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#41
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Neils, this is really VERY, VERY clever. Actually it's elegant.
We have now heard of 300+ launches a day with one winch and launches to 5200 feet AGL with another. Lets say your only tug is doing 4 - 5 launches an hour at $75 each and you're #6 in the aero tow queue. The winch across the field is making a 2500 foot launch every 3 minutes for $10. (You're #6 because you failed to notice a solo student catch a thermal off a winch launch at 10:30 so everybody else got in front of you.) The tug will need a fuel stop every 5 or so launches but the winch will run all day on one tank. It's going to be 2PM before you get an aero tow. What do you do? What's not to like about winches.? Bill Daniels "Niels Erik Danielsen" wrote in message ... "Marc Ramsey" wrote in message ... Niels Erik Danielsen wrote: In our Club in Herning Denmark we have a 25 year old Diesel Electrical winch, controled by an industrial controller. http://www.herningsvaeveflyveklub.dk/jordmateriel.shtml Prior to launch the maximum wire tension is preset according to aircraft type, and the rest of the launch is basically automatic. It looks to be quite an interesting design. Does the generator drive AC traction motors directly through the controller, or are there batteries or some other form of buffer in the system? There is no buffer, all power is generated by the generator when needed. The frame consist of a late 60' SCANIA VARBIS tractor trailer, combined with two traction motors (used as winch motors)and generator from a diesel DC electric locomotive. The engine has been replaced with a newer more powerful turbo charged SCANIA engine. (This engine is used for both road driving, and winch.) The generator is mounted as a part of the drive shaft between the gearbox and the differential.(Rotating when in gear) The differential had two gears controlled by air pressure, one for normal road speed and another for reduced speed. As the pinion for the 'normal road speed' has been removed, it has become a `neural' allowing the generator to run without driving (moving) the winch. When the winch is moved the generator is still rotating, but not magnetized. The winch drums are mounted directly on the traction motors drive shafts. The first 'computer' was analog, and consists of a custom made circuit board filled with operational amplifiers, and passive components. This computer controls: Parking brake/Differential interlocking Throttle actuator for engine. Contactors for drum selection. Contactor for wire retrieve-braking dump load. Torque by excitation of the windings in the generator The systems measures: Engine RPM Engine Actuator position Generator speed. Wire speed. Torque derived from DC current, no tensiometer needed. DC Voltage. Wind speed. Wind direction component. Position of spring loaded torque/speed command handle. Calculation of power based on Current and Voltage. In the late 90' the analog controller was replaced with an industrial micro controller, but the functions as seen from the operator is essentially unchanged. Except for the possibility of connecting a PC via. a serial cable, and record a time track of the launch parameters. The max speed and max force is set on two dials. For an ASK21 the force is set at 550daN, and max speed is set to 125 km/h, Max. force is approx the weight of the glider, and max. speed is a speed approx. halfway between normal launch speed and max speed allowed in winch launch for type of glider. Then one of the drums are selected by pressing the Left or Right push button, this starts excitation of the generator and set the engine in high idle (ca. 1200 RPM) The spring loaded command handle has a manual control range for taking up the slack and at the end of launch bring down the chute. When the handle is full forward against it's stop a 'kick-down button' is activating the automatic sequence. During the launch the diesel engine RPM is controlled to ensure enough power (Max RPM used is about 1800 RPM) The set point for the speed/torque servo is ramped up (Ramp time approx 2 sec.) to the values given by the dials. (Power peaks at about 160KW for a heavy two seater) After acceleration, during the initial climb the speed set point is automatic ramped down to approx 70% since the glider now have a speed composant tangential to the winch. The decision on when to start speed ramp down is based on time calculated from the wind composant in launch direction. (My feeling is rampdown is done 4 to 10 secs into the launch) Later during the launch the max force (torque) is also ramped down, this is also based on time. When the glider is at an angle of approx. 75° the command handle is eased a little backward and the glider hook back releases. |
#42
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Andy wrote:
Graeme Cant wrote: I must have only flown off traditional winches. My experience is the same as Bill Daniels. What over-powered monster do you fly off? I have flown off winches at 5 UK sites and 5 US sites (9 different winches). I don't think any of them were over-powered monsters but most had enough power to see this effect. Please refer to "Gliding" by Derek Piggott, which was the standard UK text when I started flying gliders. Page 80 of fourth edition - "Unless the winch is seriously underpowered, steepening the climb will result in an increase in launching speed". Andy Well, I speak only from my experience, not from a book, no matter how eminent the author, and ... it's not MY experience. Clearly it's also not Bill Daniels' and several others. I note what you say about your experience and I'll learn from it. As for Derek Piggott's experience, I recommend the 7th Edition where he has modified his teaching somewhat and simply says (p.106, K&G edition) "Steepening the climb MAY result in an increase in launch speed..." (my emphasis). Earlier on that page, however, he also says "If the launch is too fast, for example, the glider pilot pulls back more..." He seems to have revised his views between the 4th and 7th Editions. That's the problem with citing authorities - they change their mind without telling you! My experience of winches (also on two continents - Snap!) tells me that European winches are generally more serious and powerful than the ones I'm used to. Nobody on this continent could afford a Skylaunch for example and nothing like it exists in my area. Not many exist in the US either judging by the fact that, like us, they appear to find the cost of a European winch is about the same as a brace of good Pawnees. Perhaps that explains why I said that "traditional winch" and "adequate power" didn't go together. I also used the words "overpowered monster" lightheartedly... ![]() GC |
#43
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Graeme Cant wrote:
Well, I speak only from my experience, not from a book, no matter how eminent the author, and ... it's not MY experience. Clearly it's also not Bill Daniels' and several others. I note what you say about your experience and I'll learn from it. I suspect that our experience of pitch effect on speed is not really that different. Neither of us has defined the conditions in sufficient detail. I think it's true to say that for any winch that is capable of maintaining constant tow line speed, pitching the glider up will result in an increase in airspeed. It is also true to say that continuous pitch up will not result in a continuous increase in airspeed. Either the winch has insufficient power to maintain line speed, or the tension limiter reduces line speed, or the glider weak link breaks. So I believe there is a cross over point for underpowered or tension controlled winches. For pitch/speed below the cross over point, increasing pitch results in increasing speed. Above the cross over point the reverse is true. For a tension and speed controlled winch I suspect that the cross over point is early in the launch and before the glider has established normal climb attitude. Thanks for the update on "Gliding". You are right, he didn't tell me he'd changed the text ![]() Andy |
#44
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I personally don't think that a constant force regulation results in an
ideal winch tows. I have observed a number of tows in which the glider was initially accelerated to quickly so that the pilot reacted by maintaining a low climb angle. This low angle results in lower force measured by the winch and leads to a further increase of power. In a Ka8 nearing Vne the only possible action is to abort the tow. At our airfield we use a system which transmits the airspeed of the glider to the winch operator. Pared with a good winch operator and a powerful winch, this results in very good winch tows. |
#45
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Interesting. What sort of telemetry equipment are you using? I had
proposed this several years ago but the consensus was that it would be too expensive to equip each glider with a telemetry transmitter. Constant tension puts all the sensors at the winch and requires no extra equipment in the glider. George Moore has written a series of excellent papers on automatic control of winch launches. George favors the constant tension approach but with cable speed regulation in the ground roll and rotation phases to prevent overspeeding the glider. These papers are available for download from the files section of the Yahoo group "winchdesign". Bill Daniels "alex8735" wrote in message oups.com... I personally don't think that a constant force regulation results in an ideal winch tows. I have observed a number of tows in which the glider was initially accelerated to quickly so that the pilot reacted by maintaining a low climb angle. This low angle results in lower force measured by the winch and leads to a further increase of power. In a Ka8 nearing Vne the only possible action is to abort the tow. At our airfield we use a system which transmits the airspeed of the glider to the winch operator. Pared with a good winch operator and a powerful winch, this results in very good winch tows. |
#46
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You can't just control for constant force. You also need to limit the
maximum winch speed to address this exact issue. Mike Schumann "alex8735" wrote in message oups.com... I personally don't think that a constant force regulation results in an ideal winch tows. I have observed a number of tows in which the glider was initially accelerated to quickly so that the pilot reacted by maintaining a low climb angle. This low angle results in lower force measured by the winch and leads to a further increase of power. In a Ka8 nearing Vne the only possible action is to abort the tow. At our airfield we use a system which transmits the airspeed of the glider to the winch operator. Pared with a good winch operator and a powerful winch, this results in very good winch tows. |
#47
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Eric,
the forces are all the same. there is no difference in forces strengths launching to 1000ft or to 5000ft the applying forces just last longer thats all. I did hundreds of take offs on the winch. I wish we would have good winches in Australia. Here we only have historical rubbish standing around. Chris "Eric Greenwell" wrote in message news:GBu1h.4529$WB4.3254@trndny04... Gerhard Wesp wrote: That sounds a bit frightening - 3500 fpm! What are the stresses on the glider to get that kind of climb rate? How far away is disaster if the pilot twitches a bit on the controls or hits some wind shear or a thermal? Hmmm, if they are using weak links, I don't see a problem. Stress (=force) is related to acceleration, not to speed. You can go straight up at 1000000 fpm with the same force as at 10 fpm. Just takes you a bit longer to reach the speed. Of course, the net force on the glider is zero, otherwise it would accelerate, but the individual forces are much greater and vary during the launch. We've all seen the wings curve up and stay that way as the pilot rotates into the climb on a winch launch, indicating much more lift is being generated to counteract the pull of the cable. Surely the cable tension must be greater to provide a 3500 fpm launch instead of a 1000 fpm launch? I'm curious about the amount of tension needed to provide a 1000 pound glider that 3500 fpm climb. -- Eric Greenwell - Washington State, USA Change "netto" to "net" to email me directly "Transponders in Sailplanes" on the Soaring Safety Foundation website www.soaringsafety.org/prevention/articles.html "A Guide to Self-launching Sailplane Operation" at www.motorglider.org |
#48
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news wrote:
Eric, the forces are all the same. there is no difference in forces strengths launching to 1000ft or to 5000ft the applying forces just last longer thats all. I agree with that, but what I asked about was the rate of climb (fpm = feet per minute): Surely the cable tension must be greater to provide a 3500 fpm launch instead of a 1000 fpm launch? -- Eric Greenwell - Washington State, USA Change "netto" to "net" to email me directly "Transponders in Sailplanes" on the Soaring Safety Foundation website www.soaringsafety.org/prevention/articles.html "A Guide to Self-launching Sailplane Operation" at www.motorglider.org |
#49
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![]() "Eric Greenwell" wrote in message news:ei5ch.74$R_1.4@trndny08... news wrote: Eric, the forces are all the same. there is no difference in forces strengths launching to 1000ft or to 5000ft the applying forces just last longer thats all. I agree with that, but what I asked about was the rate of climb (fpm = feet per minute): Surely the cable tension must be greater to provide a 3500 fpm launch instead of a 1000 fpm launch? -- Eric Greenwell - Washington State, USA Change "netto" to "net" to email me directly "Transponders in Sailplanes" on the Soaring Safety Foundation website www.soaringsafety.org/prevention/articles.html "A Guide to Self-launching Sailplane Operation" at www.motorglider.org Not surprising. A typical launch will have the glider climbing at a 45 degree angle and 60 knots. That works out to a little over 42 knots vertical speed. Of course, that the peak climb rate. The average on a high launch can be around 35 knots. The stresses are about the same as mild aerobatics. There are a number of GPS logs on the web that show rates of climb about the same as these figures. If you want to work out the stress for yourself, the peak cable tension will roughly equal the flying weight of the glider. The cable pull vector will start horizontal and swing down to 70 degrees during the launch. At approximately 70 degrees, the CG hook will automatically "back-release" the cable. Serious fun. Bill Daniels |
#50
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I suspect that is not quite true, as the glider's wings
in the 5000ft winch launch have to lift a longer and therefore heavier length of cable into the air. However the weak link remains the same and still protects the glider. What allowed these very high launches to be achieved was the combination of a very long (3000 metre) winch run and the advent of modern lightweight synthetic UHMWPE cable. Derek Copeland At 02:42 01 December 2006, News wrote: Eric, the forces are all the same. there is no difference in forces strengths launching to 1000ft or to 5000ft the applying forces just last longer thats all. I did hundreds of take offs on the winch. I wish we would have good winches in Australia. Here we only have historical rubbish standing around. Chris 'Eric Greenwell' wrote in message news:GBu1h.4529$WB4.3254@trndny04... Gerhard Wesp wrote: That sounds a bit frightening - 3500 fpm! What are the stresses on the glider to get that kind of climb rate? How far away is disaster if the pilot twitches a bit on the controls or hits some wind shear or a thermal? Hmmm, if they are using weak links, I don't see a problem. Stress (=force) is related to acceleration, not to speed. You can go straight up at 1000000 fpm with the same force as at 10 fpm. Just takes you a bit longer to reach the speed. Of course, the net force on the glider is zero, otherwise it would accelerate, but the individual forces are much greater and vary during the launch. We've all seen the wings curve up and stay that way as the pilot rotates into the climb on a winch launch, indicating much more lift is being generated to counteract the pull of the cable. Surely the cable tension must be greater to provide a 3500 fpm launch instead of a 1000 fpm launch? I'm curious about the amount of tension needed to provide a 1000 pound glider that 3500 fpm climb. -- Eric Greenwell - Washington State, USA Change 'netto' to 'net' to email me directly 'Transponders in Sailplanes' on the Soaring Safety Foundation website www.soaringsafety.org/prevention/articles.html 'A Guide to Self-launching Sailplane Operation' at www.motorglider.org |
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