Transcript fr_a4.ppt
Term Project Presentation: Design and Analysis of a Turbine Blade Manufacturing Cell MEAE-6960H01 Professor Ernesto Gutierrez-Miravete Presenter: Ray Surace Project Overview : •Created a hybrid coding scheme for three turbine blade part numbers (P/N) to be produced in a group technology environment •Reviewed the performance of an initial turbine blade cell design with 12 workstations •Developed an improved cell design with 10 workstations •Created a facility layout using the Column-Sum Insertion Heuristic •Used a modified Approximate Three-Stage Markov Chain Model to determine the optimum size of buffers placed before and after an airfoil overlay coater •Performed a Mean Value Analysis to validate the final design of a turbine blade manufacturing cell 4/19/01 Design & Analysis of a Turbine Blade Manufacturing Cell Ray 2 Part Coding: •Three (3) P/Ns with common features were grouped to form a composite part family: P/N 100b1 200b1 100b2 Description Engine Model 100 STG 1 Turbine Blade Engine Model 200 STG 1 Turbine Blade Engine Model 100 STG 2 Turbine Blade •An alphanumeric hybrid coding scheme was derived from the machining sequence: P/N 100b1 200b1 100b2 Code 1b1y3 2b1y1 1b2n0 •The code makes use of the chain property; each character place in the code has a specific meaning: Example: P/N 100b1 Code: 1 b first digit of engine model 1 y part stage i.e. 1=STG1 part type b=blade 3 cooling hole code coating? y=yes, n=no •Cooling hole code: 0=no cooling holes, 1=laser cooling holes, 2=EDM cooling holes, 3=laser and EDM cooling holes 4/19/01 Design & Analysis of a Turbine Blade Manufacturing Cell Ray 3 Performance of 12 Workstation Cell Design : •Initial cell design incorporated 12 workstations into a ‘U-shaped” cell layout to complete machining and finishing operations on P/N 100b1, 200b1, and 100b2 turbine blade castings . Machine Number 1 2 3 4 5 1 2 3 4 5 6 6 7 isle 12 11 10 9 8 7 8 9 10 11 12 4/19/01 Description / Operation Grinder / Attachment Grind Grinder / Root and Tip Grind CMM / Grind Inspection Laser Driller / Laser Cooling Holes EDM Machine / EDM Cooling Holes Coater / Airfoil Coating Argon Purged Furnace / Heat Treat Peen Machine / Attachment Shot Peen X-Ray Machine / X-Ray Inspection Water-flow Bench / Blocked Hole & FM Inspection Air-flow Bench / Air-flow Inspection Inspection Station / Final Inspection Design & Analysis of a Turbine Blade Manufacturing Cell Ray 100b1 Operation Sequence 1 200b1 Operation Sequence 1 100b2 Operation Sequence 1 2 2 2 3 3 3 4 4 - 5 - - 6 5 - 7 6 4 8 7 5 9 8 - 10 9 - 11 10 - 12 11 6 4 Performance of 12 Workstation Cell Design : •Customer demand rates for all 3 P/Ns dictate that 9.12 parts must be produced per hour •Thus, cycle time C, must be 0.11 hrs. for each workstation •Processing time of the precipitation heat treat furnace is 24 hours; the retort can hold 150 blades. Thus, C = 0.16. This is unacceptable. •To meet customer demand rates the furnace retort must have a capacity of X 24hours 218.18 parts .11hours part •Checking utilization we find that the heat treat furnace is a bottleneck operation: Um p im i Pm Di Thus, Um, furnace= 1.46 •If a furnace with a capacity of 219 blades is purchased, WIP would increase by 69 pcs: 219 blades - 150 blades = 69 blades •By removing the heat treat furnace from the cell, the overall WIP (WIP=PxT) of the cell can be reduced by 150 pcs. : New cell design to include 10 workstations; precipitation heat treat and shot peen machines moved to a separate department 4/19/01 Design & Analysis of a Turbine Blade Manufacturing Cell Ray 5 Layout of 10 Workstation Cell Design : •Final turbine blade manufacturing cell design incorporates 10 workstations into a ‘U-shaped” cell layout: Machine Number 1 2 3 4 coater input buffer 5 5 4 3 2 1 6 7 6 coater output buffer 7 8 9 8 10 isle 9 10 4/19/01 Description / Operation Grinder / Attachment Grind Grinder / Root and Tip Grind CMM / Grind Inspection Laser Driller / Laser Cooling Holes EDM Machine / EDM Cooling Holes Coater / Airfoil Coating X-Ray Machine / X-Ray Inspection Water-flow Bench / Blocked Hole & FM Inspection Air-flow Bench / Air-flow Inspection Inspection Station / Cell Inspection Design & Analysis of a Turbine Blade Manufacturing Cell Ray 100b1 Operation Sequence 1 200b1 Operation Sequence 1 100b2 Operation Sequence 1 2 2 2 3 3 3 4 4 - 5 - - 6 5 - 7 6 - 8 7 - 9 8 - 10 9 4 6 Turbine Airfoil Manufacturing Facility Layout : •Column Sum-Insertion heuristic used to create a block plan of a turbine airfoil manufacturing facility with the following departments: –Receiving –Vendor Inspection (incoming casting inspection) –Blade Cell –Vane Cell –Heat Treat / Sot Peen Department –Shipping Receiving A Vendor Inspect Receiving I A Blade Cell I E U Vane Cell U A Blade Cell Vendor Insp. X A Heat Treat/Peen Shipping E O O O Heat Treat / Peen Vane Cell A Shipping 4/19/01 Design & Analysis of a Turbine Blade Manufacturing Cell Ray 7 Analysis of Coater Buffer Capacity : •Buffers are required before and after the coater in order to maintain a cycle time of 0.11 hrs. •An Approximate Three-Stage Markov Chain Model was modified to determine the optimum buffer size •The following modeling assumptions were made: –Cell modeled as a paced transfer line with M=10 stages –Coater capacity of 19 blades –Assumed the average mean time to failure, α-1 of workstations 1-5 and 7-10 approaches 0. Therefore α1-5,7-10 = 1e-6 –Assumed αcoater=1. Once the coater starts a cycle, any incoming parts go into the incoming buffers –The avg. mean “repair” time (coater cycle time) for the coater b-1=18.18cycles, or b=0.05 •The results of the Three-Stage model analysis are as follows: –The effectiveness of the cell without buffers, E00=.53282 –The maximum cell effectiveness is E21=.53284 –Therefore, the optimum buffer size before and after coating is Z=21 4/19/01 Design & Analysis of a Turbine Blade Manufacturing Cell Ray 8 Performance of 10 Workstation Cell Design: •A Mean Value Analysis (MVA) was performed to validate the 10 workstation blade cell design •The cell was modeled as a closed network with single servers •It was assumed that each P/N (p) may visit each workstation (j) in that part’s processing sequence once •A visit count (Vjp) table was constructed: Machine # 1 2 3 4 5 6 7 8 9 10 100b1 1 1 1 1 1 1 1 1 1 1 200b1 1 1 1 1 0 1 1 1 1 1 100b2 1 1 1 0 0 0 0 0 0 1 • To initialize the algorithm, a queue length (Ljp) of 1 was assumed in front of each workstation •The algorithm was calculated using the following formulas: 1 jp W jp u N p 1 Np L jpu L jr u 1 jp r p 1 jr (eqn. 11.24 A&S) , Xp •After three (3) iterations the algorithm converged Np M V jpW jp (eqn. 11.26 A&S) , L jp X p V jpW jp (eqn. 11.27 A&S) j 1 *The total production rate of the cell, Xtotal=9.92 parts per hour. This exceeds the demand, 9.12 parts per hour by 8%. Thus, the 10 workstation cell design is acceptable. 4/19/01 Design & Analysis of a Turbine Blade Manufacturing Cell Ray 9