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4/4/2014 Hareesha N G, Asst Prof, DSCE, Blore 1
UNIT-6: Photo-elastic (Bire-fringent) Coatings :
• Birefringence coating stresses
• Effects of coating thickness
– Reinforcing effects, Poisson’s ratio mismatch
• Stress separation techniques
– Oblique incidence, Strip coatings
08 Hours
4/4/2014 2Hareesha N G, Asst Prof, DSCE, Blore
INTRODUCTION
• In the application of coating methods, one applies a thin
layer of a reactive material to the surface of the body that
is to be analyzed.
• The thin coating is bonded to the surface and
displacements at the coating-specimen interface are
transmitted without amplification or attenuation.
• These displacements at the interface produce stresses and
strains in the coating and the coating responds.
• The analyst observes the coating response and infers the
stresses on the surface of the specimen based on the
observed behavior of the coating.
4/4/2014 3Hareesha N G, Asst Prof, DSCE, Blore
ADVANTAGES OF COATING METHODS
• The capability of applying the coating directly to the
prototype:
• The "whole"-field response of the coating: Stain gages
respond over small regions of the field and give
approximations to strain at a point. Coatings respond over
the entire surface of the specimen and give field data
rather than point data.
• There are two coating methods that are used in stress
analysis.
– Bire-fringent coating that produces a photo-elastic fringe
pattern related to the coating stresses.
– Brittle coating that fails by cracking when the coating
stresses exceed some threshold value.
4/4/2014 4Hareesha N G, Asst Prof, DSCE, Blore
BIREFRINGENT COATINGS
• The method of birefringent coatings represents an extension
of the procedures of photoelasticity to the determination of
surface strains in opaque two- and three-dimensional bodies.
• The coating is a thin sheet of birefringent material, usually a
polymer, which is bonded to the surface of the prototype
being analyzed.
• The coating is mirrored at the interface to provide a reflecting
surface for the light-When the prototype is loaded, the
displacements on its surface are transmitted to the mirrored
side of the coating to produce a strain field through the
thickness of the coating.
• The distribution of the strain field over the surface of the
prototype, in terms of principal-strain differences, is
determined by employing a reflected-light polariscope to
record the fringe orders, as illustrated in Fig.
4/4/2014 5Hareesha N G, Asst Prof, DSCE, Blore
(Contd…..)
4/4/2014 6Hareesha N G, Asst Prof, DSCE, Blore
Reflection polari-scopes commonly used in photoelastic-
coating measurements:
P-polarizer;
A-analyzer;
λ/4, quarter-wave plate.
BIREFRINGENT COATINGS (…..Contd)
• The birefringent-coating method has many
advantages over other methods of experimental
stress analysis.
• It provides full-field data that enable the
investigator to visualize the complete distribution of
surface strains.
• The method is nondestructive, and since the
coatings can be applied directly to the prototype,
the need for models is eliminated.
• Through proper selection of coating materials, the
method can be made applicable over a very wide
range of strain.
4/4/2014 7Hareesha N G, Asst Prof, DSCE, Blore
Photo stress coating being contoured
to the surface of a vehicle water pump
casting
4/4/2014 Hareesha N G, Asst Prof, DSCE, Blore 8
Commercial Reflection Polariscope
4/4/2014 Hareesha N G, Asst Prof, DSCE, Blore 9
4/4/2014 Hareesha N G, Asst Prof, DSCE, Blore 10
Photo Stress pattern revealed on a
mechanical controlled linkage
system in a passenger Air craft
4/4/2014 Hareesha N G, Asst Prof, DSCE, Blore 11
P. S. Testing under progress on a main landing gear of
Airbus A 330/A340 passenger air craft
4/4/2014 Hareesha N G, Asst Prof, DSCE, Blore 12
4/4/2014 Hareesha N G, Asst Prof, DSCE, Blore 13
Photo stress fringe pattern at a specific
area of an Airbus gear during a static
test sequence
4/4/2014 Hareesha N G, Asst Prof, DSCE, Blore 14
Final prototyping test on a landing gear from a
military fighter jet aircraft and P. S. fringe
pattern at several sections of the Landing gear
4/4/2014 Hareesha N G, Asst Prof, DSCE, Blore 15
Photo Stress fringe pattern on a partially
coated prototype of Boeing 767 main
landing gear
4/4/2014 Hareesha N G, Asst Prof, DSCE, Blore 16
Coated area on Jet engine Frames
Strain pattern at a specific location of fuel
pads and struts
4/4/2014 Hareesha N G, Asst Prof, DSCE, Blore 17
Properties which an ideal coating should exhibit
1. A high optical strain coefficient K to maximize coating response
2. A low modulus of elasticity Ec to minimize reinforcing effects
3. A high resistance to both optical and mechanical stress relaxation to
ensure stability of the measurement with time
4. A linear strain-optical response to minimize data-reduction
problems
5. A good adhesive bond to ensure perfect strain transmission
between coating and specimen
6. A high proportional limit to increase the range of strain over which
the coating can be utilized
7. Sufficient malleability to permit use on curved surfaces of three-
dimensional components
4/4/2014 18Hareesha N G, Asst Prof, DSCE, Blore
4/4/2014 Hareesha N G, Asst Prof, DSCE, Blore 19
COATING STRESSES
• Refer class notes
4/4/2014 20Hareesha N G, Asst Prof, DSCE, Blore
EFFECTS OF COATING THICKNESS
• When a photoelastic coating is bonded to a specimen, only in a few
instances are the strains transmitted to the coating without some
modification or distortion.
• More realistically, the coating is considered as a three-dimensional
extension of the specimen which is loaded by means of shear and
normal tractions at the interface.
• These tractions vary so that the displacements experienced by the
coating and the specimen at the interface are identical (as dictated by
perfect bonding).
• Thus, in the most general case:
– The average strain in the coating does not equal the strain at the
interface.
– A strain gradient exists through the thickness of the coating.
– The coating serves to reinforce the specimen.
• It is evident that these effects of thickness tend to vanish as the coating
thickness approaches zero.
• However, coatings with finite thickness (usually 0.50 to 3.00 mm, or 0.02
to 0.10 in) are required to obtain a high fringe count for accurate fringe-
order determinations.
4/4/2014 21Hareesha N G, Asst Prof, DSCE, Blore
Traction refers to the maximum frictional force that can be
produced between surfaces without slipping

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Birefringent coatings

  • 1. 4/4/2014 Hareesha N G, Asst Prof, DSCE, Blore 1
  • 2. UNIT-6: Photo-elastic (Bire-fringent) Coatings : • Birefringence coating stresses • Effects of coating thickness – Reinforcing effects, Poisson’s ratio mismatch • Stress separation techniques – Oblique incidence, Strip coatings 08 Hours 4/4/2014 2Hareesha N G, Asst Prof, DSCE, Blore
  • 3. INTRODUCTION • In the application of coating methods, one applies a thin layer of a reactive material to the surface of the body that is to be analyzed. • The thin coating is bonded to the surface and displacements at the coating-specimen interface are transmitted without amplification or attenuation. • These displacements at the interface produce stresses and strains in the coating and the coating responds. • The analyst observes the coating response and infers the stresses on the surface of the specimen based on the observed behavior of the coating. 4/4/2014 3Hareesha N G, Asst Prof, DSCE, Blore
  • 4. ADVANTAGES OF COATING METHODS • The capability of applying the coating directly to the prototype: • The "whole"-field response of the coating: Stain gages respond over small regions of the field and give approximations to strain at a point. Coatings respond over the entire surface of the specimen and give field data rather than point data. • There are two coating methods that are used in stress analysis. – Bire-fringent coating that produces a photo-elastic fringe pattern related to the coating stresses. – Brittle coating that fails by cracking when the coating stresses exceed some threshold value. 4/4/2014 4Hareesha N G, Asst Prof, DSCE, Blore
  • 5. BIREFRINGENT COATINGS • The method of birefringent coatings represents an extension of the procedures of photoelasticity to the determination of surface strains in opaque two- and three-dimensional bodies. • The coating is a thin sheet of birefringent material, usually a polymer, which is bonded to the surface of the prototype being analyzed. • The coating is mirrored at the interface to provide a reflecting surface for the light-When the prototype is loaded, the displacements on its surface are transmitted to the mirrored side of the coating to produce a strain field through the thickness of the coating. • The distribution of the strain field over the surface of the prototype, in terms of principal-strain differences, is determined by employing a reflected-light polariscope to record the fringe orders, as illustrated in Fig. 4/4/2014 5Hareesha N G, Asst Prof, DSCE, Blore (Contd…..)
  • 6. 4/4/2014 6Hareesha N G, Asst Prof, DSCE, Blore Reflection polari-scopes commonly used in photoelastic- coating measurements: P-polarizer; A-analyzer; λ/4, quarter-wave plate.
  • 7. BIREFRINGENT COATINGS (…..Contd) • The birefringent-coating method has many advantages over other methods of experimental stress analysis. • It provides full-field data that enable the investigator to visualize the complete distribution of surface strains. • The method is nondestructive, and since the coatings can be applied directly to the prototype, the need for models is eliminated. • Through proper selection of coating materials, the method can be made applicable over a very wide range of strain. 4/4/2014 7Hareesha N G, Asst Prof, DSCE, Blore
  • 8. Photo stress coating being contoured to the surface of a vehicle water pump casting 4/4/2014 Hareesha N G, Asst Prof, DSCE, Blore 8
  • 9. Commercial Reflection Polariscope 4/4/2014 Hareesha N G, Asst Prof, DSCE, Blore 9
  • 10. 4/4/2014 Hareesha N G, Asst Prof, DSCE, Blore 10
  • 11. Photo Stress pattern revealed on a mechanical controlled linkage system in a passenger Air craft 4/4/2014 Hareesha N G, Asst Prof, DSCE, Blore 11
  • 12. P. S. Testing under progress on a main landing gear of Airbus A 330/A340 passenger air craft 4/4/2014 Hareesha N G, Asst Prof, DSCE, Blore 12
  • 13. 4/4/2014 Hareesha N G, Asst Prof, DSCE, Blore 13
  • 14. Photo stress fringe pattern at a specific area of an Airbus gear during a static test sequence 4/4/2014 Hareesha N G, Asst Prof, DSCE, Blore 14
  • 15. Final prototyping test on a landing gear from a military fighter jet aircraft and P. S. fringe pattern at several sections of the Landing gear 4/4/2014 Hareesha N G, Asst Prof, DSCE, Blore 15
  • 16. Photo Stress fringe pattern on a partially coated prototype of Boeing 767 main landing gear 4/4/2014 Hareesha N G, Asst Prof, DSCE, Blore 16
  • 17. Coated area on Jet engine Frames Strain pattern at a specific location of fuel pads and struts 4/4/2014 Hareesha N G, Asst Prof, DSCE, Blore 17
  • 18. Properties which an ideal coating should exhibit 1. A high optical strain coefficient K to maximize coating response 2. A low modulus of elasticity Ec to minimize reinforcing effects 3. A high resistance to both optical and mechanical stress relaxation to ensure stability of the measurement with time 4. A linear strain-optical response to minimize data-reduction problems 5. A good adhesive bond to ensure perfect strain transmission between coating and specimen 6. A high proportional limit to increase the range of strain over which the coating can be utilized 7. Sufficient malleability to permit use on curved surfaces of three- dimensional components 4/4/2014 18Hareesha N G, Asst Prof, DSCE, Blore
  • 19. 4/4/2014 Hareesha N G, Asst Prof, DSCE, Blore 19
  • 20. COATING STRESSES • Refer class notes 4/4/2014 20Hareesha N G, Asst Prof, DSCE, Blore
  • 21. EFFECTS OF COATING THICKNESS • When a photoelastic coating is bonded to a specimen, only in a few instances are the strains transmitted to the coating without some modification or distortion. • More realistically, the coating is considered as a three-dimensional extension of the specimen which is loaded by means of shear and normal tractions at the interface. • These tractions vary so that the displacements experienced by the coating and the specimen at the interface are identical (as dictated by perfect bonding). • Thus, in the most general case: – The average strain in the coating does not equal the strain at the interface. – A strain gradient exists through the thickness of the coating. – The coating serves to reinforce the specimen. • It is evident that these effects of thickness tend to vanish as the coating thickness approaches zero. • However, coatings with finite thickness (usually 0.50 to 3.00 mm, or 0.02 to 0.10 in) are required to obtain a high fringe count for accurate fringe- order determinations. 4/4/2014 21Hareesha N G, Asst Prof, DSCE, Blore Traction refers to the maximum frictional force that can be produced between surfaces without slipping