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VP-100 Product Information
The VP-100 brings modern technology to experimental aircraft to simplify wiring and provide advanced electrical system capabilities. It groups almost all of the switches and indicators into one unit in your instrument panel. It replaces switches, circuit breakers, indicators, voltage alarms, trim relays, shunts, voltage converters and a host of other products. And it adds numerous capabilities that would otherwise be difficult to design and wire yourself. Plus, it makes wiring a modern electrical system simpler than other traditional alternatives.

The VP-100 installs in your instrument panel and provides manual switching for the avionics, contactors, flap system, and trim system. It supports a single bus, single- or dual-battery, single- or dual-alternator electrical configuration. The lighted liquid-crystal display shows overvoltage and under-voltage alerts, short-circuit and over-current alerts, flap & trim position,  and endurance bus status.

It is built using the latest technology, yet is based on time-honored electrical architectures. The system provides device switching and circuit protection, trim & flap control, overall electrical systems management, and the flexibility to adapt to each unique aircraft.

Wiring With the VP-100
Wiring your airplane is a serious project. No one can make it easy, but we can make it a lot easier. We provide complete instructions, how-to guides, tool rentals, wiring harnesses and wiring diagrams to assist with your project (you can download the documents here).

Rather than point to point to point wiring, you wire from the Vertical Power Control Unit (CU) to the electrical devices. Run a wire from the CU to the landing light. Run a wire to the battery contactor. Run a wire to the transponder. Run a bundle of five wires to a trim servo. Run two wires to the flap motor. Run a wire from each trim switch to the CU. Until you’re done. You won’t need to wire any circuit breakers or busses, or generate complicated wiring schematics.

Then use the setup menus on the character LCD screen to configure your system. You tell it what devices you have, what the circuit breaker values are, and which switch should turn each electrical device (or group of devices) on or off.

The VP-100 requires that  you wire an external starter switch and mag switch.  You can optionally connect other switches (trim, flap, or switches to control specific electrical devices) using the eight inputs on the Control Unit.

How It Works
The VP-100 from Vertical Power includes two units that are connected via a data cable. These units provide almost everything you need to wire your aircraft and are featured below:

Switch Panel
T
his mounts in the instrument panel and includes a lighted display and eight user-configurable LED-tipped switches. You no longer need to wire a master switch, avionics switch, or alternator field switches.  Flap and trim switches are provided, and you can optionally install external switches as well. The light sensor automatically dims the display and LED tip lights at night. Also included is a sheet of labels to mark each switch in a professional manner.

Control Unit
The “red box” houses solid-state circuitry the provides total protection and management of the electrical system on your aircraft. It turns electrical devices on and off, manages contactors and alternators, runs the trim and flap motors, handles short circuits, and watches for over-voltage and under-voltage conditions.  And much more. Its fault-tolerant design allows it to operate should certain internal sub-systems fail or if other system components fail.

Remote Control Key Fob
The middle button turns the system on and off. The other four buttons can be configured to your liking. For example, you can configure the remote to unlock your canopy and turn on the interior lights. It can perform a lights check for you by turning on the landing, strobe, and nav lights while you stand outside the plane.

Cables
The Switch Panel and the Control Unit connect together in about a minute with a pre-manufactured cable designed for ease of assembly.

Using the VP-100
Pressing either the key fob or the green power button on the VP-100 powers up your plane. You turn on the cabin lights with the key fob, and perform an exterior lights check during your walk around. Simply press one of the key fob buttons and your exterior lights cycle on an off. The VP-100 panel is shown below:

Labels are provided to place above and below each switch.
Click on image for a larger view

Once you’re in the pilot’s seat, the VP-100 tells you there are no electrical shorts or burned out landing lights. It indicates the trim position and battery voltage. You start the engine using the starter/mag switch (located separately from the VP-100 on the instrument panel). You then flip the alternator switch to Primary.

You turn on the other five switches which you’ve configured (using the setup menus) as follows:
Switch 1 Essential avionics that are used with the backup alternator
Switch 2 The rest of the avionics
Switch 3 Boost pump
Switch 4 Landing light
Switch 5 Strobe and nav lights
Momentary switch 1 pitch trim up and down
Momentary switch 2 panel light dimmer (up=brighter, down=dimmer)

The flaps are controlled by a panel-mounted switch which is wired to the Control Unit. The panel-mounted starter switch is wired in series with the starter contactor power circuit.

If you have a low-voltage condition during flight, the big green button will alert you by flashing red and the display with indicate a low-voltage alarm. This means you likely have a failed alternator or voltage regulator. You acknowledge the alert by pressing the small round button near the display, and then move the alternator switch down to select the backup alternator. You then load shed by turning off switches 2 through 5. When closer to the airport, you can turn on each of the switches as necessary.

During trim, flap, or dimmer operations, the display indicates the position or brightness of that control. When the switches are down (off) the LED tip lights are off, when up (on) they show green. If a device on that switch is faulted (short circuit or over-current), then the tip light flashes red. The display will tell you which circuit is faulted, and you can attempt to reset the circuit if desired.

The display also shows the total current draw of the electrical devices connected to the VP-100. This is a nice feature that allows you to compare real-time current draw with the capacity of your alternator, and it eliminates the need to install shunts or hall-effect sensors.

Once you’ve shut the engine down, simply hold the green power button for 2 seconds and the VP-100 powers off.

Control Unit
The Control Unit, when used with the VP-100, provides circuit switching, short-circuit protection, over-voltage protection, current monitoring per circuit, reversible flap and trim motor drive, circuit dimming capability, and monitoring external of external switches (such as canopy switches). It manages power to the alternator field circuit and control of the battery contactor. Regulated 12 volts is provided to the trim motors and power, ground and analog inputs for the trim and flap position sensors.

It can turn each device on individually, exactly as you configure it.

The circuit breaker value and other features such as soft start capability (used to turn on incandescent bulbs gently) is configured for each pin using the setup menus. Any number of power pins can be assigned to a switch on the VP-100.

The Control Unit uses the latest generation solid-state switches which have been designed for the automotive industry and are appropriately adapted for an aviation application. Each solid-state switch (i.e. a single integrated circuit) does the following:

• On-off switching
• Short circuit protection
• Measures current draw through that circuit
• Provides status to the microprocessor
• With a little additional circuitry it provides dimming and soft start capability

Each solid-state switch is rated for two billion operations, and this type of switch is in wide-spread use in the automotive, transportation, and marine industries.

The Control Unit operates in real-time and does not have an operating system. It communicates with the VP-100 Switch Panel using the fault-tolerant RS-422 serial protocol.

Each Control Unit is rated for 60 amps continuous load, and has the following power and sense pins:

(16) 5 amp power circuits (settable 1 to 5 amps), three of which are dimmable, two are Override circuits, and one is regulated down to +12 volts.
(5) 10 amp power circuits (settable 1 to 10 amps)
(3) 18 amp power circuits (settable 1 to 18 amps), all of which are dimmable.
(1) Main bus power input from the battery contactor.
(1) 20 amp endurance bus input from the battery.
(2) Trim circuits each includes 5 pins (two +12v regulated motor power, +2.5v, ground, and position input) for use with Ray Allen trim motor with built-in position sensor.
(1) Position sensor input, which includes 3 pins (+2.5v, ground, and position input) for use with Ray Allen position sensor. Typically this is used for the flap position sensor.
(2) Backup power inputs, tied to two of the 5A circuits.
(2) Ground when active outputs. One is for the battery contactor, the other is configurable. Typically it is used to control a cross-tie contactor or the SD-8 alternator.
(1) 10 amp starter contactor circuit
(1) 10 amp flap motor circuit
(2) 1 amp annunciator light circuits (for external lights such as a master warning)
(1) 1 amp always-on with circuit protection. Provides protected power to external keep-alive circuits, clock, etc.
(8) Switched inputs that are active when grounded. Used for trim switches, flap switches, canopy switch, etc.
(2) Switched inputs that are active when at bus voltage.
(1) RS-232 serial I/O port. Currently not used.
(3) Ground wires. These wires provide ground for the Control Unit, Switch Panel, trim motors, flap motors, and position sensors. The other devices (avionics, lights, etc.) are grounded directly to the ground bus and not through the Control Unit.

To connect a device to the Control Unit, simply run a wire from the appropriate pin on the Control Unit to the device. Ground the device as you normally would.


Flap and Trim Overview
The Control Unit drives the electric trim and flaps on your airplane, based on inputs from the VP-100 Switch Panel switches or external flap and trim switches. Any coolie hat, pushbutton , or rocker switch works fine. If you’ve ever wired an electric trim circuit, you know it takes some planning. Especially if you want to add co-pilot switches, disconnect circuitry, and provide overrides. Below is a list of features in the VP-100 flap and trim system:

Solid-state, no relays. Special safety circuitry. The control circuitry is all solid-state, meaning there are no mechanical relays to fail. For additional protection, each trim and flap circuit (as well as the starter circuit) has two solid-state control switches wired in series, and each switch is independently commanded (by two different command mechanisms) by the microprocessor. This prevents the trim from running un-commanded in the very unlikely event a solid-state switch fails closed. Compare that with a relay deck.

Easy to wire pilot trim switches and servos. Wire one side of the trim switch to ground, and the other side to the Vertical Power Control Unit. Run the five wires (included in the optional wiring harness kit) from the control unit to the Ray Allen trim servo. Use the setup menus to configure your trim operation. Done.

Easy to wire co-pilot trim switches. Run wires from the co-pilot trim switches to the Control Unit. Use the setup menus to configure your trim operation.

Flap control. Flaps can be configured to operate only when flap switch is pressed, or run to intermediate stops with a quick press of the flap switch.

Priority override. The pilot switches always override the co-pilot switches when conflicting inputs are commanded.

Runaway trim protection. If your trim switch sticks or one of the switch wires shorts, you can stop the trim from running by pressing the opposite trim button. Holding the opposite button for three seconds will disable the trim switches.

Indicators. Pitch trim indications are shown on the display when the trim is running.

Voltage regulation. The trim motor outputs are regulated to 12v so you can run Ray Allen servos in a 28V system with no external voltage regulation.

Trim compensation. You can configure the pitch trim to operate when the flaps are moving to minimize the pitching motion.

Backup Circuits
Another important consideration is having control when things don’t go as expected. For that reason, we’ve built into the Control Unit two independent backup circuits, which you can optionally connect.

When you close the external switch, power is provided directly from the battery to the power output pins then on to the devices, backing up the internal solid-state switches and providing power at all times. You may use the backup circuits to assure power to the EFIS and ADAHRS before you enter the clouds, for example. While technically not needed, the backup circuit is meant to provide extra peace of mind. The diagram below illustrates how the backup circuit works.

Software Updates and Setup
Software updates are uploaded to the VP-100 via a serial port on the Switch Panel and on the Control Unit. A laptop or nearby PC is required to download software.

Interfaces
The VP-100 does not require interfacing with third-party avionics.

Specifications
Operating Voltage: 4 volts - 32 volts normal operations, 40v for 1 second, 60v for 100 ms
Operating Temperature Range: -25 to +70 deg C
Storage Temperature Range: -30 to + 85 deg C


For additional information on Vertical Power products click on these links below

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