AGMA 01FTM1-2001 Carbide Hobbing Case Study《硬质合金滚刀范例分析》.pdf
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1、01FTM1Carbide Hobbing Case Studyby: Y. Kotlyar, Bodine Electric CompanyTECHNICAL PAPERAmerican Gear ManufacturersAssociationCarbide Hobbing Case StudyYefim Kotlyar, Bodine Electric CompanyThestatementsandopinionscontainedhereinarethoseoftheauthorandshouldnotbeconstruedasanofficialactionoropinion of
2、the American Gear Manufacturers Association.AbstractIn todays global economy, there is more and more pressure from the developing counties to produce gearsat agreaterefficiently and atalower cost. Carbidehobbing seemsas oneof thetechnological innovationsthat could give both theproductivity thus furt
3、her increasing cycle times and reducing productivity. On average, there was less than one setup per machine per day. The inexpensive conventional off-the-shelf “square” hobs had to be re-sharpened quite frequently, thus disrupting production flow. Lean manufacturing stresses the importance of JIT ma
4、nufacturing and continuous reduction of WIP. This leads to smaller lot sizes and greater setup frequency per day. 4 In summary, we had an abundance of opportunities. Quality improvements Process capability improvements Further tightening of the tolerances to produce a higher quality product Producti
5、vity improvements Reduce cycle times and increase production with the same number of people Reduce setup time Reduce process debugging time Cost improvements Cost reductions as a result of productivity improvements Lower cutting tool cost per gear or keeping it the same as HSS Reduction in rework co
6、st Additional Capacity Skiving Capabilities Reduction in outsourcing 2. Considerations for new technology We couldve benefited by improving the process in small incremental changes. Some examples are reworking the machines, buying better cutting tools, improving the fixtures, buying better blanks, a
7、nd even stressing greater control of our processes. These wouldve all brought some semblance of success. Nonetheless, we felt that we needed drastic, rather than incremental, improvement to bring the process under control and achieve cost reduction. This is why we decided to blow up everything, inve
8、stigate new carbide hobbing technology, and bring a new spirit into the factory. At the same time, we wanted to bring in technology that would work from the onset. We wanted to be conservative in our estimates; making sure that there would not be excessive process debugging. So we decided that a tes
9、t would be the ideal first step into a successful implementation of new carbide hobbing technology. 3. Hobbing Test Test Objectives. To learn more about potential challenges To understand the pros and cons of carbide hobbing as applicable to our pitch and size ranges To have the process debugged pri
10、or to purchasing the machine To specify the machine acceptance criteria based on challenges experienced during testing To compare machine suppliers To start a process of developing carbide hobbing support systems We anticipated a need for a better engineering support systems as well as a simpler, mo
11、re disciplined, process monitoring system that would give us a reliable feedback. We knew that after the major investment, the flat gear cell would be scrutinized under a microscope. Test Findings what was the best coating for our application; what was the optimum wear; what were the sharpening nuan
12、ces (i.e. edge preparation); when was the right time to strip the coating and was it possible; what was the hob life and tool cost per gear; and was there any predictability in carbide hobbing? NDP ODToothed length # gashes # startsAxial Pitch LA# cutting edgesHandTypeCurrent Total/Sharpening88964 6
13、25Material SupplierOrigin al coatingTotal Accum. # gears20 1.875 2.650 12 1 0.157 1.61 142 LHFinish Non-TopTarget Total/Sharpening35591 250 Carbide KGPHCTFurura TiAlN12127Hobbing Start Hobbing End Material Removal Hob SharpeningDateSetup Person Gear # DateSetup PersonNo. Gears madeDamage NoteGear fa
14、ceNo of teethHelix AnglePer Setup, inchPer sharpening, inchInch per Cutting edgeDate SentCompany NameTooth thickness beforeTooth thickness afterNew CoatingDate Received10/25/99 1103 26300026 10/26/99 1103 765 0.503 38 18.18 15391 15391 10811/1/99 2331 26301180 11/01/99 2331 78 0.505 48 18.18 1990 17
15、381 12211/5/99 2331 26300026 11/05/99 1103 768 0.503 38 18.18 15451 32832 23111/30/99 2331 26300026 12/02/99 2331 782 0.503 38 18.18 15733 48565 34112/2/99 2331 26301180 12/02/99 Walter 246 0.505 48 18.18 6276 54841 385 12/8/99 GPHCT2 0.272 0.265 TiAlN 12/23/992/9/00 1130 26301180 02/09/00 1130 238
16、0.505 48 18.18 6072 6072 433/28/00 1130 26330828 03/28/00 1130 104 0.605 54 16.27 3539 9612 684/24/00 1103 26300026 04/24/00 1130 770 0.503 38 18.18 15491 25103 1764/29/00 2331 26330136 04/29/00 2331 296 0.505 48 18.18 7552 32655 2295/11/00 1130 26300026 05/11/00 1130 724 0.503 38 18.18 14566 47221
17、3325/17/00 1130 26300026 05/18/00 1103 720 0.503 38 18.18 14485 61707 4336/6/00 1103 26300026 06/06/00 WALTER 724 0.503 38 18.18 14566 76273 5367/5/00 walter 26330136 07/05/00 walter 288 0.505 48 18.18 7348 83621 5877/8/00 walter 26300026 07/08/00 2331 748 0.503 38 18.18 15049 98669 6937/24/00 2331
18、26300026 07/24/00 1620 720 0.503 38 18.18 14485 113155 795 7/27/00 GCT2 0.263 0.248 TiAlN 08/11/0010/30/00 dan 26300026 10/30/00 Walter 486 0.503 38 18.18 9778 9778 6911/10/00 dan 26300026 11/10/00 Walter 490 0.503 38 18.18 9858 19636 13811/16/00 dan 26330136 11/16/00 dan 236 0.505 48 18.18 6021 256
19、57 18011/22/00 dan 26300026 11/27/00 Walter 964 0.503 38 18.18 19394 45052 31612/12/00 walter 26300026 12/13/00 dan 484 0.503 38 18.18 9737 54789 3852/12/01 2331 26300045 02/12/01 Walter 214 0.299 32 28.35 2327 57116 4013/8/01 dan 26301180 03/08/01 Walter 994 0.505 48 18.18 25361 82477 5793/12/01 da
20、n 26300026 03/12/2001walter 150 0.503 38 18.18 3018 85494 6013/12/01 walter 26301143 03/12/01 walter 112 0.505 48 21.03 2909 88403 6213/12/01 walter 26300027 03/12/01 Walter 26 0.503 40 21.03 560 88964 62510 Here is an example of one of the many challenges that we experienced. Coating fractures can
21、contribute to poor hob performance. Coating on the illustration is breaking away from the tool. Close inspection within these areas exhibit multiple coating layers that chipped on the outer surface, while the lower coating layers have remained intact. Layer Buildup. Each coating is approximately .00
22、04”. Top layer is AlNite coating, a single layer of TiAlN. Two layers of Futura coating, each 27 to 35 alternating sub layers of Titanium Nitride (TiN) and Titanium Aluminum Nitride (TiAlN). Yellow lines between layers is TiN. Light colored substrate is near the bottom. We have yet to find overall c
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