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ME 351A PROJECT
Team members
Ankit Shrivastava (11113)
Ankit Yadav (11115)
Ahsen Parwez (11416)
Deepak Dalakoti (11235)
Shivam Patel (11683)
Anurag Bhatt (11135)
Project Title – Transporters
OBJECTIVE
 Design of transporter system in Southern Labs
 Analyzing critical failure locations of the assembly
 Estimating present load capacity of the machine
 Proposed design changes for a load of 3 tonnes
SUB SYSTEMS
 Pneumatics and Pulley
 Primarily lifting mechanism
 Pneumatic piston cylinder arrangement
 Powered by motor
 Main Frame
 Supports carriage and pulleys
 Safety features like anti roll bar
 Carriage
 Platform reinforced by square steel bars
 Connected to chain and pulley assembly
Design Specifications
FBD and Analysis of
sub-system
Is allowable load
under 3 tonnes?
Identify critical
locations with n =3
Proceed to next sub
system
Design alterations
NO
YES
Choose minimum of all
loads as the rated load
PNEUMATICS AND PULLEY
Possible modes of failure
 Rupture of pneumatic cylinder
 Buckling of piston rod
 Weld failure of Pulley shaft
 T section yielding
 Chain Design
ESTIMATING CRITICAL LOADS
Failure Mode Critical load with n = 3 (in tonnes)
Rupture of pneumatic cylinder 10.72
Buckling of piston rod 81
Weld failure of Pulley shaft 3.05
T section yielding 9.9
Chain failure ASTM 60 designed for 3 tons
 Critical element - pulley shaft
 Maximum allowable load = 3.05 tonnes
 Satisfies design requirement of 3 tonnes
 No design modifications required
MAIN FRAME
Modes of failure
 Failure of load carrying bar
 Weld failure of welded chain
 Anti roll bar failure
ESTIMATING CRITICAL LOADS
Modes of failure Critical loads with n =3 (in tonnes)
Failure of load carrying bar 1.1
Weld failure of welded chain 9.8
Anti roll bar 4.2
 Critical location – load carrying bar
 Maximum allowable load < 3 tonnes
 Design changes required
DESIGN CHANGES FOR WEIGHT CARRYING BAR
 Increase weld length and leg size
 Maximum Load is 2.4 tons for h =5mm and d = 5mm
 Maximum length and leg size limited by dimensions of bar
 Change material
 440 Q&T steel
 Maximum load is 7.32 tonnes
 Economically unfeasible
 Change weld pattern
 Square weld
 Maximum load = 3.26 tonnes
 Most feasible solution
 Compromised Factor of Safety
 Measure of last resort
 For n = 2 , critical 4.8 tons
CARRIAGE
Modes of failure
 Weight sharing by square
reinforcing side bars
 Shear failure of reinforcing side
bars
ESTIMATING CRITICAL LOADS
Modes of failure Maximum load with n = 3 (in tonnes)
Weight sharing by square reinforcing
side bars
26.42
Shear failure of reinforcing side bars 6.73
 Critical location – shear failure of reinforcing
side bars
 Maximum allowable load = 6.73 tonnes
 Satisfies design requirement of 3 tonnes
 No design changes required
FINITE ELEMENT ANALYSIS
 Analysis done using design principles was cross checked using Finite
element packages commercially available.
 Inventor was used to create a CAD model of the critical systems and
analysis was done.
 We plotted the factor of safety for the structure while taking load as 3
tonnes.
 Also, displacements of critical elements were plotted to check assumptions
made during theoretical analysis
LOAD CARRYING BAR
LOAD CARRYING BAR
LOAD CARRYING BAR
LOAD CARRYING BAR
CARRIAGE WELDS & BENDING
CARRIAGE WELDS & BENDING – Y displacements
CARRIAGE WELDS & BENDING- Safety factors
CARRIAGE WELDS & BENDING- Safety factors
DESIGN SHORTCOMINGS & PROPOSED
CHANGES
 Exact length of Piston rod unknown
 Novel Use of chain with pulley modelled as pulley with cable
 Mixture of butt & fillet welds in reinforcement bars taken as all fillet welds
(inherently conservative as fillet welds are weak)
 PROPOSED CHANGE :
 Load carrying bar most critical & fails at weld to connecting plate
 Design change made : weld pattern change
 Alternative: Add reinforcement to bar like in a truss for load sharing and
larger capacity enhancement and reliability
Analysis of Lifting Machine

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Analysis of Lifting Machine

  • 1. ME 351A PROJECT Team members Ankit Shrivastava (11113) Ankit Yadav (11115) Ahsen Parwez (11416) Deepak Dalakoti (11235) Shivam Patel (11683) Anurag Bhatt (11135) Project Title – Transporters
  • 2. OBJECTIVE  Design of transporter system in Southern Labs  Analyzing critical failure locations of the assembly  Estimating present load capacity of the machine  Proposed design changes for a load of 3 tonnes
  • 3. SUB SYSTEMS  Pneumatics and Pulley  Primarily lifting mechanism  Pneumatic piston cylinder arrangement  Powered by motor  Main Frame  Supports carriage and pulleys  Safety features like anti roll bar  Carriage  Platform reinforced by square steel bars  Connected to chain and pulley assembly
  • 4. Design Specifications FBD and Analysis of sub-system Is allowable load under 3 tonnes? Identify critical locations with n =3 Proceed to next sub system Design alterations NO YES Choose minimum of all loads as the rated load
  • 5. PNEUMATICS AND PULLEY Possible modes of failure  Rupture of pneumatic cylinder  Buckling of piston rod  Weld failure of Pulley shaft  T section yielding  Chain Design
  • 6. ESTIMATING CRITICAL LOADS Failure Mode Critical load with n = 3 (in tonnes) Rupture of pneumatic cylinder 10.72 Buckling of piston rod 81 Weld failure of Pulley shaft 3.05 T section yielding 9.9 Chain failure ASTM 60 designed for 3 tons  Critical element - pulley shaft  Maximum allowable load = 3.05 tonnes  Satisfies design requirement of 3 tonnes  No design modifications required
  • 7. MAIN FRAME Modes of failure  Failure of load carrying bar  Weld failure of welded chain  Anti roll bar failure
  • 8. ESTIMATING CRITICAL LOADS Modes of failure Critical loads with n =3 (in tonnes) Failure of load carrying bar 1.1 Weld failure of welded chain 9.8 Anti roll bar 4.2  Critical location – load carrying bar  Maximum allowable load < 3 tonnes  Design changes required
  • 9. DESIGN CHANGES FOR WEIGHT CARRYING BAR  Increase weld length and leg size  Maximum Load is 2.4 tons for h =5mm and d = 5mm  Maximum length and leg size limited by dimensions of bar  Change material  440 Q&T steel  Maximum load is 7.32 tonnes  Economically unfeasible  Change weld pattern  Square weld  Maximum load = 3.26 tonnes  Most feasible solution  Compromised Factor of Safety  Measure of last resort  For n = 2 , critical 4.8 tons
  • 10. CARRIAGE Modes of failure  Weight sharing by square reinforcing side bars  Shear failure of reinforcing side bars
  • 11. ESTIMATING CRITICAL LOADS Modes of failure Maximum load with n = 3 (in tonnes) Weight sharing by square reinforcing side bars 26.42 Shear failure of reinforcing side bars 6.73  Critical location – shear failure of reinforcing side bars  Maximum allowable load = 6.73 tonnes  Satisfies design requirement of 3 tonnes  No design changes required
  • 12. FINITE ELEMENT ANALYSIS  Analysis done using design principles was cross checked using Finite element packages commercially available.  Inventor was used to create a CAD model of the critical systems and analysis was done.  We plotted the factor of safety for the structure while taking load as 3 tonnes.  Also, displacements of critical elements were plotted to check assumptions made during theoretical analysis
  • 17. CARRIAGE WELDS & BENDING
  • 18. CARRIAGE WELDS & BENDING – Y displacements
  • 19. CARRIAGE WELDS & BENDING- Safety factors
  • 20. CARRIAGE WELDS & BENDING- Safety factors
  • 21. DESIGN SHORTCOMINGS & PROPOSED CHANGES  Exact length of Piston rod unknown  Novel Use of chain with pulley modelled as pulley with cable  Mixture of butt & fillet welds in reinforcement bars taken as all fillet welds (inherently conservative as fillet welds are weak)  PROPOSED CHANGE :  Load carrying bar most critical & fails at weld to connecting plate  Design change made : weld pattern change  Alternative: Add reinforcement to bar like in a truss for load sharing and larger capacity enhancement and reliability

Editor's Notes

  1. Add a phot or two of the complete projects