F/T DAQ Installation and Operation Manual
Document #9610-05-1017-06
ATI Industrial Automation, 1031 Goodworth Drive, Apex, NC 27539 USA +1-919-772-0115 www.ati-ia.com
40
7.2.6 Gamma
En
lish
US
Metric
SI
Calibration US-7.5-25 US-15-50 US-30-100 SI-32-2.5 SI-65-5 SI-130-10
Rated Sensin
Ran
es
Fx, Fy ±7.5 lb ±15 lb ±30 lb ±32 N ±65 N ±130 N
Fz ±25 lb ±50 lb ±100 lb ±100 N ±200 N ±400 N
Tx, Ty, Tz ±25 in-lb ±50 in-lb ±100 in-lb ±2.5 Nm ±5 Nm ±10 Nm
Resolution*
Fx, Fy 1/2560 lb 1/1280 lb 1/640 lb 1/640 N 1/320 N 1/160 N
Fz 1/1280 lb 1/640 lb 1/320 lb 1/320 N 1/160 N 1/80 N
Tx, Ty 1/1280 in-lb 1/640 in-lb 1/320 in-lb 1/8000 Nm 3/16000 Nm 1/3200 Nm
Tz 1/1280 in-lb 1/640 in-lb 1/320 in-lb 1/8000 Nm 3/16000 Nm 1/3200 Nm
Physical Properties US Metric
Stiffness (Calculated)
X-axis and Y-axis force (Kx, Ky)
52×10
3
lb/in 9.1×10
6
N/m
Z-axis force (Kz)
100×10
3
lb/in 18×10
6
N/m
X-axis and Y-axis torque (Ktx, Kty)
93×10
3
in-lb/rad 11×10
3
Nm/rad
Z-axis torque (Ktz)
140×10
3
in-lb/rad 16×10
3
Nm/rad
Resonant Frequency (Measured)
Fx, Fy, Tz 1.4 kHz
Fz, Tx, Ty 2.0 kHz
Maximum Single-axis Load
Fx, Fy ±270 lb ±1200 N
Fz ±910 lb ±4100 N
Tx, Ty ±690 in-lb ±79 Nm
Tz ±730 in-lb ±82 Nm
Weight
Transducer with standard plates 0.56 lb 250 g
Transducer with ring/plug TAP 0.75 lb 325 g
Transducer with ring/plug MAP 0.8 lb 375 g
Material
Transducer Aircraft Aluminum
Standard mounting adaptor Aircraft Aluminum
Ring/Plug adaptors Aircraft Aluminum
*Resolutions are typical for a 16-bit data acquisition system.