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Piloting the wing is smooth and accurate. The wing turns efficiently 
without requiring major effort and without affecting the sink rate. Even at 
maximum load, the wing keeps its Niviuk DNA and turns easily.

Depending on the pilot’s needs and requirements, the trimmers ensure 
that a proper cruising speed can be maintained.

During the landing, the R-BUS shows its full potential and retains its  
speed like a real cruise liner of the air. These are not just empty words, 
we know this wing will land as you have always wanted to when flying 
with a passenger. Easy, well and safe!

PLEASE NOTE!

It is very important to become familiar with the correct use of the main 
steering elements: the trimmers, High Speed Tip and the main brakes. 
We recommend paying particular attention and concentration when using 
the different steering elements.

1.4 ASSEMBLY, MATERIALS

The R-BUS has all the technological innovations used on other Niviuk 
gliders. It is built with the most careful selection of current materials, 
technology and accessories available, to improve pilot comfort whilst 
increasing safety and performance.

The RAM Air Intake system (RAM).

- Is characterised by the 

arrangement of the air inlets, to ensure optimal internal pressure is 
maintained. Thanks to this design, we were able to reduce their size, 
while maintaining the same air flow at all angles to improve laminar flow.
Having greater internal pressure means better tolerance of turbulence, 
greater consistency of the profile shape across the speed range; 
excellent handling at low speed is achieved by allowing the pilot 
to extend the braking limit, there is a lower risk of collapse and 
consequently, greater control and stability.

Titanium Technology (TNT).

– A revolutionary technique using titanium. 

Using Nitinol for the internal wing construction offers great advantages: 
on the one hand it reduces the overall wing weight, which reduces the 
inertia and improves the manoeuvrability and launch inflation.
On the other hand, 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.

Reflex System Profile (RSP).

- The reflex profile of the R-BUS is 

Summary of Contents for R-BUS

Page 1: ...USER S MANUAL R BUS...

Page 2: ...w wing concept A great traveller ready for great journeys This is the user manual and we recommend you read it carefully The NIVIUK Team USER S MANUAL NIVIUK GLIDERS R BUS This manual provides you wit...

Page 3: ...T PLAN 9 3 4 PRE FLIGHT CHECK LIST 9 3 5 WING INFLATION CONTROL AND TAKE OFF 10 3 6 LANDING 10 3 7 FOLDING INSTRUCTIONS 10 4 IN FLIGHT 10 4 1 DOUBLE STEERING SYSTEM 11 4 2 FLYING IN TURBULENCE 11 4 3...

Page 4: ...raglider invalidates the certification It is important to note that different sized wings will react differently during manoeuvres Even within the same size at maximum or minimum load the behaviour an...

Page 5: ...y TNT A revolutionary technique using titanium Using Nitinol for the internal wing construction offers great advantages on the one hand it reduces the overall wing weight which reduces the inertia and...

Page 6: ...tated by the automation of this process Every wing is individually checked with a final visual inspection The fabric used to manufacture the glider is light resistant and durable The fabric will not e...

Page 7: ...cturer s specification on attachment points PLEASE NOTE Check that all the connections used maillons carabiners quick outs etc are appropriate and certified to carry the all up load 2 4 HARNESS TYPE T...

Page 8: ...nal way 2 6 ADJUSTING THE BRAKES The length of the main brake lines and the High Speed Tip are adjusted at the factory However they can be changed to suit the pilot s flying style or lengthened to acc...

Page 9: ...ing and less fuel consumption Accelerated position as the trimmer is released the travel of the C and D risers increases progressively and therefore the angle of attack changes This way the wing will...

Page 10: ...life of your paraglider It should be concertina packed with the leading edge reinforcements flat and the flexible rods stacked one on top of the other This method will keep the profile in its origina...

Page 11: ...sists of a line with three attachment points located at the wingtip It enables the pilot to correct the direction easily and accurately without using the main brake controls and therefore the performa...

Page 12: ...deflated 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 the default flying speed Frontal collapse Due...

Page 13: ...ed 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 on this line until it is taught as it should help undo th...

Page 14: ...taneously smoothly pull them outward and downward The wingtips will fold in Let go of the risers to re inflate them automatically If they do not re inflate gently pull on one of the brake lines and th...

Page 15: ...OBATIC FLIGHT Although the R BUS was tested by expert acrobatic pilots in extreme situations it was not designed for it We do not recommend using this glider for acrobatic flying Acrobatics is still a...

Page 16: ...g is not compressed and it should be stored loosely without direct contact with the ground Humidity and heating can have an adverse effect on the equipment 7 3 CHECKS AND CONTROLS A complete inspectio...

Page 17: ...oes not cover misuse of the equipment DISCLAIMER Paragliding is an activity requiring concentration specific knowledge and sound judgment Beware Learn your skills under the supervision and guidance of...

Page 18: ...G 15 15 CORD MAXIMUM m 3 24 3 37 MINIMUM m 0 71 0 74 AVERAGE m 2 62 2 72 LINES TOTAL METERS m 426 444 HEIGHT m 8 41 8 75 NUMBER 288 288 MAIN 3 1 5 3 2 3 1 5 3 2 RISERS NUMBER 4 A A B C D A A B C D TRI...

Page 19: ...E SUPPLIER UPPER CASCADES PPSL 120 LIROS GMHB GERMANY MIDDLE CASCADES PPSL 120 LIROS GMHB GERMANY MIDDLE CASCADES PPSL 200 LIROS GMHB GERMANY MIDDLE CASCADES TNL 80 TEIJIM LIMITED JAPAN MIDDLE CASCADE...

Page 20: ...20 10 3 RISERS LAYOUT...

Page 21: ...21 10 4 LINE PLAN...

Page 22: ...7612 17 7392 7359 18 7328 7331 RISERS LENGTH m m A A B C D 350 350 350 350 350 STANDARD 350 350 350 402 455 TRIMMER OPENED LINES HEIGHT m m A B C D E br Tip br 1 8364 8261 8294 8412 8565 8182 9479 2...

Page 23: ...The importance of small details niviuk com...

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