h/p/cosmos 150/50 mercury Operating And Service Manual page 129

OP49 Type of frequency inverter (FI)
control
OP51 Error statistics of the digital FI
control
Note:
At each emergency stop the number
of timeout errors is increased
automatically by at least one
numerator because the transmission
line to the FI is interrupted by
hardware.
OP89 System for elevation measurement
(option not relevant for treadmills
without elevation or ladder
ergometers)
Note:
Normally the correct system for
elevation measurement is set by
selecting the correct device type
(administrator option number 3).
Only in very few cases and for
special models is this option
needed.
© 2012 h/p/cosmos sports & medical gmbh
Setting of FI control. Two types are available for selection:
Analogue 0 to 10 V
Digital via RS-485
The lower display row reports the errors of three different error types.
§
acknowledged), i.e. the FI has not accepted the last command
(transmission error, ...).
$
messages is wrong (transmission error, ...).
%
timeout period (60 ms).
The following kinds of elevation measurement can be selected:
0 = no elevation available.
N
1 = elevation control: increment disc with light barrier 60 incr. per
N
motor rotation or hall effect sensor with 60 incr. per motor rotation:
elevation element with a 4 mm spindle for: 0 - 25% elevation
(QUASAR/PULSAR from 1991 to 2001)
2 = elevation control: increment disc with light barrier 60 incr. per
N
motor rotation or hall effect sensor with 60 incr. per motor rotation:
elevation element with a 5 mm spindle for: 0 - 25% elevation
(h/p/cosmos saturn since 1994)
3 = elevation control: increment disc with light barrier 60 incr. per
N
motor rotation or hall effect sensor with 60 incr. per motor rotation:
elevation element with a 5 mm spindle for: 0 - 35% elevation
(h/p/cosmos venus since 1997)
4 = elevation control: linear motor for 0 - 24% elevation, increment
N
sensor, lift range 240 mm (h/p/cosmos mercury models since 1997)
5 = elevation control: linear motor for 0 - 28% elevation, increment
N
sensor, lift range 300 mm (h/p/cosmos quasar 4.0 since 2002)
6 = elevation control: linear motor for 0 - 25% elevation, increment
N
sensor, lift range 300 mm (h/p/cosmos pulsar 4.0 since 2002)
7 = hydraulic-cylinder for 0 - 11 % elevation angle.
N
lift range 430 mm (series PLM Mustang 2200)
8 =hydraulic-cylinder for 0 - 11 % elevation angle.
N
lift range 302 mm (series PLM Trainer)
9 = linear motor „HN" + lifting arm. 0 - 25% elevation angle.
N
lift range 252 mm (h/p/cosmos mercury since 2007)
10 = linear motor „HN" + lifting arm. -10...+18% elevation angle.
N
lift range 300 mm (h/p/cosmos quasar since 2007)
11 = linear motor „HN" + lifting arm. -10...+15% elevation angle.
N
lift range 300 mm (h/p/cosmos pulsar since 2007)
12 = increment disc with light barrier or inductive sensor
N
60 incr. per motor rotation: elevation element with 8mm spindle.
-4...25 % elevation (h/p/cosmos saturn 450/300rs as of 2008)
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email@h-p-cosmos.com
optional settings: administrator options
§ $ %
AnA
rS-
Number of NAK errors: the FI has sent an NAK (not
Number of total test errors: the test total of the received FI
Number of timeout errors: the FI has not answered within the
created 04.05.2012 printed 04.05.2012
LOG
485
page: 129 of 191