudible sound is used to reveal certain conditions which are not perceptible in the normal hearing range, it is first necessary to know how ultrasound is transmitted and received.

may be of any conducting material such as aluminum, silver, gold, or chromium. However, coatings are difficult to deposit on lithium sulphate crystals so thin metallic foils are often cemented to the crystal.

11. TRANSDUCER MATERIALS. Three transducer materials which can be used in the manufacture of ultrasonic search units are natural quartz crystals, lithium sulfate, and polarized crystalline ceramics.

a. Quartz. Principal advantages are: electrical and thermal stability, insolubility in most liquids, high mechanical strength, wear resistance, excellent uniformity and resistance to aging. A limitation of quartz is its comparatively low electromechanical conversion efficiency.

b. Lithium Sulfate. Principal advantages are:

ease of obtaining optimum acoustic damping for best resolution, intermediate conversion efficiency, and negligible mode interaction.

c. Polarized Ceramics. Principal advantages are: high conversion efficiency which yields high search unit sensitivity. Because of lower mechanical strength and relatively high electrical capaci.

tance, their use is generally restricted to frequencies below 15 Mega-Hertz (MHz). Another limitation is some interaction between various modes of vibration.

In order for a crystal to utilize its piezoelectric characteristics, it is placed in a circuit much like a condenser. That is, both faces are coated with a conducting material with no contact between the two faces. (See Figure 1.) Coatings for crystals 5 COAXIAL CABLE CONNECTION

12. PIEZOELECTRIC EFFECT. Ultrasonic testing may use the piezoelectric effect to generate ultrasonic vibrations. Crystals, when subjected to an alternating electric charge, expand and contract under the influence of these charges. Conversely, it was found that these materials when subjected to alternating compression and tension developed alternating electric charges on their faces. (See Figure 2.) This was named the piezoelectric effect.

The heart of an ultrasonic testing system is this method of converting electrical energy into mechanical vibrations, and converting the mechancial vibrations back into electrical energy.

ALTERNATING VOLTAGE APPLIED •

TO AN X-CUT CRYSTAL

CRYSTAL EXPANDS CRYSTAL CONTRACTS FIGURE 2.--Generation of Ultrasonic Vibration Generation of the ultrasonic pulse is usually accomplished by producing a radio-frequency wave train of the desired frequency at a precise time and converting this into vibrations by means of piezoelectric transducers. Some ultraconsic instruments do not use a radio-frequency wave train, but instead, use a shock pulse and allow the search unit to select the frequency of operation.

13. TRANSDUCER TYPE SEARCH UNITS. The PLATED BACK search unit consists of a shell for mechanical pro- CRYSTAL tection, a means to conveniently handle or mount PLATED FACE the unit for use, the transducer element, electrical connections, and a backing material to dampen the backward directed energy that is transmitted FIGURE 1.-Angle Beam Search Unit by the crystal. (See Figure 3.)

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ELECT. 14. TRANSDUCER GROUPS. There are three gen- ELECT. CONNECTION eral groups of transmitter-receiver search units:

LEAD TO CRYSTAL SHELL a. Common Transmitter-Receiver (T-R). These search units employ a single crystal and have com- BACKING mon connections to the transmitter and receiver

- MATERIAL amplifier units. (See Figure 5.)

SPECIMEN PIEZOELECTRIC CRYSTAL 2 CRYSTAL FIGURE 3.-Diagram of an Ultrasonic Search Unit — LUCITE BLOCK Transducers are available in a wide variety of types which include:

a. X-Cut crystals for longitudinal-wave gen- T SPECIMEN eration. (See Figure 4.)

b. Y-Cut crystals for shear-wave generation.

(See Figure 4.)

FIGURE 5.-Common Transmitter-Receiver Search Unit

c. Dual crystals with common holder.

d. Mosaics three or more crystals.

e. High frequency, 50 MHz or more.

f. Alternate crystal materials.

g. Sandwich and tandem arrangements.

h. Curved crysals to fit the specimen.

i. Wheel search units.

¡. Focused search units.

k. Temperature search units (for measuring wall thickness at temperature up to 1,100°F).

/ AXIS Since the search unit acts as both transmitter and receiver, it transmits a pulse of 1 to 4 microseconds duration; then acts as a receiver for a period up to several thousand microseconds. This cycle of transmitting and receiving is repeated at a rate of 50 to 5,000 times per second, or higher if required for high-speed automatic scanning.

b. C o m b in e d Transmitter-Receiver (T-R).

These search units have two transducers mounted on a single head and insulated acoustically from each other. One transducer is connected to the pulser and the other is connected to the receiver.

The combined T-R search unit is used for testing close to the entry surface and for thickness measurements from .040" to 2.0" when the opposite side is rough or corroded. The transmitting search unit projects a beam of vibrations into the material; the vibrations travel through the material and are re-

X-CUT X AXIS IRANSMITTING RECEIVING

- Y AXIS CRYSTAL CRYSTAL

FRONTAL

PARENT MEMBERS

SPECIM (LUCITE)

CRYSTAL Y-CUT Z AXIS • FLAW FIGURE 4.-Natural Quartz Crystal (X and Y Cut) Transducers are available that are smaller than ⅛" diameter and larger than 1" x 4". However, for most ultrasonic testing, standard diameters of -BACK SURFACE ¼", ½", and 1.0" are used. FICURE 6.--Combined Transmitter-Receiver Search Unit

fleeted back to the receiving search unit from any discontinuities or from the opposite boundary if Ly parallel to the entrant surface. --(See Figure 6.)

- c. Separate Transmitter-Receiver U-RI or Pitch-Catch, Search Units. Two heads are employed in these units having separate electrical connections to the transmitter and the receiving units.

One head is used as the transmitting unit while the other head is the receiving unit. (See Figure 7.)

. Materials which are coarse grained tend to scatter the ultrasonic sound beam; these materials can be effectively inspected using separate T-R search units that are mounted on individual wedges of a suitable plastic solid. When separate wedges are used, the angle of incidence may be varied according to the section thickness to be examined.

FIGURE 7.--Separate Transmitter-Receiver Search Unit

15.-20. RESERVED.

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Chapter 3. WAVE PROPAGATION

21. ULTRASONIC WAVES. Ultrasonic waves can be propagated to some extent in any elastic material. This propagation occurs as a displacement of the successive elements of the material. If one part of a solid is distributed or displaced in some manner, molecules in other parts of the solid will be affected, but not instantaneously. As successive molecules in the medium are displaced, the disturbance is propagated away from its point of origin. (See Figure 8.) Since the lattice structure of all materials is elastic, a restoring force exists which tends to return each molecule to its original position. Because of inertia, these particles will tend to oscillate about their original undisturbed position until they come to rest. This molecule-tomolecule propagation results in a continuous train of disturbances called a compression-rarefaction wave. If the frequency of motion is above 20,000 cycles per second (cps) the waves are referred to as ultrasonic compressional waves. A small group of these waves, which occur together and are not preceded or followed by other waves, is called a wave train or a pulse. A pulse may have one of several different forms depending upon the individual wave amplitude, and the way the waves build up and decay. The most used modes of vibration are longitudinal, shear, surface, and plate waves.

IMPACI The longitudinal mode of wave transmission is probably the most widely used in ultrasonic testing and is also the easiest to see with respect to the method of propagation. This wave is easily generated, detected, and has a high velocity of travel in most media.

Longitudinal waves are used for the detection and location of defects that present a reasonably large frontal area to the surface from which the test is being made.

2 PARTICLE VIBRATION

DIRECTION OF PROPAGATION FIGURE 9.-Longitudinal Waves

23. SHEAR WAVES. The wave is said to be shear (transverse) when the movement of the particles are perpendicular to the direction of the wave motion. (See Figure 10.) These waves have a lower velocity than do longitudinal waves (in steel and other metals, about half). Because of their slower speed, shear waves have shorter wave lengths than those of longitudinal waves of the same frequency. This shorter wave length makes shear waves more sensitive to small inclusions, and consequently they are more easily scattered within the specimen.

PARTICLE VIBRATION

REFLECTION FIcURE 8.-Mechanical Analogy of Wave Propagation

22. LONGITUDINAL WAVES. The wave is said to be longitudinal (compressional) when the movement of the particles is parallel to the direction of the wave motion. (See Figure 9.)

DIRECTION OF PROPAGATION FIGURE 10.-Shear Waves The principal advantage of these waves is in applications that require an ultrasonic beam to be transmitted into the test object at a small angle to the surface. (See Figure 11.)

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SEARCH UNIT

CRYSTAL

PLASTIC WEDGE

SPECIMEN

DIRECTION OF SOUND

VIBRATION DIRECTION FIGURE 11.-Transmitting A Wave at a Small Angle

24. SURFACE (RAYLEIGH) WAVES. Surface waves travel with little attenuation in the direction of propagation, but their energy decreases rapidly as the wave penetrates below the surface. The particle displacement of the wave motion follows an elliptical orbit consisting of both the longitudinal and shear wave motion. (See Figure 12.)

PARTICLE VIBRATION FOLLOWS

AN ELLIPTICAL ORBIT

DIRECTION OF PROPAGATION FIGURE 12.-Surface Waves Velocity of surface waves depends upon the material and is about nine-tenths of the shear-wave velocity. Surface waves are likely to be affected, in their propagation, by variations in hardness, plated coatings, shot peening, or surface cracks, and are easily dampened by dirt or grease on the surface of the specimen. Surface waves can often be produced as an unwanted effect, especially when the contact surface is rough.

The waves are not limited to flat surfaces. They will travel around curves and surface contours.

Sharp corners, such as the boundaries of plates or flaws, will reflect these waves. In fact, it is this characteristic or traveling around contours which makes surface waves so useful in surface flaw detection. (See Figure 13.)

SEARCH UNIT CRYSTAL FIGURE 13.-Surface Wave Technique

25. PLATE (LAMB) WAVES. When ultrasonic vibrations are introduced into a relatively thin sheet, the energy propagates in the form of plate waves.

Unlike the longitudinal, shear, and surface modes, the plate wave velocity is dependent both on frequency and plate thickness. A complex particle motion exists somewhat like the elliptical orbits described for surface waves. Greatly simplified, they can be divided into two basic types: The symmetrical type are known as dilational waves and the asymmetrical type as bending waves.

Examples of these two modes are illustrated in Figure 14.

ASYMMETRIC SYMMETRIC FIGURE 14.-Plate Waves Plate waves can be used for detecting nonbonded areas in laminated structures such as sandwich panels. By sending waves along the outer surface, any areas of the top sheet that are not 'securely bonded in place can be made to vibrate in one of these modes. By sensing such local areas of vibration, lack of proper bonding can be detected.

26.-30. RESERVED.

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Chapter 4. ULTRASONIC VIBRATIONS

31. TESTING METHODS. Ultrasonics employ lowamplitude stresses which do not permanently affect a specimen because of the short wave lengths and relatively low energy of the ultrasonic vibrations which are transmitted through the material. On the other hand, destructive mechanical tests, such as static physical tests and forced vibration fatigue testing involve high-amplitude stresses. These highamplitude stresses may cause heating, nonlinear effects, permanent deformation, and eventual rupture of the specimen.

Sound waves beyond the hearing range of the human ear are referred to as ultrasonic vibrations.

The term embraces all vibrational waves of a frequency greater than approximately 20,000 Hz.

Ultrasonic vibrations of the lower frequencies act in essentially the same manner as do audible waves.

Most commercial ultrasonic testing is done at frequencies from 200 KHz to 25 MHz; however, application exists for frequencies as low as 2 KHz and as high as 200 MHz.

In practical testing, selection of frequency depends on sensitivity desired and sound penetration required; high frequency for sensitivity and low frequency for penetration. In general, sound waves of all frequencies will penetrate fine-grain material.

However, as the grain structure becomes more coarse, interference in the form of scattering may be expected when using higher frequencies (shorter wave lengths) and greater depth of penetration will be obtained by going to lower frequencies (longer wave lengths). The resonant frequency of a crystal is determined primarily by its thickness, the higher the frequency the thinner the crystal. For this reason, crystals with frequencies above 10 MHz are generally considered too fragile for contact testing. All testing frequencies, however, can be used in immersion testing.

Ultrasonic vibrations have several important characteristics:

a. They travel relatively long distances in solid materials.

b. They travel in well-defined sound beams.

c. The velocity of a specific vibrational wave mode is constant through a given homogenous material.

d. Most of the energy contained in one vibrational wave train is dissipated before the succeeding pulse is introduced to avoid confusing indications.

e. Vibrational waves will be reflected at boundaries of different elastic and physical properties.

f. Vibrational waves may change their mode of vibration when passing between materials having different elastic and physical properties or when reflected from boundaries at certain angles.

32. REFLECTION OF ULTRASONIC WAVES. Reflection of the ultrasonic vibrations will occur at the boundary between two different materials if a mismatch of acoustic impedance is encountered. The ultrasonic beam will be reflected at the interface exactly like light waves. For instance, the silvered back of a mirror has a high impedance mismatch to air, and light reflects from it at a very high efficiency. A plain piece of polished crystal has a very low impedance mismatch with air, and consequently, reflects very little.

When ultrasonic energy impinges upon the interface between two different mediums, part will

ANGLE OF REFLECTIONS = TO

ANGLE OF INCIDENCE

SOUND REFLECTION

FROM BACK

SURFACE

SOUND REFLECTED BACK

TO SEARCH UNIT FIGURE 15.-Reflection of Ultrasound 9

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be reflected, and the rest will be allowed to pass CRYSTAL ANGLE OF BEAM IN into the second medium, depending upon the im- WEDGE the path traveled by the vibrations and whether pedance ratio between the two materials. Also, [SURFACE WAVES they return to their source depends upon the angles at which the beam impinges upon the reflecting - LONGITUDINAL surfaces, as well as the number and location of WAVES these surfaces. (See Figure 15.)

33. REFRACTION AND MODE CONVERSION OF ULTRASONIC WAVES. Ultrasonic beams introduced at an angle into a specimen are refracted.

The velocities in the wedge material and the metal are different, therefore, the longitudinal vibrations will be refracted when passing into the metal. (See Figure 16.) At certain angles, conversion to other

ANGLE OF BEAM IN

WEDGE MATERIAL

• WEDGE MATERIAL

ANGLE OF BEAM

IN METAL FIGURE 18.-Generating Surface Waves

34. BEAM DIVERGENCE. Beam divergence varies with frequency and crystal diameter. The higher frequencies give more directivity to the sound beam.

Also, a large diameter crystal is more directive than one of a smaller diameter when operated at the same frequency. (See Figure 19 and 20.)

3 M.C. 2% M.C. 1 M.C. ½ M.C.

QUART QUARTZ

ANGLE OF BEAM

IN TEST MATERIAL 56"/ FT 1½"/FT 3'/FT FIGURE 16.-Refraction of the Ultrasonic Beam modes of vibration, such as shear (see Figure 17) FIGURE 19.-Beam Divergence of Sound Waves in Steel and surface waves (see Figure 18) occurs.

WHERE: «= angle normal to the beam in the wedge. QUARTZ ß= angle of refracted beam in -LONGITUDINAL specimen. ..13 € = 229,000 368 C1 = velocity of incident vibra- 29* SURFACE = 115,000 tions in the wedge (usually the longitudinal velocity). 90° c2 = velocity of vibration in the material under inspection TRANSVERSE OR for the desired wave mode. 1: 126,000 SILAR STEEL CRYSTAL \ ANGLE OF BEAM IN WEDGE FIGURE 20.-Diagram of Longitudinal Sound Striking a Surface

- LONGITUDINAL WAVES

35.-40. RESERVED.

2SHEAR WAVES

ANGLE OF BEAM

IN METAL FIGURE 17.-Generating Shear Waves 10