Flight Systems Anemoi 26005-485 Manuel utilisateur

Installation / Operation

Manual

 
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Installation / Operation Manual 
anemoi 
 
Contents 
 
1. Preface..............................................................................................................................................3
1.1 Limited Warranty......................................................................................................................3
1.2 Sunburned Display Warranty....................................................................................................3
2. System Description...........................................................................................................................4
3. Technical Specifications....................................................................................................................6
3.1 Available Accessories................................................................................................................7
4. Mechanical Installation ....................................................................................................................8
4.1 Display Unit...............................................................................................................................8
4.2 Sensor Unit...............................................................................................................................8
4.3 Temperature sensor installation............................................................................................ 10 
4.4 P_TOTAL and P_STATIC Connectors ....................................................................................... 10 
4.5 Drawings Display Unit............................................................................................................ 11 
4.6 Drawings Sensor Unit ............................................................................................................ 12 
5. Electrical Installation ..................................................................................................................... 14 
5.1 Display 1 / Display 2 Connector............................................................................................. 15 
5.2 GPS NMEA Connector............................................................................................................ 15 
5.3 POWER Connector................................................................................................................. 17 
5.4 GPS Receiver Connector........................................................................................................ 18 
5.5 Wiring Diagram...................................................................................................................... 19 
6. Operation....................................................................................................................................... 20 
6.1 Startup................................................................................................................................... 20 
6.2 Display pages......................................................................................................................... 20 
Wind Page...................................................................................................................................... 21 
AHRS page ..................................................................................................................................... 21 
Data page....................................................................................................................................... 21 
6.3 Operation on ground............................................................................................................. 21 
6.4 In-Flight operation................................................................................................................. 22 
Use of data indicated by anemoi................................................................................................... 22 
Data interpretation and reliability................................................................................................. 22 
6.5 Setup Menu........................................................................................................................... 23 
Calibrate PRS ................................................................................................................................. 24 
Rotate Screen ................................................................................................................................ 24 
Disable AHRS ................................................................................................................................. 24 
Align DOF....................................................................................................................................... 25 
Exit................................................................................................................................................. 25 
6.6 Errors ..................................................................................................................................... 26 
Sensor error................................................................................................................................... 26 
-no data-........................................................................................................................................ 26 
6.7 Firmware / Software Update................................................................................................. 27 
7. Abbreviations and Terms............................................................................................................... 28 
 

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1. Preface

Thank you for purchasing an RS Flight Systems anemoi. We are pleased that you have chosen our

product and are confident that it will meet all your expectations. In case of questions or problems with

the unit, feel free to contact:

Service and Support:

Ülis Segelflugbedarf GmbH

Untergasse 1

63688 Gedern | Germany

+49 6045 950100

info@segelflugbedarf24.de

Development and Production:

RS Flight Systems GmbH

Oberer Luessbach 29-31

82335 Berg | Germany

anemoi@rs-flightsystems.com

The anemoi system is designed exclusively for VFR use as an aid to navigation. All information is

presented for reference only. Wind, AHRS and air data are provided as an aid to situation awareness.

Information in this document is subject to change without notice. RS Flight Systems reserve the right

to change or improve their products and to make changes in the content of this material without

obligation to notify any person or organization of such changes or improvements.

1.1 Limited Warranty

This RS Flight Systems product is warranted to be free from defects in materials or workmanship for

two years from the date of purchase. Within this period, RS Flight Systems will, at their sole discretion,

repair or replace any components that fail in normal use. Such repairs or replacement will be made at

no charge to the customer for parts and labor, provided that the customer shall be responsible for any

transportation cost. This warranty does not cover failure due to abuse, misuse, accident, or

unauthorized alterations or repairs. RS Flight Systems displays damaged by direct or magnified sunlight

are not covered under warranty. To obtain warranty service, contact Ülis Segelflugbedarf or RS Flight

Systems directly.

1.2 Sunburned Display Warranty

The anemoi display screen can be damaged or burned by strong sunlight magnified by canopies in

certain positions. We suggest covering your device from direct sunlight, especially if the canopy is

open. anemoi displays damaged by direct or magnified sunlight are not covered under warranty.

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2. System Description

The anemoi comprises one sensor and one display unit. Its functionality is as follows:

•Precise indication of wind vector, artificial horizon (AHRS) and flight data (TAS, GS, OAT, FL)

•Stand-alone system architecture

•Sunlight-readable backlit display

•Simple and self-explanatory operation (one push button)

•Minimum installation effort of sensor unit –uninfluenced by magnetic fields

•Compact display unit with versatile installation options

•Simple data transfer and software update via microSD card

•Suitable for 12 VDC aircraft electrical systems

•High level of manufacturing and quality control

•Engineering and production exclusively done in Germany

Figure 2-1: Sensor Unit

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Figure 2-2: Display Unit

Figure 2-3: Wiring Harness Kit

Figure 2-4: Connection Kit

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3. Technical Specifications

Sensor Unit

Display Unit

Dimensions

(width, height, depth)

130 x 55 x 35 mm

5.12 x 2.17 x 1.38 in

44 x 30 x 10 mm

1.73 x 1.18 x 0.39 in

Mounting Depth

incl. connectors

70 mm

2.76 in

25 mm

1.00 in

Mounting

4x M4 screws

120 x 40 mm

4.72 x 1.57 in

Taped

Connector Cutout: 14 x 16 mm

0.55 x 0.63 in

Display Cutout: 26 x 26 mm

1.02 x 1.02 in

Total Mass

180 g

0.4 lbs

20 g

0.04 lbs

Housing

Machined aluminum, surface black

anodized

Polyamide 12

Supply Voltage

12 VDC

Power Consumption

100 mA

Display

1.3-inch LCD, 240 x 240 pixels

Firmware Update

microSD card, up to 32 GB, FAT32 formatted

Operating

Temperature Range

-20 to +60 oC

-4 to +140 oF

Operating Altitude

< 7,620 m

< 25,000 ft

Humidity

< 95 %, non-condensing

Table 3-1: Technical Specification

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3.1 Available Accessories

Part No.

Name

Description

10-757

anemoi Wind Indication

System

Live wind indication system for aircraft

Kit consists of Sensor Unit and Display Unit

Power supply: 12 VDC

Sensor Unit: 130 x 55 x 35 mm

Display Unit: 44 x 30 x 10 mm

Includes wiring harness 10-752 and connection kit 10-756

26005-455

anemoi Display Unit

Display Unit for anemoi live wind indication system

240 x 240 pixels TFT screen, ultra-bright

Dimensions: 40 x 30 x 10 mm

26005-485

anemoi Sensor Unit

Sensor Unit for anemoi live wind indication

Power supply: 12 VDC

Dimensions: 130 x 55 x 35 mm

10-752

Wiring Harness Kit anemoi

Power wires, length 0.5 m (1.5 ft)

Temperature Sensor, length 1.0 m (3 ft)

10-781

Wiring Harness Kit anemoi

(3m)

Power wires, length 3.0 m (10 ft)

Temperature Sensor, length 3.0 m (10 ft)

10-756

Connection Kit anemoi

Connection Kit for anemoi wind indicator system. Includes:

- Display cable RJ12 0.5 m (1.5 ft)

- NMEA cable RJ45 0.5 m (1.5 ft)

- NMEA RJ45 Y-splitter (1:1)

- 2x T-Reduction Nozzles instrument hose

- Silicone hose 3 x 5 mm (0.12"), length 1.0 m (3 ft)

10-782

Connection Kit anemoi

(3m)

Connection Kit for anemoi wind indicator system. Includes:

- Display cable RJ12 3.0 m (10 ft)

- NMEA cable RJ45 3.0 m (10 ft)

- NMEA RJ45 Y-splitter (1:)

- 2x T-reduction nozzles instrument hose

- Silicone hose 3 x 5 mm (0.12"), length 6.0 m (20 ft)

10-744

Cable RJ12 0,5m

anemoi Display Unit cable

Length: 0.5 m (1.5 ft)

10-778

Cable RJ12 3,0m

anemoi Display Unit cable

Length: 3.0 m (10 ft)

10-745

Cable RJ45 0,5m

NMEA cable anemoi

Length: 0.5 m (1.5 ft)

10-779

Cable RJ45 3,0m

NMEA cable anemoi

Length: 3.0 m (10 ft)

10-746

Y-Adapter RJ45

Y-Adapter for RJ45 cable

1:1 Splitter, shielded

10-747

T-Reduction Nozzle 6-4-6

T-reduction nozzle 6mm-4mm-6mm (0.24"-0.16"-0.24")

Connection of anemoi static pressure and total pressure hose

10-759

Silicone Hose 3x5 mm

Silicone hose, transparent

Inner diameter: 3 mm (0.12”)

10-875

Klixon Circuit Breaker

7277-2-1

Small size and lightweight circuit breaker

Rating: 1 A

10-887

Mounting Adapter anemoi

57mm

anemoi adapter for 57 mm (2.25") instrument panel cutout

13100-177

GPS GNSS Receiver

High precision GPS GNSS receiver

Accepts the signals of up to 50 satellites at the same time

Sensibility max. -162 dBm, IPX6 protection class

Cable length: 1.5 m (5 ft)

Dimensions: 65 x 45 x 22 mm

Table 3-2: Accessories

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4. Mechanical Installation

Upon delivery, undertake visual inspection of the package contents for signs of transport damage and

verify the information on the type plate sticker against your order. Do not open the device housing.

For longer storage of the device, select a dry and clean environment. Make sure that the device is not

stored near strong heat sources and that no metal chippings or other dirt can get into the device or its

connectors.

4.1 Display Unit

The display unit is mounted either in front of the instrument panel or behind the instrument panel.

Second variant needs a rectangular cutout (dimensions in Table 3-1). Two mounting examples are

shown in Figure 4-1 and Figure 4-2.

Figure 4-1: Front side mounting

Figure 4-2: Rear side mounting

4.2 Sensor Unit

The sensor unit can be mounted behind the instrument panel or in the fuselage. By default, the anemoi

is delivered with a 0.5 m (3.0 ft) wiring harness kit. As an accessory, a 3.0 m (10 ft) wiring harness kit is

available. The sensor unit is mounted with 4x M4 screws. The screw hole positions can be taken from

Figure 4-9.

The mounting position of the sensor unit is shown in Figure 4-3.

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Figure 4-3: Mounting cutout sensor unit

The sensor unit needs to be aligned with the aircraft axes by the following margins:

- Yaw axis: +-1°. Misalignment leads to inaccurate wind indication during longer straight flight

segments without moderate changes in airspeed and heading.

- Roll axis: +- 3°. Misalignment leads to permanent offset of the roll angle indicated by the artificial

horizon (AHRS), and potentially falsifies wind indication during longer straight flight segments.

- Pitch axis: +-7°. Alignment can be adjusted and chosen within a relatively wide-angle range with

no noticeable effect on wind indication. The mounting pitch attitude of the sensor unit will be

indicated as “zero pitch”on the artificial horizon (AHRS).

The sensor unit must always be mounted so that the labeled side of the device is “up”. A vertical

mounting is not possible.

The sensor unit can be mounted in four different yaw orientations, indicated as A, B, C, D on the top

side of the sensor unit. If the sensor unit is installed with direction A pointing in the DOF (direction of

flight) no further action is required upon installation. If the sensor unit is installed in the directions of

B/C/D, the DOF must be set in the menu once after installation, as explained in chapter 6.3: Setup

Menu under “Align DOF”.

Three-dimensional CAD-models of the units and the cutout of the display unit are available at the RS

Flight Systems website.

As waste heat is dissipated via free convection, leave at least a 5 mm gap from the aluminum surfaces

to any other object. Forced cooling is not necessary.

The installation must be in accordance with the appropriate guidelines approved by the respective

aviation authority. The person installing the device is responsible for compliance with all applicable

legislation.

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4.3 Temperature sensor installation

It is recommended to install the temperature probe as closely to outside air temperature (OAT) as

practically possible, e. g. inside the nose tip or in the front air vent of the aircraft.

Errors in temperature measurement (usually, too warm measurement due to heating from cockpit

systems) can have an impact on the airspeed calibration and therefore negatively influence wind

calculation. However, the system’s sensitivity to temperature errors is quite low, and the anemoi

software is even capable of adjusting to permanent temperature measurement offsets within the first

15 minutes after takeoff. Nevertheless, good temperature measurement is necessary for ideal

performance of the wind indication.

4.4 P_TOTAL and P_STATIC Connectors

P_TOTAL must be connected with the total pressure tube, P_STATIC with the static pressure tube. The

pressure connectors and pressure tubes need to be properly sealed as leakage leads to errors in the

external airspeed indicator and altimeter. During pre-flight check both instruments need to be checked

for their proper functionality.

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