background image

19

RAPID DESCENTS

Spiral dive:

Big ears: 

A spiral dive is the fastest way to lose altitude, however, the very high G-forces make 
it difficult to sustain a spiral dive for long and it can place high loads on the pilot and 
glider. By tensing ones abdominal muscles and a higher body tension you can to 
some extent resist the high G-forces. Don't forget proper breathing! As soon as any, 
even slight, light dizziness or impaired vision is noticed the spiral should be exited 
immediately.

The Envy 2 has a very effective spiral dive. This allows rapid descent without stalling. 
To enter a spiral dive the pilot should weight-shift on one side while slowly pulling the 
brake gradually on the same side as weight-shifting. During a spiral dive the angle of 
bank can be controlled by increasing or reducing the amount of inside brake. When 
spiral diving the Envy 2 it is recommended that the outside brake is lightly applied. 
This helps stabilize the wing and enables an easier and safer exit from the spiral. To 
exit, release the inside brake slowly. The Envy 2 did not show a tendency to remain 
in a stable spiral during testing. At high sink speeds or if the pilot keeps his weight on 
the inside, the wing can stay in a continued deep spiral and has to be actively exited. 
This is done by weight shifting to the outside and gentler braking of the outside wing.

WARNING!!  Nearly all gliders will have a tendency to stay in the spiral if the sink-rate 
exceeds around 15-m/s, depending on weight-shifting, wing loading and G-force. In 
fact most gliders need a counter-input to end a turn. 

Attention!  Due to energy retention, the glider will climb a lot after a deep spiral-dive 
release. If you apply inner brake and decelerate the glider for two or three turns, big 
pendulum effects can be avoided. 

WARNING!!  Practise spiralling with caution and lower sink-rates to get a feel for the 
gliders behaviour. A pilot who is dehydrated or not accustomed to spiralling can lose 
consciousness in a steep spiral dive!

When in big-ears, the horizontal speed is higher than the sink rate, unlike a spiral dive or 
a B-line stall. This rapid descent technique is used to quickly and horizontally exit a 
dangerous area in the desired direction. In order to collapse the outside wing, pull the 
outside A-lines.   

When the pilot holds the outside A1-risers on both sides and pulls them down, the 
Envy 2 easily tucks the outside wings and enters a stable descent mode. The pilot 
keeps hold of the brake handles along with the outside A1-risers in his hands. By 
braking on one side and weight-shifting, the canopy remains steerable.

20

In order to increase the sink rate as well as the horizontal speed, this manoeuvre 
should be done together with use of the speed system. Apply the speed system after 
big ears are induced (step into the speed-bar before you grab the outer A1-risers). 
Big-ears substantially reduces the risk of canopy stability problems in turbulent air. To 
exit Big-ears release the A1-risers. The canopy does slowly self-recover. If not, or to 
quicken the recovery, the pilot can gently apply brakes to the glider.

WARNING!  Never do big-ears in spirals, as this may drastically reduce the number 
of lines taking the already high loads, causing structural failure.

Attention! All rapid descent techniques should first be practised in calm air and with 
sufficient height so the pilot can use them in emergency situations!  By far the best 
technique is to fly correctly and safely, so you never have to descend rapidly!

B-line stalls: 

Summary: 

To induce a B-line stall symmetrically pull down slowly on both B-risers, until the canopy 
folds (parallel to its long axis). The airflow over the top surface is almost fully detached and 
the canopy enters a vertical descent flight mode without forward movement. Further 
pulling of the B-risers reduces the surface area more and increases the sink rate. (Up to 8 
m/s) Be careful, pulling too far or too rapidly may cause a frontal horseshoe to form. To exit 
from this flight mode release the B-risers at first rapidly but then gently (1 sec). The canopy 
surges forward re-attaching the airflow over the top surface and resumes normal flight. 
When the B-risers are released, the brakes should not be activated. This will give the 
canopy the chance to gain speed and resume normal flight. On exit from a B-line stall on no 
account just release the B-risers, as this can cause overloading. If canopy does not 
recover apply both brakes gently to recover or pull the A-risers, until the canopy regains 
forward speed.

For all extreme manoeuvres and rapid descents please note:

!

first practise manoeuvres with an instructor during safety training!

!

before inducing any manoeuvre the pilot must check that there are no other airspace 
users below him!

!

during the manoeuvre the pilot must have the canopy within his view!

Содержание Envy 2

Страница 1: ... TECHNOLOGY LTD 1 máje 823 756 61 Rožnov pod Radhoštěm Czech Republic Tel 420 571 842 235 Tel fax 420 571 842 332 e mail mailbox macpara cz www macpara com 2 ENVY 2 ENVY USER MANUAL Version 1 0 Stand 30 05 2009 ...

Страница 2: ... most out of your glider and enjoy many nice flights MAC PARAwish you many pleasant flights with your Envy 2 Paragliding is a sport which demands besides the optimum equipment a high degree of attentiveness good judgement and theoretical knowledge Paragliding can be a dangerous sport which may lead to injury and death This paraglider meets at the time of delivery requirements of the EN European No...

Страница 3: ... glider remains stable and controllable over a wide range of normal and abnormal flight conditions Nevertheless turbulence and gusting winds can lead to a partial or complete collapse of the canopy Therefore never fly in such conditions Any changes made to this paraglider invalidate the certificate of airworthiness 4 OVERALL PLAN Main karabineer Brake handle Main brake line Brake line Stabilizer L...

Страница 4: ...A mark on the main brake line indicates the position of the brake handle This adjustment on the one hand allows sufficient brake to be applied during extreme flying situations and when landing while on the other hand this ensures that brakes are not permanently applied to the canopy especially when fully accelerated This trimming should not be altered For differentiation purposes the A lines are c...

Страница 5: ...2 Top Sail Trailing Edge SKYTEX 40 E38A 100 nylon 6 6 33 Dtex 40 g m 2 Bottom Sail SKYTEX 40 E38A 100 nylon 6 6 33 Dtex 40 g m 2 Main ribs Diagonals SKYTEX 40 E29A 100 nylon 6 6 33 Dtex 40 g m 2 Ribs SKYTEX 40 E38A 100 nylon 6 6 33 Dtex 40 g m 2 Reinforcement Main Ribs Grille Polyester 200 g m 2 Reinforcement Ribs W382 Polyester 180 g m EDELMAN RIDDER CO Achener Weg 66 D 88316 ISNY IM ALLGEAU GERM...

Страница 6: ... after flying extreme manoeuvres or after tree landings or similar Inspection of the canopy for tears or damage especially the seams which join the ribs to the upper and lower surfaces but also the area of the attachment tapes and brake line connections Inspection of the lines for damage to the stitches The line lengths must be checked after 50 hours flying time and whenever the flight behaviour o...

Страница 7: ...t they do not catch on anything It is equally important to untangle the brake lines so that they are clear and can not catch on any thing during launch The brake lines should run freely through the pulleys to the trailing edge of the canopy Make sure the risers are not twisted this can prevent the brake lines from running freely through their pulleys It is often impossible to untangle lines during...

Страница 8: ...still occur release the speed system immediately and correct the collapse as described below Attention Do not apply brakes when fully accelerated Braking increases lift near the trailing edge The main lift point moves backwards Due to this the wing can loose stability for a short time Flight Accelerated Flight 14 Steering turns Active Flying Thermaling and Soaring Approach and Landing The Envy 2 i...

Страница 9: ...dling always use a certified combination of engine harness and glider If in doubt check with your federation Contact the manufacturer or importer for the current legality of motorized flight WARNING The Envy 2 is not suitable for jumps from aircraft WARNING The Envy 2 is not designed to be used for aerobatics MOTORISED FLIGHT 16 Asymmetriccollapse Cravat Line over Front Tuck Anegativeangleofattack...

Страница 10: ...ider may surge almost 90 and suffer an extensive asymmetric collapse The danger of overcorrecting and overreacting exists during all extreme flight manoeuvres Thus any corrective action must be gentle and steady and done with feel 18 Spin or negative spin Wingover Alternative emergency steering Pulling brake on one side too fast or too hard can result in a negative spin During a spin the canopy tu...

Страница 11: ...s When the pilot holds the outside A1 risers on both sides and pulls them down the Envy 2 easily tucks the outside wings and enters a stable descent mode The pilot keeps hold of the brake handles along with the outside A1 risers in his hands By braking on one side and weight shifting the canopy remains steerable 20 In order to increase the sink rate as well as the horizontal speed this manoeuvre s...

Страница 12: ... to the centre cell as this can cause constant stress on the centre cell centre cell always to the outside Clean the paraglider with water and a soft sponge Do not use any chemicals or spirits for cleaning as these can permanently damage the cloth Deterioration a few tips LOOKING AFTER YOUR PARAGLIDER 22 Storage Repairs and checks Disposal In Conclusion Store the paraglider in a dry space at ambie...

Страница 13: ... t leave any waste don t make needless noise and respect the sensitive biological balance in the mountain eco system especially in the takeoff area LINE PLANS Line descriptions The following printed line plans show the line configurations and line lengths TREATING NATURE WITH RESPECT 24 Line plan Envy 2 Envy 2 23 S ...

Страница 14: ...25 Line plan Envy 2 Envy 2 25 M 26 Line plan Envy 2 Envy 2 28 L ...

Страница 15: ...7281 7360 8350 2 7061 6962 7034 7167 7239 8010 3 7098 7009 7078 7209 7270 7820 4 7037 6956 7016 7140 7201 7650 5 6937 6866 6914 7024 7066 7565 6 6950 6886 6929 7023 7052 7405 7 6814 6758 6801 6846 7240 8 6649 6609 6638 6674 7160 9 6582 6551 6559 6589 7155 1 0 6524 6488 6492 7085 Stab 1 1 6345 6228 6207 6219 7025 6965 6940 7010 Center A B C D E BR 1 6835 6741 6813 6940 7015 7950 2 6730 6636 6704 68...

Страница 16: ...510 7562 7683 7728 8295 6 7602 7532 7579 7682 7712 8140 7 7453 7392 7438 7488 7960 8 7272 7228 7261 7300 7870 9 7199 7165 7174 7207 7865 1 0 7136 7096 7100 7750 Stab 1 1 6939 6811 6789 6802 7690 7600 7570 7650 Center A B C D E BR 1 7470 7367 7446 7585 7667 8700 2 7355 7252 7327 7466 7541 8345 3 7394 7301 7373 7510 7573 8150 4 7330 7246 7308 7438 7501 7970 5 7226 7152 7202 7317 7360 7880 6 7240 717...

Страница 17: ... 6 x maximum take off weight and higher then 600 kg for theA B arrays Replacements for damaged lines must be with new original lines Line lengths are taken from the lines data page Components of the check Porosity Overall strength check Line strength check MANUAL FOR PARAGLIDER CHECKS 32 Line length measurement Canopyline attachmentpointscheck Canopyfabriccheck Lines Connectorcheck Risers Finalche...

Страница 18: ... 27 95 30 81 Area projected m2 20 98 23 34 25 33 27 93 Span flat m 11 53 12 16 12 67 13 30 Aspect ratio flat 5 74 5 74 5 74 5 74 Root cord m 2 56 2 70 2 81 2 95 Cells 56 56 56 56 Weight kg 5 80 6 0 6 25 6 6 Weight range kg 65 83 77 97 88 110 105 135 Min speed km h 23 25 23 25 23 25 23 25 Trim speed km h 36 38 36 38 36 38 36 38 Max speed accelerator km h 50 53 50 53 50 53 50 53 Glide ratio 8 8 8 8 ...

Отзывы: