Niviuk IKUMA 2 Скачать руководство пользователя страница 5

5

extraordinary quality.   

It is lightweight; even lighter in flight and easy to pilot, with outstanding 
turbulence buffering and a surprising range of speed for incredible glides.

1.4 CONSTRUCTION, MATERIALS

The IKUMA 2 has all the technological innovations used on other Niviuk 
gliders and is built with the most careful selection of current materials. It 
has all the current technology and accessories available to improve pilot 
comfort whilst increasing safety and performance.
In the design of all Niviuk products the team aims to ensure development 
and continuous improvement. The technologies developed in recent 
years have allowed us to develop greater, better wings. It is in this 
context that we would like to introduce the technologies included in this 
new model. 

RAM Air Intake 

- this system is characterised by the arrangement of the 

air inlets, to ensure optimal maintenance of internal pressure. Thanks to 
this design, we were able to reduce their size, while maintaining the same 
air flow at all angles to improve laminar flow. More consistency across 
the whole speed range and better performance without compromising on 
safety.

Titanium Technology (TNT)

 - a revolutionary technique using titanium. 

Using Nitinol in the internal construction provides a more uniform profile 
and reduces the weight to gain efficiency in flight. Nitinol provides the 
highest level of protection against deformation, heat or breaks. The 
leading edge is more rigid and the wing surface remains perfectly taut, 
without creases or parasitic drag.  This optimises glide in all phases of 
the flight.  Because the flexible rods always return to their original shape, 
the integrity of the profile is never affected.  Nitinol provides the highest 
level of protection against deformation, heat or breaks.

Structured Leading Edge (SLE)

 - the use of the SLE considerably 

reduces the amount of Mylar which was used in previous Niviuk wings 
and this also reduces the weight of the leading edge. Therefore it is 
easier to inflate this wing than a paraglider without this system.

3D Pattern Cut Optimisation (3DP)

 – the latest generation of wings 

require a new fabric panel pattern and cutting system. Creating separate 
panels for each of the sections at the front of the wing means the sail 
fabric is more taut and crease-free. During the cutting, the optimal 
orientation of the fabric section is selected, depending on its final 
location. If the fabric pattern is properly aligned with the axes of load, it 
suffers less deformation after repeated use, to the long-term benefit of 
the leading edge.

3D Leading Edge (3DL)

 - adding an extra seam to the longitudinal 

axis of the glider helps, on the one hand, give more consistency and 
volume to the profile (a more efficient 3D contour) and on the other, joins 
and shapes the leading edge panels. The fabric is guided by the panel 
position to ensure fewer creases and better load distribution. The result 
is a cleaner profile, which benefits the wing in terms of performance and 
durability.

Structured Trailing Edge (STE) 

- Optimises the profile without 

deforming it. The circulation of the air is more fluid, ensuring a cleaner 
airflow.  When changing the angle of attack or when accelerated, the 
profile remains more uniform and the after braking, the wing returns to 
trim more progressively, faster and more actively. 

Drag Reduction Structure (DRS)

 - The trailing edge has been reinforced 

with small ribs in order to distribute the pressure more evenly. This results 
in excellent manoeuvrability and greater control and precision.

Radial Sliced Diagonal (RSD)

 - A reinvention of the wing’s internal 

structure. This new design is based on individual diagonal panels 
arranged in radial form, which increase the efficiency of the internal 

Содержание IKUMA 2

Страница 1: ...IKUMA 2 User s manual...

Страница 2: ...or small details which is reflected in this new design by the NIVIUK R D team with Olivier Nef at the helm We are confident you will enjoy flying this glider and will soon discover the meaning of our...

Страница 3: ...IN FLIGHT 10 4 1 FLYING IN TURBULENCE 10 4 2 POSSIBLE CONFIGURATIONS 11 4 3 ACCELERATED FLIGHT 12 4 4 FLYING WITHOUT BRAKE LINES 12 4 5 KNOT S IN FLIGHT 12 5 LOSING ALTITUD 13 5 1 BIG EARS 13 5 2 B3...

Страница 4: ...safety and very forgiving flight characteristics Gliders with high collapse resistance outside normal flight Description of the skills required by the pilot to fly an EN B wing Designed for all pilots...

Страница 5: ...heat or breaks Structured Leading Edge SLE the use of the SLE considerably reduces the amount of Mylar which was used in previous Niviuk wings and this also reduces the weight of the leading edge The...

Страница 6: ...ollowing specific maintenance instructions as recommended by the fabric manufacturer Niviuk gliders are made of premium materials that meet the requirements of performance durability and certification...

Страница 7: ...6 43 cm Size 28 44 44 cm Size 30 43 44 cm Care should be taken with the chest strap setting as the distance of the chest strap setting will affect the handling of the glider If the chest strap is too...

Страница 8: ...manufacturer The majority of harnesses have a speed system pre installed The standard connection of the speed bar to the speed system is via Brummel hooks where two slots in the hooks are interlocked...

Страница 9: ...consideration this extra distance during acceleration With this profile deformation there is a risk of generating turbulence and causing a frontal or asymmetric collapse 3 THE FIRST FLIGHT 3 1 CHOOSE...

Страница 10: ...a pack the wing with each rod on top of the other and then fold the wing as required This folding system ensures that both the fabric and the reinforcements of the internal structure are kept in perfe...

Страница 11: ...opening of the collapsed glider side Do not over brake or slow down the flying side of the wing control the turn Once the collapsed side is open make sure you return to normal flying speed Frontal col...

Страница 12: ...e turn Then locate the 3STI stabilo line attached to the wing tip trapped between the other lines This line has a different colour and is located on the outside position of the B riser Pull this line...

Страница 13: ...andles because there will be an increased risk of stalling the wing or entering a negative spin Before attempting to clear a knot make sure there are no other pilots flying in the vicinity 5 LOSING AL...

Страница 14: ...liner wings can often prove difficult With the current 2 or 3 liner wings the inability to pull big ears or the risk involved in doing so concerns many pilots who want to have a controlled rapid desce...

Страница 15: ...body With practice you will fully appreciate and understand it Only practise this manoeuvre at high altitude and with enough ground clearance To start the manoeuvre first weight shift and pull the bra...

Страница 16: ...re equipped with the latest technological advances gained from the experience of our R D team Careful maintenance of your equipment will ensure continued top performance Apart from the general checks...

Страница 17: ...est in this type of lines However one of the obligations derived from the use of these lines is the need to maintain the trim of your IKUMA 2 within the stipulated ranges We recommend checking the lin...

Страница 18: ...u have not been properly trained to use it Do not take advice or accept any informal training from anyone who is not properly qualified as a flight instructor 9 GARANTEE The equipment and components a...

Страница 19: ...19...

Страница 20: ...2 1 4 3 2 1 4 3 2 1 4 3 2 1 4 3 3 1 A A B C A A B C A A B C A A B C A A B C mm 145 145 145 145 145 Kg 65 85 75 95 85 105 95 115 105 130 Kg 4 1 4 4 4 6 4 9 5 2 B B B B B 10 TECHNICAL DATA 10 1 TECHNICA...

Страница 21: ...PLIER UPPER CASCADES DC 60 LIROS GMHB GERMANY UPPER CASCADES DC 40 LIROS GMHB GERMANY MIDDLE CASCADES DC 60 LIROS GMHB GERMANY MIDDLE CASCADES DC 40 LIROS GMHB GERMANY MIDDLE CASCADES A 8000 U 70 EDEL...

Страница 22: ...10 3 RISERS PLAN 22...

Страница 23: ...10 4 SUSPENSION PLAN 23...

Страница 24: ...0 340 340 383 470 A B C D BR 1 6930 6841 6938 7021 7384 2 6882 6794 6874 6961 6965 3 6842 6754 6833 6919 6822 4 6852 6765 6862 6941 6850 5 6794 6710 6807 6885 6699 6 6761 6678 6761 6839 6538 7 6710 66...

Страница 25: ...0 340 340 383 470 A B C D BR 1 7820 7716 7828 7921 8321 2 7768 7664 7756 7855 7851 3 7728 7625 7715 7812 7692 4 7741 7638 7749 7838 7726 5 7680 7579 7689 7777 7560 6 7644 7544 7637 7725 7381 7 7586 74...

Страница 26: ...55 7841 6 7912 7815 7911 8001 7657 7 7856 7765 7859 7943 7620 8 7873 7784 7895 7956 7758 9 7782 7704 7788 7585 10 7686 7614 7691 7524 11 7576 7519 7595 7496 12 7544 7478 7560 7594 13 7267 7240 7258 14...

Страница 27: ...A 5 A 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 B 19 A 20 A 21 A 22 A 23 A Classification B In accordance with standards EN 926 1 2015 EN 926 2 2013 and LTF NFL II 91 09 PG_1628 2019...

Страница 28: ...A 3 B 4 A 5 A 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 B 19 A 20 A 21 B 22 A 23 0 Classification B In accordance with standards EN 926 1 2015 EN 926 2 2013 and LTF NFL II 91 09 PG_16...

Страница 29: ...niviuk com...

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