Failure modes and preventive measures of crane hooks
Failure of a crane hook can lead to serious accidents, so its failure mode must be systematically analyzed and targeted preventive measures taken. The following is a detailed summary of the main failure types, root causes and solutions.
1. Common failure modes and cause analysis
1. Plastic deformation (permanent bending)
-
Phenomenon : The hook body or hook neck undergoes irreversible bending.
-
reason :
-
Overload : Exceeding the rated load (such as more than 1.5 times the static load).
-
Material defect : Inadequate yield strength due to improper heat treatment.
-
Shock load : sudden acceleration/stop causes a sudden increase in dynamic stress.
-
2. Fatigue fracture
-
Phenomenon : Cracks extend from high stress areas (such as the base of the hook neck) to fracture.
-
reason :
-
Cyclic loading : Frequent lifting leads to cumulative damage (see Miner's law).
-
Stress concentration : insufficient design fillet or surface processing defects.
-
Corrosive environment : accelerates crack initiation (such as marine salt spray).
-
3. Brittle fracture
-
Phenomenon : Sudden fracture without plastic deformation, and the cross section is granular.
-
reason :
-
Low temperature operation : insufficient material toughness (e.g. impact energy < 27J at -20°C).
-
Hydrogen embrittlement : Insufficient dehydrogenation after electroplating or pickling.
-
4. Wear and corrosion
-
Phenomenon :
-
Hook wear : The friction of the sling causes the size to exceed the limit (>10% of the original size).
-
Rust penetration : localized corrosion in chemical/marine environments.
-
-
reason :
-
Insufficient lubrication : Dry friction of rotating parts.
-
Failure of protective layer : paint peeling or plating damage.
-
5. Thread failure (detachable hook)
-
Phenomenon : Thread slippage, tooth collapse or loose connection.
-
reason :
-
Not tightened according to torque : insufficient or excessive preload.
-
Foreign matter intrusion : Dust/rust residue increases wear.
-
2. Preventive measures
1. Prevention during the design phase
Failure Mode | Design strategies |
---|---|
Plastic deformation | Safety factor ≥ 4 (GB/T 10051), FEA verifies stress distribution under extreme load. |
fatigue fracture | Optimize the hook neck transition radius (R≥10mm) and use shot peening to increase the surface compressive stress. |
Brittle fracture | Use low-temperature toughness materials (such as 34CrNiMo6) and prohibit electroplating. |
Wear/Corrosion | The hook mouth is welded with a wear-resistant layer (such as Hardox 500), and 316 stainless steel is used for marine environment. |
Thread failure | Use fine thread + anti-loosening nut (such as Nord-Lock washer). |
2. Manufacturing and process control
-
Material inspection :
-
Chemical composition analysis (spectrometer) + mechanical properties test (tensile, impact).
-
-
Heat treatment monitoring :
-
After the quenching and tempering process (quenching + tempering), the hardness is controlled at HB 200~300.
-
-
Non-destructive testing (NDT) :
-
100% magnetic particle testing (MT) to detect surface cracks, and ultrasonic testing (UT) in critical areas.
-
3. Usage and maintenance measures
Failure Mode | Maintenance measures |
---|---|
Overload deformation | Install a torque limiter to automatically cut off the lifting power supply when overloaded. |
Fatigue crack | MT inspection is carried out every 6 months and any cracks found will be scrapped immediately. |
Corrosion and wear | Apply anti-rust grease (such as Castrol Rustilo) every month and use plastic sheath in chemical environment. |
Loose threads | Check the torque regularly (e.g. M36 bolts require 1200 N·m) and use thread lockers. |
4. Personnel training and monitoring
-
Operation Specifications :
-
Oblique pulling and emergency stopping are prohibited, and the sling angle is ≤60°.
-
-
Intelligent monitoring :
-
Strain sensors are installed to monitor loads in real time, and vibration sensors are used to warn of bearing failures.
-
III. Typical Cases and Lessons
Case 1: Fatigue fracture accident
-
Background : A crane hook at a port broke after 5 years of use, causing a container to fall.
-
Reason : The root of the hook neck was not shot peened and the fatigue crack expanded to a critical size.
-
Improvement : Make it mandatory to replace the hook every 2 years and add TOFD inspection.
Case 2: Thread slippage causes thread shedding
-
Background : The hook thread in the metallurgical workshop failed and the ladle tilted.
-
Cause : The lock nut was not used and the high temperature caused the grease to carbonize.
-
Improvement : Use high temperature resistant thread locking agent (such as Loctite 272).
4. Failure Analysis Process
-
On-site protection : Take photos to record the fracture morphology and damaged areas.
-
Laboratory testing :
-
Fracture analysis : SEM scanning electron microscope is used to observe the crack source (such as fatigue striations).
-
Metallographic examination : Check for heat treatment defects (such as decarburization layer).
-
-
Root cause reporting : Propose design/maintenance improvement plans.
V. Conclusion
Key principles :
-
Prevention is better than cure : Reduce risk through design redundancy and regular testing.
-
Combination of technology and management : Intelligent monitoring makes up for the blind spots of manual inspection.
-
Everyone involved : From designers to operators, the consequences of failure must be clear.
Failure prevention tips :
-
"Strong materials, large rounded corners, frequent inspections, no overloading"
-
"Cracks don't last overnight, rust should be removed promptly"
By systematically analyzing failure modes and implementing strict preventive measures, the safety of hooks can be improved by more than 50%!
Failure of a crane hook can lead to serious accidents, so its failure mode must be systematically analyzed and targeted preventive measures taken. The following is a detailed summary of the main failure types, root causes and solutions.
1. Common failure modes and cause analysis
1. Plastic deformation (permanent bending)
-
Phenomenon : The hook body or hook neck undergoes irreversible bending.
-
reason :
-
Overload : Exceeding the rated load (such as more than 1.5 times the static load).
-
Material defect : Inadequate yield strength due to improper heat treatment.
-
Shock load : sudden acceleration/stop causes a sudden increase in dynamic stress.
-
2. Fatigue fracture
-
Phenomenon : Cracks extend from high stress areas (such as the base of the hook neck) to fracture.
-
reason :
-
Cyclic loading : Frequent lifting leads to cumulative damage (see Miner's law).
-
Stress concentration : insufficient design fillet or surface processing defects.
-
Corrosive environment : accelerates crack initiation (such as marine salt spray).
-
3. Brittle fracture
-
Phenomenon : Sudden fracture without plastic deformation, and the cross section is granular.
-
reason :
-
Low temperature operation : insufficient material toughness (e.g. impact energy < 27J at -20°C).
-
Hydrogen embrittlement : Insufficient dehydrogenation after electroplating or pickling.
-
4. Wear and corrosion
-
Phenomenon :
-
Hook wear : The friction of the sling causes the size to exceed the limit (>10% of the original size).
-
Rust penetration : localized corrosion in chemical/marine environments.
-
-
reason :
-
Insufficient lubrication : Dry friction of rotating parts.
-
Failure of protective layer : paint peeling or plating damage.
-
5. Thread failure (detachable hook)
-
Phenomenon : Thread slippage, tooth collapse or loose connection.
-
reason :
-
Not tightened according to torque : insufficient or excessive preload.
-
Foreign matter intrusion : Dust/rust residue increases wear.
-
2. Preventive measures
1. Prevention during the design phase
Failure Mode | Design strategies |
---|---|
Plastic deformation | Safety factor ≥ 4 (GB/T 10051), FEA verifies stress distribution under extreme load. |
fatigue fracture | Optimize the hook neck transition radius (R≥10mm) and use shot peening to increase the surface compressive stress. |
Brittle fracture | Use low-temperature toughness materials (such as 34CrNiMo6) and prohibit electroplating. |
Wear/Corrosion | The hook mouth is welded with a wear-resistant layer (such as Hardox 500), and 316 stainless steel is used for marine environment. |
Thread failure | Use fine thread + anti-loosening nut (such as Nord-Lock washer). |
2. Manufacturing and process control
-
Material inspection :
-
Chemical composition analysis (spectrometer) + mechanical properties test (tensile, impact).
-
-
Heat treatment monitoring :
-
After the quenching and tempering process (quenching + tempering), the hardness is controlled at HB 200~300.
-
-
Non-destructive testing (NDT) :
-
100% magnetic particle testing (MT) to detect surface cracks, and ultrasonic testing (UT) in critical areas.
-
3. Usage and maintenance measures
Failure Mode | Maintenance measures |
---|---|
Overload deformation | Install a torque limiter to automatically cut off the lifting power supply when overloaded. |
Fatigue crack | MT inspection is carried out every 6 months and any cracks found will be scrapped immediately. |
Corrosion and wear | Apply anti-rust grease (such as Castrol Rustilo) every month and use plastic sheath in chemical environment. |
Loose threads | Check the torque regularly (e.g. M36 bolts require 1200 N·m) and use thread lockers. |
4. Personnel training and monitoring
-
Operation Specifications :
-
Oblique pulling and emergency stopping are prohibited, and the sling angle is ≤60°.
-
-
Intelligent monitoring :
-
Strain sensors are installed to monitor loads in real time, and vibration sensors are used to warn of bearing failures.
-
III. Typical Cases and Lessons
Case 1: Fatigue fracture accident
-
Background : A crane hook at a port broke after 5 years of use, causing a container to fall.
-
Reason : The root of the hook neck was not shot peened and the fatigue crack expanded to a critical size.
-
Improvement : Make it mandatory to replace the hook every 2 years and add TOFD inspection.
Case 2: Thread slippage causes thread shedding
-
Background : The hook thread in the metallurgical workshop failed and the ladle tilted.
-
Cause : The lock nut was not used and the high temperature caused the grease to carbonize.
-
Improvement : Use high temperature resistant thread locking agent (such as Loctite 272).
4. Failure Analysis Process
-
On-site protection : Take photos to record the fracture morphology and damaged areas.
-
Laboratory testing :
-
Fracture analysis : SEM scanning electron microscope is used to observe the crack source (such as fatigue striations).
-
Metallographic examination : Check for heat treatment defects (such as decarburization layer).
-
-
Root cause reporting : Propose design/maintenance improvement plans.
V. Conclusion
Key principles :
-
Prevention is better than cure : Reduce risk through design redundancy and regular testing.
-
Combination of technology and management : Intelligent monitoring makes up for the blind spots of manual inspection.
-
Everyone involved : From designers to operators, the consequences of failure must be clear.
Failure prevention tips :
-
"Strong materials, large rounded corners, frequent inspections, no overloading"
-
"Cracks don't last overnight, rust should be removed promptly"
By systematically analyzing failure modes and implementing strict preventive measures, the safety of hooks can be improved by more than 50%!
Failure of a crane hook can lead to serious accidents, so its failure mode must be systematically analyzed and targeted preventive measures taken. The following is a detailed summary of the main failure types, root causes and solutions.
1. Common failure modes and cause analysis
1. Plastic deformation (permanent bending)
-
Phenomenon : The hook body or hook neck undergoes irreversible bending.
-
reason :
-
Overload : Exceeding the rated load (such as more than 1.5 times the static load).
-
Material defect : Inadequate yield strength due to improper heat treatment.
-
Shock load : sudden acceleration/stop causes a sudden increase in dynamic stress.
-
2. Fatigue fracture
-
Phenomenon : Cracks extend from high stress areas (such as the base of the hook neck) to fracture.
-
reason :
-
Cyclic loading : Frequent lifting leads to cumulative damage (see Miner's law).
-
Stress concentration : insufficient design fillet or surface processing defects.
-
Corrosive environment : accelerates crack initiation (such as marine salt spray).
-
3. Brittle fracture
-
Phenomenon : Sudden fracture without plastic deformation, and the cross section is granular.
-
reason :
-
Low temperature operation : insufficient material toughness (e.g. impact energy < 27J at -20°C).
-
Hydrogen embrittlement : Insufficient dehydrogenation after electroplating or pickling.
-
4. Wear and corrosion
-
Phenomenon :
-
Hook wear : The friction of the sling causes the size to exceed the limit (>10% of the original size).
-
Rust penetration : localized corrosion in chemical/marine environments.
-
-
reason :
-
Insufficient lubrication : Dry friction of rotating parts.
-
Failure of protective layer : paint peeling or plating damage.
-
5. Thread failure (detachable hook)
-
Phenomenon : Thread slippage, tooth collapse or loose connection.
-
reason :
-
Not tightened according to torque : insufficient or excessive preload.
-
Foreign matter intrusion : Dust/rust residue increases wear.
-
2. Preventive measures
1. Prevention during the design phase
Failure Mode | Design strategies |
---|---|
Plastic deformation | Safety factor ≥ 4 (GB/T 10051), FEA verifies stress distribution under extreme load. |
fatigue fracture | Optimize the hook neck transition radius (R≥10mm) and use shot peening to increase the surface compressive stress. |
Brittle fracture | Use low-temperature toughness materials (such as 34CrNiMo6) and prohibit electroplating. |
Wear/Corrosion | The hook mouth is welded with a wear-resistant layer (such as Hardox 500), and 316 stainless steel is used for marine environment. |
Thread failure | Use fine thread + anti-loosening nut (such as Nord-Lock washer). |
2. Manufacturing and process control
-
Material inspection :
-
Chemical composition analysis (spectrometer) + mechanical properties test (tensile, impact).
-
-
Heat treatment monitoring :
-
After the quenching and tempering process (quenching + tempering), the hardness is controlled at HB 200~300.
-
-
Non-destructive testing (NDT) :
-
100% magnetic particle testing (MT) to detect surface cracks, and ultrasonic testing (UT) in critical areas.
-
3. Usage and maintenance measures
Failure Mode | Maintenance measures |
---|---|
Overload deformation | Install a torque limiter to automatically cut off the lifting power supply when overloaded. |
Fatigue crack | MT inspection is carried out every 6 months and any cracks found will be scrapped immediately. |
Corrosion and wear | Apply anti-rust grease (such as Castrol Rustilo) every month and use plastic sheath in chemical environment. |
Loose threads | Check the torque regularly (e.g. M36 bolts require 1200 N·m) and use thread lockers. |
4. Personnel training and monitoring
-
Operation Specifications :
-
Oblique pulling and emergency stopping are prohibited, and the sling angle is ≤60°.
-
-
Intelligent monitoring :
-
Strain sensors are installed to monitor loads in real time, and vibration sensors are used to warn of bearing failures.
-
III. Typical Cases and Lessons
Case 1: Fatigue fracture accident
-
Background : A crane hook at a port broke after 5 years of use, causing a container to fall.
-
Reason : The root of the hook neck was not shot peened and the fatigue crack expanded to a critical size.
-
Improvement : Make it mandatory to replace the hook every 2 years and add TOFD inspection.
Case 2: Thread slippage causes thread shedding
-
Background : The hook thread in the metallurgical workshop failed and the ladle tilted.
-
Cause : The lock nut was not used and the high temperature caused the grease to carbonize.
-
Improvement : Use high temperature resistant thread locking agent (such as Loctite 272).
4. Failure Analysis Process
-
On-site protection : Take photos to record the fracture morphology and damaged areas.
-
Laboratory testing :
-
Fracture analysis : SEM scanning electron microscope is used to observe the crack source (such as fatigue striations).
-
Metallographic examination : Check for heat treatment defects (such as decarburization layer).
-
-
Root cause reporting : Propose design/maintenance improvement plans.
V. Conclusion
Key principles :
-
Prevention is better than cure : Reduce risk through design redundancy and regular testing.
-
Combination of technology and management : Intelligent monitoring makes up for the blind spots of manual inspection.
-
Everyone involved : From designers to operators, the consequences of failure must be clear.
Failure prevention tips :
-
"Strong materials, large rounded corners, frequent inspections, no overloading"
-
"Cracks don't last overnight, rust should be removed promptly"
By systematically analyzing failure modes and implementing strict preventive measures, the safety of hooks can be improved by more than 50%!
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