Temper Brittleness
&
Fracture Toughness
Temperature of Tempering

Specified Temp
 1st tempering - 520 - 550ºC
 2nd tempering - 530 - 570ºC

Tempered at (1st & 2nd)
 380 - 460ºC
( most of the barrels were tempered between
this range prior to 1996)
METALLURGICAL REPORT SUMMARY
FAILED INVESTIGATED CONCLUSION
IMPORTED 30 19 No remarkable metallurgical
deficiency that could lead to
failure
INDIGENOUS 7 7 No metallurgical deficiency.
(T2 - 500C Overload failure
& above)
INDIGENOUS 13 12 a) Temper brittleness due to
(T2 – 460 C low tempering temperature
& below) -(8 Cases)
b) No metallurgical deficiency
(3cases)
-
Salvaging of Low Temperature Tempered
Barrels
 Barrels tempered at temp. 401-430ºC be
grouped based on trace elements contents
(As, Sb, Sn, P) , since they play major role in
development of temper brittleness.
• Grouping of Barrels (Sn + Sb + As + P)
• Category A - > 0.025
• Category B - 0.025 % - 0.02 %
• Category C - < 0.02 %
• Category D - <0.02%, but Impact Value Lower
than specified min
on th Drawing.( 2 )

Proposal of DMRL
Effect of Trace Elements
Decisions
Category A - Rejected
Category B - • Re-tempered at 500ºC for 4 hrs
• Each barrel Subjected to high pressure proof
•Two barrels subjected to life cycle proof
Category C - • Initially 3 barrels from first batch of
100 be subjected to life cycle proof
• next 1 barrel from every 100 barrels
subjected to life cycle test
Category D - • Not to be considered now
 Barrels tempered below 400ºC not considered
Implementation of the Decision

436 Nos of such barrels were identified

435 Nos analysis of trace elements
completed

Barrels were categorised and confirmed by
rechecking at DMRL as under
A B C D
40 42 347+5* 1
* 5 barrels used for LIFE CYCLE firing
Life Achieved
Barrel EFC Bore Dia(mm)
L/882 304.25 128.15
L/993 303.63 127.60
L/762 304.125 128.15
L/868 309.00 128.40
L/1610 312.75 128.13

All the Barrels were brought to CQA
(Metals) for further study of fire crack
growth
Report on Fire Crack Growth

Barrels were parted longitudinally across its
whole length and examined visually for any
abnormality

Discs from various section were cut and extent
of crack depth was measured
Barrel No Max Depth Of
Crack(mm)
L/762 0.39
L/882 0.70
L/933 0.30
L/868 0.42
L/1610 0.34
Evaluation from Fracture
Toughness Point of View

Fracture toughness & critical crack lengths for
failure were calculated

Fracture toughness of few tempered brittle failed
barrels were estimated

Fracture toughness of 4 low temperature
tempered ‘C’ category barrels were estimated

Fracture toughness of Russian barrel was
estimated

Fracture toughness of correctly tempered MSF
barrels were estimated
Calculated KIC Values & Critical
Crack Length
KIC acr Expected Life
(mm) Initial Crack (2mm) Initial Crack (3mm)
85.00 2.630 49 -
90.00 3.593 113 38
93.34 5.00 192 117
95.00 10.73 508 433
100.00 13.17 622 547
 Where acr is critical crack length
 Taking into consideration that life of the barrel is 250
FSAPDS rds or 250 EFC, critical value for fracture
toughness with ultrasonic acceptance standard 2mm
hole size works out to be 95 MNm-3/2
Tested Value ( KIC )

Russian Failed Barrel - 102

Failed temper brittle (Indian) - 85

MSF (tempered correctly) -
102/113

‘C’ cat barrel - 95/105

This data generally agrees with calculated
values

Data also fairly agree with literature
Failure of T-72
Barrels
Photographs
Barrel No. L/876 – Blown of region of barrel
Barrel No. L / 876 – Small longitudinal crack on inner
surface
Barrel No. L / 876 – Point of initiation of fracture from
the region containing longitudinal crack on inner surface
Barrel No. L / 876 – propagation of fire crack in inter
crystalline mode
Barrel No. L /0199 – Barrel piece in as received condition
Barrel No. L / 0199 – Inter crystalline crack
Barrel No . L / 0199 – Macro Photograph. Presence
of transverse crack inside the wall
Barrel No. L / 0199 – Secondary Inter Crystalline
crack from the main fracture
Barrel No L / 014 – Transverse crack on inner surface of
the barrel piece
Bore
Outer Surface
Barrel No. L / 014 Fracture surface where inside crack
extended to outer surface
Barrel No. L / 014 – Fracture surface away from severed zone
Barrel No. L / 014 – Fracture towards inner
surface where crack progresses transversely
Barrel No. L / 231 – Failed barrel
Barrel No L/231- Some fragments of the barrel
Barrel No. L / 753 – Transverse fracture surface of segments
Barrel No L / 753 – Fragments of barrel

Temper Embrittlement Examaple 2.good ppt

  • 1.
  • 2.
    Temperature of Tempering  SpecifiedTemp  1st tempering - 520 - 550ºC  2nd tempering - 530 - 570ºC  Tempered at (1st & 2nd)  380 - 460ºC ( most of the barrels were tempered between this range prior to 1996)
  • 3.
    METALLURGICAL REPORT SUMMARY FAILEDINVESTIGATED CONCLUSION IMPORTED 30 19 No remarkable metallurgical deficiency that could lead to failure INDIGENOUS 7 7 No metallurgical deficiency. (T2 - 500C Overload failure & above) INDIGENOUS 13 12 a) Temper brittleness due to (T2 – 460 C low tempering temperature & below) -(8 Cases) b) No metallurgical deficiency (3cases) -
  • 4.
    Salvaging of LowTemperature Tempered Barrels  Barrels tempered at temp. 401-430ºC be grouped based on trace elements contents (As, Sb, Sn, P) , since they play major role in development of temper brittleness. • Grouping of Barrels (Sn + Sb + As + P) • Category A - > 0.025 • Category B - 0.025 % - 0.02 % • Category C - < 0.02 % • Category D - <0.02%, but Impact Value Lower than specified min on th Drawing.( 2 )  Proposal of DMRL
  • 5.
  • 6.
    Decisions Category A -Rejected Category B - • Re-tempered at 500ºC for 4 hrs • Each barrel Subjected to high pressure proof •Two barrels subjected to life cycle proof Category C - • Initially 3 barrels from first batch of 100 be subjected to life cycle proof • next 1 barrel from every 100 barrels subjected to life cycle test Category D - • Not to be considered now  Barrels tempered below 400ºC not considered
  • 7.
    Implementation of theDecision  436 Nos of such barrels were identified  435 Nos analysis of trace elements completed  Barrels were categorised and confirmed by rechecking at DMRL as under A B C D 40 42 347+5* 1 * 5 barrels used for LIFE CYCLE firing
  • 8.
    Life Achieved Barrel EFCBore Dia(mm) L/882 304.25 128.15 L/993 303.63 127.60 L/762 304.125 128.15 L/868 309.00 128.40 L/1610 312.75 128.13  All the Barrels were brought to CQA (Metals) for further study of fire crack growth
  • 9.
    Report on FireCrack Growth  Barrels were parted longitudinally across its whole length and examined visually for any abnormality  Discs from various section were cut and extent of crack depth was measured Barrel No Max Depth Of Crack(mm) L/762 0.39 L/882 0.70 L/933 0.30 L/868 0.42 L/1610 0.34
  • 10.
    Evaluation from Fracture ToughnessPoint of View  Fracture toughness & critical crack lengths for failure were calculated  Fracture toughness of few tempered brittle failed barrels were estimated  Fracture toughness of 4 low temperature tempered ‘C’ category barrels were estimated  Fracture toughness of Russian barrel was estimated  Fracture toughness of correctly tempered MSF barrels were estimated
  • 11.
    Calculated KIC Values& Critical Crack Length KIC acr Expected Life (mm) Initial Crack (2mm) Initial Crack (3mm) 85.00 2.630 49 - 90.00 3.593 113 38 93.34 5.00 192 117 95.00 10.73 508 433 100.00 13.17 622 547  Where acr is critical crack length  Taking into consideration that life of the barrel is 250 FSAPDS rds or 250 EFC, critical value for fracture toughness with ultrasonic acceptance standard 2mm hole size works out to be 95 MNm-3/2
  • 12.
    Tested Value (KIC )  Russian Failed Barrel - 102  Failed temper brittle (Indian) - 85  MSF (tempered correctly) - 102/113  ‘C’ cat barrel - 95/105  This data generally agrees with calculated values  Data also fairly agree with literature
  • 14.
  • 15.
    Barrel No. L/876– Blown of region of barrel
  • 16.
    Barrel No. L/ 876 – Small longitudinal crack on inner surface
  • 17.
    Barrel No. L/ 876 – Point of initiation of fracture from the region containing longitudinal crack on inner surface
  • 18.
    Barrel No. L/ 876 – propagation of fire crack in inter crystalline mode
  • 19.
    Barrel No. L/0199 – Barrel piece in as received condition
  • 20.
    Barrel No. L/ 0199 – Inter crystalline crack
  • 21.
    Barrel No .L / 0199 – Macro Photograph. Presence of transverse crack inside the wall
  • 22.
    Barrel No. L/ 0199 – Secondary Inter Crystalline crack from the main fracture
  • 23.
    Barrel No L/ 014 – Transverse crack on inner surface of the barrel piece Bore Outer Surface
  • 24.
    Barrel No. L/ 014 Fracture surface where inside crack extended to outer surface
  • 25.
    Barrel No. L/ 014 – Fracture surface away from severed zone
  • 26.
    Barrel No. L/ 014 – Fracture towards inner surface where crack progresses transversely
  • 27.
    Barrel No. L/ 231 – Failed barrel
  • 28.
    Barrel No L/231-Some fragments of the barrel
  • 29.
    Barrel No. L/ 753 – Transverse fracture surface of segments
  • 30.
    Barrel No L/ 753 – Fragments of barrel

Editor's Notes

  • #2 For certain alloy steels there is a band zone of tempering temperature 375 to 5000C ( depending on composition). Tempering in this region leads to a phenomenon called temper brittleness. This barrel material falls in this category.Some of the Indian barrels tempered in this range certainly failed catastrophically due this phenomenon. Another interesting fact is that this phenomenon is reversible in nature, ductility is regained when again tempered at correct temperature. Temper brittlenes develops due to presence of certain trace elements in high proportions eg. AS, SB, Sn, P.- show transperancy This phenomena is thought to be responsible for failures of Indian origin barrels. Show two transparencies for graphical representation of temper brittleness Go back to previous slide with button
  • #3 Dimension of the problem can be gauged that almost 120 crore is involved
  • #4 This last two slides clearly establishes that there is also problem with ammunition. In all cases of failure CQA(Amm) maintained that ammunition is above board. But statistics says otherwise.
  • #5 Next comes the most interesting part is the salvaging of the barrel,which incidentally gave us a direction for further investigation; glaring statistics which was neglected earlier. It was really difficult for OFB to digest loss of 120 crore Grouping was decided based on aircraft specification
  • #7 .
  • #10 Life achieved and crack depth showed that barrel is far too safe and still can fire another 100 rds