background image

INDU Airspeed — Manual

1. Introduction

1

Introduction

First of all, we would like to thank you for purchasing our device. Indu airspeed is an electronic
device, which mimics classical airspeed construction and combines it with the state of the art
electronics. This results in the best of both worlds; a perfect and intuitive analogue reading
combined with high precision of modern electronics.

This manual describes the technical description of the unit, installation and operation.

1.1

General Description

The airspeed is an electromechanical device. It consists of high precision electronic differen-
tial pressure sensor, which provides dynamic air pressure information in digital form. The
electronics reads the sensor and drives stepper motor turning a needle. Airspeed information
is also shown on a colour LCD display. When connected to a CAN bus the airspeed outputs
airspeed and OAT

1

data which can be used by other

Kanardia

devices.

Display is divided linearly in 230

scale with colour LCD display in the center. Scale is custom

made and must be specified when ordering the device.

There is a special version

1

of airspeed indicator that can display true airspeed (TAS) and

outside air temperature (OAT) information on LCD display. This requires an external OAT
probe to be connected to airspeed and an Indu Altimeter to be present on same CAN bus.

1.2

Technical Specification

Table 1 shows some basic technical specification of Indu airspeed.

Description

Value

Weight

57 mm: 160 g (cca 210 g with OAT probe)
80 mm: 200 g (cca 250 g with OAT probe)

Size

57 mm: 62 x 62 x 42 (61 with connectors) mm
80 mm: 82 x 82 x 42 (61 with connectors) mm

Operational voltage

6 to 32 V

Power consumption

1.26 W

Current

105 mA at 12 V
53 mA at 24 V

Operating temperature

-30

C

to +85

C

Humidity

30 % to 90 %, non condensing

Panel hole

80 mm (3.15 inch) diameter, standard fit

Airspeed sensor

12 bit, 0 to 50 hPa, 325 km/h, resolution less than 0.1 km/h
Option

1

: 0 to 100 hPa, 460 km/h

OAT

12 bit, range -55 to 125

C

, 0.5

C

accuracy

Communication

CAN bus, 29 bit header, 500 kbit, Kanardia protocol

Table 1:

Basic technical specifications.

1

Must be specified at the time of order. Please refer to “INDU Airspeed Ordering Form” for more details.

4

©

Kanardia

2016

Содержание INDU Airspee

Страница 1: ...INDU Airspeed Manual Kanardia d o o June 2016 Kanardia d o o Revision 1 0...

Страница 2: ...e license gives you right to copy reproduce and modify this document if you cite Kanardia d o o as the author of the original work you distribute the resulting work only under the same or similar lice...

Страница 3: ...ings 7 2 Installation Maintenance 8 2 1 Mounting Dimensions 8 2 2 Connections 8 2 2 1 Static Pressure Pst 8 2 2 2 Total Pressure Ptot 9 2 2 3 CAN Bus CAN 9 2 2 4 Power POWER 9 2 2 5 Outside Air Temper...

Страница 4: ...the center Scale is custom made and must be specified when ordering the device There is a special version1 of airspeed indicator that can display true airspeed TAS and outside air temperature OAT info...

Страница 5: ...e is then custom made for each individual order Scale holds color coded markings in order to give the pilot immediate reference The following markings are possible VNE Red line on the top of yellow ar...

Страница 6: ...iguration with flaps retracted Note that bottom of green arc usually starts at 10 higher value VS0 Bottom of white arc Stall speed or minimum flight speed in landing config uration Note that bottom of...

Страница 7: ...ured1 to show three types of warnings on LCD display VA exceeded Yellow IAS value designates that the IAS value has exceeded the design maneuvering speed VA Figure 4a VNE exceeded Red IAS value design...

Страница 8: ...re 5 Instrument panel cutout and mounting hole Note Figure is not in scale 2 2 Connections Figure 6 illustrates all connections at the back side of the instrument 2 2 1 Static Pressure Pst The instrum...

Страница 9: ...OWER Connect supplied connector at the back of the airspeed The connector has a notch on one side which protects from wrong orientation Connect blue lead to negative ground terminal and red lead to po...

Страница 10: ...d thread the external nut to the probe The lock tight is necessary to avoid losing the cap due to vibrations 5 Tighten the internal nut so that the probe sits firmly and apply lock tight on the nut Do...

Страница 11: ...ment is connected to INDU Altimeter via CAN bus 5 Visual warnings optional Aircraft type ___________________ Filled by _______________________ name and signature Red zone IAS value on LCD display is c...

Страница 12: ...nd is provided must be returned to Kanardia and becomes Kanardia s property Exclusions and Limitations This Limited Warranty applies only to hardware products manufactured by or for Kanardia that have...

Страница 13: ...damages resulting from any breach of warranty or condition or under any other legal theory including but not limited to loss of use loss of revenue loss of actual or anticipated profits including los...

Отзывы: