-rw-r--r-- | fanduct.scad | 3 |
1 files changed, 2 insertions, 1 deletions
diff --git a/fanduct.scad b/fanduct.scad index 690a4c8..8d0414f 100644 --- a/fanduct.scad +++ b/fanduct.scad | |||
@@ -31,25 +31,26 @@ fanduct_elevation = 3; // fanduct elevation above nozzle tip | |||
31 | fanduct_blowtarget = -2; // what to blow at | 31 | fanduct_blowtarget = -2; // what to blow at |
32 | fanduct_h = 6; // inner height of the duct | 32 | fanduct_h = 6; // inner height of the duct |
33 | fanduct_w = 7; // inner width of the duct | 33 | fanduct_w = 7; // inner width of the duct |
34 | fanduct_shell=1.2; // shell thickness | 34 | fanduct_shell=1.2; // shell thickness |
35 | fanduct_ir = heater_clearance+5; // inner radius | 35 | fanduct_ir = heater_clearance+5; // inner radius |
36 | 36 | ||
37 | jet_angle = 60-2; // angular width of the jet | 37 | jet_angle = 60-2; // angular width of the jet |
38 | 38 | ||
39 | hotend_clearance = heater_clearance; | 39 | hotend_clearance = heater_clearance; |
40 | 40 | ||
41 | snapper_d = 8; snapper_overlap=0.2;// snip snap | 41 | snapper_d = 8; snapper_overlap=0.2;// snip snap |
42 | 42 | ||
43 | smooth_f = 120; | 43 | draft=true; |
44 | smooth_f = draft? 30 : 120; | ||
44 | 45 | ||
45 | to_midduct = fanduct_ir+fanduct_shell+fanduct_w/2; | 46 | to_midduct = fanduct_ir+fanduct_shell+fanduct_w/2; |
46 | dual_spots = [ [+space_behind_nozzle, -(to_midduct+nozzles_apart/2)], | 47 | dual_spots = [ [+space_behind_nozzle, -(to_midduct+nozzles_apart/2)], |
47 | [- to_midduct, -(to_midduct+nozzles_apart/2)], | 48 | [- to_midduct, -(to_midduct+nozzles_apart/2)], |
48 | [- to_midduct, 0] ]; | 49 | [- to_midduct, 0] ]; |
49 | 50 | ||
50 | module fanduct(type=type,ductshape=ductshape,dual=dual) { | 51 | module fanduct(type=type,ductshape=ductshape,dual=dual) { |
51 | // ***duct is all around! | 52 | // ***duct is all around! |
52 | module duct(what) { | 53 | module duct(what) { |
53 | module single() { | 54 | module single() { |
54 | if(what=="in") { | 55 | if(what=="in") { |
55 | sh = fanduct_w+2*fanduct_shell; sv = fanduct_h+2*fanduct_shell; | 56 | sh = fanduct_w+2*fanduct_shell; sv = fanduct_h+2*fanduct_shell; |