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-- front/symmetrical tuck collapse

A front tuck /collapse is a symmetric tuck of the leading edge of the wing, starting from the cen-
tre of the canopy to the wing tip. This can be either a tucking of just the central part of the lead-
ing edge of the glider, which can sometimes cause a front 'horseshoe' or 'rosette-ing' of the glid-
er, or even a complete 'blow-out' of the whole canopy in extreme situations.

When flying, a front tuck may occur while leaving a strong thermal, or more often while using the
speed system in turbulent air, or sometimes whilst flying down-wind of another paraglider 

&

being

'waked' by the wing tip vortices of the glider and turbulence wake turbulence of the pilot.

Remember, the pilot can learn to help stop collapses by flying 'actively', but if a front tuck does
occur it will easily clear itself. Re-inflating the wing can be helped by correct pilot input and, once
the glider is overhead, symmetrically applying 40 % of both brakes 

&

then releasing immediately

will get pressure back in to the glider and speed up the recovery. Do not brake when the glider is
behind you, as this can stall the wing, but wait for the glider to come forwards above your head,
then brake.

-- 

asymmetric stall (spin)

This is a very difficult situation for the pilot to provoke with the 

ZEPHYR-2

, given it's very

low stall speed, you have to really abuse the controls a lot to manage it. Even so, this situa-

tion can be induced if, say, the pilot is turning very slowly in a thermal (near the stall point),

and wants to tighten the turn even more, and at the same time as smoothly lifting the out-

side brake (which is the correct thing to do), if the pilot simultaneously brakes more on the

inside brake, this may stall the inside wing which will then go into spin. One half of the wing

flies forwards, whilst the other flies backwards (negative). In this case to return to normal

flight, one has to raise the inside brake, returning air speed to the inside wing, which will

cause the wing to surge and dive forwards. This dive can be more or less violent, depending

on what stage that the flat spin is in, how much the spin had been allowed to develop, and

the moment at which the brake is lifted. If the pilot wants to intervene to dampen this dive,

they will have to adopt a position (roughly) of something more than half brake, which must

then be released as soon as the dive is stopped, or the wing may then go back into a stall or

spin. Another option is to put the glider directly into a full stall immediately that the spin is

entered, and from this the exit is more symmetric with less chance of a twist.

> landing

Choose a large field clear of all obstructions 

&

in a clean laminar airflow.

A  different  technique  is  needed  for  different  wind  strengths.  Every  landing  should  be

judged differently even if it’s your local site.
On final approach the pilot should have hands up (keeping a feel of the wing in case of

unexpected turbulence) so the glider has energy for a flare. In light or nil winds the pilot

will need a committed symmetric flare at around 1 meter above the ground. 

Содержание ZEPHYR-2 L

Страница 1: ...ZEPHYR 2 m a n u a l ...

Страница 2: ......

Страница 3: ...3 Windtech w w w w i n d t e c h e s ZEPHYR 2 S M L flight manual ...

Страница 4: ...ng wind 9 thermal flying 9 flying in turbulence 10 asymmetric tuck 10 frontal tuck 10 asymmetric stall spin 11 landing 11 weather to fly 12 emergency procedures quick descent techniques 12 big ears 12 spiral drive 13 b stall 13 maintenance 14 warranty 14 technical specifications 15 line measurements 17 flight log 19 ...

Страница 5: ...ive boost and take you easily to new levels of acheivement We strongly recommend that before you even unfold the ZEPHYR 2 you read this man ual carefully in order to be aware of any general limitations performance characteristics take off and flight characteristics landing procedures dealing with emergency situations and general maintenance We appreciate your feedback so please send us your commen...

Страница 6: ...t the user s own risk As with any adventure sport paragliding is a high risk activity especially without taking the appropriate precautions therefore it must be absolutely understood that Windtech the dealer do not accept any responsibility for accidents losses injuries direct or indirect damage following the use or misuse of this product design materials The ZEPHYR 2 offers total securi ty along ...

Страница 7: ...over weight can adversely affect the stability of the ZEPHYR 2 flown as such it will no longer be certified best glide the speed system Best glide in nil wind and still air is obtained at trim speed that is brakes fully released and no accelerator speed bar applied It is always best to fly with a light pressure on the brakes keeping a feel on the wing in case of unexpected turbulence When flying i...

Страница 8: ... kg of force for the majority of manoeuvres To reach the stall never recommended on any type of paraglider requires more than 9kg flight Each and every glider has a checklist note passed though our strict quality control in the factory This included line measurement ground inflation and flight testing Contact your dis tributor for more information about this and if your glider has not been pre inf...

Страница 9: ... many reverse launch meth ods techniques which the pilot can learn To progress well with your flying and to be a good pilot it is necessary to master at least one of the techniques If you can achieve 100 control your glider on the ground then you will be a better safer pilot in the air this will also help you to understand the dynamics of a paraglider in flight thermal flying The ZEPHYR 2 is truly...

Страница 10: ...ble situations asymmetrical tuck collaps An asymmetric tuck collapse is when part one side of the wing say 20 or even anything up to 90 of the span tucks or collapses usually induced by turbulence but sometimes also though poor pilot control in turns and wing overs The ZEPHYR 2 is tested and certified to automatically recover without correction by the pilot but with the correct input the pilot can...

Страница 11: ... pilot is turning very slowly in a thermal near the stall point and wants to tighten the turn even more and at the same time as smoothly lifting the out side brake which is the correct thing to do if the pilot simultaneously brakes more on the inside brake this may stall the inside wing which will then go into spin One half of the wing flies forwards whilst the other flies backwards negative In th...

Страница 12: ... flying in tur bulent air Remember that even an airline jet can crash due to rotors and bad weather emergency procedures quick descent techniques The following techniques are more advanced should be practiced ONLY with qualified radio supervision and adequate safety back up Always be prepared and consider what will happen if things go wrong With enough altitude it is possible to safely master thes...

Страница 13: ...rn the correct exit method i e progressively release the inside brake b stall The B line stall is a real stall even though the wing appears to be flying above your head the lam inar airflow over the wing is completely lost During B Stall the canopy falls perpendicularly to the ground straight down but drifting with the wind at a sink rate of 5 to 12 m s with an angle of attack of 90 degrees To ent...

Страница 14: ... all bottom lines This is very impor tant to maintain the flying and safety characteristics of the wing The rest of the lines must also be checked and if they have deteriorated then they need to be changed Test some of the lines that are not changed for minimum 40 of the rated strength If the line fails you should replace them all before using your glider Small tears in the sail can be repaired by...

Страница 15: ...ojected aspect ratio Max chord m Min chord m Nº cells Line lenght m Canopy weight kg Pilot weight kg Weight in fly Min max speed km h Max speed trim km h Certification speeds with medium range weight pilot at sea level S 26 30 22 90 12 00 9 63 5 56 4 05 2 70 0 47 54 7 46 5 2 55 70 75 90 22 54 38 Pend L 30 30 26 2 12 99 10 30 5 56 4 05 2 90 0 50 54 8 08 5 9 80 100 100 120 22 54 38 Pend ...

Страница 16: ...16 ...

Страница 17: ... 8 B3 R A1 M A2 M B1 M B2 M BR 1 BR 2 BR 3 BR 4 BR 5 BR 6 BR 7 BR 8 BR 9 BR 10 BR 11 BR 12 BR 13 BR 14 BR 15 BR 16 BR 17 BR 18 BR1 R BR2 R BR 0 BR1 M BR2 M BR3 M BR4 M BR5 M BR6 M B4 R A 11 B 11 C 11 C3 R C2 R C2 M C1 M A 12 B 12 C 12 D 12 A3 M B3 M C3 M BR7 M 27 28 26 19 22 21 23 20 18 17 14 15 16 12 10 11 6 5 7 8 9 13 24 25 2 1 4 3 Z E P H Y R 2 S M L ...

Страница 18: ...18 B A C D ç B A D ç C ...

Страница 19: ...19 flight log size date site duration flight details ZEPHYR 2 ...

Страница 20: ...POWERED BY WINDTECH francisco rodríguez 7 33201 g i j ó n spain p o box 269 33200 p 34 985 357 696 fax 34 985 340 778 email info windtech es web www windtech es ZEPHYR 2 ...

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