Astronics Vertical Power Installation And Operating Manual Download Page 11

Page 7 

PPS Installation and Operating Manual

Rev. C.2 (January 19, 2018)

When planning your electrical system, assume the alternator provides 

80% of its rated output (in amperes), and therefore your total continuous 

load (don’t worry about trim or flaps or other transient loads) should not 

exceed 80% of rated alternator capacity.

3.4 Wire Sizes and Circuit Protection

A table below shows wires sizes versus loads for a typical homebuilt-size 

airplane. The wire size can be larger than necessary but should not be 

smaller. Circuit breakers (and fuses) protect the wiring, not the device. If 

the breaker is too large, then the wire may overheat and fail. If too small, 

then the device may fault (breaker trips) because it draws too much 

current.
Most kit aircraft companies and avionics companies provide 

recommendations for sizing wires and breakers. You can use these 

recommendations. Or, you can borrow or purchase an ammeter (typically 

under $50 at Radio Shack, etc.) measure the current draw of each 

electrical device and then determine the sizes yourself. When you know 

the current draw for each device, use the chart below to size the power 

wires. For simplicity, the wiring harnesses available from Vertical Power 

use the wire sizes in the table.

Up to (amps) 

 Use wire size (AWG)

5 A

20

10 A

18

15 A

14

80 A

4

300 A (starter)

2

Data signal

22

Recommended wire gauges

3.5 Grounding - 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 entire path from the power source 

to the device and back to the source. The ground wire must be the same 

wire gauge or a larger diameter (smaller gauge number) as the wire that 

provides power to the device.
A ground loop is when electricity takes two different paths, and each path 

has a different resistance. Ground loops are most noticeable in aircraft 

audio equipment, and can produce a variety of problems, most notably 

unwanted noise.
Several options for grounding your system are provided below. Choose 

the one that best fits your needs. Keep in mind that more wiring means 

more weight (although likely negligible). Also, note that in all the 

examples below the avionics grounds are kept together.

• 

Option 1: Run a ground wire from each and every electrical 

device back to a common grounding point, typically a ground bus 

on the firewall.

• 

Option 2: Run ground wires from all the avionics to an 

intermediate grounding point, then run a larger wire from the 

local ground bus to the firewall ground. Run wires from all the 

other devices to the firewall ground.

• 

Option 3: Run the ground wires from the avionics to the firewall 

ground, and run the other ground wires to a local ground (a metal 

part of the airframe located near the device).

The GND Stud connection to the PPS shall be ≤ 2.5 mΩ.

Failure to meet this requirement will damage the PPS and 

lead to an unsafe condition.

Summary of Contents for Vertical Power

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

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

Page 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...

Page 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...

Page 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...

Page 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...

Page 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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