WIND DRIFT VECTORIAL RULER MANUAL Set

19
020 030 040 050
06
200 210 220 23
0
0
24
0
0
0
0
Wind drift vectorial
ruler
30
Breveté
Modèle déposé
Made in France
[email protected]
mobile: 33.6.06.54.81.24
W
Patented
Registered design
3
01
17 50
07
S
80
01
1900
020
040
050
200 210 220 230
030
0
24
02
5
06
0
0
0
02
26 80
50
40
Règle vectorielle de
dérive vent
07
0
S
010
190
200 210 220 230
24
020 030 040 05
0
0
06
0 25
BEARING
GROUND SPEED
&
D
FT SPEE
&
G
HEADIN
AIRCRA
BEARING
Nm Ech. 1 000 000 ème
0
0
16
34
0
0
33
15
110 120 130 14
0
290 300 310 320
100
W
280
70
02
26 0
08
BEARING
GROUND SPEED
&
D
FT SPEE
&
G
100
280
W
70
0
50
07
25
16
34
0
0100
N
50
290 300 310 3
280 110 120 130 1420 33
0
0
100
1
1
...And if my aircraft runs over the speeds scale of the ruler?
80
GROUND SPEED
&
HEADIN
0
0
34
16
0
0
15
110 120 130 14
0
290 300 310 320
33
60
03
35 70
100
70
0
W
08
60 45
3
Nm Ech. 1 000 000 ème
110
02
26 80
BEARING
GROUND SPEED
&
D
FT SPEE
&
G
HEADIN
AIRCRA
Nm Ech. 1 000 000 ème
BEARING
GROUND SPEED
&
D
FT SPEE
&
G
HEADIN
AIRCRA
Nm Ech. 1 000 000 ème
34
0
16
0
0
33
15
140
290 300 310 320
120 130
100
280
10° 20° 70 30°
01
17 50
AIRCRAFT SPEED
&
HEADING
70
0
40
30° 20° 10°
110 120 130 1
02
26 0
0
80
40
15
290 300 310 32
0
0
228800
33
0 16
34 0
0
0
W
07
0 210 220 23
02
90 20
020 030 040 05
40
0
06
0 25
0,6
80
You can use the WIND DRIFT VECTORIAL RULER:
* When preparing your navigation
* In cabin while navigate (Very light and of adapted
dimensions)
* On maps (whatever it is (500 000ème,
1000 000ème, or VAC) thanks to its transparency
* Maps out; it becomes opaque and reading easy.
100
290
0
30
0
0
13
31
0
S
1
80 010
90 35
E
280
12
0
0 270 280 29
50 26
100 1 0 3
080
02
00
10
24 070
12
0 31
0 060
3
13 0
2 50
0
3
Use possibilities
90
E
3
0
15
0 330
14 20
0
34
1600
350
S
010
020
170 180 190 200
21
02
2
04 0
03
0
Azimuth:
Shows ground track,
shows air heading (taking account the wind)
Breveté
Modèle déposé
Made in France
[email protected]
mobile: 33.6.06.54.81.24
2
260
080 090 100 110
1.1. The ground track you want follow (read on
azimuth(2),
1.2. Ground speed, due to wind,
1.3. wind drift,
1.4. Distances scale: Nm ("Air high speed"
model) or Km/h ("Air low speed" model) (map 500 000)
1.5. Distances scale: Nm ("Air high speed"
model) or Km/h ("Air low speed" model) (map 1000 000)
30
00
08 60
250
070
1 "Ground" ruler (Ground speed & bearing). Indicates:
70
90
110 120 130 1
2
0
06
0 240
05 30
1
30
Breveté
Modèle déposé
Made in France
[email protected]
mobile: 33.6.06.54.81.24
01
17 50
Règle vectorielle de
dérive vent
Patented
Registered design
40
15
290 300 310 32
0
0
2800
28
33
0 16
34 0
0
Wind drift vectorial
ruler
100
N
50
40
E
0 360 010 02
40 35
0
190
170
200 030
03
33 160
21
0 04
0 150
22 0
32 40
0
0
Patented
Registered design
0
0
I
W
50
07
25
50
40
Règle vectorielle de
dérive vent
0
0
Wind drift vectorial
ruler
34
24
50
0
01
60
020 030 040 0
0100 200 210 220 2350 06
0
0
19
N
0
0
1
0,5
110
30
10 0
Fb
90
2
120 Fb
EED 60
AIR SP
(AIS)
D
EE
SP
& IN
IG
OR
25
15
60
03
35 70
ND
06
00
7
24
0
33
60 45
230
320
10° 20° 70 30°
1
200
310
30° 20° 10°
90
100
Breveté
Modèle déposé
Made in France
[email protected]
mobile: 33.6.06.54.81.24
40
Breveté
Modèle déposé
Made in France
[email protected]
mobile: 33.6.06.54.81.24
020 030 040 050
210 220
19
290
80
30
0100
N
110 120 130 140
300
80
Patented
Registered design
Règle vectorielle de
dérive vent
1
280
90 35
60
03
35 70
100
25
0,6
70
2
130
50
60 45
90
100
D
EE
SP
& IN
IG
OR
2
Patented
Registered design
30
140 20
Wind drift vectorial
ruler
10° 20° 70 30°
E
Règle vectorielle de
dérive vent
ND
00
08 60
Wind drift vectorial
ruler
40
0,4
0,5
50
40
40
30° 20° 10°
90
50
170
160 15
150Fb
80
80
50
25
0
90 35
2
I
W
40
10
30
N
70
D
EE
SP
D
IN & IN
W
G
I
OR
4
0,6
00
08 6 0
60 45
5
190
180
25
110
30
100
Fb
EED
AIR SP
(AIS)
0
200Fb 0,3
20
130
40
50
kts
0,4
10° 20° 30°
100
1kt=2km/h - 10%
T=DxFb
140 20
120 Fb
1
110 120 130 1
30° 20° 10°
90
10
160 15
150Fb
AIR SPEED
(AIS)
80
70
0
10
170
30
90 35
80
5
190
180
0 030 040 05
00
10 02
200 210 220 23
60
0
24
0 07
0
0
60 190
03
35 70
0
200Fb 0,3
0,6
70
60 45
40
15
290 300 310 32
0
0
2800
28
33
0 16
34 0
0
110
30
100
Fb
10° 20° 70 30°
100
b 0,5
60
kts
20
120 F
1.3
40
30° 20° 10°
E
3.2
25
80
100
1kt=2km/h - 10%
T=DxFb
Nm Ech. 500 000 ème
50
90 35
90
10
140 20
130
70
0,6
0,5
EED 60
AIR SP
(AIS)
110
30
100
Fb
2
0,4
40
EED 60
AIR SP
(AIS)
80
25
120 Fb
0,5
00
08 60
1.5
0
50
25
120 Fb
90
1.4
130
110
30
10 0
Fb
D
EE
SP
D
IN & IN
W
G
I
OR
Nm Ech. 500 000 ème
160 15
150Fb
140 20
40
0
10
170
30
50
Manual
3.1
3.3
0,4
140 20
07
20
1.2
160 15
150Fb
0 210 220 23
02
90 20
020 030 040 05
40
0
06
0 25
180
AIRCRA
Nm Ech. 1 000 000 ème
30
10
170
30
S
5
190
160 15
150Fb
5
190
180
20
10
170
0
200Fb 0,3
1
80 010
200Fb 0,
3
10
kts
3
kts
Nm Ech. 500 000 ème
10
190
180
1kt=2km/h - 10%
T=DxFb
0,4
4.2. Wind direction (from),
0
5
130
& origin" ruler. Indicates:
4 Wind speed
4.1. Wind strength,
3.4
0
0
200Fb 0,3
40
3
1kt=2km/h - 10%
T=DxFb
kts
20
3
1.1
0
2
10
1kt=2km/h - 10%
T=DxFb
01
17 50
4.1
0
Nm Ech. 500 000 ème
3.2. Foreseen "air" speed,
3.3. Wind drift.
(3.2 & 3.3 read on "Ground" ruler(1))
3.4. A hole, at the end of the "Aircraft speed &
heading" ruler allows you write "Air" point on the map.
WIND SPEED
&
ORIGIN
4
1
(Aircraft speed & heading). Indicates:
3 "AIS" ruler3.1.
Heading due to windt (reading on azimuth (2),
Nm Ech. 500 000 ème
WIND DRIFT VECTORIAL RULER
MANUAL
Set elements
4.2
1- With azimuth, set your heading (here 030).
2- With "AIR SPEED" cursor (AIS) set the foreseen speed along
"Aircraft speed & heading" ruler (here110kts read on "Ground
speed & bearing" ruler.
3- With "WIND SPEED & ORIGIN" cursor, set the wind strength
(here 25 kts) and its direction (estimated with the azimuth; ici
270°)
4- DRIFT (here 11°), GROUND SPEED (here 123 kt) and approaching BASE FACTOR (here 0,5) automatically are shown (red
button and graduations) on "Ground speed & bearing" ruler,
together with NEW HEADING (here 019) on the azimuth.
5- Thanks to scales in Nm ("Air high speed" model) or Km ("Air
low speed" model), situated on both sides of "ground" ruler
(Ground speed & bearing), it only remains for you to measure the
distance to travel and multiply it with the base factor (Fb) to
know the necessary time for your navigation; and the to precisely
calculate your oil quantity.
...It's very easy! Divide by 2 all speeds, BUT NOT THE DRIFT
READING.
example: "Air high speed" model
I foresee 040 heading, a 160 kt speed without wind
and 30 kt wind from 180°. I set respectively 80 kt and 15 kt
on the ruler and I directly read the DRIFT (without division),
that is 7°. My new heading on the azimuth is 047. My new
speed 184 kts (92 kts x 2).
"Air low speed" model
I foresee 040 heading, a 160 km/h speed without
wind and 30 kt wind from 180°. I set respectively 80 km/h
and 15 kt on the ruler and I directly read the DRIFT (without
division), that is 12°. My new heading on the azimuth is 052.
My new speed 200 kms/h (100 kms/h x 2).
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