| B400 AV | B500 VE | B2000 | TE Probe |
The B500 VE System replaces the B50 with the addition of new technology and functions. It consists of the B500 variometer, the B500 GCD glareshield controller and display and the B500 GPS global navigation system receiver.
The B500 The vario display and climb mode audio are the same as the B400 AV with the addition of red and green LEDs near the zero point of the variometer. When climbing the green LED is ON when the variometer is above the running 20 second value. In cruise the red and green LEDs indicate when the airmass is rising or sinking. In cruise mode, the vario optionally becomes a TE vario, a netto or a relative netto. Two blue LEDs and two amber LEDs provide the speed command display and the fly faster and fly slower sounds are the same as in the B50 - two alternating tones for fly slower and two very rapidly alternating tones for fly faster. There is a silent zone around the correct speed to fly and when the relative vario goes above the Macready setting the sound changes to the normal TE vario.
The B500 VE has a two channel audio and is supplied with left and right speakers. The audio sounds can be switched depending on various circumstances. When thermalling the sound is switched to one speaker when the circle should be opened in that direction. When cruising the speed command sounds come from the side where the next turnpoint lies. (depends on final glide computer) Various B500 VE functions are customizable by connecting the unit to a PC, including the audio silent zone. Software updates are accomplished the same way. Total energy is by probe for the same reasons as with the B400 AV. TE probes provide by far the best and most reliable TE compensation. There is a B500 mode where the pilot can select static (uncompensated) vario or pitot/satic compensation for the motor glider case. The B500 VE has an outside air temperature (OAT) probe and the temperature is displayed on the GCD. GPS and air data is supplied by the B500 VE to external computers and navigation devices by serial messages at 1 Hz in the same manner as done by the B50.
The B500 GCD now includes a Mini SD card slot for GCD program upgrades, B500 settings and turnpoint database updates. The B500 GCD has a push button top left and under it a rotary encoder with push button action and the rest of the area is occupied by a 122 x 32 graphics LCD with display area measuring 60.5 x 19 mm. The push button changes the display page and the rotary encoder push button moves the cursor to the variable the pilot wishes to change whereupon rotating the encoder changes the variable. There is no enter function. For example, on the main page the MaCready setting is the only variable, so just rotating the encoder is all that is required to change this. To change bugs, ballast or volume press the page button to get to the next page where this is displayed, press the encoder knob to move the cursor to “Ballast” and then rotate the encoder to change the ballast setting. The B500 GCD receives GPS and air data from the B500 variometer unit/B500 GPS and in addition to the display of the average rates of climb the B500 is controlled by the GCD and the pilot can enter Macready, bugs contamination, ballast state, control B500 audio volume and balance and in addition a simple GPS navigation display with turnpoint database, wind and final glide computer can be shown. This makes the instrument ideal for club gliders while the B500 VE also supplies RS-232 serial air and GPS data to any desired full function glide and navigation computer such as the Borgelt B2000 or any of the PDA type devices. While in theory the B500 VE could be controlled by a PDA or other air data computer such as the Borgelt B2000, using the GCD keeps the variometer housekeeping functions separate from the glide computer which simply picks up these changes in the serial data stream going to it from the B500 VE. This simplifies both the control of the variometer and of the glide computer.
Manual (requires Adobe Reader)
The PDA_PS In addition, when fitted with the optional Serial Data Combiner board, the PDA_PS substitutes the logger or FLARM (whichever is selected) data for the B500 GPS data. If logger or FLARM data is not available B500 GPS data is supplied. This means that logger pressure altitude or FLARM aircraft data and pressure altitude may be passed to the PDA. To cope with the large quantity of data in some messages, input baud rates higher than 4800 are allowed and the data is passed to the PDA at this higher rate. Auto bauding is used so this is transparent to the user. The Serial Data Combiner board is automatically included in PDA Power Supplies sold by OxAero.
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