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Page 8 

PPS Installation and Operating Manual

Rev. C.2 (January 19, 2018)

3.6 Switch Nomenclature

The chart below shows the most common switch types. A parenthesis 

() around a switch position indicates it is a momentary, spring-loaded 

position.

Switch Type

 Designation

 Symbol

 Mechanism

Single Pole, 

Single Throw

SPST

OFF-ON

OFF-(ON)

Single Pole, 

Double Throw

SPDT

ON-NONE-ON

ON-OFF-ON

(ON)-OFF-(ON)

ON-OFF-(ON)

Double Pole, 

Single Throw

DPST

OFF-ON

OFF-(ON)

Double Pole, 

Double Throw

DPDT

ON-NONE-ON

ON-OFF-ON

(ON)-OFF-(ON)

ON-OFF-(ON)

PPS Control input pins

3.7 Current Sensing (Shunt)

When planning your aircraft electrical wiring you must consider whether 

to wire an ammeter (usually a shunt or hall effect sensor provided with 

the engine monitor) on the wire connecting the alternator(s) to the 

main bus. The ammeters indicate the amount of current the alternator is 

providing.
A shunt is not required to tell if the alternator is working. It is very easy 

to tell if the alternator is working correctly by simply looking at voltage. 

If you see 14 (or so) volts with the engine running then it is working. If 

you see 12 (or so) volts it is not working or not turned on or the devices 

are drawing more current than the alternator can provide (note, engine 

must be running). If you set your low voltage alarm on the EFIS at 13 

volts, then you will get a low voltage alarm if the alternator fails.
The PPS provides the alternator current (shunt) output, which shows 

the amount of current the alternator is providing to power the devices 

and charge the battery. The VP-X total current reading shows the total 

amount of current the devices attached to the VP-X are using. The delta 

between the two is the battery charging current, which goes to zero after 

re-charging any loss from starting the engine or charging a run-down 

battery.
If the battery charging current is important to you, the PPS also provides 

a battery current (shunt) output as well. If not, then simplify your wiring 

and don’t utilize this PPS output. Your call. And of course each builder’s 

needs are different so there is no absolutely right answer.
The EFIS displays a VP-X page which shows individual device current 

as well as total current through the VP-X. The EFIS also has an ‘Amps’ 

gauge that is used to show the readings from the shunt. In some cases the 

EFIS ‘Amps’ gauge can be used to display total system current from the 

VP-X. Please check with your EFIS manufacturer for details.
If you don’t use the PPS current outputs then the shunt wires on the 

engine monitor/ EFIS are not used.

Содержание Vertical Power

Страница 1: ...20180119 Rev C 2 Copyright 2018 by Ballard Technology Inc Primary Power System PPS Primary power control for experimental and light sport aircraft Installation and Operating Manual January 19 2018 Re...

Страница 2: ...ts 6 3 3 Alternator Options 6 3 4 Wire Sizes and Circuit Protection 7 3 5 Grounding IMPORTANT 7 3 6 Switch Nomenclature 8 3 7 Current Sensing Shunt 8 4 Installation and Test 4 1 Planning 9 4 1a Tools...

Страница 3: ...product is safe reliable and accurate and to determine this product is operating properly after installation DO NOT INSTALL THIS PRODUCT If the aircraft owner pilot and or installer are unwilling to t...

Страница 4: ...29 2017 Updates based on product changes incl new pinouts Aug 24 2017 Updated grounding instructions Sep 25 2017 Updated grounding diagram and Table 4 2b Jan 19 2018 Updated current values added Start...

Страница 5: ...ndependent batteries alternators battery contactors and a cross tie contactor Multiple PPS units can be used to implement a dual bus architecture Please contact support for more information on dual bu...

Страница 6: ...maintain it but contributions come from builders Top 10 Wiring Mistakes A free 12 page paper describing the most common wiring mistakes and how to get started wiring your aircraft Additional document...

Страница 7: ...or will latch open if the slow trip current the fast trip current of 1200 amps or the instantaneous maximum current of 1500 amps is exceeded The slow trip current emulates the trip curve for a standar...

Страница 8: ...nt fault indication BUS GND ALT DIST FAULT Latched Over current fault indication BUS GND STARTER ACTIVE Starter Active indication BUS GND BATT CURRENT Main Battery current sense 1 mV A relative to 7 5...

Страница 9: ...imilar and not because you blindly copied him We believe the most important free advice we can offer is the following CLARIFY YOUR MISSION In this age of gadgets it is all too tempting to add just one...

Страница 10: ...lit and sent to individual devices through circuit protection devices fuses and circuit breakers and switches The VP X assumes the role of busses circuit protection and a host of single function modul...

Страница 11: ...g IMPORTANT Many people think that the power or positive wire is the most important wire to provide electricity to a device The electrical ground is just as important as electricity must flow the enti...

Страница 12: ...drawing more current than the alternator can provide note engine must be running If you set your low voltage alarm on the EFIS at 13 volts then you will get a low voltage alarm if the alternator fail...

Страница 13: ...with planning Some items may vary depending on the requirements of your specific installation Crimper insulated terminals 20 AWG Crimper TE Connectivity Hand Crimper 601966 1 or equivalent and TE Conn...

Страница 14: ...ay not be needed depending on alternator PPS Wiring Overview with the Vertical Power VP X Aircraft with a remote mounted battery may require the addition of a battery contactor near the battery as sho...

Страница 15: ...e connected Maximum wire length 24 in Twist together sense lines on pins 9 and 20 to reduce common mode noise Twist together sense lines on pins 19 and 18 to reduce common mode noise PPS basic install...

Страница 16: ...basic installation with the Vertical Power VP X Comprehensive Installation with the Vertical Power VP X The image below details comprehensive PPS connector wiring for an aircraft wired with the Verti...

Страница 17: ...airframe 4 2a Mount the PPS The PPS should be mounted to the firewall or other desired location using 4 10 bolts not included A drill punch template is provided on the next page You can print this as...

Страница 18: ...Page 14 PPS Installation and Operating Manual Rev C 2 January 19 2018 PPS Mounting Template...

Страница 19: ...tor battery starter and grounds 4 2c Control Status Wiring Per your installation plan route wires for the switches and indicators Crimp and install these wires into the circular connector The PPS uses...

Страница 20: ...d must connect both pins 26 and 27 to GND maximum wire length 24 inches 26 27 RSVD Reserved do not connect 28 4 3 Ground Test The ground test steps are performed in two parts the first part without th...

Страница 21: ...nderstand how to operate the PPS and clear faults This section provides a series of recommended steps which should be incorporated into the overall flight test plan as you deem appropriate Review the...

Страница 22: ...put terminal Use multi meter to verify that Master switch input primary or alternate voltage is ground must be below minimum input voltage Use multi meter to verify that Main contactor switch input vo...

Страница 23: ...aximum intermittent Alternator Input 80 A maximum continuous Analog Current Monitor Outputs Common mode reference of 7 5 VDC Scale 1 mV Amp Short circuit protected 7 3 Environmental Physical Component...

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