h/p/cosmos pluto - Page 154

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© 2015 h/p/cosmos sports & medical gmbh author: fh email@h-p-cosmos.com created 30.01.2015 printed 30.01.2015 page: 154 of 216
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.
The lower display row reports the errors of three different error types.
§ Number of NAK errors: (not acknowledged)
The FI has not accepted the last command (transmission error, …).
$ Number of total test errors: the test total of the received FI
messages is wrong (transmission error, …).
% Number of timeout errors: the FI has not answered within the
timeout period (60 ms).
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.
The following kinds of elevation measurement can be selected:
0 = no elevation available.
1 = elevation control: increment disc with light barrier 60 incr. per
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
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
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
sensor, lift range 240 mm (h/p/cosmos mercury since 1997)
5 = elevation control: linear motor for 0 - 28% elevation, increment
sensor, lift range 300 mm (h/p/cosmos quasar 4.0 since 2002)
6 = elevation control: linear motor for 0 - 25% elevation, increment
sensor, lift range 300 mm (h/p/cosmos pulsar 4.0 since 2002)
7 = hydraulic-cylinder for 0 - 11 % elevation angle.
lift range 430 mm (series PLM Mustang 2200)
8 = hydraulic-cylinder for 0 - 11 % elevation angle.
lift range 302 mm (series PLM Trainer)
9 = linear motor „HN“ + lifting arm. 0 - 25% elevation angle.
lift range 252 mm (h/p/cosmos mercury since 2007)
10 = linear motor „HN“ + lifting arm. -10…+18% elevation angle.
lift range 300 mm (h/p/cosmos quasar since 2007)
11 = linear motor „HN“ + lifting arm. -10…+15% elevation angle.
lift range 300 mm (h/p/cosmos pulsar since 2007)
12 = increment disc with light barrier or inductive sensor
60 incr. per motor rotation: elevation element with 8mm spindle.
-4…25 % elevation (h/p/cosmos saturn 450/300rs as of 2008)
13 = inclination sensor digital with para control 5
hydraulic elevation element.
-5…25 % elevation (h/p/cosmos saturn 450/300rs since 2013)
14 = linear motor „HN“ + lifting arm. 0 - 20% elevation angle.
lift range 252 mm (h/p/cosmos pluto since 2015)