Каталог Stellram фрез со сменными пластинами - страница 256
Навигация
Каталог Stellram твердосплавные цельные фрезы
Каталог Stellram токарный инструмент
Каталог Stellram системы со сменными пластинами для фрезерования с высокими подачами
Каталог Stellram высокопроизводительные фрезерные системы
Каталог Stellram материалы и сплавы
5702VZD & 5720VZ
Machinability by Materials (Aluminium)
| Alloy G | Alloy Diti | CHE | MICAL CO | MPOSITIO | N LIMITS | (WT%) | Typical | Rm | Machinability | Machinability | Typical | vcm/min | fzmm/Z | |||||
| roup | esgnaon | Cu | Si | Fe | Mn | Mg | Zn | Cr | Ti Pb Bi | Al | Others | tremper | (Mpa) | Chip formation | Applications | min. - max. | max. | |
| Al | 1050 1100 | 0.05 0.05~0.20 | 0.25 Si+Fe1.0ma | 0.4 x | 0.5 0.05 | 0.05 - | 0.05 0.1 | - - | - - - - - - | 99.50min 99.00min | - - | H14 H14 | 105 90 | D D | A A | Chemical equipment Sheet metal work Coiled tube | 600 - 3000 | 0,2 |
| 2011 | 50.~60. | 0.4 | 0.7 | - | - | 0.3 | - | - 0.2 0.6 | remaining | - | T3 | 310 | A | A | ||||
| 2014 | 3.9~5.0 | 0.5~1.2 | 0.7 | 0.4~1.2 | 0.2~0.8 | 0.25 | 0.1 | 0.15 - - | remaining | - | T6 | 430 | B | A | Screw machine products | . | ||
| AlC | 2017 | 3.5~4.5 | 0.2~0.8 | 0.7 | 0.4~1.0 | 0.4~0.8 | 0.25 | 0.1 | 0.15 - - | remaining | - | T4 | 390 | B | A | Tuck frame. Aircraft structure. | 400 2500 | 025 |
| -u | 2024 | 3.8~4.9 | 0.5 | 0.5 | 0.3~0.9 | 1.2~1.8 | 0.25 | 0.1 | 0.15 - - | remaining | - | T4 | 465 | B | A | Jet engine impellers. Aircraft engine | - | , |
| 2218 | 3.5~4.5 | 0.9 | 1 | 0.2 | 1.2~1.8 | 0.25 | 0.1 | - - - | remaining | Ni1.7~2.3 | T72 | 331 | B | B | cylinder heads. | |||
| 2224 | 3.8~4.4 | 0.12 | 0.15 | 0.30~0.9 | 1.2~1.8 | 0.25 | 0.1 | 0.15 - - | remaining | - | A | A | ||||||
| Al-Mn | 3003 | 0.05~0.20 | 0.6 | 0.7 | 1.0~1.5 | - | 0.1 | - | - - - | remaining | - | H14 | 140 | D | B | Cooking utensils. Chemical equipment. | 200 - 2500 | 0,2 |
| Al-Si | 4032 | 0.5~1.3 | 11.0~13.5 | 1 | - | 0.8~1.3 | 0.25 | 0.1 | - - - | remaining | Ni0.5~1.3 | T6 | 379 | B | D | Pistons. | 200 - 1000 | 0,18 |
| 5052 | 0.1 | 0.25 | 0.4 | 0.1 | 2.2~2.8 | 0.1 | 0.15~0.3 | 5 - - - | remaining | - H34 | H14 | 260 | C | A | Architectural. | |||
| 5056 | 0.1 | 0.3 | 0.4 | 0.05~0.20 | 4.5~5.6 | 0.1 | 0.05~0.2 | 0 - - - | remaining | - | H12 | 300 | C | A | Cable Sheeting. Welded pressure | |||
| Al-Mg | H32 | vessels. Hydraulic tubes | 400 - 3000 . | 0,25 | ||||||||||||||
| 5083 | 0.1 | 0.4 | 0.4 | 0.4~1.0 | 4.0~4.9 | 0.25 | 0.05~0.2 | 5 0.15 - - | remaining | - | H112 | 335 | C | A | Transportation | |||
| 5086 | 0.1 | 0.4 | 0.5 | 0.20~0.7 | 3.5~4.5 | 0.25 | 0.05~0.2 | 5 0.15 - - | remaining | - H116 | H32 | 300 | C | A | equipment. | |||
| 6061 | 0.15~0.40 | 0.4~0.8 | 0.7 | 0.15 | 0.8~1.2 | 0.25 | 0.04~0.3 | 5 0.15 - - | remaining | - | T6 | 300 | C | B | ||||
| 6063 | 0.1 | 0.2~0.6 | 0.35 | 0.1 | 0.45~0.9 | 0.1 | 0.1 | 0.1 - - | remaining | - | T5 | 200 | C | B | ||||
| 6070 | 0.15~0.40 | 1.0~1.7 | 0.5 | 0.40~1.0 | 0.50~1.2 | 0.25 | 0.1 | 0.15 - - | remaining | - | T6 | 379 | C | C | Heavy duty structure. Furniture Architectural | |||
| Al-Mg-Si | 6151 | 0.35 | 0.6~1.2 | 1 | 0.2 | 0.45~0.8 | 0.25 | 0.15~0.3 | 5 0.15 - - | remaining | - | T6 | C | C | . . Heavy duty welded | 400 - 2500 | 0,2 | |
| 6262 | 0.15~0.40 | 0.4~0.8 | 0.7 | 0.15 | 0.8~1.2 | 0.25 | 0.04~0.1 | 4 0.15 0.4 0.7 | remaining | - | T9 | 400 | B | B | structure. Pipeline. Heat Sink. | |||
| 6351 | 0.1 | 0.7~1.3 | 0.5 | 0.4~0.8 | 0.40~0.8 | 0.2 | - | 0.2 - - | remaining | - | T6 | 310 | D | C | ||||
| 6463 | 0.2 | 0.20~0.6 | 0.15 | 0.05 | 0.45~0.9 | 0.05 | - | - - - | remaining | - | T6 | 241 | C | B | ||||
| 7001 | 1.6~2.6 | 0.35 | 0.4 | 0.2 | 2.6~3.4 | 6.8~8.0 | 0.18~0.3 | 5 0.2 - - | remaining | - | O | B | A | |||||
| 7003 | 0.2 | 0.3 | 0.35 | 0.3 | 0.50~1.0 | 5.0~6.5 | 0.2 | 0.2 - - | remaining | Zr0.05~0.25 | T5 | 400 | B | A | ||||
| 7050 | 2.0~2.6 | 0.12 | 0.15 | 0.1 | 1.9~2.6 | 5.7~6.7 | 0.04 | 0.06 - - | remaining | Zr0.08~0.15 | T73 | 530 | B | A | High strength structure. | |||
| Al-Zn | 7075 | 1.2~2.0 | 0.4 | 0.5 | 0.3 | 2.1~2.9 | 5.1~6.1 | 0.18~0.2 | 8 0.2 - - | remaining | - | T6 | 570 | B | A | Aircraft structure. Bat. | 400 - 3000 | 0,25 |
| 7178 | 1.6~2.4 | 0.4 | 0.5 | 0.3 | 2.4~3.1 | 6.3~7.3 | 0.18~0.3 | 5 0.2 - - | remaining | - | T6 | 600 | B | A | ||||
| 7475 | 1.2~1.9 | 0.1 | 0.12 | 0.06 | 1.9~2.6 | 5.2~6.2 | 0.18~0.2 | 5 0.06 - - | remaining | - | T61 | 565 | B | A |
Machinability
A EXCELLENT
B GOOD-TO-EXCELLENT
C GOOD
D NOT GOOD
Vc = π x D x n / 1000 m/min = mm x RPM
: Cutting speed, π = 3.1416
D: Tool diameter, N: RPM, Vc
Choose a cutting speed in the range of values, compatible with
the cutter max rotation capacity (engraved on the body)
and your spindle stability.