X-Git-Url: https://git.gag.com/?a=blobdiff_plain;f=packages%2FZX62-B-5PA.py;h=4a3f16d480e71078ef1a5b92ce9ec53d338e227a;hb=4aab2096873a554562985db3a16cc4804a778827;hp=6e4b533e9ed451adea4ffb380f7ace444f8d43b4;hpb=656ae294b1b46e0d56fbf9407c5efe27b4b3b28f;p=hw%2Faltusmetrum diff --git a/packages/ZX62-B-5PA.py b/packages/ZX62-B-5PA.py index 6e4b533..4a3f16d 100755 --- a/packages/ZX62-B-5PA.py +++ b/packages/ZX62-B-5PA.py @@ -32,6 +32,11 @@ BoxWidth = 7.9 EdgeHeight = 4.8 EdgeWidth = 2 * (WingInner + WingWidth) +# freedfm.com round-off error bites us if we make this 700... +MinAnnular = 725 +MinClearance = 600 +MaskDelta = 300 + import sys # we're going to use the 1/100 of a mil fundamental unit form @@ -51,8 +56,8 @@ print ' Pad[', \ mm2mils100(0), \ mm2mils100(PinHeight - PinWidth/2), \ mm2mils100(PinWidth), \ - mm2mils100(PinSpacing - PinWidth), \ - mm2mils100(PinWidth + 0.2), \ + (MinClearance*2), \ + mm2mils100(PinWidth)+(MaskDelta*2), \ '"D+" "3" 0x0100]' print ' Pad[', \ @@ -61,8 +66,8 @@ print ' Pad[', \ mm2mils100(-PinSpacing), \ mm2mils100(PinHeight - PinWidth/2), \ mm2mils100(PinWidth), \ - mm2mils100(PinSpacing - PinWidth), \ - mm2mils100(PinWidth + 0.2), \ + (MinClearance*2), \ + mm2mils100(PinWidth)+(MaskDelta*2), \ '"D-" "2" 0x0100]' print ' Pad[', \ @@ -71,8 +76,8 @@ print ' Pad[', \ mm2mils100(PinSpacing), \ mm2mils100(PinHeight - PinWidth/2), \ mm2mils100(PinWidth), \ - mm2mils100(PinSpacing - PinWidth), \ - mm2mils100(PinWidth + 0.2), \ + (MinClearance*2), \ + mm2mils100(PinWidth)+(MaskDelta*2), \ '"HS" "4" 0x0100]' print ' Pad[', \ @@ -81,8 +86,8 @@ print ' Pad[', \ mm2mils100(-PinSpacing*2), \ mm2mils100(PinHeight - PinWidth/2), \ mm2mils100(PinWidth), \ - mm2mils100(PinSpacing - PinWidth), \ - mm2mils100(PinWidth + 0.2), \ + (MinClearance*2), \ + mm2mils100(PinWidth)+(MaskDelta*2), \ '"VBUS" "1" 0x0100]' print ' Pad[', \ @@ -91,8 +96,8 @@ print ' Pad[', \ mm2mils100(PinSpacing*2), \ mm2mils100(PinHeight - PinWidth/2), \ mm2mils100(PinWidth), \ - mm2mils100(PinSpacing - PinWidth), \ - mm2mils100(PinWidth + 0.2), \ + (MinClearance*2), \ + mm2mils100(PinWidth)+(MaskDelta*2), \ '"GND" "5" 0x0100]' # the two ground / mounting tabs in line with signal pins @@ -103,8 +108,8 @@ print ' Pad[', \ mm2mils100(TabInner + TabWidth - TabHeight/2), \ mm2mils100(TabHeight/2), \ mm2mils100(TabHeight), \ - mm2mils100(PinSpacing - PinWidth), \ - mm2mils100(TabHeight + 0.2), \ + (MinClearance*2), \ + mm2mils100(TabHeight)+(MaskDelta*2), \ '"tab1" "G" 0x0100]' print ' Pad[', \ @@ -113,8 +118,8 @@ print ' Pad[', \ mm2mils100(-TabInner - TabWidth + TabHeight/2), \ mm2mils100(TabHeight/2), \ mm2mils100(TabHeight), \ - mm2mils100(PinSpacing - PinWidth), \ - mm2mils100(TabHeight + 0.2), \ + (MinClearance*2), \ + mm2mils100(TabHeight)+(MaskDelta*2), \ '"tab2" "G" 0x0100]' # the two ground / mounting tabs near the center of area @@ -125,8 +130,8 @@ print ' Pad[', \ mm2mils100(PadInner + PadWidth - PadHeight/2), \ mm2mils100(PadCenter), \ mm2mils100(PadHeight), \ - mm2mils100(PinSpacing - PinWidth), \ - mm2mils100(PadHeight + 0.2), \ + (MinClearance*2), \ + mm2mils100(PadHeight)+(MaskDelta*2), \ '"tab3" "G" 0x0100]' print ' Pad[', \ @@ -135,8 +140,8 @@ print ' Pad[', \ mm2mils100(-PadInner - PadWidth + PadHeight/2), \ mm2mils100(PadCenter), \ mm2mils100(PadHeight), \ - mm2mils100(PinSpacing - PinWidth), \ - mm2mils100(PadHeight + 0.2), \ + (MinClearance*2), \ + mm2mils100(PadHeight)+(MaskDelta*2), \ '"tab4" "G" 0x0100]' # the two "wing tab" ground / mounting pads on the sides @@ -147,8 +152,8 @@ print ' Pad[', \ mm2mils100(WingInner + WingWidth/2), \ mm2mils100(PadCenter + WingHeight/2 - WingWidth/2), \ mm2mils100(WingWidth), \ - mm2mils100(PinSpacing - PinWidth), \ - mm2mils100(WingWidth + 0.2), \ + (MinClearance*2), \ + mm2mils100(WingWidth)+(MaskDelta*2), \ '"tab5" "G" 0x0100]' print ' Pad[', \ @@ -157,8 +162,8 @@ print ' Pad[', \ mm2mils100(-WingInner - WingWidth/2), \ mm2mils100(PadCenter + WingHeight/2 - WingWidth/2), \ mm2mils100(WingWidth), \ - mm2mils100(PinSpacing - PinWidth), \ - mm2mils100(WingWidth + 0.2), \ + (MinClearance*2), \ + mm2mils100(WingWidth)+(MaskDelta*2), \ '"tab6" "G" 0x0100]' # box around actual connector size, with line at PCB edge