Dây phun hồ quang tafa - usa
Wire Name |
Material |
Diameter |
Coverage (/ft2/0.001") (/m2/100 µm) |
Spray Rate (/h/100 A) |
Approved Specs |
Application Data |
AI-1800 |
Nickel Aluminum Molybdenum |
1/16" (1.6 mm) |
0.8 oz |
10 lbs |
|
• Bond Coat • Oxidation, Shock and Abrasion Resistance |
1.0 kg |
4.5 kg |
|||||
|
|
|||||
Alcro |
Iron Chrome Aluminum |
1/16" (1.6 mm) |
0.8 oz |
10 lbs |
|
• Good for Buildup • Excellent Wear Resistance |
1.0 kg |
4.5 kg |
|||||
01A |
Aluminum 12% Silicon |
1/16" (1.6 mm) |
0.3 oz |
6 lbs |
AWS C2.25/C2.25M PWA 36935 (PWA 271-35 Rev G) GE B50TF92 (Chemical Composition) |
• Dimensional Restoration • Aircraft Approved |
0.3 kg |
2.8 kg |
|||||
|
|
|||||
|
|
|||||
|
|
|||||
01P |
Aluminum 1100 |
11gauge (2.3 mm) |
0.3 oz |
6 lbs |
AWS C2.25/C2.25M |
• Corrosion Protection |
1/8" (3.2 mm) |
0.3 kg |
2.8 kg |
||||
01S |
Aluminum 6% Silicon |
1/16" (1.6 mm) |
0.3 oz |
6 lbs |
AWS C2.25/C2.25M FP5045 Type VIII, Rev AB |
• Dimensional Restoration • Aircraft Approved |
|
0.3 kg |
2.8 kg |
||||
01T |
Aluminum |
1/16" (1.6 mm) |
0.3 oz |
6 lbs |
AWS C2.25/C2.25M FP5045 Type VI, Rev AB GE Manual # 70-49-40 (Alternate to 70-49-01) |
• Corrosion Protection • Electrical Conductivity • Aircraft Approved |
1/8" (3.2 mm) |
0.3 kg |
2.8 kg |
||||
|
|
|
||||
|
|
|
||||
02A |
Zinc Aluminum |
2 mm |
0.8 oz |
21 lbs |
|
• Corrosion Protection |
11gauge (2.3 mm) |
1.0 kg |
9.5 kg |
||||
1/8" (3.2 mm) |
|
|
||||
3/16" (4.8 mm) |
|
|
||||
02T |
Zinc Tin |
2 mm |
0.9 oz |
45 lbs |
|
• Capacitors: Solderable Coating |
|
1.1 kg |
20.4 kg |
||||
02W |
Pure Tin |
2 mm |
0.9 oz |
50 lbs |
AWS C2.25/C2.25M |
• Sputtering Targets • Electrical Contacts • EMI/RFI Shielding |
|
1.1 kg |
22.7 kg |
||||
|
|
|
||||
02Z |
Zinc |
1/16" (1.6 mm) |
0.9 oz |
21 lbs |
AWS C2.25/C2.25M |
• Corrosion • EMI/RFI Shielding • Electrical Conductivity |
2 mm |
1.1 kg |
9.5 kg |
||||
1/8" (3.2 mm) |
|
|
||||
3/16" (4.8 mm) |
|
|
||||
04T |
Babbitt |
1/16" (1.6 mm) |
0.9 oz |
50 lbs |
AWS C2.25/C2.25M |
• Bearing Reclamation • Capacitors |
2 mm |
1.1 kg |
22.7 kg |
||||
1/8" (3.2 mm) |
|
|
||||
05T |
Copper |
1/16" (1.6 mm) |
0.9 oz |
11 lbs |
|
• Electric Conductivity • Copper Reclamation • Decorative Coatings |
1/8" (3.2 mm) |
1.1 kg |
5.0 kg |
||||
|
|
|
||||
06C |
Nickel Chrome |
1/16" (1.6 mm) |
0.8 oz |
11 lbs |
Conforms to PWA 1317D |
• Oxidation Resistance • Aircraft Approved |
|
1.0 kg |
5.0 kg |
||||
06T |
Nickel |
1/16" (1.6 mm) |
0.8 oz |
10 lbs |
AWS C2.25/C2.25M |
• Corrosion Protection at High Temperatures |
|
1.0 kg |
4.5 kg |
||||
10T |
Aluminum Bronze |
1/16" (1.6 mm) |
0.9 oz |
9 lbs |
|
• Bond Coat • Reclamation • Cavitation • Aircraft Approved |
1/8" (3.2 mm) |
1.1 kg |
4.1 kg |
||||
|
|
|
||||
|
|
|
||||
11T |
Aluminum Bronze Nickel |
1/16" (1.6 mm) |
0.9 oz |
9 lbs |
|
• Cavitation • Reclamation of Sliding Components • Corrosion Protection |
|
1.1 kg |
4.1 kg |
||||
|
|
|
||||
|
|
|
||||
12T |
Brass |
1/16" (1.6 mm) |
0.9 oz |
9 lbs |
|
• Use Where Tobin Bronze is Required • Pump Impellers • Bronze Castings |
|
1.1 kg |
4.1 kg |
||||
|
|
|
||||
|
|
|
||||
13T |
Molybdenum |
1/16" (1.6 mm) |
1.1 oz |
10 lbs |
PWA 36913 (PWA 271-13 Rev F) AWS C2.25/C2.25M MSSR 9507/102 |
• Galling and Scuffing Resistance • Aircraft Approved |
1/8" (3.2 mm) |
1.3 kg |
4.5 kg |
||||
|
|
|
||||
14T |
Titanium |
1/16" (1.6 mm) |
0.4 oz |
3 lbs |
ASTM B348/Grade 1 ASTM F67-89/Grade 1 (Chemical Composition) |
• Medical Implants |
|
0.5 kg |
1.4 kg |
||||
|
|
|
||||
16T |
Silicon Bronze |
1/16" (1.6 mm) |
0.9 oz |
9 lbs |
|
• Cosmetic Repairs • Decorative Coatings • Automotive Approved |
|
1.1 kg |
4.1 kg |
||||
|
|
|
||||
30S |
Silver Copper Zinc |
1/16" (1.6 mm) |
1.0 oz |
12 lbs |
GE B20A4 (Chemical Composition) GE Manual # 70-49-44 FAA RDE#00-630 CFM70-48-16-340-007 |
• Stationary Seals in Aircraft Engines • Good Rub Wear Characteristics |
|
1.2 kg |
5.4 kg |
||||
|
|
|
||||
|
|
|
||||
30T |
Low Carbon Steel |
1/16" (1.6 mm) |
0.9 oz |
10 lbs |
|
• Dimensional Restoration of Mismachined and Worn Parts |
|
1.1 kg |
4.5 kg |
||||
38T |
High Carbon Steel (0.80 C) |
1/16" (1.6 mm) |
0.9 oz |
10 lbs |
AWS C2.25/C2.25M |
• Reclamation • Wear and Erosion Resistance • ID Fans |
|
1.1 kg |
4.5 kg |
||||
|
|
|
||||
39T |
High Carbon Steel (1.0 C) |
1/16" (1.6 mm) |
0.9 oz |
10 lbs |
|
• Excellent Wear Resistance • Harder than 38T |
|
1.1 kg |
4.5 kg |
||||
45CT® |
Nickel Chrome Titanium |
1/16" (1.6 mm) |
0.9 oz |
11 lbs |
|
• Protection Against High Temperature Sulfidation |
|
1.1 kg |
5.0 kg |
||||
55T |
18/5 Stainless 200 Series Stainless |
1/16" (1.6 mm) |
0.8 oz |
10 lbs |
AWS C2.25/C2.25M FP5045 Type IV, Rev AB |
• Low Carbon • Low Shrinkage • Good Machinability • Aircraft Approved |
1/8" (3.2 mm) |
1.0 kg |
4.5 kg |
||||
|
|
|
||||
|
|
|
||||
58T |
Copper Nickel Indium |
1/16" (1.6 mm) |
0.8 oz |
10 lbs |
GE B50TF72 CL A (Chemical Composition) GE Manual #70-49-05 |
• Fretting Resistance • Dense, Low Oxide Coatings • Aircraft Approved |
|
1.0 kg |
4.5 kg |
||||
|
|
|
||||
60T |
420 Stainless Steel |
1/16" (1.6 mm) |
0.8 oz |
10 lbs |
AWS C2.25/C2.25M OMAT#3/45D FP5045 Type V, Rev AB |
• Reclamation • Low Shrinkage Allows Thick Buildups • Good Wear Resistance • Aircraft Approved |
1/8" (3.2 mm) |
1.0 kg |
4.5 kg |
||||
|
|
|
||||
61T |
430 Stainless Steel |
1/16" (1.6 mm) |
0.8 oz |
10 lbs |
|
• Slightly More Machinable and Better Corrosion Resistance than 60T |
|
1.0 kg |
4.5 kg |
||||
|
|
|
||||
70T |
Nickel Copper |
1/16" (1.6 mm) |
0.8 oz |
10 lbs |
AWS C2.25/C2.25M |
• Marine Corrosion Protection • Print Rolls |
|
1.0 kg |
4.5 kg |
||||
71T |
Nickel Chrome Molybdenum |
1/16" (1.6 mm) |
0.8 oz |
11 lbs |
|
• Prohibits Caustic Corrosion • Paper Mill Digesters |
|
1.0 kg |
5.0 kg |
||||
75B® |
BondArc® Nickel 5% Aluminum |
1/16" (1.6 mm) |
0.9 oz |
10 lbs |
PWA 36937 (PWA 271-37 Rev F) GE Manual # 70-49-38 (Alternate to 70-49-10) OMAT#3/229 FP5045 Type XV, Rev AB BF Goodrich Ltr 1623 CFM 70-48-14-340-005 AWS C2.25/C2.25M |
• Bond Coat • Aircraft Approved • Oxidation /Abrasion Resistance at High Temperatures |
|
1.1 kg |
4.5 kg |
||||
|
|
|
||||
|
|
|
||||
77T |
Alloy C-276 type: Nickel Chrome Molybdenum |
1/16" (1.6 mm) |
0.9 oz |
11 lbs |
|
• Acidic and Hot Gas Corrosion Resistance |
|
1.1 kg |
5.0 kg |
||||
|
|
|
||||
78T |
Alloy 718 type: Nickel Chrome Molybdenum |
1/16" (1.6 mm) |
0.8 oz |
11 lbs |
GE Manual # 70-49-45 CFM 70-48-17-340-008 |
• Aircraft Engine Dimensional Restoration • Acidic and Hot Gas Corrosion Resistance |
|
1.0 kg |
5.0 kg |
||||
|
|
|
||||
|
|
|
||||
79B |
Nickel 20% Aluminum |
1/16" (1.6 mm) |
0.9 oz |
10 lbs |
OMAT#3/90A FP5045 Type II, Rev AB |
• High Temperature Oxidation and Abrasion Resistance • Aircraft Approved |
1/8" (3.2 mm) |
1.1 kg |
4.5 kg |
||||
|
|
|
||||
80T |
18/8 Stainless Steel 304 Series Stainless |
1/16" (1.6 mm) |
0.8 oz |
10 lbs |
AWS C2.25/C2.25M |
• Corrosion Protection • Dimensional Restoration • Print Rolls |
|
1.0 kg |
4.5 kg |
||||
|
|
|
||||
85T |
316 Stainless Steel |
1/16" (1.6 mm) |
0.8 oz |
10 lbs |
|
• Corrosion Protection • Dimensional Restoration |
|
1.0 kg |
4.5 kg |
||||
88T |
300 Series Stainless |
1/16" (1.6 mm) |
0.8 oz |
9.5 lbs |
|
• Corrosion Protection • Dimensional Restoration • Print Rolls |
|
1.0 kg |
4.3 kg |
||||
|
|
|
||||
204M |
Kirksite type |
1/16" (1.6 mm) |
0.8 oz |
22 lbs |
Proprietary Alloy |
• Used to Create Metal Faced Tooling |
|
1.0 kg |
10 kg |
||||
35 MXC® |
Iron-based High Carbon Alloy |
1/16" (1.6 mm) |
0.8 oz |
8.5 lbs |
|
• Traction and Anti-Skid Coatings • Wear Resistance |
|
1.0 kg |
3.9 kg |
||||
37 MXC |
Iron Chrome Carbon |
1/16" (1.6 mm) |
1.0 oz |
8 lbs |
|
• High Hardness • Excellent Wear Resistance |
|
1.2 kg |
3.6 kg |
||||
73 MXC |
Nickel Chrome Aluminum |
1/16" (1.6 mm) |
0.8 oz |
8.5 lbs |
PWA 36947 (PWA 271-47 Rev F) MSSR 9507/14 GE Manual # 70-49-39 (Alternate to 70-49-21) FP5045 Type XVIII, Rev AB |
• Oxidation and Corrosion Resistance • Aircraft Approved |
|
1.0 kg |
3.9 kg |
||||
|
|
|
||||
74 MXC |
Nickel Aluminum Molybdenum |
1/16" (1.6 mm) |
0.8 oz |
8.5 lbs |
MSSR 9507/35 GE B50TF166 (Chemical Composition) FP5045 Type XVI, Rev AB |
• Medium Hardness for Bearing Wear Applications • Particle Erosion Resistance • Aircraft Approved |
|
1.0 kg |
3.9 kg |
||||
76 MXC |
Nickel Chrome Aluminum Yttrium |
1/16" (1.6 mm) |
0.8 oz |
7 lbs |
GE B50TF296 (Chemical Composition) |
• Bond Coat to Ceramics • Oxidation and Heat Resistance • Aircraft Approved |
|
1.0 kg |
3.2 kg |
||||
90 MXC |
Iron Chrome Nickel |
1/16" (1.6 mm) |
1.0 oz |
7 lbs |
|
• Corrosion and Wear Protection |
|
1.2 kg |
3.2 kg |
||||
95 MXC |
Iron Chrome Boron |
1/16" (1.6 mm) |
1.0 oz |
8 lbs |
|
• Corrosion and Wear Protection • ID Fans • Boiler Tubes |
|
1.2 kg |
3.6 kg |
||||
96 MXC |
Iron Nickel Chrome |
1/16" (1.6 mm) |
1.0 oz |
7.5 lbs |
|
• High Temperature Corrosion Protection • Abrasion Resistance |
|
1.2 kg |
3.4 kg |
||||
97 MXC |
Nickel Chrome Tungsten Carbide Iron |
1/16" (1.6 mm) |
1.0 oz |
6.5 lbs |
|
• Abrasion and Wear Resistance |
|
1.2 kg |
3.0 kg |
||||
98 MXC |
Iron Chrome Nickel |
1/16" (1.6 mm) |
1.0 oz |
8 lbs |
|
• Corrosion and Wear Protection |
|
1.2 kg |
3.6 kg |
||||
106 MXC |
Cobalt Nickel Chrome Tungsten |
1/16" (1.6 mm) |
0.9 oz |
6.5 lbs |
|
• Abrasion and Fretting Resistance in High Temperature Environments |
|
1.1 kg |
3.0 kg |
||||
444 MXC |
Nickel Chrome Aluminum Molybdenum |
1/16" (1.6 mm) |
0.8 oz |
8.5 lbs |
EMS 56762 |
• Wear and Corrosion Resistance • Dimensional Restoration of Bearing Areas |
|
1.0 kg |
3.9 kg |