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5

gliders. Furthermore it is full of small details destined to enhance the 
pilots’ comfort and to improve the performance of the SLE, RAM, DRS, 
TNT and 3 line profile.

The use of the SLE (Structured Leading Edge) allows reinforcement of the 
leading edge preventing any deformation during turbulence. The airflow 
is also vastly improved over the entire front span of the glider.
(See 

http://niviuk.com/technology.asp?id=JNKPKPN4

)

The RAM AIR INTAKE technology presents an internal positioning for the 
air entrance to allow an optimal maintenance of the internal pressure as 
well as an improving of the laminar flow on intrados. What’s the result?
Gaining turbulent air absorption in the leading edge, more consistent at 
every speed and a better performance while assuring maximum security.
(See 

http://www.niviuk.com/technology.asp?id=JNKQKNP4

)

DRS.-The trailing edge has been reinforced with small ribs that make this 
part flatter in order to spread the pressure out evenly. It means better 
air-flow and less drag on this important part of the glider. The addition 
of these ribs gives exceptional handling (better and more efficient when 
turning) and more control and precision.

TNT.- It is a technical revolution. It underlines building the internal 
structure of the glider with Nitinol to make the profile more uniform and 
the glider lighter for better flight performance. Moreover, the Nitinol is 
resistant to deformations, hot temperatures and breaks as well as more 
resistant to the glider folding process.

3LT.-Its powerful profile, a detailed internal architecture structure and the 
use of high-tech strength materials make possible a significant reduction 
of the total length of suspension lines in order to reduce the parasite 
resistance and the weight of the glider to gain efficiency.

Not a single millimeter of error is possible in the manufacturing process 
from Olivier’s computer to the cutting of the fabric. An automatic process 

controlled by a laser-cutting program cuts each of the sections that 
compose the different parts of the wing. This program not only cuts the 
pieces of fabric but it also paints the guideline marks that will aid the 
assembly; it also numbers the separate pieces of material. All this is 
carried out before human handling of the pieces begins. So we eliminate 
possible and understandable errors that may occur during this delicate 
procedure.

The lines are semi-automatically manufactured and all the sewing is 
finished under the supervision of our specialists. The jigsaw puzzle of the 
assembly process is made easier using this method. We minimize the 
processes while making the quality control more efficient. All the different 
parts of the canopy are cut and assembled under the strict conditions 
induced by the automation of the whole process. 
It is strongly recommended that all lines are thoroughly checked by the 
pilot prior to every flight and ultimately checked by a service centre or 
Niviuk dealer after every 100 hours of flight. We should not forget that we 
are using materials with great performance but that they need a rigorous 
check before every flight. 

All NIVIUK Gliders go through an extremely thorough and efficient final 
inspection.
Every single line of each glider is measured individually once the final 
assembly has concluded. Each wing is then individually inflated for the 
last visual revision.

Each glider is packaged following the maintenance and conservation 
instructions recommended for the advanced materials. NIVIUK Gliders 
are made of first class materials as demanded by the performance, 
durability, and homologation requirements of the present-day market. 

Information about construction materials is given on the last pages of this 
manual.

Содержание IKUMA 21

Страница 1: ...USER S MANUAL IKUMA...

Страница 2: ...this wing and that you will soon understand the meaning of our slogan The importance of small details This is the user s manual that we recommend you to read in detail The NIVIUK Gliders Team USER S...

Страница 3: ...TIONS 8 4 IN FLIGHT 8 4 1 FLYING IN TURBULENCE 8 4 2 POSSIBLE CONFIGURATIONS 8 4 3 USING THE ACCELERATOR 10 4 4 FLYING WITHOUT BRAKE LINES 10 4 5 KNOTS IN FLIGHT 10 5 LOSING HEIGHT 11 5 1 EARS 11 5 2...

Страница 4: ...ion on the flight test report made by the certification laboratory and specially attention to the test pilot comments Point 25 on the flight test report On the flight test report there is all necessar...

Страница 5: ...e glider to gain efficiency Not a single millimeter of error is possible in the manufacturing process from Olivier s computer to the cutting of the fabric An automatic process controlled by a laser cu...

Страница 6: ...rd EN12491 This certification allows it to be flown with most of the harnesses on the market even the ones that use cocoon We strongly recommend that you adjust the distance of the chest strap accordi...

Страница 7: ...without any pilot input Both brake lines should be symmetrical and measure the same length The most recommended knots are the clove hitch knot or bowline knot When changing the brakes length it is ne...

Страница 8: ...in passive flight thus offering a high level of safety in turbulent conditions Nonetheless the pilot always has to pilot according to the prevailing weather conditions the pilot is the ultimate safety...

Страница 9: ...dy to any side WITHOUT PULLING ON THE BRAKE LINES Deep stall The possibility of the IKUMA falling into this configuration during normal flight is very unlikely This could happen if you are flying at a...

Страница 10: ...mountainside or in very turbulent conditions If necessary you will have to constantly adjust the movements and pressure on the accelerator whilst constantly adjusting the pressure applied to the brak...

Страница 11: ...rst discovered by our Niviuk team Pilots in 2009 while flying a competition prototype wing which because of its line plan and high aspect ratio would not allow big ears to be applied In fact big ears...

Страница 12: ...re leaning You can regulate the intensity of the turn by applying a little outside brake A paraglider flying at its maximum turn speed can reach 20 m s equivalent 70 km h vertical speed and stabilize...

Страница 13: ...ipment in the trunk of your car Temperatures inside a car parked in the sunlight can be very high Inside a rucksack and in the sunlight temperatures can reach 60 C Weight should not be laid on top of...

Страница 14: ...14 The entire equipment and components are covered by a 2 year guarantee against any manufacture fault The guarantee does not cover misuse or abnormal use of the materials...

Страница 15: ...IMUM m 2 33 2 44 2 52 2 62 2 74 MINIMUM m 0 54 0 56 0 58 0 61 0 63 AVERAGE m 1 92 2 01 2 07 2 16 2 26 LINES TOTAL METERS m 220 230 238 247 259 HEIGHT m 6 67 6 98 7 2 7 49 7 83 NUMBER 165 165 165 165 1...

Страница 16: ...DC 060 LIROS GMHB GERMANY UPPER CASCADES DC 100 LIROS GMHB GERMANY UPPER CASCADES A 8000 U 50 EDELRID GERMANY MIDDLE CASCADES TNL 080 TEIJIM LIMITED JAPAN MIDDLE CASCADES DC 060 LIROS GMHB GERMANY MID...

Страница 17: ...10 3 RISERS ARRANGEMENT 17...

Страница 18: ...c9 c10 c11 d1 d2 d3 d4 br1 br2 br3 br4 d5 d6 br5 br6 br7 br8 br9 br10 2A1 2A2 3 A 1 2B1 2B2 3 B 1 2C1 2C2 3 C 1 2 D 1 2 D 2 2A3 2A4 2B3 2B4 2C3 3A2 3B2 3C2 2C4 2 D 3 2 A 5 s t a b 2BR1 2BR2 3BR1 4BR1...

Страница 19: ...186 10 5535 5471 5496 6145 11 5364 5353 5381 RISERS LENGHT m m A B B C 480 480 480 480 STANDARD 360 380 400 480 ACCELERATED LINES HEIGHT m m A B C D br 1 6517 6427 6538 6614 7308 2 6397 6309 6379 6466...

Страница 20: ...720 10 6013 5943 5970 6678 11 5827 5815 5846 RISERS LENGHT m m A B B C 480 480 480 480 STANDARD 360 380 400 480 ACCELERATED LINES HEIGHT m m A B C D br 1 7039 6943 7062 7146 7880 2 6913 6819 6893 6989...

Страница 21: ...7 7767 3 7205 7110 7197 7297 7515 4 7245 7156 7310 7395 7559 5 7147 7072 7169 7272 7422 6 7015 6953 7017 7123 7293 7 6923 6875 6933 7296 8 6875 6834 6919 7310 9 6881 6843 6972 7365 10 6612 6536 6566 7...

Страница 22: ...6 A 7 A 8 A 9 A 10 B 11 A 12 A 13 A 14 B 15 A 16 A 17 A 18 A 19 A 20 A 21 A 22 A 23 0 24 Class B In accordance with EN standards 926 2 2013 926 1 2006 PG_0962 2015 Date of issue DMY 13 11 2015 Manufac...

Страница 23: ...4 1 B 2 A 3 A 4 A 5 A 6 A 7 A 8 A 9 A 10 B 11 A 12 A 13 B 14 B 15 A 16 A 17 A 18 A 19 A 20 A 21 A 22 A 23 0 24 Class B In accordance with EN standards 926 2 2013 926 1 2006 PG_0964 2015 Date of issue...

Страница 24: ...der s weight kg 5 7 Range of trimmers cm 0 Number of risers 3 Total speed range with accessories km h 25 Projected area m2 24 56 Harness used for testing max weight Inspections whichever happens first...

Страница 25: ...The importance of small details niviuk com...

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